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Night At The Museum: Battle Of The Smithsonian Cheats for Nintendo WiiHome / Nintendo Wii /
This page contains Cheats for Night At The Museum: Battle Of The Smithsonian organized by sections for Nintendo Wii. This game has "Action" as genre, made by Pipeworks Software, Inc., released on May 5, 2009. If you can't find a hint or secret in our list, then please check this page periodically for the latest updates.
- Developer: Pipeworks Software, Inc.
- Publisher: Majesco Games
- Genre: Action
- Release: May 5, 2009
- ESRB: Everyone 10+
Get the Animal Ignot in the "Natural History Museum" level. Search the circular middle room with the "tree" object in the middle until you find a picture with trilobites on the wall. Shine your flashlight at it with the Animal power selected to start the puzzle...From: jaredmiller
Video Walkthroughs
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Stuck in this game? Set a specific, clearly defined question and let other gamers answer your question or view answers to previously asked questions. If you think you are an expert then please try to help others with their questions.
How can I get in the elevator??? Please help me!!!...
Posted on: 01-01-2015
How do I get the key in the 2nd room in the Washington art museum...
Posted on: 07-15-2014
What is the intention of the close up shot during the dialogue between larry and brandon...
Posted on: 09-05-2013
I am stuck on the part where you have to jump through the paintings to get to the other side. I have been stuck on this level for awhile now. I can't understand what I am suppose to do. I have gone th...
Posted on: 04-07-2013
How do you empower the painting on Night At The Museum: Battle Of The Smithsonian...
Posted on: 02-12-2012
How do i get thru the airplane hanger?...
Posted on: 09-02-2011
Stuck at the very start, got to empty locker room, outside press the a button has instructed and nothing happens, cant get in...
Posted on: 03-11-2010
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Archbishop and "the First Martyr of Canterbury." He was born in 953 and became a monk in the Deerhurst Monastery in Gloucester, England, asking after a few years to become a hermit. He received ... continue reading
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subset: commoncrawl


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President Obama Recruits Another Rap Star to Talk About Addiction
This time, POTUS sat down with Macklemore.
This time, POTUS sat down with Macklemore.
Obama has had some epic hip-hop moments in the White House and beyond. Check out some of them.
Larry Wilmore calls President Obama the n-word in a joking way during the White House Correspondents' Dinner.
A photo experiment showed that racial bias may largely contribute to Tea Party support.
Find out who he's giving the credit.
Was POTUS disrespected at White House Correspondents' Dinner?
Looks like he'll be staying away from Michelle's Snapchat.
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Obama invited artists to the White House again. This time it was epic.


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|Publication number
|Publication type
|Application number
|Publication date
|Jul 16, 1985
|Filing date
|Sep 12, 1983
|Priority date
|Sep 13, 1982
|Fee status
|Also published as
|Publication number
|Louis A. Bernard
|Original Assignee
|Societe Nationale Industrielle Aerospatiale
|Export Citation
|BiBTeX, EndNote, RefMan
|Patent Citations (15), Referenced by (11), Classifications (9), Legal Events (4)
|External Links: USPTO, USPTO Assignment, Espacenet
The present invention relates to manoeuvring devices ensuring the displacement of loads or machines supported by wheels on a flat platform, between at least two predetermined zones on the platform, and the invention relates more particularly to devices for manoeuvring a helicopter between a landing and take-off area and a garage area contiguous thereto and preferably protected by a hangar, for example on the deck of a ship, so that the displacement of the helicopter from one of these areas to the other is carried out in complete safety, without rupture of the link between the helicopter and the deck of the ship even when the ship is navigating in bad weather.
At the present time, numerous ships, particularly warships, industrial fishing boats and oil prospecting ships, as well as numerous barges and platforms for drilling or developing offshore oil fields, are equipped with a flight deck and an adjacent garage zone, on which a hangar is possible mounted, and adapted for at least one helicopter attached to the unit in question. On ships of relatively low tonnage, such as corvettes or destroyers, the landing and take-off area as well as the adjacent garage area, which are of very limited surfaces, are defined on a deck at the rear of the ship.
In order to facilitate landing, which is the most delicate and most difficult operation, particularly under poor atmospheric conditions, landing aid devices have been developed, in order to reduce the risks of accident.
One of these devices, which is currently used, comprises a hatch opening substantially in the deck of the ship and in which two lateral jaws are actuated by manoeuvring members, generally hydraulic or pneumatic, closing on a probe fast with the helicopter and suspended vertically therebeneath, when said probe has penetrated in the hatch, after the lowering of the helicopter towards the deck provoked by the traction on a landing cable wound on a landing winch and whose end was previously hooked to the lower end of the probe.
This device is used in the following manner: to land, the helicopter hovers with respect to the ship, above the deck. In this configuration, as the horizontal speed of the helicopter with respect to the sea is always low, safety regulations impose that the helicopter moves windward, and therefore the ship too, which must consequently take an "aviation heading", and must most often change course for a time sufficient for the landing. From the hovering helicopter, a messenger cable is lowered onto the deck of the ship, and an end hook on the landing cable is hooked to the messenger cable, which is then raised into the helicopter so that the hook is hooked to the lower end of the probe. This probe is then suspended beneath the fuselage of the helicopter whilst being rigidly fixed thereto and the landing cable, which passes through a central orifice at the bottom of the hatch, most often defined by a circular opening, is then wound on the landing winch disposed beneath the deck, with the result that, by a substantially vertical traction, the helicopter is drawn towards the deck. When the probe has penetrated in the opening of the hatch, the jaws close and clamp the probe therebetween, maintaining the helicopter applied against the deck, whatever the movements of the latter due to the roll and pitch of the ship, and whatever the force of the wind.
It is observed that the sequence of these different landing operations is relatively long and that the ship is therefore forced to change course and make a deviation for an appreciable length of time. This might not be possible if the ship is near the coast, rocks, etc., or may be dangerous if it is a warship thus forced to leave its position within a fleet in combat formation, and to move away from this fleet, consequently exposed to submarine and air attacks, and at the same time weakening the defence system of the fleet. For these reasons, and due to the dimensions and complexity of the structure of such a device on and beneath the deck of a ship, due to its cost and the cost of the considerable modifications which must be made to the ship's superstructure, another landing aid device is being used more and more often.
This second device is a device for quickly securing the helicopter to the deck by a mooring gear or harpoon. A mooring gear, transported by the helicopter, is projected substantially vertically into a grid solidly fixed on the deck of the ship, when the helicopter touches the deck. The mooring device, which is controlled hydraulically, engages and hooks in this grid, then exerts by traction on the grid a force retaining the helicopter on the deck of the ship. This embodiment is advantageous insofar as the specific fittings on the helicopter are no more complex than those of the device comprising a probe, a landing cable and nippers, whilst the specific fittings on the ship are considerably simplified, since it suffices to fix a grid, for example a circular one, in the plane of the deck and in an opening in the central zone of the landing area, which does not present any particular difficulty. Moreover, when the helicopter is equipped with a landing gear with pivoting wheels, in particular of the tricycle type with auxiliary front landing gear, the helicopter may rotate about the mooring gear hooked in the grid, under the effect of the thrust exerted by the rotation of the rotors of the helicopter in order to be aligned in a desired direction, either windward for take-off, or to be displaced on the deck towards a garage area.
In fact, after the helicopter has landed on the deck and after it has been secured by one or the other of the two devices mentioned above, the helicopter must be displaced towards a garage area, preferably into a hangar, in order to proceed with the necessary maintenance and repair operations and/or to clear the landing and take-off area to allow at least one other helicopter to land or take off.
This displacement may also constitute an extremely dangerous operation when atmospheric conditions are poor and when the deck is inclining too much due to the roll of the ship, because the control of the helicopter may be lost during this displacement, and during the indispensable prior operations for lining up the helicopter with a view to this displacement, as the position occupied by the helicopter secured to the deck, after it has landed, may vary considerably from one landing to another.
For these reasons, numerous devices for manoeuvring a helicopter on the ship's deck have already been imagined.
French Pat. No. 2 036 986 describes a device comprising two rails fixed beneath the deck and which ensure the longitudinal guiding (i.e. in the direction of passage from the landing area to the garage area) of two motorized carriages driving toothed pinions which mesh in racks borne by the two rails. Each of the carriages is connected to one end of a crosspiece disposed on the deck, which thus ensures longitudinal displacement. Another carriage is guided along the crosspiece and motorized thereon in order to ensure transverse displacement, whilst a rocking lever, mounted to pivot about a vertical axis at the end of a substantially horizontal arm of the carriage borne by the crosspiece, is hooked on the main landing gears of a helicopter and allows angular orientation of said helicopter. The helicopter is pushed or drawn by this device, depending on whether it is equipped with a landing gear incorporating auxiliary front landing gear or with a tail wheel, and its path on the deck is obtained by combination of the longitudinal displacement of the crosspiece, the transverse displacement of the carriage, and the rotation of the rocking lever. This device, which is complex and cumbersome, can be used only after considerable work has been done on the ship, and it must comprise a specific carriage-rocking lever assembly for each type of helicopter. Moreover, the main landing gears must be equipped with axles for picking up the personalized carriage-rocking lever assembly, and, in the case of a helicopter equipped with an auxiliary front landing gear, the latter must present a considerable offset of wheel. Finally, this device is not directly compatible with the two landing aid devices described hereinabove, since, to hook the rocking lever on the main landing gears without being hindered by the probe or the mooring gear which project beneath the fuselage of the helicopter in the zone precisely disposed substantially between the main landing gears, it is necessary to retract the probe or the mooring device into the helicopter, which is consequently momentarily no longer positively or materially retained on the deck. This is inacceptable.
Certificate of Addition No. 2 157 678 to the French Patent mentioned above describes a similar device in which two guide rails on the deck of the ship guide end bogies of a crosspiece displaced longitudinally by a mechanism of longitudinal sidebands driven in the rails by motorized drums, and the transverse displacement carriage is mounted to slide freely on the crosspiece whilst, as before, the angular orientation of the helicopter is ensured by the rocking lever fixed to the main landing gears and pivoting on the carriage about a vertical axis.
In order to prevent any sudden displacement of the helicopter, either in angular orientation or in transverse displacement, due to the roll of the ship, the device comprises a braking and damping mechanism.
This device presents the same drawbacks as the one described in the main Patent, but, in addition, the path of the helicopter pushed or drawn by this device depends on the orientation given to the wheel or to the wheels of the front landing gear, or to the swivelling tail wheel, for example by a deck hand who also supervises passage through the hangar door since materially there is nothing to ensure that the helicopter follows a sure path.
U.S. Pat. No. 3,830,452 describes a device comprising a guide rail fixed on the deck and along which circulates a carriage driven by a cable passing in the rail and wound on a winch. The carriage is equipped with a sleeve pivoting about a vertical axis as well as about an axis parallel to the axis of the rail, and in which is slidably mounted a box-girder with toothing cooperating with an immobilizing pawl fixed to the sleeve, in order to block the box-girder, of which the two ends are fixed by the interior to the axles of the wheels of the main landing gears, opposite the sleeve and therefore the carriage, after the helicopter has aligned itself on the rectilinear rail. The device also comprises two lateral winches winding two cables hooked on either side of the rear part of the fuselage of the helicopter, in order to allow the latter to be aligned on the rail. The helicopter is drawn via the box-girder after a succession of centering, locking and alignment operations, which is long and fastidious.
In fact, after the ends of the box-girder have been fixed to the axles of the wheels of the main landing gears, a first rough alignment is effected with the aid of the lateral winches. A limited displacement of the carriage on the rail by traction on the cable in the direction of the garage area then provokes a certain slide of the box-girder in the sleeve. Due to the pawl, the box-girder is then immobilized in the sleeve and the helicopter is definitively aligned on the direction of the rail, with the aid of the lateral winches. It is only after then having detached from the helicopter the cables of the lateral winches that the helicopter is effectively displaced towards the garage area, displacing the carriage with the aid of the cable and the winch installed to this end.
This device, which can be used only for manoeuvring helicopters comprising a tail wheel or an auxiliary rear landing gear, is not at all compatible with the landing aid device of the grid-mooring gear type, as the arrangement of a grid in the central zone of the landing area means that part of the rail must be eliminated, with the result that the carriage can no longer be suitably placed for the box-girder that it bears to be fixed on the main landing gears. Moreover, as the pivot axis of the carriage, half way between the main landing gears, merges with the axis of the mooring gear, it is necessary to release the mooring gear from the grid and to retract it into the helicopter in order to be able to fix the box-girder, assuming that this is possible. It follows that the helicopter is momentarily no longer materially retained on the deck of the ship, which is a critical, inacceptable situation taking into account the various movements to which the deck is subjected. Finally, the carriage/box-girder assembly of this device is cumbersome and of complex structure, and the main landing gears of the helicopter must be modified to pick up the box-girder.
U.S. Pat. No. 4,397,254 describes a manoeuvring device compatible with the landing aid devices constituted by the grid/mooring gear device and the probe/landing cable/nippers device. This manoeuvring device comprises a runway on the deck and a carriage mobile on said runway. This carriage bears a vertically mobile probe whose upper end is placed in a device incorporating nippers mounted in the lower part of the fuselage of the helicopter. The probe is borne by a frame which moves transversely on the carriage with respect to the longitudinal direction of the runway and which may be locked in suitable position beneath the nippers of the helicopter, in order to cooperate therewith to maintain the helicopter applied against the deck.
This device is therefore similar to the landing aid device incorporating probe and nippers are borne by the helicopter and the probe is fixed on the carriage moving on the deck.
However, the carriage is equipped, in addition, with a second frame, adapted to move longitudinally with respect to the carriage, and which bears a grid compatible with a mooring gear of a landing aid device of the grid/mooring gear type, with the result that, after landing and cooperation of the mooring gear of the helicopter with a grid in the deck, then the cooperation of the probe of the carriage with the nippers of the helicopter, the mooring gear may be detached from the grid in the deck then engaged in the grid of the second frame of the carriage, after this second frame has been positioned beneath the retracted mooring gear. The helicopter thus rigidly connected to the deck by two links (the probe and the mooring gear) may then be displaced by traction on the carriage.
This device therefore presents the drawbacks of being very complex and of necessitating important, expensive fittings both on the ship and on the helicopter. Moreover, despite the possibility of transverse displacement of the frame which bears the probe with respect to the carriage, it is indispensable to proceed with operations for orientation of the helicopter, for example by special manoeuvres of the front landing gear, to ensure a precise, definitive alignment of the helicopter before its actual displacement, such alignment having to allow the cooperation of the mooring gear with the grid of the carriage and a two-point guiding necessary for the straightness of the helicopter's displacement.
U.S. Pat. No. 3,640,490 describes combined installations for aiding landing and for manoeuvring a helicopter on the deck of a ship, which group together on the one hand a landing aid device of the type incorporating probe, landing cable and nippers, and on the other hand a manoeuvring device chosen from several variants as a function of the type of landing gear with which the helicopter is equipped.
According to a first installation, adapted more particularly for helicopters equipped with a tail wheel, the nippers are borne on a carriage mounted in a rail fixed in the bridge and displaced by traction on a cable wound on a hauling winch.
This installation is complex due to the numerous fittings to be made on the ship, in order to allow a displacement of the device incorporating nippers with the carriage (electro-hydraulic equipment comprising a hydraulic system for manoeuvring the nippers, and set of cables and winches with cable tensioner and accumulator beneath the deck). Moreover, this installation is disadvantageous as the dimensions in height, particularly of the nipper-holding carriage, are large, which is detrimental during landing and prevents reception of certain helicopters and, on the other hand, because the helicopter is towed by the carriage only via the probe which is suspended beneath the fuselage, so that this retractable probe must be mounted on the fuselage by a very rigid, therefore heavy and complex fixing device.
According to a second installation, the carriage for displacing the helicopter on the deck does not bear the nippers, but they are combined with a turntable mounted in the central zone of the landing area. After having landed, the helicopter rests on the turntable and is maintained thereon by the tightening of the nippers on the probe. The table is then turned in order to align the helicopter with a section of take-over rail connected by a switching rail to one or the other of two displacement rails each leading towards one of two garage positions in the hangar. A bearing and drive carriage equipped with hoisting jacks is guided on the rails and placed beneath the helicopter, so that a mechanism for blocking the carriage is joined to the probe, which is allowed due to the cooperation of the turntable and the take-over rail. The helicopter is then also connected to the carriage at the different hoisting jacks and the latter are supplied by a hydraulic system borne by the carriage, in order to raise the helicopter with respect to the turntable, so that, by traction on a cable connected to the carriage and disposed in the axis of the rail chosen, and after release of the probe by the nippers, it is possible to displace the carriage bearing the helicopter towards the corresponding location in the hangar.
This second installation is also disadvantageous due to the complexity of the fittings to be made on the ship, particularly at the combination of the nippers and the turntable and their drive in rotation, especially if it is desired that this table be used to receive helicopters of a certain tonnage. Moreover, a mechanism comprising a cable, a winch and a double rack must be installed for angular positioning of the take-over rail. Finally, the bearing and drive carriage is both complex and cumbersome as its structure must withstand the load of the helicopter and this carriage is equipped with a mechanism for blocking the probe, a hydraulic mechanism for hoisting the helicopter and the corresponding hydraulic system, as well as a device for guiding on the rails. Furthermore, it appears difficult to envisage using such an installation for landing and for the displacements of helicopters which are not equipped with a landing gear incorporating skids.
According to a third installation, more particularly intended for helicopters of which the landing gear comprises an auxiliary front landing gear, the landing aid device is such that the nippers are installed beneath a circular opening in the deck and in which the probe must penetrate, and two rails for guiding a helicopter drive carriage are substantially tangential to this circular opening. After it has landed and after the probe has been clamped in the nippers, the helicopter is aligned substantially parallel to one of the rails by manoeuvring a tranverse winch and two cables hooked on either side of the rear part of the fuselage. A drive carriage, provided on one side with a lateral sleeve in which is slidably mounted a dog for gripping the probe and, on the other side, with a lateral arm whose end is provided with a hooking mechanism, is positioned beneath the helicopter so that the dog grips the probe and the hooking mechanism is fixed to the standard towing attachment which is located on the main landing gear on the corresponding side of the helicopter. The nippers then release the probe and the carriage is then drawn by a cable and a towing winch towards the hangar. This embodiment, although simpler than the preceding ones, presents the drawbacks that the carriage must be specific of the helicopter received if it is desired that the arm hooking mechanism be suitably connected to one of the main landing gears, and that for each rail tangential to the opening for passage of the probe in the deck and for each carriage moving along one of the rails, there is a prohibited zone in this opening, in which the probe cannot be gripped by the dog of the carriage due to the position of the corresponding sleeve projecting into the opening. In this case, the probe can be gripped only by the dog of the carriage guided by the other rail, but if the corresponding location in the hangar is already occupied by another helicopter, it becomes impossible to guide the helicopter which has just landed into the hangar.
Furthermore, it should be remembered that this installation, as well as the other two described in the last Patent mentioned above, are compatible only with a landing aid device of the type incorporating probe, landing cable and nippers, and that they therefore suffer from all the limitations associated with this solution, particularly that the ship must take an aviation heading as explained above, with all the dangers that this represents. Moreover, these three embodiments all necessitate an operation for alignment of the helicopter prior to the displacement towards the hangar, and therefore means specific to this end.
It is an object of the present invention to remedy the above drawbacks, by proposing a device of simple and inexpensive structure, which is easily positioned without imposing important modifications of the helicopter and of the ship's superstructure.
It is a further object of the invention to provide a device adapted to manoeuvre helicopters of which the landing gear comprises at least one swivelling wheel and which is directly compatible, without it being necessary to proceed with special fittings, with the landing aid devices of the grid/mooring gear type and of the probe/landing cable/nippers type.
To this end, the device according to the invention, adapted to manoeuvre a machine supported by at least one swivelling wheel, such as a helicopter, between two predetermined zones on a flat platform, such as a landing and take-off area and a garage area on the deck of a ship, and which comprises a towing mechanism, adapted to drive the machine from one zone to the other, at least one guide rail installed on the platform and extending from one zone to the other, along which at least one guiding carriage provided with a member for connection to the machine is adapted to move, is characterized in that it further comprises at least one guide bar adapted to be connected by one end to the swivelling wheel and to be engaged and guided by the other end in a guide rail, so that the machine is automatically and progressively recentred and aligned on the rail at the beginning of the displacement from one zone towards the other, due to the combined effects of the carriage and of the guide bar.
According to the invention, when the carriage guide rail is curved, particularly in its part which extends over the garage area, in order to benefit most from the surface available at this spot, the guide bar is engaged in a guide rail different from the carriage guide rail, so that the curves of the carriage guide rail are negotiated without the tyres of the main landing gears skidding, whilst the helicopter remains plumb above the carriage.
On the other hand, if the carriage guide rail is rectilinear, which facilities displacements in the two directions from one zone to the other, this rail may simultaneously be used as rail for guiding the guide bar.
This solution is very advantageous not only when the ship is equipped for the first time with a manoeuvring device, as it suffices to install one rail on the deck per garage location in the hangar, but also when the ship is already equipped with a manoeuvring device of the type described in U.S. Pat. No. 3,640,490, which may be considerably simplified by the elimination of all the prior alignment means (turntable or transverse winches) and of which the operation is largely improved by modifications according to the invention. In fact, in this case, the guide rail, the carriage and the towing mechanism of the pre-existing device are the only elements maintained, and it suffices to add thereto at least one guide bar to obtain a device according to the invention, such that the combination constituted by the helicopter, the carriage, the guide bar and the rail effects self-centering during the displacements, without necessitating elements for prior centering and alignment and for locking in centred position.
According to the invention, the end of the guide bar which is not engaged in the rail may be connected either to the tail wheel or to the wheel or wheels of an auxiliary front landing gear of the helicopter, depending on the type of landing gear with which the helicopter is equipped, and the end of the guide bar engaged in the rail is disposed either between the point of connection of the other end of the guide bar and the point of fixation on the helicopter of the member for connection to the carriage, or to the outside of the segment connecting these two points, in the direction of the displacement, depending on whether the helicopter is displaced in one or the other direction from one of the zones to the other.
The device preferably comprises two guide bars of unequal length, the one of smallest length being used with its end engaged in the rail disposed between the point of fixation on the helicopter of the member for connection to the carriage and the point of connection of the other end of the guide bar.
In a preferred embodiment associated with the landing aid device incorporating grid and mooring gear, which is easy to install on a ship, which does not require the presence of personnel on the deck, allows the pilot of the helicopter complete freedom and permits landing in all directions, without the ship taking the "aviation heading", as well as the pivoting of the helicopter with rotors rotating, by the orientation or offset of the front wheel, if the landing gear comprises an auxiliary front landing gear, the member for connection of the carriage to the helicopter is a telescopic connecting rod, mounted to pivot on the carriage by one end and of which the other end is adapted to be mounted to pivot on a fitting fast with the structure of the helicopter beneath the fuselage thereof, in the median longitudinal plane of the helicopter, and this telescopic connecting rod permanently exerts a traction on the helicopter, during manoeuvring thereof, in order to increase its stability on the ship's deck. This telescopic rod may be replaced by a simple cable tensioned by a jack located on the carriage.
In this case, the towing mechanism advantageously comprises two winches, disposed in the axis of the carriage guide rail, on either side of the path of the helicopter, and two cables each wound on one of the two winches, and such that one of the cables is adapted to be hooked to a point of fixation on the front of the helicopter, in order to displace the latter from one zone to the other when the corresponding winch operates as towing winch, whilst the other cable is adapted to be hooked to a point of fixation on the rear of the helicopter, in order to displace the latter in opposite direction when the corresponding winch operates as towing winch.
During these displacements, the two cables are preferably hooked to the helicopter and one of the winches operates as a towing winch whilst the other operates as retaining winch, the two cables being constantly maintained tensioned.
In order to clear at least partially the zone of the grid of the landing aid device which separates the carriage guide rail from the point of hooking of the mooring gear in the grid, the device according to the invention further comprises a small connecting rail which makes it possible to bring the carriage sufficiently near to the structural fitting of the helicopter for the telescopic connecting rod to be connected to this fitting.
The invention will be more readily understood on reading the following description with reference to the accompanying drawings, in which:
FIG. 1 shows in plan an overall view of the rear deck of a ship equipped with a landing aid device of the grid/mooring gear type and with a device according to the invention, as well as a helicopter with tricycle landing gear incorporating a front auxiliary landing gear.
FIG. 2 shows a view similar to FIG. 1, after the helicopter has pivoted.
FIG. 3 is a partial plan view of the helicopter upon landing.
FIG. 4 is a view similar to FIG. 3 after the helicopter has pivoted.
FIG. 5 is a view similar to FIG. 3, after the guide bar has been positioned.
FIG. 6 is a view similar to FIG. 3 at the beginning of displacement of the helicopter towards the hangar.
FIG. 7 is a view similar to FIG. 3 showing the helicopter in the course of displacement towards the hangar.
FIG. 8 is a view similar to FIG. 3, showing the helicopter in the course of displacement towards the take-off area.
FIGS. 9 and 10 are schematic views, respectively in perspective and in section along the axis of a rail of a device according to FIGS. 1 to 8, of which the rail is fixed in the deck.
FIG. 9a is a view in perspective of the carriage equipped with a variant connecting cable.
FIG. 11 is a partial sectional view showing, in front view, the fixed rail, the carriage and the connecting rod of the device according to FIGS. 9 and 10.
FIG. 12 is a view similar to FIG. 11 of a device of which the rail projects with respect to the deck.
FIG. 13 is a side view of the device shown in FIG. 12.
FIG. 14 is a view similar to FIG. 1 of the rear deck of a ship equipped with a landing aid device of the type comprising a probe, nippers and a landing cable, and as described in the U.S. Patent mentioned above, of a device according to the invention, and on which a helicopter has just landed.
FIG. 15 is a view similar to FIG. 14 which shows the helicopter at the beginning of its displacement towards the hangar.
FIG. 16 is a partial plan view showing the helicopter after having landed and after the guide bar has been positioned, and
FIG. 17 is a view similar to FIG. 16 showing the helicopter at the beginning of displacement towards the hangar.
Referring now to the drawings, in FIGS. 1 and 2, the after deck 1 of a ship is divided into a landing and take-off area 2, located at the rear of the ship, and a garage area 3 adjacent thereto and protected by a hangar, in which two helicopters equipped with a tricycle landing gear with auxiliary front landing gear may be secured. In the plane of the landing area 2 there is installed a grid 4, centred on the longitudinal axis of the ship, of a landing aid device which also comprises, on each helicopter 5, a mooring gear or harpoon indicated at 6, borne by the helicopter 5 in the longitudinal and median plane of the latter, between the two main landing gears.
The device for manoeuvring the helicopter 5 between the landing area 2 and the garage area 3 comprises two rectilinear guide rails 7 which extend from the grid 4 substantially to the back of the garage, in divergent manner, and a winch 8, on which is wound a front cable 9 whose free end is equipped with a hook, and disposed at the end of each rail 7 in the hangar, whilst another winch 10, on which is wound a rear cable 11, whose free end is also equipped with a hook, is disposed to the rear of the ship, substantially at the point of merger of the axes of the two rails 7.
As shown in FIGS. 9 to 11, the rails 7 are fixed in the deck 1 and are each in the form of an elongated parallelepipedic box, which opens in the deck 1 via a groove in the median part of its upper face, and a carriage 12 is received in each rail 7. Each carriage 12 comprises vertical bearing rollers 13 disposed at the four corners, and two lateral, horizontal rollers 14, ensuring guiding against the lateral walls of the rails 7, as well as an upper vertical attachment 15 passing in the opening in the deck 1 and on which one end of a telescopic rod 16 is mounted to pivot about a transverse axis with respect to the direction of the rail 7, and with a certain transverse angular clearance, the other end of said rod being adapted to be mounted to pivot with the aid of a pin 17 on a structural fitting 18 fixed beneath the fuselage of the helicopter 5, substantially plumb with the axis of rotation of the main rotor thereof. As shown in FIG. 9a, the carriage 12 may be connected to the helicopter 5 by means of a cable 43 tensioned by a jack 44 of which the body 45 is fixed longitudinally on the carriage 12. The cable 43 is fixed to the end of the rod 46 of the jack 44 and passes over a pulley 47 of horizontal axis, disposed at the end of the carriage 12. The end of the cable is provided with a heart-shaped thimble 48 to allow its connection with a hook rigidly fast with the lower structure of the helicopter 5. On the ship, the manoeuvring device also comprises two guide bars of unequal length, of which the longer, 19, is shown schematically in FIGS. 5, 7 and 10, and the shorter, 20, in FIG. 8, and of which each comprises at one end a roller 21 for engagement in one of the rails 7 and at the other end, a fork joint 22 fixed to the two ends of the axle of the two twin wheels 23 (i.e. mounted side by side on a common axle) of the auxiliary front landing gear of the helicopter 5.
As shown in FIG. 9, the longer guide bar 19 may be constituted by a fork joint 22 removably mounted at one end of a bar 24 so as to be rigidly connected thereto, for example by connecting elements of square section, preventing any relative rotation, and the other end of the bar 24 is removably and pivotally mounted on the engaging roller 21 which is provided with two rollers 25 rolling in the rail 7, mounted at the ends of the horizontal bar of a T-shaped element, of which the vertical bar passes in the opening in the deck 1, in order to be fixed to the bar 24, whilst the shorter guide bar 20 is simply constituted by the assembly of the fork joint 22 directly on the engaging roller 21.
However, the guide bars 19 and 20 may be made in other different ways so that the engaging roller 21 can be easily introduced into the rails 7.
The device is completed on the helicopter 5 by a front fixing attachment 26, on the auxiliary front landing gear, which is none other than the towing attachment which is always provided on this landing gear to allow possible de-bogging of the helicopter, and which, within the device according to the invention, is adapted to hook one of the front cables 9, and the device is finally completed by a rear fixing attachment 27, beneath the rear part of the fuselage, and adapted for hooking the rear cable 11.
The front fixing attachment 26, the structural fitting 18 for fixing the telescopic rod 16, the mooring gear 6 and the rear fixing attachment 27 are disposed in that order from the front to the rear of the helicopter, and in the median longitudinal plane thereof.
In order to be able to fix the guide bars, two other attachments are provided at the ends of the axle of the wheels 23 of the auxiliary front landing gear.
This device is used as follows: just after landing, the helicopter 5 is for example in the position shown in FIGS. 1 and 3. The mooring gear 6 is hooked in the grid 4 solidly fixed to the deck 1 and the landed helicopter 5 is held on the deck 1. The rotors of the helicopter still rotating, the helicopter then pivots about the mooring gear 6 by the orientation of wheels 23 of the front landing gear, due to the implantation of the mooring gear 6 in the median longitudinal plane, between the main landing gears, and the helicopter pilot causes the apparatus to pivot as indicated by arrow F until the attachment fitting 18 beneath the fuselage is substantially vertical with respect to that rail 7 which leads to the location in the garage intended for this helicopter 5, as shown in FIGS. 2 and 4. The carriage 12 is displaced by rolling it in the corresponding rail 7 from the hangar, and it is positioned beneath the helicopter 5, then the telescopic rod 16 is hooked to the fitting 18 with the aid of pin 17, and the rod 16 is tensioned, with the result that it exerts a traction on the helicopter 5 in order to increase the stability thereof on the deck 1 of the ship, and to lock the helicopter 5 on the carriage 12. After the rotors have stopped, the blades of the helicopter can then be folded, for example all rearwardly, as shown in FIG. 10, and the longer guide bar 19 is mounted by the fork joint 22 on the axle of wheels 23 of the front landing gear and engaged in the corresponding rail 7 by roller 21, at a point located in front of the front landing gear, in the direction of the hangar, after a corresponding orientation of the front wheels 23. The corresponding front cable 9 is then hooked on the attachment 26 of the front landing gear, and the rear cable 11 on the rear attachment 27, and these cables are tensioned by winches 8 and 10, as shown in FIG. 5. As the helicopter 5 is then retained on the deck 1 not only by the tensioned connecting rod 16 but also by the cables 9 and 11, it is then possible to detach the mooring gear 6 from the grid 4. After detachment of this mooring gear 6, a traction is exerted on cable 9 by winch 8 operating as towing winch, whilst winch 10 operates as retaining winch, with the result that the rear cable 11 always remains tensioned and unwinds progressively as the front cable 9 winds on winch 8. The helicopter 5 is thus displaced towards the hangar, in a movement determined by the displacement of the carriage 12 attached to the fitting 18 and of the roller 21 of the guide bar 19 in the rail 7, in the direction indicated by arrows F' in FIG. 6. From the beginning of the displacement of the helicopter 5, due to the presence and position of the guide bar 19 with respect to the carriage 12, the helicopter 5 automatically and progressively recentres and aligns on the axis of the rail 7, as shown in FIG. 6, and very rapidly, the helicopter 5 takes the position aligned on the rail 7, as shown in FIG. 7, up to its position on its garage location in the hangar, as shown in dot-and-dash lines in FIG. 3. In the hangar, the telescopic rod 16 is maintained in place on the helicopter 5, and the latter is in addition secured by means of chains. The front cable 9 and rear cable 11 are then unhooked.
To bring the helicopter 5 from the hangar to the take-off area 2, the rod 16 still being tensioned between the helicopter 5 and the carriage 12, the small guide bar 20 is fixed on the axle of wheels 23 by its fork joint 22 and its roller 21 is introduced and engaged in the rail 7, at a point located between the wheels 23 and the connection of the carriage 12 to the fitting 18 by the telescopic rod 16, then the front cable 9 is hooked on the front attachment 26 and the rear cable 11 on the rear attachment 27, and the cables 9 and 11 are tensioned. The chains for securing the helicopter are removed and winch 10 is operated as towing winch and winch 8 as retaining winch, so as to displace the helicopter 5 in the direction indicated by arrow F", as shown in FIG. 8, in the direction of grid 4. When the helicopter is such that the mooring gear 6 is above the grid 4, the mooring gear 6 is engaged therein, then the two cables 9 and 11 are unhooked, the guide bar 20 is removed and the telescopic rod 16 is released. The rotors of the helicopter 5 may then be rotated, the helicopter then faces the wind by rotating about the mooring gear 6 and then takes off, unhooking the latter.
After landing, to allow the carriage 12 to move sufficiently close to the fitting 18, so that the telescopic rod 16 can be fixed to the helicopter 5, whenever the mooring gear 6 is engaged in the part of the grid 4 located towards the rear of the ship, it may be necessary to position a section of connecting rail (not shown) in line with the chosen rail. This may be very easily carried out when the rail projects from the deck 1, as is shown in FIGS. 12 and 13. In this case, the rail 7' is laterally connected to the deck by inclined sections 28 and, for a precise type of helicopter, allocated to the ship, the width of the rail 7' may be adapted to that of the two twin wheels 23 of the auxiliary front landing gear, in order to obtain additional guiding. Similarly, the width of the inclined sections is chosen for the total width of the rail 7' and of the two inclined sections 28 to be compatible with the centre-to-centre distance of the wheels of the main landing gears, in order to obtain an improved guiding of the main landing gear.
Moreover, it will be noted that the rectilinear rails 7 and 7' make it possible, without difficulty, to carry out the manoeuvres in both directions between the hangar and the take-off and landing area 2. If rails 7 or 7' are curved, in order to benefit most from the surface available in the hangar for example, the displacements will be effected in the same manner, but the roller 21 of the guide bars 19 and 20 will be engaged in a rail other than rails 7 and 7', so that the curves of these rails 7 and 7' are passed without the helicopter 5 ceasing to be above carriage 12.
FIGS. 14 to 17 schematically show another embodiment of the manoeuvring device according to the invention and the operation thereof.
This second embodiment of manoeuvring device is compatible with a landing aid device of the type comprising a landing cable, a probe and nippers, as described hereinabove. The manoeuvring device comprises, in this case, a guide and drive carriage, displaced along a rail by a cable and a winch of the type described for example in U.S. Pat. No. 3,640,490 mentioned above.
With this guide rail and with this carriage which cooperates with the probe of the helicopter, and with which a ship may already be equipped, there are associated two guide bars 19 and 20 which are fixed, as before, by the fork joint 22 to the axle of that (or those) of the wheels of the landing gear of the helicopter which swivels, and of which the engaging roller 21 is engaged in the rail.
FIGS. 14 and 15 show a rear deck 1 of a ship and a helicopter 5, identical to those shown in FIGS. 1 and 2. Elements identical to the elements shown in FIGS. 1 to 13 are given the same references.
The rails 37 and the guide and drive carriages 42 as well as their drive means, are those of a manoeuvring device already existing on the ship, and of which the components are used in the manoeuvring device according to the invention.
In FIG. 14, after landing, the helicopter is held against the deck 1 by its probe which is clamped in the nippers, and then by its link with carriage 42. Then, as shown in FIGS. 14 and 16, the guide bar 19 is positioned in the same manner as described in the preceding embodiment. The blades of the helicopter 5 are then folded, for example all rearwardly, as soon as the rotors stop, and the drive means of the carriage 42 are operated, and, as soon as it begins to taxi, as shown in FIG. 17, the helicopter 5 recentres and aligns progressively and automatically on the axis of the rail 37 chosen due to the presence and to the position of the bar 19 with respect to the carriage 42. Very rapidly, the helicopter is aligned as shown in FIG. 15, whilst being displaced towards the hangar.
The displacement in opposite direction, from the hangar towards the take-off area 2, is effected as in the first example, by substituting the small guide bar 20 for the large one 19, by engaging its roller 21 in the rail 37 between the front wheels 23 of the front landing gear and the carriage 42.
It is thus noted that, in both embodiments, the combination of a helicopter, a carriage, a rail and a guide bar at least effects a self-centring, in the course of manoeuvring, so that the latter is more rapid and it is no longer necessary to mount a special device for alignment and for locking in alignment.
By simply substituting the two guide bars for prior alignment and locking devices, operational safety of existing installations combined with a landing aid device of the type comprising a landing cable, a probe and nippers, is largely improved.
On the other hand, when first fitting a ship with a landing aid device of the grid/mooring gear type, or when a ship is already equipped with such a device, it is advantageous to install a manoeuvring device according to FIGS. 1 to 13, as, in addition to the advantages mentioned above, the carriage is drawn by the helicopter and is therefore not a tractor carriage, as is the case in all similar prior art installations, with the result that this carriage is not subjected to bending forces, and the telescopic rod for connecting the carriage to the helicopter exerts a pulling force on the helicopter, which applies the latter on the deck and increases stability thereof during the manoeuvres.
In addition, the helicopter is automatically oriented at the beginning of taxiing without the tyres of the main landing gears skidding.
Finally, in this case, it is not necessary for the ship to take an "aviation heading".
Although the two embodiments of the manoeuvring device according to the invention have been described hereinabove in their use for a helicopter equipped with a landing gear incorporating an auxiliary front landing gear having swivelling wheels, these two devices may also be used on helicopters equipped with a swivelling tail wheel.
|Cited Patent
|Filing date
|Publication date
|Aug 2, 1928
|Mar 4, 1930
|Schmelz Ernst M
|Aircraft-launching apparatus
|Jun 12, 1936
|Jan 19, 1937
|Albin L Ekstrom
|Vehicular apparatus
|Aug 6, 1943
|Oct 16, 1945
|Loeser Jr Oscar
|Method and apparatus for mooring airships
|Apr 2, 1962
|Dec 22, 1964
|Superior Scaffold Co
|Ground handling system for aircraft
|Mar 9, 1966
|Nov 12, 1968
|John H. Miller
|Race track with cooperating race car retaining means
|Jul 24, 1967
|Aug 5, 1969
|Wilson C Shepheard
|Rack rail aircraft moving locomotive
|Jan 13, 1970
|Feb 8, 1972
|Nat Defence Canada
|Shipborne conveying means
|Jun 22, 1973
|Aug 20, 1974
|Kaman Aerospace Corp
|Monorail traverse system
|May 7, 1979
|Mar 16, 1982
|Mario Pesando
|Traverser and components therefor
|Jul 15, 1980
|Aug 9, 1983
|Westland Aircraft Limited
|Apparatus for moving a helicopter along a deck
|Sep 3, 1981
|Mar 17, 1982
|MacTAGGART SCOTT & COMPANY LIMITED
|Improvements in or relating to aircraft handling systems
|Title not available
|Title not available
|Title not available
|Oct 22, 1982
|Apr 28, 1983
|Bruce-Walker, Patrick
|A system for load handling
|Citing Patent
|Filing date
|Publication date
|May 9, 1984
|May 5, 1987
|Blohm + Voss Ag
|Apparatus for moving aircraft
|Jun 16, 1986
|Nov 29, 1988
|Mactaggart, Scott (Holdings) Limited
|Aircraft handling systems on ships
|Mar 28, 1991
|Mar 24, 1992
|Aerospatiale Societe Nationale Industrielle
|Helicopter traversal system
|May 26, 1992
|Sep 28, 1993
|Riva Calzoni S.P.A.
|Device for gripping and handling helicopters, particularly for ships' decks, platforms and the like
|Jan 20, 1995
|Nov 5, 1996
|Mactaggart Scott (Holdings) Limited
|Aircraft restraining system
|Nov 7, 1996
|Feb 1, 2000
|Mactaggart Scott (Holdings) Ltd.
|Aircraft handling apparatus
|Oct 2, 2012
|Abe Karem
|Seabasing ship
|Dec 23, 2008
|Oct 1, 2013
|Abe Karem
|Seabasing ship
|Oct 22, 2009
|Jul 22, 2014
|Airbus (S.A.S.)
|Method for moving an aircraft along the ground
|Oct 22, 2009
|Oct 27, 2011
|Airbus Operations
|Method for moving an aircraft along the ground
|May 23, 1992
|Dec 16, 1992
|RIVA CALZONI S.p.A.
|Device for gripping and handling helicopters, particularly for ships' decks, platforms and the like
|U.S. Classification
|244/116, 114/261, 104/244.1
|International Classification
|Cooperative Classification
|European Classification
|Sep 12, 1983
Owner name: SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE, 37 BO
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:BERNARD, LOUIS A.;REEL/FRAME:004173/0770
Effective date: 19830905
Owner name: SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE, FRANC
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:BERNARD, LOUIS A.;REEL/FRAME:004173/0770
Effective date: 19830905
|Jan 11, 1989
|Fee payment
Year of fee payment: 4
|Jan 12, 1993
|Fee payment
Year of fee payment: 8
|Jan 13, 1997
|Fee payment
Year of fee payment: 12


text:
John Wall's return gives Wizards win over Hawks
WASHINGTON -- In the fourth quarter, when he had shook off the nerves and rust and finally found his legs, John Wall starting yelling: "I'm back."
"That's what I was saying the whole time," Wall said. "To anybody. I was just happy to be playing basketball. To whoever was in my way, that's what I was saying."
Wall made his season debut Saturday night, giving his teammates a lift with 14 points and four assists in 21 minutes, highlighted by a left-handed behind-the-back assist when the Washington Wizards were putting the game away in the final minutes.
Saturday night's 93-83 victory over the Atlanta Hawks gave the worst-in-NBA Wizards their first winning streak of the season, and a psychological high point now that their franchise player is healthy again.
"Still the same year," Wizards guard A.J. Price said. "But definitely new life."
Trying not to get carried away in his return from a knee injury, Wall went 5 for 11 from the field and 4 for 5 from the free throw line, saluting the crowd as it gave him a standing ovation when he entered with 4:56 remaining in the first quarter, and again when he fed rookie Bradley Beal for a fast-break dunk, and one more time at the final whistle.
"I was just nervous to see how I would feel. ... My homeboys-slash-brothers were joking, happy the whole day," Wall said. "I'm just trying to stay calm and take a nap."
Although his playing time will be limited while he gets himself in full playing shape, Wall appeared to have his old speed and explosiveness back. It was his first time teaming with No. 3 overall draft pick Beal, and they gave the fans a taste of the speedy backcourt they had waited so long to see.
"The game is different now," Wizards coach Randy Wittman said.
Beal and Price finished with 16 points apiece, and Martell Webster added 15 for the Wizards, who are 6-28 but have strung together two wins in a row following their upset of Oklahoma City on Monday.
Jeff Teague scored 19 points, Al Horford had 16 points and 12 rebounds, and Josh Smith added 11 points for the Hawks, who trailed the entire second half and have lost five of six. Atlanta had won 18 of its previous 19 against Washington, including six in a row.
The Hawks were let down by their defense and took too many 3-point shots (24), but Wall was a difference as well.
"He's gonna give them a different dynamic," Hawks guard Lou Williams said. "Tonight, I think he played well enough to get them over the hump."
The lowlight for the Hawks came when Ivan Johnson missed a wide-open layup by throwing the ball completely over the basket and catching it on the other side, thus committing a traveling violation. The basket would have cut the Wizards' lead to four with about 9 minutes to play.
"We had opportunities, and just some plays went wrong," Teague said. "We had some turnovers."
Wall was expected to miss about two months when he was diagnosed with a stress injury to his left kneecap in late September. He began increasing his basketball activity last month, but it wasn't until Wednesday that he had his first full-throttle practice with the team.
After three consecutive days of pain-free workouts, Wall was given medical clearance Friday to suit up. He hit the floor a couple of times Saturday trying to take a charge, but bounced up with no apparent issues with his knee.
Even with Wall's return, the Wizards are far from healthy. Jordan Crawford (sore left ankle) and Cartier Martin (hyperextended left knee) remain sidelined, and four other players are having their playing time monitored. Trevor Booker returned Saturday after missing 24 games with a strained right knee. Price and Trevor Ariza returned from long injury layoffs in Monday's win over the Thunder, and Nene is nursing tendinitis in his right knee.
And, by the way, Wittman told his players that, in his opinion, they don't really have a winning streak yet.
"They say a winning streak is three, so we've got to get this third one," he said.
Game notes
The Hawks were called for three technicals: Smith and Williams in the first quarter, and Teague as part of a double-technical with Kevin Seraphin in the fourth. ... Wizards F Jan Vesely played four minutes and committed five fouls. ... It must be NFL playoff time: Random cheers were heard throughout the game whenever the Baltimore Ravens made a big play in their overtime win over the Denver Broncos.
ESPN Fan Shop Powered By
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Thunder's small-ball group continues to mystify Draymond Green, Warriors
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text:
I Needed That.
We'd all love a 75-inch TV screen on which to view our favorite shows. But not all of us can drop the cash needed to get one of those broadcasting beauties (or even have the space needed to house them).Thankfully, there's an alternative. With the SainSonic Mini LED Portable Projector (only $59.99 in the Boing Boing Store), you can project a picture […]
If you want to add some real firepower to your programming repertoire, learn Java–one of the most adaptable, widely-used programming platforms around. You can easily do that with this Ultimate Java bundle, now just $69 in the Boing Boing Store.Across 14 lectures and 117 hours of content, the educators at online academy eduCBA will walk you through […]
Every company wants to harness the power of social media, but few understand how to make that happen. Be one of those select few with this Social Media Marketing Course & Certification package, now just $29 in the Boing Boing Store.Over 12 modules of course material, you'll learn what it takes to increase a brand's […]
I Needed That.
Very dramatic crescendo. By the time I got to "Using Tape for loose ends" my heart was pounding.
The increasing font size is one thing, but combine it with the distressing language of problems, failures and dangers…I imagine a textiles apprentice having a panic attack.
If a problem persists, we recommend that you contact
Sewing and Embroidery Warehouse
what the hell wysiwyg editor did they create this in that lets you get away with this and doesn't render it properly?
Microsoft FrontPage 4 lyfe
I'm sure it looks fine in Internet Explorer.
In fact, when I contacted Sewing and Embroidery Warehouse about it, they said the same thing – It looks fine in IE.
OK. I'll admit I opened it in IE first, and it renders just fine. To the point of me getting a bit WTF? I just opened it in Chrome and nearly spit food at the monitor.
There's a woman here in PS who bills herself as a professional web designer and uses FrontPage. She charges ~ $50 an hour. And gets it.
sad for her clients that they don't know better.
OMG my down arrow had been waiting for this for its entire life.
Hah, I don't know why that made me giggle so much. Tracing around that "P" starting the final line with my touchpad to work out what letter it was was more fun than it should have been.
Thank you! It will drive my wife nuts.
it takes 2 days to scroll past a "T" near the bottom
Holy hell, I looked at that site while listening to the phase-shifted Beatles.
OK, I'm feeling like a total idiot here… I can't duplicate it.
I mean, I can copy/paste their code and see it, but if I try:

 line 1

 line 2

 line 3

 line 4

 line 5
It doesn't work. I've tried the table structure, linebreaks, the doctype. I KNOW I'm missing something really silly, it's just been awhile since I've done any html.
Can someone ease my pain?
(The first time I tried posting, BB's site added the closing tags – heh)
make sure to use the right doctype:
<!DOCTYPE html PUBLIC "-//W3C//DTD HTML 3.2//EN">
and combine the lack of closing h3 tags with the magical also unclosed and repeated tag of:
<width="25%" align="left">
it isn't the h3 tag causing this, it is the width tag propagating, closing h3 tags would have prevented this.
It's greatly appreciated. I can stop farking with it now.
I tried it with my standard "XHTML 1.0 Strict" doctype and it still works.
I wonder why the width tag does that?
no problem! :-) that sort of thing drives me mad too, lol.
more then happy to help!
excellent question and to be honest I'm not entirely sure. intuitively I'd think it'd make it 75% smaller each time, but nope.
<!DOCTYPE html PUBLIC "-//W3C//DTD HTML 3.2//EN">

<width="25%" align="left">Test 1

<width="25%" align="left">Test 2

<width="25%" align="left">Test 3

<width="25%" align="left">Test 4
Have you tried adding the CSS line? The h3 { font-size:1.17em }?
Embroidery really is all about the Process.
What's wierd is it looks fine on my android phone. I see it happen on my desktop computers using chrome, ie, firefox or safari, but using my android phone's default web browser or Dolphin's browser all the text is the same size. Not sure how that happens but perhaps the person doing the coding only proofed it on a mobile device.
Just for kicks, in Firefox open Web Developer->Inspect and click on "3D view".
someone please animate this and set it to the opening music from Star Wars.
Being an editore, it took me a bit to get past the headline, which at first made me think that it was a shooting guide by some group called "Embroidery Trouble."
Hey tumblr people I made a poetry of it
They haven't styled h3, so it takes on the browser default styling. In the case of Chrome, h3 is 117% the size of the containing element. So, when you nest tags like this, it gets bigger and bigger.. I assume the same thing happens in Firefox. But if IE styles h3 as having an actual fixed size (like, say, 18 pixels), then it would look alright.
actually, ran some tests…just leaving the h3 tags open doesn't work. you need the magical width tag they also don't close in order to get this effect. see my reply above.
First legitimate belly laugh of the day. LOVED IT
Okay that was seriously funny. I just kept scrolling waiting for when one letter would take up the whole screen!
I tried to turn it into an image with Paparazzi, but it crashed… any clues on how to visualize this at once?
Edit: i learned that zoom.it accepts webpages, but it rendered it correctly: http://zoom.it/f0vJ :(
Comments are closed.


text:
Topanga, CAUSA
Cap Haitien, Haiti
November 1, 2012
New to area n love a nice wine!
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text:
LondonUnited Kingdom
November 8, 2013
No introduction yet
Are you interested in enjoying some of the great things in London?The group will involve events such as; Restaurants, Comedy, Music - classical, pop, jazz, whatever floats your boat, Opera, Theatre, Art Exhibitions, Museums, London Tourist attractions that us Londoners would never normally go to (unless showing visitors around town).
I'll happily arrange some events, but I'm more than happy for others to put suggestions in. For events requiring tickets, I'll put a max group size on, so we can keep the group personal.
If anyone is interested in assisting in arranging meetings, then I'd be happy to hear from you.
I'll aim to arrange one thing every fortnight, or more once there are more people with more suggestions.
As for members - young-minded people who want to meet and enjoy common interests in enjoying some of the London life.
And who knows, we could look at embracing some of the rest of Europe?s culture and environment if there's interest in the occasional weekend away.
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Blasts from the Past
Of Goats and Greens
A blog for food and cookery and discussions of weird things like nutrition, restaurant excursions, growing food in my own garden and on my planned homestead; and anything related.
I'm personally mostly interested in foods made from healthy fats and healthy carbs, low amounts of processed sugars or starches, and I definitely steer to a preference for Real Food. (Would someone's great-grandparent have recognized the item as food?) I've a strong interest in vegetables, seafood, eggs, and "ethnic" foods from around the world. Yes, I do make use of "odd bits". No, I don't bake desserts much -- I really don't have much of a "sweet-tooth". Currently all my recipes are gluten-free, or readily have that option.
Please leave me comments!
Mess O' Tagsapple Asparagus Avocado Beef Brussels Sprouts Cabbage Chicken chicken hearts Cilantro Cucumber Duck Egg Eggplant Eggs Fennel Fish Gluten-Free Goat Goat Cheese Indian Korean Lamb Lettuce Mango Mushroom mushrooms Okra onion Onions Paleo Pork Potatoes Raw Recipe Recipes Salad Salmon Salsa sashimi Shiitake Shrimp Smoked Salmon Soups & Stews Spinach Sweet potato Tomato Turnip Vegan option vegetarian Yogurt
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Monthly Archives: February 2012
Adventuring in Manhattan – Dining Out
I got invited to hang out at a beer bar and an Ethiopian restaurant down in New York City Saturday a week ago (February the 18th), which sounded like a fine idea, especially since it has been years since I've … Continue reading
Posted in Commentary, Dining Out Tagged Ethiopian, French, Goat Cheese, Lamb, Manhattan, Tuna 4 Comments
Bobcat Surprise. And My "The Meal" Photo and Basic Recipe (Salad)
For our first trick, we're going to roast a bobcat… No, only kidding. This is the feller that strayed into my side yard yesterday. The photos are less than stellar, but he (she?) wasn't going to stand still for it. … Continue reading
Posted in Commentary, Garden 1 Comment
The Meal — an attempt to document a meal or a snack photographed Friday 12:00 noon EST, Feb 24th..
I'm not sure what the significance of this all is, but for me it will be a minor bit of fun that I'll go ahead and participate in. http://www.arthousecoop.com/projects/themeal — The Meal. Apparently, they want photographers interested in what they … Continue reading
Posted in Commentary Leave a comment
Another Shad Roe Recipe
All right. I posted about shad roe last year. But no, I found an early shad roe in the supermarket over the last weekend. It's pricey, but I was sort of on the depressed side, and figured it could cheer … Continue reading
Posted in Cooking, Mushrooms, Seafood Tagged Shad roe 4 Comments
Monkfish, Asparagus, Shiitake
1.5 tablespoon quality butter (in my case, pastured Kate's Homemade Butter) 1.5 tablespoon extra virgin olive oil Juice of 1/2 lemon 1/4 cup of extra dry vermouth 1 pound = 1.25 pound of monkfish, sliced into 1/2 inch or smaller … Continue reading
On a Wing and a Prayer
Okay, up front here, serious disclaimer and curmudgeon alert (but we will get to the recipe sooner or later): watching grass grow is more interesting and rewarding to me than watching pro sports, especially football or baseball. Basketball at least … Continue reading
Posted in Appetizers, Commentary, Cooking, Meats, Poultry Tagged Chicken 1 Comment


text: Malaysia takes 'wait-and-see' approach to Sabah standoff: report Posted at Feb 23 2013 01:27 PM | Updated as of Feb 23 2013 09:27 PM MANILA, Philippines -- Malaysian security forces are taking a "wait-and-see" approach on the Sabah standoff. Malaysian news portal The Star Online reports negotiations continue with the group of Rajah Muda Kiram although the Friday deadline to deport them had expired. A Malaysian deputy prime minister is quoted as saying the cautious approach being taken is evidence of the Malaysian government's capability to deal with any situation, adding everything possible is being done to work out a peaceful solution to the "sensitive" problem. Deputy Prime Minister Tan Sri Muhyiddin Yassin also stressed it is crucial that the standoff be resolved without any bloodshed. ANC Dateline Philippines, February 23, 2013 Share Facebook Twitter GPlus LinkedIn Pinterest Kakaotalk Viber WeChat Read More: malaysia sabah /entertainment/06/01/16/aiko-bonds-with-new-boyfriend-son-in-sagada/sports/v2/06/01/16/five-keys-to-the-nba-finals/entertainment/06/01/16/michael-pangilinan-has-yet-to-meet-gabby-concepcion/entertainment/06/01/16/look-james-nadine-in-first-magazine-cover-as-couple/business/06/01/16/henares-keeps-hands-off-plans-of-incoming-bir-chief


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Thresher shark parts sought by study
Bacterial brain infection stranding young sharks
Daniel Powell 2:52 p.m., May 29
Mission Beach alley near Belmont Park
Photo by hphart
Posted March 21, 2012
Daniel Powell 2:52 p.m., May 29
Barbarella Fokos 1:41 p.m., May 29
Robert Bush noon, May 29
Barbarella Fokos 11 a.m., May 29
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Various Authors 4:58 p.m., May 28
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The Wall Street Journal
Sally Beatty
Community, Education
This article can be viewed by downloading the PDF.
Journalist Sura Jeselsohn writes about a recent visit to the Weizmann Institute's Clore Garden of Science. Long fascinated by America's Biosphere project and the idea of self-contained systems, she was delighted to find the Ecosphere and its educational environment. She also praises the Clore Garden for its fun exhibits.
Project-Based Fundraising empowers people of all ages to join the Weizmann Institute's search for answers to humanity's greatest challenges—from fighting cancer to protecting the environment to exploring space. This platform features 12 vital Weizmann research projects in need of support. After selecting a project that inspires you, you can set up your own fundraising page, and mobilize friends and family to join your efforts. Learn more—and get involved.


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The MX42 is a four channel stereo passive (requiring no power) mixer. The unit mixes up to four stereo RCA signals such as CD or cassette players with VCR units, even computer sound cards or MP3 players. All signals are mixed via stereo 100K ohm potentiomenters to stereo RCA output connectors.…
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5 Keys to Fulfill Vision & 3 Pitfalls to Address
Apply these keys to help you harness the power of shared vision in your church.
Rethinking Discipleship: Begin With the End in Mind
"Tell me and I will forget; show me and I will remember; involve me and I will understand."
Take 5 Minutes to Save a Life for Eternity
It took over 40 years for the opportunity to say thank you.
Kingdom Economics: Reversals
As sons and daughters of the most high God, we know that any negative reversal can change into something good.
What You Need to Be Teaching Young Men About Sex
Pastors and ministry leaders, this is the right way to do it.
6 Common Mistakes Churches Make on Social Media
Are there some that you can correct for your church's social media accounts?
Who Told You to Try Again?
We learn from mistakes that trying again may not be God's will.
3 Ways to Make Easter Weekend Special for Your Church Family
Do these things, and you might just prompt people to return.
How You Can Worship God With Tech Gear
By David Leuschner
I used to think the worship team members were "the people who lead music on the platform."
When Should I Hire an Executive Pastor?
It is a rare thing to find a church that has grown past this number of members without the addition of someone in this role.
Meek Is Not Weak
Inner peace comes from knowing who hides you.
5 Reasons to be Grateful for the Local Church
And they are based on a foundation of Scripture.
How to Keep the Volunteers on Your Worship Team Motivated
By Joshua Mohline
Building and managing a team is the most rewarding and, at the same time, the most challenging endeavor a worship leader can undertake.
12 Things Pastors Least Like About Their Jobs
Incredibly, the responses to a survey were quick and numerous.
5 Ways Pastors Can Impact the Businesses of Church Members
Church leaders have a critical role in the establishment of the kingdom of God in the marketplace.
I Choose to Believe in Miracles
God has not changed. The same God who parted the Red Sea is your God too.
Why You Should Put Your Church's Future in God's Hands
By Warren D. Bullock
It all involves faith-filled planning.
What Has Happened to Genuine Relationships Within the Church?
It becomes a real concern when the unchurched become jaded and offended when their church experiences are less than friendly.
Stay in Your Own Lane
Here's why double-minded leaders are ineffective.
Pastor's Wives, Your Support for Your Husband Matters Immensely
Here are five ways you can do that.
Cultivating Kids' Devotion to God
By Lenny La Guardia
Formula-driven children's ministry has dominated the modern church. Often as a result, many curriculum developers have limited rather than empowered what children are expected to do in ministry.
New Law a Major Victory for Pastors Who Refuse to Compromise the Bible
Mat Staver of Liberty Counsel says more needs to be done to protect religious freedom.
How Dare You Call a Church Dead!
Speak life into a struggling church.
Kingdom Economics: Trading for Abundance
For an abundant life in this world and eternal life in the next, we need to make a divine trade.
Mark Rutland: Funeral Drums, Life and Transition
Living through change in the good hands of an unchanging, unchangeable God
Will Contemporary Worship Kill the Choir?
There are certainly differing opinions.
I Don't Care Enough to Pray
Complacency is an observable sign of a disconnect.
The 4 Common High-Attendance Days in Churches
We would be negligent if we did not see the gospel opportunities in reaching new people who might come during one of these spikes.
Jonathan Cahn Proclaims Isaiah's Prophecy At United Nations
Churches Continue to Face Budget Shortfalls
Has it become the new normal for American churches to "just get by?"
My Gut Says Yes, but the Holy Spirit Says NO
Leaders must be willing to hear "no" and obey.
9 Reasons You Should Make the Most of Big Days for Growth
High-attendance days at church can be meaningful in more ways than simply putting bodies in the pews. Find out how.
Turning Tragedy Into Heartfelt Ministry
By Anthony Petrucci
The pastors of Shoreline Church have provided a model for leaders grieving in the wake of family tragedy.
7 Ways Churches Should Die With Dignity
So what can we offer the leaders of dying churches?
The Fix-It-Up Chappie
Sometimes it's better to let it remain broken.
5 Ways to Overcome Ministry Burnout
Here's a remedy for you languishing soul.
Marketplace Ministry: Doing the Greatest Work on Earth
By Linda Fields
Christians influence the marketplace under the blessing of God.
5 Steps When Needed Changes Seem Overwhelming
What do you do in these situations?
Lions May Roar, but Leaders Nurture
Roaring lions seek only to devour.
Writing a New Chapter in Your Ministry
There is a purpose for every season in your life. Seek Him and don't relent until you are clear on what He has for you.
In His Image, God Created Us to Work
By Mark Tedford
This is how the study of apologetics made this man a better steward of his family business.
20 Amazing Implications of the Dominion Covenant
This is what God meant when He gave us "dominion" over this planet.
Leadership Storms
Thunder and lightning surround decision makers.
Kingdom Economics: Do You Have a Career or a Calling?
As citizens of the kingdom, we need to regularly examine our motives.
Christian Chamber of Commerce: Networking for the Kingdom-Minded
By Di-Anne Elise
The CCC provides an environment where business and faith meet, and relationships are formed.
The First Lesson the Lord Taught Me as a Minister
And it's something that will stick with you for a lifetime.
Referees Cannot Take the Game Away
Brown Church Development Group interview
How to Grow Past Your Failures
Here are five common causes of failure and how to overcome them.
ECPA's Stan Jantz Addresses Christian Publishing Marketplace Issues
By Christine D. Johnson
Read this Q-and-A with Stan Jantz, new executive director of the Evangelical Christian Publishers Association.
7 Reasons Monthly Church Business Meetings Are Dying
And, few tears are being shed over it.
Ministry Life
- 4 Reasons VBS Is Important to the Local Church
- How Are We Challenging Our Kids With Theology?
- Moms in Ministry: Where's the Balance?
- 3 Ways to Minister to Your Students' Parents During the Summer
- 6 Ways for Lonely Leaders to Develop Friendships
- 9 Ways Your Church Can Use Twitter on Sundays
- Why Pastors Should Get Away This Summer
- MT 21 Gospel-Driven Business: Snyder Manufacturing Corp.
- 9 Reasons Why We Love Our Children's Ministers
- Message to Seniors in the Lord's Work: Never Retire
Ministry Leadership
- Do You Suffer From 'Analysis Paralysis'?
- When You Come, Everything Else Must Go
- Help! My Small Groups Aren't Growing
- Finding Purpose in Every Season of Your Life
- Intentionality in What Is Said Can Take People a Long Way
- Kingdom Economics: Painful Adjustments
- 7 Relational Skills of Great Church Leaders
- Kingdom Economics: Last Days' Divergence
- 7 Thoughts for Leaders on Managing Conflict
- The Tragic Elimination of the Apostolic From the Church
Ministry Facilities
- 7 Steps to Make an Effective Pre-Service Video
- How Your Building Is Killing Your Growth
- Growing and Giving in the Digital Church
- 3 Creative Ways to Kill Creativity and How to Get It Back
- 10 Amazing Unseen Things That Can Happen in Your Church Every Sunday
- Impact Ministry: The More-With-Less Church
- The Digital Gospel Goes Global
- Prayerful Consideration: To Build or Not to Build
- How Your Church Can Get an Internet TV Channel
- 3 Reasons for Not Using a Tablet for Speaking Notes
Ministry Outreach
- 3 Secrets I've Learned From 30 Years of Church Planting
- 9 Things That Have Replaced Traditional Outreach in Churches
- 5 Ways to Turn Your Life Into One of Purpose
- 3 Simple Questions to Help Mold Guests' Opinions of Your Church
- What We Must Do to Prepare for the Harvest
- What Laypeople Need to Know About Speaking in 'Big Church'
- The Guide to Better Transitions in Your Weekend Services
- Research: Americans Say Christians Face Increased Persecution
- 2 Major But Under-the-Radar Changes in American Churches
- How to Think Beyond Local Ministry
- Why God Doesn't Want Us to Fear the Unknown
- Breaking Addiction: A New Kind of Recovery Ministry for Your Church
- Your Ministry Journey: Don't Lose the Wonder
- Faith of the Candidates: An Interview With Marco Rubio
- Oral Roberts: God Is at Your Point of Need
- Ed Stetzer: Defining the Church as Evangelicals
- Spiritual Maturity Reaches Way Beyond Salvation
- 10 Ways to Make Visitors Feel Welcome
- Samuel Rodriguez: Lessons From 2012 Election
- The Danger in Living for the Next Big Thing
Charisma News
- State Department Knew About Hillary Clinton's Email Server Sooner Than It Told Congress
- Will This Bible Translation Bring Millennials Back to Church?
- Former President Jimmy Carter Makes Serious Accusation Against Donald Trump
- Here's Why Perry Noble Says He Won't Meet With Donald Trump Next Month
- Democrats Renew Fight Over Faith-Based Contractors
- WATCH: How the Chewbacca Mom Received the Gift of Tongues
- How Donald Trump Has Already Locked Up the GOP Nomination
- Did Pope Francis Really Take Another Step Toward a One World Religion?
- Will Glenn Beck Get Another Visit From the Secret Service?
- Pastor and His 3 Sons Die in Devastating Crash After Bible College Graduation


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