Aircraft system with gas turbine engine powered compressor
AssigneeRtx Corporation
InventorsSteven W. Burd, Christopher A. Eckett
Life of this patent
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AssigneeRtx Corporation
InventorsSteven W. Burd, Christopher A. Eckett
Estimating the term…
An aircraft system is provided that includes a gas turbine engine, a gearbox and at least one compressor. The gas turbine engine includes a compressor section, a turbine section, a combustor section and a rotating structure. The combustor section is fluidly coupled with and between the compressor section and the turbine section. The rotating structure includes a compressor section rotor within the compressor section and a turbine section rotor within the turbine section. The at least one compressor includes a compressor rotor rotatably driven by the rotating structure through the gearbox. The gas turbine engine may be dedicated to powering the at least one compressor.
An aircraft system, comprising:
An aircraft system, comprising:
A method, comprising:
Dependencies are inferred from the claim text.