This concerns the GE90X fanjet engine which generates 130,000 LBS of thrust at takeoff
This is almost a duplicate of another question: What is the GE90-115b turbine power output in horsepower?
With the fan removed, and power used for e.g. ship propulsion or a power plant, the engine core can deliver about 66 MW or 90,000 horsepower continuously.
Takeoff thrust is higher than continuous, and the core does contribute some thrust. So to match 130,000 lbf, a fan this size would require external power in the range of 80-85 MW or about 110,000 hp.