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US 5222360 A Abstract A gas turbine engine has a core frame separable from a vane frame for removably attaching the vane frame to a core structure through a mid ring. The mid ring includes an annular forward panel and an annular aft panel, each of which has a radially outer flange and a radially inner flange. The inner flanges are welded to the core frame and the outer flanges are bolted to the vane frame. A plurality of circumferentially spaced stiffeners extend between the forward and aft panels, with each of the stiffeners including a pair of stringers extending diagonally across the stiffeners. Panels may be incorporated with the stringers between the triangular shaped areas adjacent the forward and aft panels of the stiffener. The bolted connection between the mid ring and the vane frame includes a plurality of tongue and groove joints formed in the flanges of the mid ring and vane frame. The tongue and groove joints provide additional radial support for the core engine within the vane frame. Preferably, the tongue and groove joints are formed with angular sides so that conformance between the joints can be achieved by simply tightening the bolts attaching the joints. In one embodiment, the tongue and groove joints may only be used at preselected circumferential positions with the remainder of the flange connections using overlapping lap joints.
Claims(17) 1. In a gas turbine engine having a core frame separable from a vane frame for removeably attaching the vane frame to a core structure through a mid ring attachment, an improved mid ring comprising:
an annular forward panel and an annular aft panel, each of said panels having a radially outer flange and a radially inner flange, said inner flanges being welded to the core frame and said outer flanges being bolted to the vane frame; and a plurality of circumferentially spaced stiffeners extending between said forward panel and said aft panel, each of said stiffeners comprising a first stringer extending diagonally from said radially inner flange of said forward panel to said radially outer flange of said aft panel and a second stringer extending diagonally from said radially inner flange of said aft panel to said radially outer flange of said forward panel. 2. The mid ring of claim 1 wherein said first and second stringers intersect at approximately a mid-point of each of said stiffeners forming a pair of connected, generally triangular members having two sides formed by portions of each of said stringers and a third side formed by one of said forward and aft panels, each stiffener including a pair of support panels, each one of said pair of support panels filling a respective one of said triangular members.
3. The mid ring of claim 1 wherein each of said stiffeners comprises a support panel extending from said forward panel to said aft panel, said stiffeners comprising flanges fixedly attached to said support panel.
4. The mid ring of claim 3 and including a web extending circumferentially from a circumferential edge of selected ones of said stiffeners to a mid point intermediate a pair of stiffeners, said web being attached to said stiffener along one edge and to one of said forward and aft panels along another edge.
5. The mid ring of claim 4 wherein said web is triangularly shaped.
6. The mid ring of claim 5 wherein said web extends from one of said stiffeners to said aft panel.
7. The mid ring of claim 6 wherein said mid ring is formed as a plurality of arcuate segments having a preselected number of stiffeners extending between an arcuate section of said forward panel and an arcuate section of aft said panel.
8. The mid ring of claim 1 and including a plurality of circumferentially spaced apertures formed in each of said outer flanges of said forward and aft panels for receiving bolts for attaching said mid ring to said vane frame.
9. The mid ring of claim 8 wherein said outer flange of said aft panel has a larger radius than said outer flange of said forward panel such that said mid ring is axially removable from said vane frame by axially sliding said mid-ring in an aft direction after disconnection from said vane frame.
10. The mid ring of claim 8 wherein said outer flange of each of said forward and aft panels is circumferentially scalloped to form alternately peaks and valleys, the peaks in one of said flanges being axially aligned with the valleys in the other of said flanges whereby said mid ring is axially removeable from with said vane frame.
11. The mid ring of claim 8 and including a pair of spaced circumferential flanges on a radially inner circumference of said vane frame, said flanges being positioned to mate with respective ones of said outer flanges on said mid ring, one of said spaced flanges and said outer flanges at preselected mating positions being formed with a groove and the other of said spaced flanges and said outer flanges being formed with a tongue for mating with a corresponding one of said grooves, said attaching bolts extending through said tongue and groove connection.
12. The mid ring of claim 11 wherein each of said tongue and groove are formed with angularly oriented side walls at said preselected circumferential connection points.
13. The mid ring of claim 11 wherein said spaced circumferential flanges are connected to said outer flanges with lap joints at mating positions other than said preselected mating positions.
14. The mid ring of claim 11 wherein said preselected mating positions correspond to connection points between said vane frame and said mid ring adjacent the vertical top of said mid ring when said mid ring is in an assembled position on an engine in an operative position.
15. In a gas turbine engine having a core frame separable from a vane frame for removably attaching the vane frame to a core structure through a mid ring attachment, an improved mid ring comprising:
an annular forward panel and an annular aft panel, each of said panels having a radially outer flange and a radially inner flange, said inner flanges being welded to the core frame and said outer flanges being bolted to the vane frame; a pair of spaced circumferential flanges extending radially inward from the vane frame, said radially inner flanges being positioned to mate with respective ones of said outer flanges on said mid ring, one of said space flanges in said outer flanges being formed with a groove and the other of said space flanges in said outer flanges being formed with a tongue for mating with a corresponding one of said groove; and apertures formed through said tongue and groove connections between said flanges for receiving bolts for releasably attaching said mid ring to said vane frame. 16. The mid ring of claim 15 wherein each of said tongue and groove is formed with an angularly oriented sidewall such that tightening of said bolts aligns said tongue and groove flanges into preselected positions.
17. The mid ring of claim 16 wherein said tongue and groove connections are formed at preselected locations on said flanges, said tongue being removed at other locations wherein said flanges are connected thereby forming a lap joint.
Description This is a continuation-in-part of co-pending application Ser. No. 07/708,263 filed May 28, 1992 and assigned to the assignee of the present invention. Reference is hereby made to the following copending U.S. patent applications dealing with related subject matter and assigned to the assignee of the present invention: 1. "Gas Turbine Engine Structural Frame With Multi-Yoke Attachment of Struts To Outer Casing" by Kenneth J. Lenhart et al, assigned U.S. Ser. No. 07/766,249 and filed Sep. 27, 1991. 2. "Gas Turbine Enging Structural Frame With Multi-Clevis Ring Attachment of Struts To Outer Casing" by Laura A. Fowler et al, assigned U.S. Ser. No. 07/766,255 and filed Sep. 27, 1991. 3. "Gas Turbine Engine Structural Frame With Outer Casing Flange Pockets Gripping Strut Outer Ends" by James W. Brantley, assigned U.S. Ser. No. 07/766,298 and filed Sep. 27, 1991. The present invention relates to apparatus for the assembly/disassembly of a turbofan gas turbine engine and, more particularly, to an apparatus for removably attaching a core frame to a vane frame with a stable mid ring. Turbofan gas turbine engines generally include a core engine coupled in driving relationship to a forward mounted fan module. The fan module, in a high-bypass ratio engine, includes a large diameter single stage fan and a multiple stage intermediate pressure compressor or booster. The fan is surrounded by a fan casing supported by a plurality of structural members compositely referred to as a vane frame, which frame is supported on a hub frame extending from the core engine. The core engine includes a high pressure compressor, a combustor, and a multi-stage turbine for extracting energy from combustion gases exiting the combustor for driving the compressors and fan. Mounting of such high-bypass engines on an aircraft generally requires one or more structural supports which connect the engine to a structural member, sometimes referred to as a strut or pylon, on a wing or fuselage, depending upon the mounting location. The structural supports extend through an aerodynamic cowling, sometimes referred to as a nacelle, and couple to the engine core frame. Coupling may be to the fan casing (or shroud) and to the casing surrounding the turbine. In general, some form of structural yoke is attached to the engine casing and some structural supports attach to the yoke. As gas turbine engines have become more powerful and larger, a concern has developed with handling and transporting of such engines. In particular, engines are now being developed with fans and fan casings having diameters in the range of twelve feet. Transporting of such engines by air or ground is not practical with current commercial aircraft and over-the-road transportation guidelines. Accordingly, it is desirable to provide a method of assembly and disassembly of such engines which permits transport without exceeding aircraft or ground transport size limitations. The problems associated with handling and transporting of such large engines extends beyond shipments to the installation, removal, and handling of the engines in aircraft servicing. It is therefore further desirable to provide a method and apparatus for servicing of such engines which overcome the problems associated with such large diameter fans. In the aforementioned U.S. patent application Ser. No. 07/708,263, one of the connection points between the hub frame and vane frame is shown as a mid ring connection. The combined frames are attached to an aft fan case. The core structure or hub frame, out to a radius of approximately twenty-nine inches, is preferably a one piece casting. A ring with an inner radius of approximately twenty-nine inches and outer radius of approximately thirty-five inches is welded onto the hub frame casting structure making it a one piece fabricated hub structure. Bypass vanes are attached to a vane frame structure at its inner diameter ring of approximately thirty-five inch radius and extend to an outer ring of approximately sixty-three inches radius. The vane frame inner ring and the hub frame outer ring are joined to form a separable joint which defines a mid ring relative to the fan frame assembly. Consequently, this separable joint or the ring portions thereof, whether the hub frame outer ring or the vane frame inner ring, are interchangeably known as the mid ring. The mid ring separable joint is composed of a forward flange joint and an aft flange joint. Since the forward joint and the aft joint have space limitations, they are at or nearly at the same radius. To remove the hub frame, with the core engine attached, the hub frame is required to move aft leaving the vane frame with the vane nacelle which may or may not remain with the aircraft. Consequently, the forward mid ring flange of the hub frame must pass through the aft mid ring flange of the vane frame. Accordingly, some method must be provided for accomplishing this function. In addition, the core struts extend into the hub frame mid ring where the walls flare into flat panels. These flat panels are interrupted by large holes which help to isolate the weld joints from the rest of the structure. The flat panels, extending from the front to the aft mid ring flanges, may not be stable under expected shear forces. Thus, a more stable hub frame structure is needed. Furthermore, there is a concern that the tolerance accumulations between the front flange and the aft flange in the axial direction may not be accommodated without excessive stress being generated in the flange fasteners and the flange structure at assembly. The above and other disadvantages of prior systems are overcome by an engine assembly having an outer and inner portion with the outer portion comprised of a fan case, and a plurality of structural and aerodynamic members, which is separable from the inner portion of the engine which extends from a spinner assembly to the primary nozzle and includes the engine components located radially inward from a thrust reverser. More particularly, a gas turbine engine has a core frame which is separable from a vane frame to thus allow the vane frame to be removably attached to the core structure through a mid ring attachment. The mid ring attachment comprises an annular forward panel and an annular aft panel, each of which has a radially outer flange and a radially inner flange. The inner flanges are welded to the core frame and the outer flanges are bolted to the main frame. In one embodiment, a plurality of circumferentially spaced stiffeners extend between the forward panel and the aft panel. Each of the stiffeners includes a pair of stringers extending diagonally across the stiffener from flange to flange to provide a more stable stiffener for the mid ring. The space above the diagonally crossed stiffeners may be left open to provide an area in which axial adjustment of the position of the upper flanges may be made during installation in order to accommodate manufacturing tolerances. The stiffeners may be further enhanced by additional webs connected between the stiffeners and one of the forward and aft panels. Preferably, the flanges of the mid ring are attached to the flanges of the vane frame by bolts. In an illustrative embodiment, the flanges are formed such that one of the flanges has a tongue and the mating flange has a groove so that the joint formed by connection of the flanges provides maximum radial strength. Furthermore, the tongue and groove joints may be formed as wedges so that tightening of the bolts to connect the flanges serves to align the joints. A more complete appreciation of the invention and many of the attendant advantages thereof will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein: FIG. 1 is a simplified partial cross-sectional drawing of an exemplary gas turbine engine; FIG. 2 is a simplified schematic side view illustration of an engine assembly incorporating an improved mid ring connection according to the present invention; FIG. 3 is a close-up, simplified schematic illustration of the rotor and booster regions of the engine of FIG. 2 showing the mid ring connection; FIG. 4 is an enlarged view of one of the stiffeners used in the mid ring frame; FIG. 5 is an axial view of an alternate embodiment of a mid ring in accordance with the present invention; FIG. 6 is a perspective view of one of the circumferential segments of a mid ring constructed in accordance with the present invention; FIG. 7 is an axial view of a section of the gas turbine engine showing the struts which extend from the inner flowpath wall to the inventive mid ring; and FIG. 8 illustrates an alternate form of stiffener arrangement for use in Applicant's inventive mid ring. When referring to the drawings, it is understood that like reference numerals designate identical or corresponding parts throughout the several views. Referring first to FIG. 1, there is shown a partial cross-sectional drawing of an exemplary high-bypass ratio gas turbine engine 10 having a core engine portion indicated at 12 and a stator or fan portion indicated at 14. The core or engine portion 12 may be referred to as the rotor module. The rotor module or core engine 12 includes an intermediate pressure compressor or booster stage 16, a high pressure compressor stage 18, a combustor stage 20, a high pressure turbine stage 21, and a low pressure turbine stage 22 all aligned on an engine centerline 23. The core engine 12 further includes fan blades 24 and the spinner assembly 28. The fan portion 14 comprises fan cowling 27 and fan casing 26. The fan cowling 27 surrounds the fan casing 26 and radially encloses the fan portion of the engine 10. The fan spinner assembly 28 located forward of the fan blades 24 connects to a rotor assembly 38 (shown in FIG. 2), rotor assembly 38 being a part of the core engine 12. To the aft of fan blades 24 is located a plurality of circumferentially spaced outlet guide vanes or fan frame struts 30 which are a part of the fan portion 14. The outlet guide vanes 30 connect the engine core 12 to the fan portion of the engine 10 and provide structural support. At the rear of engine 10 is located primary nozzle 33 which includes an outer member 34 and an inner member 35. A fan shaft 37 driven by turbine stage 22 extends through the engine and is coupled in driving relationship with booster stage 16. Fan shaft 37 turns fan blades 24 via fan rotor assembly 38 (shown in FIG. 2). As will be apparent from FIG. 1, handling of the engine 10 is a major problem for very large diameter fan blades 24. While it is possible to remove the blades 24, the practice in the art is to treat the blades 24, booster stage 16, and fan case 26 as a unitary module. Some engines are constructed with a two-piece fan shaft separable aft of the booster stage 16 approximately along the line 23. These engines are identified as split fan engines. Assembly and/or disassembly of split fan engines is complicated since it is difficult to attach the fan forward shaft and the fan mid shaft properly. In such fan split methods of separating an engine, the forward module includes the fan case 26, structural outlet guide vanes 30, fan spinner assembly 28, fan blades 24, along with fan rotor 38, booster stage 16 and the forward portion of shaft 37. Thus, it has not been practical to separate the fan module and large external components for the core engine to facilitate handling. Furthermore, it is not desirable to separate an engine where such separation includes a rotating interface since such an interface may involve bearings or critical alignments. Turning now to FIG. 2, a simplified schematic illustration of the present invention's engine assembly 10, which is similar to FIG. 1, shows an inlet 40 and fan cowling 27 located at the extreme front of the engine 10, the circumferential shape of the inlet forming an air passage by which air can enter the engine. To the aft of inlet 40 is fan case 26 which may be connected to fan cowling 27. Fan case 26 surrounds the fan blades 24 which are located radially inward therefrom. To the aft of fan blades 24 lie the fan outlet guide vanes (OGV's) 30 whose distal end portions in the outward radial direction are connected to fan casing 26. In addition, the front engine mount 42 connects to the wing pylon 44 which is attached to aircraft wing 46. Broken line 48 of FIG. 2 indicates the outer portion of engine 10 and includes the inlet 40, fan casing 26 and fan outlet guide vanes 30. The radially inward distal end portion of each fan outlet guide vane 30 is attached to fan outlet guide vane support member 50 and by means of bolts 52. Referring to FIG. 2 and FIG. 3 together, support member 50 comprises the aforementioned mid ring for connecting the vane frame to the hub frame which extends through booster casing 54. The vane frame, indicated at 100, includes the vanes 30 and their inner and outer shrouds 102 and 104. The core or hub frame comprises a plurality of struts which extend through the airflow path in casing 54 and terminate at the mid ring connection. In the mid ring area, the walls of the struts flare into flat panels attached to a forward mid ring bulkhead or panel 106 and an aft mid ring bulkhead or panel 108. To the aft of fan cowling 27 and fan outlet guide vanes 30 is located a D-duct type thrust reverser 56 which includes a fan portion 58, a core portion 60 and links 62. The links 62 extend circumferentially around core portion 60. Located radially inward from core portion 60 of thrust reverser 56 is thrust link 64 which is attached at one end to pylon 44 at location 66, location 66 being to the aft of thrust reverser 56. The other end of thrust link 64 is connected to fan frame 54 by means of brackets (not shown) which extend circumferentially around booster case 54. To the aft of location 66 is rear engine mount 68 which connects pylon 44 to a frame 31 on core engine 12. The inner portion 72 of the engine 10 may be defined as that portion of the engine extending from the spinner assembly 28 to the primary nozzle 33 which is located radially inward of the thrust reverser 56. The inner portion of the engine does not include the fan outlet guide vanes 30 which have been defined to be a part of the outer portion of the engine as they are inside broken line 48 of FIG. 2. FIG. 3 is an enlarged, partial cross-sectional illustration of the fan blade and OGV attachment portion of the present invention and shows fan blade 24 connected to blade platform 74. The blades 24 are secured to rotor assembly 38 by means of anti-clank spring 76. Aft spinner 78 is connected to rotor assembly 38 by means of bolt 80 and forward spinner 82 is connected to aft spinner 78 by means of bolt 84. Pin 86 connects the blade platform 74 to rotor assembly 38. Acoustic panels 92 are connected to the booster casing 54 by means of a tongue and groove slip joint 94. The acoustic panels are also connected to booster casing 54 by bolts 96. The fan outlet guide vanes 30 are connected to support 50 by bolts 52 and 98. Turning now to FIG. 4, there is shown an enlarged and more detailed view of mid ring 50 viewed in a tangential direction. The forward panel 106 and aft panel 108 each have radially inner flanges 110 and 112, respectively, and radially outer flanges 114, and 116, respectively. The radially inner flanges 110 and 112 are cast, molded, or machined to mate with respective ones of the inner forward and aft bulkheads 118 and 120. Preferably, the flanges 110 and 112 are attached to the inner bulkheads 118 and 120 by electron beam welding. The radially outer flanges 114 and 116 are releasably attached to the inner shroud ring 102 of the vane frame by means of a plurality of circumferentially spaced bolts 52 and 98. For attachment purposes, the shroud ring 102 includes forward and aft radially inwardly extending flanges 124 and 126 having a plurality of circumferentially spaced apertures 128 for receiving the bolts 52 and 98. In a preferred form, the bolts 52 and 98 are threaded into captive nuts 130A and 130B which are attached to the inside surface of flange 114 and flange 126, respectively. The connection between the mid ring 50 and vane frame shroud 102 is designed to provide an engine quick change joint. However, the joint is required to have no motion or yielding under limit loads and no complete failure under ultimate load, i.e., a blade out at take-off. Under these conditions, there is a high radial load transmitted across the mid ring to vane frame joint. To resist such loading, the joint must not slip. However, it has been shown that friction alone in a conventional flat face lap joint is not sufficient to carry such high radial loads without slipping. The present invention overcomes this slipping problem by incorporating a tongue and groove shear joint connection in which the flange 114 and the flange 116 each include a protruding tongue indicated at 132A and 132B, respectively, with each tongue fitting into a corresponding groove 134A and 134B in flanges 124 and 126, respectively. When the flanges 114 and 116 are clamped to corresponding ones of the flanges 124 and 126, high radial shear loads are transmitted in bearing across the tongue and groove instead of through friction as in the conventional lap type flange. For the same size of bolt and bolt clamp force, this tongue and groove shear joint can withstand the design maximum radial shear loads without slippage. Furthermore, it will be noted that the tongue 132 and groove 134 are each formed with beveled sides. Preferably, the sides are beveled at 45�. This arrangement forms an angle wedge which is self aligning when the flanges are attached one to the other. The size and weight of the engine modules involved in this flange connection would make a conventional rabbeted joint extremely difficult to assemble or disassemble. However, the wedge shaped tongue and groove joint provides for ease of assembly and also assists in aligning the joint as the bolts 52 and 98 are tightened. FIG. 4 also illustrates the radial positioning of the joint at flange 114 and the joint at flange 116. It will be noted that the flange 114 is positioned at a radius which is less than the radius of the inner end of flange 126. This arrangement allows the mid ring to be slid axially aft such that the flange 114 passes under the flange 126 to allow the core engine to be removed from the vane frame assembly. Referring briefly to FIG. 5, there is shown an axial view of an alternate embodiment of the mid ring 50 and vane frame shroud 102 in which the edges of the flange 114 and flange 126 are scalloped such that the peaks of flange 114 fit within the valleys of flange 126. This alternate embodiment allows the flange 114 to pass through the space occupied by flange 126 again permitting the mid ring to slide axially aft out of the vane frame assembly. An analysis of the radial loading at the joints between the flanges 114, 124, and 116, 126 has shown that the maximum loading at these flanges is not uniform for the full 360� joint. Accordingly, it has been found that the use of the wedge connection, that is, the tongue and groove arrangement shown in FIG. 4, may not be required for the full 360� connection between the mid ring 50 and shroud 102. In applications in which such wedge joints are not required for the full 360�, it may be possible to reduce the mass of the flanges 114 and 116 by machining off the tongue portion 132 and utilizing a conventional overlapping lap joint at selected locations. In general, it has been found that peak loading on the mid ring occurs within preselected angular orientations at the top of the mid ring with the engine in an assembled and operative position. Accordingly, those areas of the mid ring and shroud 102 connection could be formed with tongue and groove joints while other areas of the shroud mid ring connection could utilize conventional lap joints. In order to provide stability between the forward panel 106 and aft panel 108, the panels are interconnected by a plurality of circumferentially spaced stiffeners or shear panels 136. Each of the stiffeners 136 comprises a first flange or stringer 138 extending diagonally from flange 112 to flange 114. A second flange or stringer 140 extends diagonally from flange 110 to flange 116. The stringers 138 and 140 form an X-shaped frame structure providing stabilizing stiffness between the forward panel 106 and aft panel 108. On each side of the X-shaped structure between the adjacent panels 106 and 108, there is defined a triangular area which preferably incorporates sheet metal support panels 142 and 144. The panels 142 and 144 are desirably cast or molded in combination with the stringers 138 and 140 to form a composite structure. More particularly, in the manufacturing process, the forward and aft panels 106 and 108 may be cast integrally with the stiffeners 136 to form a circumferential segment which may be joined with additional circumferential segments to form the complete annular mid ring 50. In addition, it may be desirable to add support panels in the triangular space radially inward of the stringer 140 and stringer 138. It will be noted that the diagonal stringers 138 and 140 form an X-shaped structure that provides stability to the stiffeners which is essentially comprised of the support panels 142 and 144. The diagonal stringers 138 and 140 provide axial support to the separable joints at flanges 114 and 116. Compliance between these separable joints is accomplished by the absence of material in the space above the stringers 138 and 140 adjacent the radial inward face of shroud 102. The absence of material in space above the diagonal stringers 138 and 140 allows sufficient flexibility of the forward and aft panels 106 and 108 so that they may flex in the axial direction to accommodate a tolerance stack-up between the separable connections at flanges 114 and 116. Additional flexibility of the panel in the axial direction may also be accommodated by eliminating the shear or support panel below the stiffeners 138 and 140. Turning now to FIG. 6, there is shown a perspective view of one of the circumferential segments of mid ring 50. The forward and aft panels 106, 108 and their associated flanges 114, 116 are shown on a schematic end of this view. What is more clearly shown in FIG. 6 is the addition of circumferential webs 146 and 148 in each space between the stiffeners 136. The webs 146 and 148 are angularly oriented such that one side of each web is attached to an edge of a stringer 140 and another side of each web is attached to the aft flange 116. The webs 146 and 148 thus provide support in the circumferential direction to minimize the tendency of the stiffeners 136 to buckle or vibrate in a circumferential direction. FIG. 7 is an axial view of a section of a gas turbine engine showing the struts which extend from the core inner flowpath wall 150 through the core outer flowpath wall 151 to the mid ring 50. Taken in cross-section, it can be seen that the struts are hollow having opposite sidewalls 152A and 152B which terminate at about the point at which the inner stiffeners 136 begin within a mid ring 50. The outer stiffeners 136 occurring at each end of each mid ring segment are not aligned with struts but are rather aligned on an oblique spreading out from a radial line in order to more evenly distribute their support circumferentially. FIG. 8 illustrates an alternate form of stiffener structure in which the stiffener is primarily a shear panel 160 surrounded by a diagonal stringer 162 and an axially oriented stringer 164. The shear panel 160 is connected to the top of the strut wall 166 along the line 168 by electron beam welding. The hub frame remains a one piece fabricated structure with a hub mid ring 50 welded to the hub casting. The diagonal stringer 162 extends from the forward lower flange 110 to an intersection with the inner web 146 near the separable joint at flange 116. In the extreme, the flange 162 could be formed as a complete 360� shell within the mid ring 50. The diagonal connection formed by flange or stringer 162 provides axial strength to the mid ring 50. Since the panel 160 does not extend to the forward panel 106, the hub portion of the separable joint at flange 114 is relatively free to flex forward or aft allowing the hub mid ring flanges 114 and 116 to be compliant, in the axial direction, with the vane frame forward and aft flanges 124 and 126. The apertures 170 and 172 are provided to accommodate electron beam welding of the joints between flanges 110, 118, and 112, 120. In another embodiment of FIG. 4 or FIG. 8, the diagonal stringers provide axial support to the separable joints at flanges 114 and 116. The diagonal stringers also provide stiffness to the shear or support panels connecting the forward and aft panels 106 and 108 to improve stability of the panels and stability of the overall hub frame structure. Compliance between the flange joints at flanges 114 and 116 is improved by the absence of material in the space above the diagonal stringers. This allows sufficient flexibility between the flanges 114, 116, 124, and 126 to permit flex or motion in the axial direction to accommodate any tolerance stack-up during manufacture. Furthermore, since manufacturing size limitations do not permit the entire hub frame including the mid ring connector to be cast in one piece, the hub frame mid ring 50 is cast separately in one or more pieces and a central portion of the hub frame is cast in one piece. The smaller radius circumferential weld locations at flanges 110 and 112 allow a smaller and more manageable hub casting. Furthermore, movement of the welds to smaller radius positions allows the complete mid ring sections all to be cast in a one piece ring above the circumferential welds at flanges 110 and 112. The tongue and groove shear joints also provide much higher resistance to joint slippage than conventional joints for the given size and number of bolted connections. The tongue and grove joint is also self aligning due to the wedge shaped faces on the tongue and groove joints thereby facilitating concentric assembly of very large engine modules. Circumferential variation in the type of joint, i.e., using the tongue and groove in certain locations and an overlapping lighter weight joint in other locations results in a lighter weight constructions of the mid ring assembly. While the invention has been described in what is presently considered to be a preferred embodiment, other modifications and variations will become apparent to those skilled in the art. It is intended therefore that the invention not be limited to the specific embodiment but be interpreted within the full spirit and scope of the appended claims. Patent Citations
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Open AccessThis article is
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Materials 2013, 6(10), 4609-4625; doi:10.3390/ma6104609
The Synthesis of α-MoO3 by Ethylene Glycol
Received: 7 August 2013 / Revised: 17 September 2013 / Accepted: 12 October 2013 / Published: 17 October 2013
(This article belongs to the Section Manufacturing Processes and Systems)
Download PDF [1243 KB, uploaded 17 October 2013]
Abstract: This study investigated the use of ethylene glycol to form α-MoO3 (molybdenum trioxide) from ammonium molybdate tetrahydrate at various sintering temperatures for 1 h. During the sintering process, the morphologies of the constituents were observed using scanning electron microscopy (SEM), and Fourier transform infrared (FTIR) spectroscopy was used to explain the reaction process. In this work, the results obtained using X-ray photoelectron spectroscopy (XRD) demonstrated that, when the molybdenum trioxide powder was treated thermally at 300 °C, the material exhibited crystallinity. The peaks were indexed to correspond with the (110), (040), (021), (111), and (060) crystallographic planes, and the lattice parameters of a, b, and c were about 3.961, 13.876, and 3.969 Å. Using these observations, we confirmed that orthorhombic α-MoO3 was formed for sintering temperatures from 300 to 700 °C. Pattern images were obtained by the selected area electron diffraction pattern (SAED) technique, and the d distance of the high resolution transmission electron microscopy (HRTEM) images were almost 0.39 and 0.36 nm, and the Mo 3d5/2, Mo 3d3/2, and O 1s of X-ray photoelectron spectroscopy (XPS) were located at 233.76, 237.03, and 532.19 eV, which also demonstrated that α-MoO3 powder had been synthesized.
ethylene glycol; molybdenum trioxide; crystallization; sintering
This is an open access article distributed under the
Creative Commons Attribution License which permits unrestricted use, distribution,
and reproduction in any medium, provided the original work is properly cited.
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MDPI and ACS Style
Chiang, T.H.; Yeh, H.C. The Synthesis of α-MoO3 by Ethylene Glycol. Materials 2013, 6, 4609-4625.
AMA StyleChiang TH, Yeh HC. The Synthesis of α-MoO3 by Ethylene Glycol. Materials. 2013; 6(10):4609-4625.
Chicago/Turabian StyleChiang, Tzu H.; Yeh, Hung C. 2013. "The Synthesis of α-MoO3 by Ethylene Glycol." Materials 6, no. 10: 4609-4625.
Published by MDPI AG, Basel, Switzerland
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text: 2 Forget it..Posted: 05/01/2010Just watch the trailer! It covers the whole story and all the best jokes...The movie is slow at start, then it just gets slower.The idea is brilliant, but the execution is horrible. You will laugh about 3 times and giggle about 10-15 times. Other than that, you'll just climb the walls waiting for something to happen..


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Louise BirkheadModel Female London, England, United Kingdom My MM URL: http://www.modelmayhem.com/louisebirkhead
Mayhem # 816832
About MeHi, I'm Louise Birkhead, I'm 22years old and I've been modelling for 8years now and love it!
As i said above, I love my modelling and I'm very williing to try out different things - to a certain extent haha. I have met loads of great people through MM and hope that I will carry on meeting more! If you'd be interested in working with me dont hesitate to contact me, I'm afraid I only do paid work now, as I have done more than enough tests etc etc and its now time to start earning... I'm based in North London but very willing to travel. Hope to hear from you all soon! Louise Friends |


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Lockheed Martin GMLRS Alternative Warhead Logs Successful Flight-Test Series, Shifts To Next Testing Phase
DALLAS, April 16, 2014 /PRNewswire/ -- Lockheed Martin (NYSE: LMT) successfully conducted the fifth and final Production Qualification Test (PQT) for the new Guided Multiple Launch Rocket System (GMLRS) Alternative Warhead recently at White Sands Missile Range, N.M.
During the long-range test, four rockets were fired from a HIMARS launcher and destroyed their respective targets approximately 65 kilometers away. The test is the final milestone before the Developmental Test/Operational Test (DT/OT) phase, which will incorporate soldiers into the system testing. The DT/OT phase will begin this summer and will conclude with the Initial Operational Test & Evaluation exercise in the fall of 2014.
"This next phase of testing will be critical in determining operational effectiveness," said Ken Musculus, vice president of Tactical Missiles for Lockheed Martin Missiles and Fire Control. "We are committed to the customer and their success on the battlefield, and these tests ensure production of a trustworthy and effective solution."
In April 2012, Lockheed Martin received a $79.4 million contract from the U.S. Department of Defense (DoD) to develop the Alternative Warhead Program (AWP). Under the terms of the contract, the Engineering, Manufacturing and Development phase of the program runs 36 months, focusing on system performance, warhead qualification and producibility.
The Alternative Warhead is designed to engage the same target set and achieve the same area-effects requirement as the GMLRS submunitions warhead, but without the lingering danger of unexploded ordnance. The Alternative Warhead is being developed by ATK under subcontract to Lockheed Martin. The AWP is part of a U.S. Department of Defense plan to create a GMLRS variant that meets the DoD's cluster munition policy. The Lockheed Martin GMLRS Alternative Warhead program will also be compliant with the provisions of the Convention on Cluster Munitions international treaty.Check Out Our Best Services for Investors
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Jimmies win 3 out of 4
Presentation College played above its record, but the Jimmies left Aberdeen with three wins in four games.
Entering the first weekend of North Star Athletic Association play, the Saints were just 4-22. But they earned a split Saturday and nearly another Sunday, but the University of Jamestown rallied late to win the fourth and final game and take the series 3-1.
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Joan Dennis
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Glucose with your blood … It isn't some sort of cozy define for your personal blood. This blood vessels is composed of diverse factors By way of example sugar. Certainly, There may be mister as aspect of your respective blood vessels, but to get a regular calculated degrees. http://All4Webs.com/t/f/joseph764vciqblog/home.htm
Joan Dennis joined the JazzTimes community on Jan 11, 2014


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Lyrics Depot | |
Lyrics » ICP (Insane Clown Posse) Lyrics » Blaaam!!! Lyrics |
Lyrics Depot is your source of lyrics to Blaaam!!! by ICP (Insane Clown Posse). Please check back for more ICP (Insane Clown Posse) lyrics. |
Blaaam!!! LyricsArtist: ICP (Insane Clown Posse)Album: Wraith: Shangri-la (feat. Anybody Killa) [Anybody Killa] Story time, bitch! All across the East Side [Violent J] What? I represent Delray! [Shaggy 2 Dope] Delray! [Anybody Killa] So? [Violent J] South West Side! [Violent J & Shaggy 2 Dope] This Gypsy aunt of mine You're the lucky one She died and left behind An ancient piece of time I didn't know what it was You're the lucky one Knuckle deep in dust Edges played with rust I started to get pissed You're the lucky one This lamp is all I get A worthless piece of shit But once I rubbed it clean You're the lucky one A genie popped on the scene Brought true my every dream [Chorus] I was like BLAAAM! Free hoes BLAAAM! Nyquil BLAAAM! Faygo Anything I want I was like BLAAAM! Sharp axe BLAAAM! Good weed BLAAAM! Hot tracks Everything I need [Violent J & Shaggy 2 Dope] Now I'm in a fizzle You're the lucky wizzle Hotties on the wizzle Still a juggalizzle I drive a platinum car You're the lucky one It has a tennis court and a bar You know who I are Money out the ass You're the lucky one I'm wishing while it last Genie's moving fast [Chorus] I want my BLAAAM! Free bank BLAAAM! Necks cut BLAAAM! My shank Anything I want I want my BLAAAM! Hot wings BLAAAM! Good weed BLAAAM! Big thangs Everything I need [Violent J & Shaggy 2 Dope] Now I am a king You're the lucky one I have everything Nothing's challenging Nothing makes me proud You're the lucky one I stand out in the crowd While others beg out loud I remember when You're the lucky one Money was so thin But dreams were all up in Looking at my lamp You're the lucky one Would I give it all back? Shit, fool, give me that [Chorus] I'll be like BLAAAM! Bitch slaps BLAAAM! Cheap wine BLAAAM! Dub H (waffle house) Anything I want I'll be like BLAAAM! Half pipe BLAAAM! Good weed BLAAAM! Moonlight Everything I need I'll be like BLAAAM! Free hoes BLAAAM! Nyquil BLAAAM! Faygo Anything I want I'll be like BLAAAM! Sharp axe BLAAAM! Good weed BLAAAM! Hot tracks Everything I need [Anybody Killa & Shaggy] BLAAAM! The moral of the story is BLAAAM! Those who never had shit BLAAAM! And then get shit WHAT? Need to get shit BLAAAM! So if you got shit BLAAAM! Or you need shit BLAAAM! Get some shit GO GET YOUR SHIT Fuck this shit Where JD at?
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Ad budgets are not being cut in 2011, claims WPP's Sorrell
By Maisie McCabe, campaignlive.co.uk, Friday, 16 September 2011 12:30PM
There is no sign that WPP clients have started to slash advertising budgets so far this year, although the outlook is "soggier" towards the end of the year, according to WPP's bullish chief executive, Martin Sorrell.
Speaking to Campaign after his session at the Royal Television Society Cambridge Convention today, the WPP leader said although companies are more cautious, WPP has "seen no sign of people cutting budgets".
Initial forecasts had suggested that the UK ad market could rise around 2% year on year in the fourth quarter of 2011 but there has been speculation that many marketers were cutting spend towards the end of the year.
Global revenues at WPP grew by 6.1% in the first half of 2010. Sorrell said trading in August was in line with the first half of the year but that he expected there to be a "soggier back end" to the year.
Sorrell said growth in ad spend in recent years has been driven by companies deciding to invest in advertising and marketing services in order to grow their businesses and brands rather than making capital investment.
Sorrell said: "Given what [advertisers] read on newspapers and see on the screen they are going to be more nervous. Given what consumers read in newspapers and see on their screens they are going to be more nervous.
"If you're running a company it's going to make you more cautious about capital investment, about making the margins higher. We have seen no sign of people cutting budgets."
When questioned about the cost of TV advertising compared with other media during the session in front of around 150 TV executives Sorrell said clients still "feel like it's not as competitive a market place as they'd like".
He continued: "Media inflation has cost them a lot and has inflated faster than other costs. The fact they [now] have alternatives makes them feel much better. They feel like free-to-air TV had a stranglehold."
Sorrell questioned the role of social media. He said: "I have some fundamental doubts about the ability to monetise social media. If you attempt to interrupt a social interaction with a commercial message then you will run into trouble."
In future, media owners and agencies need to work closer together, Sorrell said. "The relationship between our clients and ourselves as proxy for our clients, there has to be closer with the people in this room.
"That is the fundamental problem. Convergence and behavioural targeting, sponsorship and ad-funded programming with require us to work much closer with the people in this room and in a less adversarial way."
This article was first published on campaignlive.co.uk
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Two Guys, a Girl and a Pizza Place: Season 1, Episode 5Two Guys, a Girl and an Apartment (8 Apr. 1998) 8.6
Mrs. Wexler moves out of the apartment block so Sharon and the boys work out a way to vet the new occupant. However, they have very different ideas of who it should be. Melissa moves in to Pete's displeasure, which forces them to break up. Director:Marjorie Weitzman |
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Major League Baseball | ||||||||||||||||||||||||||||||||||||||||
· Scoreboard · Statistics · Transactions · Current odds · Live odds · Teams Index · News · Game matchups · Pitching report cards · Probable pitchers · Weather · College Baseball · Minor League Baseball |
American League · Injuries · Power Poll · Previews · Recaps · Rotations · Schedule · Standings · Statistics |
National League · Injuries · Power Poll · Previews · Recaps · Rotations · Schedule · Standings · Statistics |
Saturday, August 30 (All times Eastern) Cleveland Indians (69-64) at Kansas City Royals (74-60), 7:10 p.m. Probable Starting Pitchers: Cleveland - Trevor Bauer (5-7, 4.18) Kansas City - James Shields (12-7, 3.45) (SportsNetwork.com) - The Kansas City Royals will try not to lose any more ground atop the AL Central when they resume a three-game series versus the Cleveland Indians Saturday at Kauffman Stadium. The Royals dropped Friday's series opener to Cleveland, 6-1, and their lead in the division is now just a half-game ahead of Detroit. Jason Vargas was saddled with the loss in the start and gave up four runs and 10 hits in six innings. Alcides Escobar highlighted the offense with four hits and an RBI, as Kansas City fell for the fourth time in the last six tries. "That was a tough loss," Escobar said. "I got four hits, but we only got one run. There's nothing we can do about it now." Kansas City is 2-3 in a stretch of 10 straight games at home and will also welcome Texas to town for three games. The Royals are still 14-6 in the last 20 games at Kauffman Stadium. Hoping to right the ship for KC Saturday will be starting pitcher James Shields. Shields is 12-7 with a 3.45 earned run average and looks to get back on track after going 3-0 in four starts before Monday's 8-1 loss to the New York Yankees in which he gave up six runs and 10 hits in 6 2/3 innings. Shields is 4-5 in 12 home starts and 4-5 with a 3.69 ERA in 15 career starts against the Indians. Cleveland has won two in a row and five of its last six games, and will try again to spoil KC's hopes of division supremacy. In Friday's win at Kauffman Stadium, Danny Salazar pitched five scoreless innings for the win and Carlos Santana finished with a two-run homer and three RBI. Michael Brantley posted three hits for the Indians, who pulled within 4 1/2 games of the Royals in the Central standings. "I have certain teams, Minnesota, Kansas City, that I do well against," noted Santana, who hit five homers at Kauffman Stadium in the Tribe's last series there. "I have good sense when I come here." Trevor Bauer gets the ball for the Tribe Saturday and he is 5-7 with a 4.18 earned run average. Bauer defeated Houston in Sunday's 3-1 decision with six shutout innings and nine strikeouts, and the Indians have won each of his last three appearances. Bauer was 0-3 in his previous six trips to the mound and is only 1-5 in nine road assignments this season. He lost his only career start against the Royals on June 11 this season in a 4-1 setback at Kauffman Stadium, charged with three runs and seven hits in 5 1/3 innings. The Indians and Royals will wear 1974-style uniforms Saturday night and have split 14 contests this season. 08/30 10:23:47 ET Powered by The Sports Network. |


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Complejo Turistico Los Molles
- Continental Breakfast
- Shuttle bus service
- Suites
- Room service
- Swimming pool
- Restaurant
TripAdvisor Reviews Complejo Turistico Los Molles Malargue
Travel Blogs from Malargue
Castillos de Pincheira
... do this twice in the same day. Threads in discussion boards suggest that this is so Argentinian banks can get double the commission.
We drove up to Castillos de Pincheira about 30 miles out of town. This is a gorge along Rio Malargue with unusual rock formations. There was a place that you could picnic, barbeque or swim at but we had not come prepared.
Having seen the rock ...
To Malargue
... and we know from bitter experience virtually nowhere opens on New Year's Day. We food a small corner shop and bought some basic provisions before heading west to the Andes and then south to Malargue.
On the way, a chap waved us down and said that our rear tyre was wobbling. We couldn't see anything wrong but nevertheless kept the speed down to 80 kph just ...
... who are late through their stupidity while the rest of us have to sit for an hour waiting. The passengers, even in Argentina, are still sheep, just sitting there and not questioning anything – as ever, left up to me, to query why the 50 other punctual people on the bus have no rights!
It was therefore gone 9.30pm by the time I got there and wasn't able to look hard for ...
Our way to Peninsula Valdes
... abgebaut wird. Als Belohnung f�r den Umweg erblickte er an der Laguna Nueva Flamingos! Somit entschieden wir, an der Lagune eine Nacht zu verbringen, um die unerwartete �berraschung zu geniessen. Nach weiteren 850km und einem sch�nen Ruhetag am Rio Negro inkl. Bircherm�esli ;), erblickten wir in der Abendd�mmerung das weite Meer und Puerto Madryn. Endlich mal wieder viiiiel Wasser!
Malargue - Caving and Skiing
... After lunch they took us for a walk to a waterfall. The waterfall was, well frankly not very impressive, but it was never going to be in a desert. However, the fossils that were scattered around were. And all the rocks smelled of oil/petrol, which i thought was pretty amazing.
Meanwhile, Irish was back at the restaurant, debating the use of the local toilet. As we all load onto the bus, Irish makes a run for the toilet. He returned a ...


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Flatmate wanted in Deas Wharf, Kirkcaldy - 3 months £275/month
I'm doing a PGDE Primary School teaching and my placement is in Fife. My friend - a surveyor and registered landlord - has a brand new 2 bed flat in Kirkcaldy to rent which he will private let me for the short term. I'm looking to rent for 3 months i


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Nov 11, 2010, 03:19 PM | |
... I posted a bunch of pictures of the CMPro T-45 I got last week here, just the plane out of the box for now.
Seems nicely made & relatively lightweight compared to other CMPro stuff I have the fan, motor (Neu) & esc combo, the Springair 602's seem to fit just fine. http://www.rcgroups.com/forums/showt...1336098&pp=100 . |
Nov 11, 2010, 04:18 PM | ||
Also, I've had good luck with EPF Hobby's DSR46T units. I upgraded to the metal side plates as well. They have a new set with trailing link struts & metal sides. They will be strong enough for this plane if it is in the 8-9lb range. http://www.southerncrossrc.com/virtu...lete-titan-set |
Nov 11, 2010, 04:54 PM | ||
United States, CA, Corona
Joined Feb 2006
7,261 Posts
I opened the box, just had to do it. The below quote is good advice based on what I saw and felt. The main wing is thin, built up and covered with CMP thick covering. It will resist wrinkles, but there are several hollow points built into the wood to lighten it up.
Some of you guys could actually over build it into a flying brick. This baby needs to be kept light. It should be built like a heavy foamy. I'm not even sure about the Midi Pro with an ARC motor. I gotta jump over and see what Herb is doing, for some reason the 90mm setup looks to be too big. OK I jumped over, Herb has it taped together so from basics it looks like the 90mm Midi will fit perfect, the ducts fit. Note Herb's warning about the wings, very thin and very small. A hard landing might push the gear all the way through. There are some negatives. This plane has to be built light... Quote:
Nov 11, 2010, 05:02 PM | |
I have no involvement with T-45's of any scale, but came across this cool photo of a new and different scheme for the hawk. Ya'll enjoy.
http://www.airliners.net/photo/USA--...awk/1811273/M/ |
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Add fresh and delicate pattern to her bed with this pretty paisley design.
Please allow 5-7 business days for delivery. Delivery estimate includes monogrammed and gift-wrapped items.
To confirm delivery time frames in your area, please call 800.993.4923.
Item | Price | Delivery Surcharge |
Lara Extra Standard Pillowcase, Lavender/Blue | reg. price $14.50 sale $8.99 | $0 |


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It's my understanding there are two types of wort chillers, immersion and counterflow. The immersion chller sits in the wort and cold water is run through the copper coil? With the counterflow chiller, the cold water/ice is outside the coil and the wort runs through the copper coil into the fermenting bucket? Is there an advantage of one style over the other? My kit came with the counterflow type where the wort is run through the copper. How do you clean / sanitize it? Thanks, Dennis
I checked with the place I got the beermaking kit and wort chiller from. The owner designed the chiller and has it manufactured to his specs. He said it's a "kind of" counterflow chiller in that the wort runs through the copper tubing but instead of the tubing being in a jacket and running cold water, the chiller is mounted inside of a 5 gallon bucket that ice and water are put in. The copper coil is immersed in the cold bath. As the wort runs through the tubing, it's cooled to about 70 - 75 degrees. A nice feature of this design is that you don't waste a lot of water with it. I'll let you know how it works when I use it in a few days. Dennis


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SandbagsProperty owners responsible for sandbagsSubmitted by WWAY on Wed, 01/07/2015 - 10:13pm.READ MORE:
The North Topsail Beach Board of Aldermen decided to pass along some of the sandbag costs to homeowners at a meeting Wednesday night.
Full story... » Officials in N. Topsail meet about sandbags planSubmitted by Ashley Cimino on Wed, 11/19/2014 - 10:46pm.READ MORE:
Officials in North Topsail Beach met Wednesday night to figure out how to pay for several super sized sandbags on the north end of the island.
Full story... » Continued beach erosion exposes more sandbags at The RiggingsSubmitted by Marissa Jasek on Fri, 10/05/2012 - 3:11pm.READ MORE:
With beach renourishment way overdue, residents at a Pleasure Island condo complex say the sandbags protecting their homes have been more exposed than they normally are.
Full story... » N. Topsail Beach uses sandbags to combat severe erosionSubmitted by Marissa Jasek on Mon, 04/30/2012 - 9:38pm.READ MORE:
Topsail Reef is at the mercy of Mother Nature. The eight buildings, housing 240 homes needed protection from some major erosion, caused by a combination of Hurricane Irene, winter storms and high tides. The condo complex elected to have sandbags installed as a temporary fix.
Full story... » NC Coastal Resources Commission says sandbags must be removedSubmitted by Nadine Maeser on Fri, 09/17/2010 - 9:18am.READ MORE:
Sandbags are the last line of defense for many beach front homeowners, but the North Carolina Coastal Resources Commission says they have to go. The removal of the sandbags in Kure Beach is a very sensitive subject.
Full story... » |


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The Innisfree Companies
Latest News: December 1, 2010 WE HAVE MOVED! We are pleased to announce that The Innisfree Companies have moved to new offices in downtown Sausalito. (Note: Phone and FAX numbers have not changed.) Our new location is: The Innisfree Companies phone:
415-332-6250 Thank you for contacting The Innisfree Companies. Our new web site is under construction and will be available shortly. In the meantime, please contact us at email: email@example.com
Last Updated: December 10, 2010 |


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- Information for:
- Explore BSC
- Are you ready?
Admitted students experienced Birmingham-Southern at the Select 'Southern event held on March 1-2, 2015.
- Campaign for Excellence
Admitted students experienced Birmingham-Southern at the Select 'Southern event held on March 1-2, 2015.
The 2014 Battle of the Greeks takes place from Monday, March 17 through midnight on Thursday, April 10. This year the fraternities and sororities whose alumni have the highest alumni giving percentage and raise the most money for the Annual Fund during the Battle of the Greeks will receive points in the Greek Week competition.
Help your chapter earn points for the Greek Week title—make a gift online at www.bsc.edu/egiving. Be sure to check back here for updates and "like" the Battle of the Greeks Facebook page at www.facebook.com/battleofthegreeks to hear the latest news. Then, spread the word! If you're using social media, use the hashtag #2014GreekBattle to keep the conversation going.
Alumni Giving Percentage by Chapter as of April 10, 2014
(Includes Greek alumni who have given to BSC since June 1, 2013 )
Overall BSC Alumni Giving Percentage: 20.4%
Annual Fund Totals by Chapter as of April 10, 2014
(Gifts made to the Annual Fund between March 17 and Aptil 10, 2014 )


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Find an Internship or Volunteer in Rowland Heights, California ( CA )
If you're looking for internships or volunteer work in Rowland Heights, California or even to get a summer job, you've come to the right place! With over 30,000 around the county, chances are that GrooveJob.com has the right job for you and wants to be your only source for finding internships and volunteer positions in Rowland Heights, California.
We've got plenty of intern and volunteer work in Rowland Heights, California. Check out the list of employers below who have positions in Rowland Heights. Remember to check back with Groovejob.com on a regular basis. We add new internships and volunteer jobs listings to our database every week, so you'll find new opportunities every time you check back with us.
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Click for Intern or Volunteer at SEAWORLD ADVENTURE PARK | Click for Intern or Volunteer at INROADS | |
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Filed Under: How to pose with a tool. WERK!
The voting isn't over yet, but c'mon it's in the bag at this point. I remember buying this magazine when I was younger and getting aroused. I still have my copy…I think. SMH Update: Voting is over. Michael wins! Yay!
Dangerous Lee Takes The SmarteRita "Get Waisted" Challenge My Thoughts On Angelina Jolie's Double Mastectomy Cash Money Records Ignorantly Signs Paris Hilton Jody Watley Favorites, Retweets & Responds to Dangerous Lee! Keep it Dangerous! Moment With Captain Kirk! Picking The Right Hair Color For Your Skin Tone Is Religion Relevant In Modern Times? 6 Unique Ways To Release Your Anger Why The Bathroom … Continue reading
Not long ago, computers were used mainly for, well, computations. But with the advances that seem to be coming at ever faster rates, computers have left the realm of purely mathematical application and made a place for themselves in every field of interest. The earliest computer designers could never have foreseen how one day the … Continue reading
In a world of wars, diseases, poverty and politics some think taking a selfie is killing us as a people *blank stare*. Really? Check these Facebook comments and add your 2 cents!
Photographers will secretly tell friends that they'd snap pictures of anyone, anything or anywhere regardless who says what. Onlookers would probably snub photography sessions in certain situations where photos aren't necessary, would cause harm to self-image or could be borderline totally unappreciated. Amidst forays of good reasons pictures are excellent keepsakes reside several situations where … Continue reading
Are YOU Flint Positive?
Today, photographers are constantly experimenting and trying to create unique shots. We live in an age where unique visuals can be such an asset, and your photography could turn up in unexpected places on the Internet. Separating your own artwork from the artwork of so many others is an increasingly difficult task for all creative … Continue reading


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What does IFC mean in General?
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- International Finance Corporation, IFC(noun)
- a United Nations agency that invests directly in companies and guarantees loans to private investors; affiliated with the World Bank
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Bemidji Pioneer
Driver knocks out N.D. town's water service; charged with DUI
Prairie Island nuclear plant unit shut down; operators investigate fire alarm
Man found dead on Mille Lacs reservation with gunshot wound
Alexandria man accused of soliciting 13-year-old girl for sex
Juveniles arrested in Ebro drive-by shooting
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GIRLS PREP BASKETBALL: Red Lake rolls Laporte, Walker routs Blackduck in Section 8A openers
SWIMMING: Lumberjacks to compete in four events at state meet
MEN'S HOCKEY: Beavers fighting to stay home (video)
COMEBACK FALLS SHORT: Bemidji rallies but can't dethrone defending champ Edina (photo gallery)
Bring on the champs: Bemidji takes on two-time defending champion Edina in Class AA quarterfinals
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Margie Carlson
Mae Viola Larson
Neal LeRoy Hazelton
Mary A. Rytter
John Frank Falk
Scotty Allison: Veterans Day on the Hill this week
John Eggers: How can you help all kids graduate?
Blane Klemek: The European starling a species of bird that seems to be around everyday
Don't let negativity sink your boat
Northland Stargazing: Open clusters, saints' days, and the vernal equinox
Off The Record Blog: 'Parks And Recreation' Goes Out On A High Note
Art briefs - Sunday March 1
PIONEER PREVIEWS: Ensemble's concert harkens to spring
Pioneer Previews: Much to do as March approaches
Art briefs - Sunday Feb. 22
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A hefty turnout for the Northland Fat Bike Rally (photo gallery)
PAUL NELSON FISHING COLUMN: March a favorite time for many anglers
PAUL NELSON FISHING COLUMN: Anglers' attention turns to perch as season winds down
Peterson, Northland Tackle honored by Fishing Hall of Fame
Blane Klemek: Here one day and gone the next
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Lopez-Aube engagement
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Tom Purcell: Overreaching in plain English
Eric Fisher and Dan Dorman: Workforce housing key to economic growth in Greater Minnesota
Joseph Cotto: Altruism no substitute for helping yourself
Joe Gandelman: Giuliani: America's hack
Ron Paul: DHS: What is it good for?
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Weather Forecast
January 27, 2015
UPDATE 5:30 P.M.: Injured man identified in Monday night house explosion
BEMIDJI -- Bemidji firefighters responded to a report of an explosion Monday night at a residence southwest of Bemidji near the Grant Valley Township line. The Beltrami County Sheriff's Office issued a preliminary release Monday night that included a caller at 5:49 p.m. reporting...
January 27, 2015 - 1:48pm
January 1, 2015
Fire sparks community response: Bemidji donors rush to aid Tuesday's fire victims
BEMIDJI -- As a new year arrives, friends are rallying to provide a chance at renewal for a Bemidji teacher and her family dealing with more than enough adversity. Debby Yates, a special education teacher at Central Elementary, was with her family in Rochester, Minn., on Tuesday,...
news / local
January 1, 2015 - 5:03pm
December 8, 2014
Two dead, three injured in northern Minnesota fire
DEER RIVER, Minn. -- Two people died in a fire early Saturday at a home in northeastern Cass County, authorities reported Sunday. Three other people escaped with minor injuries from the rural Deer River residence, the Cass County Sheriff's Office reported. According to the...
news / region
December 8, 2014 - 10:41am
October 9, 2014
Fire at Bemidji business Thursday afternoon
BEMIDJI -- The Bemidji Fire Department responded to a fire at Jim's Small Engine Repair shop Thursday afternoon. At approximately 3 p.m. a call came in of a fire on the 2300 block of Roosevelt Road SE. Occupants in the attached home escaped the structure and were tended to by...
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October 9, 2014 - 4:34pm
August 7, 2014
Frohn Township house fire a total loss
BEMIDJI -- A home in Frohn Township was fully engulfed in flames when Bemidji and Cass Lake firefighters responded to the scene Wednesday afternoon....
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August 7, 2014 - 5:02pm
Frohn Township house fire a total loss
BEMIDJI -- A home in Frohn Township was fully engulfed in flames when Bemidji and Cass Lake firefighters responded to the scene Wednesday afternoon....
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August 7, 2014 - 8:57am
July 10, 2014
Bemidji woman sentenced for attempted eviction by arson
BEMIDJI -- A woman who attempted to burn down her trailer house to evict her son was convicted of felony first-degree arson Monday. Mary June Klasen, 57, of Bemidji was arrested for arson when she lit two fires at her mobile home at Roosevelt Manor Mobile Home Park on April 30....
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July 10, 2014 - 2:02pm
June 7, 2014
167 calls for Bemidji Fire Department in May
BEMIDJI -- The Bemidji Fire Department responded to 167 calls for service during May, according to the monthly release from the department. An estimated $119,760 in property loss was reported for May. The department estimates $2,025,570 worth of property has been saved and $253,927...
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June 7, 2014 - 11:11pm
June 2, 2014
Woman charged with arson confesses in court
BEMIDJI -- A Bemidji woman plead guilty to arson in Beltrami County Court Monday. Mary June Klasen, 57, confessed to starting her mobile home on fire in an attempt to evict her son on April 30. She was arrested for felony first-degree arson. Klasen stated in court Monday she has...
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June 2, 2014 - 8:31pm
May 29, 2014
UPDATED: Arson suspected in Cass Lake area wildfire
CASS LAKE -- Arson is suspected to be the cause of the Cass County fire on Wednesday afternoon that consumed more than 75 acres and prompted...
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May 29, 2014 - 8:23am
May 19, 2014
Despite recent rains, burning restrictions still in effect for area
BEMIDJI -- Burning restrictions remain in place for Beltrami, Becker, Hubbard, and Wadena counties, a press release from the Minnesota Department of Natural Resources said Monday. "Restrictions will remain until sufficient green up occurs," the release said. Burning restrictions...
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May 19, 2014 - 6:32pm
May 9, 2014
Fed up mom starts trailer on fire to remove son
BEMIDJI -- A mother went to extreme lengths to get her son to move out of her home last Wednesday -- she started her trailer on fire. When a Beltrami County Sheriff's Deputy responded to a report of a fire burning in Roosevelt Manor Mobile Home Park in Bemidji on April 30, Mary...
news / local
May 9, 2014 - 5:29pm
March 5, 2014
School officials rally community in wake of Dickinson fire
With ashes on his head, ashes in one of his schools and an administrator behind bars, Dickinson Catholic Schools President Steve Glasser told students, parents and community members Wednesday at Queen of Peace Catholic Church that it's time to move forward after Monday's fire...
news / region
March 5, 2014 - 3:09pm
Family escapes Hubbard County fire by climbing out window
A Hubbard County family had to climb through a bedroom window of their mobile home early Tuesday morning to escape a fire. The fire, on U.S. Highway 71, rekindled about 9 a.m., when Park Rapids firefighters called for more manpower and water from Menahga. "It's a total...
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March 5, 2014 - 2:29pm
February 24, 2014
Fire contained in Northern Township
BEMIDJI — The Bemidji Fire Department responded to a house fire at 10:35 a.m. Monday morning in Northern Township. The fire was located in the 7000 block of Fairgrounds RD NW. Bemidji Firefighters arrived on scene to find the home full of smoke with a fire on the main floor. Firefighters...
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February 24, 2014 - 10:09pm
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Christian Walling
Mr. Christian Bailey Walling, 17, of Bamberg, passed away on Saturday, August 16, 2014. He was the son of Mr. Michael James Still and Mrs. Kelli Hughes Walling.
Funeral services will be held 4 p.m. Wednesday, August 20, 2014, in the Bamberg-Ehrhardt High School Gym. Burial will follow at the Bamberg County Memory Gardens. Visitation was held from 5 to 8 p.m. Tuesday, August 19, 2014, at the First Baptist Church in Bamberg.
Bailey was a rising senior at Bamberg-Ehrhardt High School and was also very involved with the youth program at the First Baptist Church. He loved hunting, fishing, soccer, and spending time with his family and friends.
Survivors include his father, Michael James Still (Demaris Jowers); and his mother, Mrs. Kelli Renee Hughes Walling (Johnny Parker); sisters, Ashlynn McKynzie Still and Kayleigh Renee Parker; brothers Alexander Batchler and James Mclane Walling; grandparents, Larry and Jennifer Still and Roger and Patti Hughes; great-grandparents Allivean Still and the late Ervin Still and Evelyn Forshey and the late Jack Forshey; and a number of aunts, uncles, cousins and special friends.
In lieu of flowers, the family request that memorials be made to the Youth Program, First Baptist Church, P. O. Box 355, Bamberg, S.C. 29003.
Cooner Funeral Home LLC., Bamberg is assisting the family with arrangements.
The People-Sentinel 8/20/14
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Assassin's Creed: Brotherhood
Question from Wayne-123
Is it the 3 one?
I whet to now.
4 years ago
Accepted Answer
thelakattack answered:
Quite confusing wording.
But no. It's 2.5, think of it that way.
4 years ago
Marinus11 answered:
Nope. The third one will probably not take place during the Renaissance and you also won't be playing Ezio.
4 years ago
dogknight6 answered:
Actually this is the sort of add on and video game so you play as Ezio (Carrying on from ACII) but it will be the 3rd game
4 years ago
This question has been successfully answered and closed
More Questions from This Game
Question | Status | From |
Are there games similar to AC Brotherhood? | Unanswered | gamerman11385 |
Terracotta Pots & Nutmeg? | Unanswered | CALZORZ |
IS there a way to get a 100% chance on a 5 star assassin trainee mission ? | Open | manic2 |
How do I get my assassin trainees to 10th level ? | Answered | manic2 |
What happens to an assassin trainee who fails his contract mission ? | Answered | manic2 |


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Montana This is a State discussion forum and a no bashing zone. This area is here for members who are looking for serious answers for serious questions or discussion and are not looking for comments of a sarcastic or "bashing" nature. Please be aware that if you violate this policy you are in danger of losing your posting privileges on this website Without Warning.The calling out or posting of another members user name in the title of a thread a members personal information IE phone number or address is prohibited. |
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07-14-2007, 11:48 PM | #5 (permalink) |
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holy shit another montana person! whats that make like 3 of us on here now? haha. its all good. good to know ur here. And i agree on the summer sux thing...couple months till Griz football starts and then its back into snowmobile time! perfect.
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text: School of Mathematics and Statistics, Napier University, 219 Colinton Road, Edinburgh EH14 1DJ, UK Abstract. An impulse-based model is developed to represent a coupling between turbulent flow in the atmosphere and turbulent flow in the ocean. In particular, it is argued that the atmosphere flowing horizontally over the ocean surface generates a velocity fluctuation field in the latter's near-surface flow. The mechanism for this can be understood kinematically in terms of an exchange of tangentially-oriented fluid impulse at the air-sea interface. We represent this exchange numerically through the creation of Lagrangian elements of impulse density. An indication of the efficacy of such a model would lie in its ability to predict the observed fractal dimension of lateral trajectories of submerged floats set adrift in the ocean. To this end, we examine the geometry of lateral tracer-paths determined from the present model. Citation: Summers, D. M.: Impulse exchange at the surface of the ocean and the fractal dimension of drifter trajectories, Nonlin. Processes Geophys., 9, 11-23, doi:10.5194/npg-9-11-2002, 2002. |


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March 5, 2015
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Click Here to access the online Public Inspection File
Viewers with disabilities can get assistance accessing this station's FCC Public Inspection File by contacting the station with the information listed below. Questions or concerns relating to the accessibility of the FCC's online public file system should be directed to the FCC at 888-225-5322, 888-835-5322 (TTY), or email@example.com.


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Blog Of The Nation PoJu Takes Denver August 27, 2008 Our Political Junkie's in Denver, with all the highlights from Sen. Kennedy through Sen. Clinton, plus the latest attack ads and political news. Listen Loading… Download Playlist
Tell Me More DNC Backstage Pass: On The Ground In Denver August 26, 2008 TMM Host Michel Martin blogs from the Democratic National Convention in Denver, where she says tensions abound within the party.
Blog Of The Nation Michelle LaVaughn Robinson Obama August 25, 2008 We've gotten to know Barack Obama, so today it's all about Michelle Obama. Listen Loading… Download Playlist
Tell Me More Wisdom from Dr. Carson June 25, 2008 Will the personality of candidate's spouse be of any significance to you at all when choosing a president in November?
Tell Me More John and Cindy, Barack and Michelle, Hillary and Bill ... February 20, 2008 If you're in Texas or Ohio, and are an undecided voter, what does all of this mean to you?


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Sometime around about April Fools' Day, Joan Walsh jumped the shark. Since then, she's got caught out and called out in remarks that were just the teensy-weensiest bit racist, although Joan, being Joan and a bona fide bastion of the Progressive Left abjectly and vociferously denied that she was racist in anyway, whilst at the same time just as vociferously resenting any claim that African Americans could have to being part and parcel of the base whom Joan declares the President has abandoned so callously.
One thing led to another, and Joan got more than a bit rude with several people who disagreed with her point of view on certain things - most notably the fact that since the President declared his intent to run for re-election in 2012, Joan's been on a massive downer and appears to be suffering from DODS - Delayed Obama Derangement Syndrome.
In her last blog, usually written after an appearance on Chris Matthews's Hardball, she admitted that Obama appeared to have a "mirage" of support - which means that he might have the appearance of support amongst his base (whoever and whatever his base may be), but it really isn't support as such.
That confused me. Does that mean people will say they'll support him and then vote the Republican ticket? Or that they'll say they voted but in reality they stayed at home? Who knows? Still, that didn't confuse me as much as her next assertion, made in a Twitter exchange on June 23rd:-
@dpleasant @LaurieInQueens I'm convinced some of the most vicious pro-Obama people are paid by GOP
Mouths closed yet? Chins picked up off the floor?
Yep, you read right. Joan thinks that some of the most "vicious" Obama supporters are paid GOP trolls. She was most likely referring to me, in our last direct exchange, when she accused me of working for Breitbart, simply because I disagreed with her gratuitous criticism. More apt were my accusations that she was climbing on the Obama-bashing bandwagon to prove her own relevancy and to fit in more as an "esteemed" (but unpaid, according to Joanie - yeah, sure) political contributor for MSNBC.
(If you think all those "political contributors" just sit around the table shooting the breeze with Joe and Cenk and Chris and Larry and newly-minted lyin' liar Rachel just for a cuppa Starbucks and a camera in their face for nothing, you seriously need to get out more.)
I know Joan's recently read "Nixonland" and I know the GOP are famous for their infiltration tactics as a part of their ratfucking techniques, but gone are the days of Donald Segretti. Instead, if Joan bothered to open her eyes and ears, she'd find that there are a lot of pretty intelligent, normal, hard-working, everyday people who see exactly what the President has done, how he's done it and - above all - why he's had to do things the way he has. Such people are these that they understand how government works, they know the President doesn't legislate, and, furthermore, they know that in a democracy, one discusses, debates and compromises.
These people know that change that lasts is often incremental. Some of us might remember when FDR implemented Social Security and how it covered a fraction of the people it covers today. Others might remember Jim Crow, still more might remember when a female teacher got paid considerably less than a male counterpart.
These people are the ones who remember that the President has always said that change comes from the bottom up, which is a euphemism for the aristocratic FDR's direct command of "make me."
And these are the people who listened to Candidate Obama's speeches and realised, if not from their content than from reading his work, The Audacity of Hope, that the man presented himself as nothing more than a Left of Centre pragmatist in the mold of his hero, Abraham Lincoln.
If these people are now vociferous to the point of vicious in their support of the President, it's simply because we're effing mad at the trust fund kids from the Progressive end of the political spectrum slamming the President on everything he does and doesn't do to their specification. We're sick and tired of being called Obamabots and derided on sites like Daily Kos, which was allegedly founded as a Democratic website and has turned into a den of hatred for people specialising in pissing on the President and pushing the meme that he's done nothing, yet all the while proclaiming that this criticism is constructive and it's purely done in the name of political policy.
My blue Democratic ass.
The Right walk around with signs of the President dressed like witch doctor with a bone through his nose, and the Firebaggers at FDL get a pass when they refer to him as "boogalu Bush."
The Right accuse him of being a Kenyan mau-mau, while Progressives openly refer to him as the "Affirmative Action President."
Joan would do well to remember that it was a fellow PUMA who started the birther myth in earnest, and she would do well not to forget the PUMA woman who stridently declared she would support no other than John McCain, when Hillary dropped out of the race, because she simply couldn't understand why Democrats would set aside a well-qualified white woman in favour of a black man.
The Right assert that the President is a weak leader, and Joan obliges by pushing the same meme. The Right treat him with open disrespect, while the Left act like Miss Scarlett about to smack Prissy from sheer frustration.
His supporters are sick and tired of being referred to as sycophants for "Dear Leaders" and called "Obama-Lovers" by her newest pet blogger, Glenn Greenwald, who appears to be the tail wagging Salon's dog to such a degree that Joan has to slavishly echo his critique.
In short, our "vicious" support of the President is simply nothing more than a reaction to an irresponsible, lazy, assumptive and downright untrustworthy media who like to think that the majority of Americans are totally incapable of thinking for themselves and need political action explained to them, but always with a spin. And if you're canny enough to disagree, you're deserving of the rudness thrown in your direction.
So, sorry, Joan, "vicious" supporters of the President aren't paid GOP trolls, but whiners, whingers, moaners, and relentless fault-finders and criticizers such as you and the mean girls and guys around you are the underminers taking the corporate penny of people whose agenda is to see the President fail.
Mirror, mirror on the wall, who's the ratfucker after all?
Obama will be a one-term president...and a Michele Bachmann or Sarah Palin or one of the other jokers will take his place.
They will be winners like King Pyrrhus was a winner!
Good comments.


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This script is Copyright (C) 2003-2011 Tenable Network Security, Inc.
Synopsis :
Arbitrary code can be run on the remote server.
Description :
The remote rsync server is vulnerable to an array index
An attacker may use this flaw to gain a shell on this host
Solution :
Upgrade to rsync 2.5.2 or newer.
Risk factor :
Critical / CVSS Base Score : 10.0
CVSS Temporal Score : 8.3
Public Exploit Available : true