Gas turbine aircraft engine with power variability

Details Gas turbine aircraft engine with power variability Gas turbine aircraft engine with power variability

B - Operations, Transporting

64

D

B64D 35/00 (2006.01) B64D 35/02 (2006.01) F02C 7/36 (2006.01)

Patent

CA 2657252

A gas turbine aircraft engine with power variability is provided. The gas turbine aircraft engine comprises a compressor and a turbine mounted on a common shaft, and, a continuously variable transmission coupled to the shaft for transmitting power to a propulsion load.

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