Invention Grant
US08181442B2 Gas turbine aircraft engine with power variability 有权
燃气轮机飞机发动机功率变化

Gas turbine aircraft engine with power variability
Abstract:
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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