Method for the control of aero gas turbine engines

Details Method for the control of aero gas turbine engines Method for the control of aero gas turbine engines

B - Operations, Transporting

64

D

B64D 31/00 (2006.01) F02C 9/00 (2006.01) F02C 9/42 (2006.01)

Patent

CA 2558674

This invention relates to the exchange, removal or addition, as applicable, of media and/or power between the individual shafts of an engine, between individual engines and between the engines and the aircraft. Thus, the present invention provides for additional degrees of freedom enabling engine parameters to be addressed in terms of a reduction or avoidance of negative resonances or beats.

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