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

2006-09-05

2006-09-05

Swiatek, Robert P. (Department: 3643)

Aeronautics and astronautics

Aircraft power plants

C416S034000

Reexamination Certificate

active

07100868

ABSTRACT:
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 provides for additional degrees of freedom, enabling engine parameters to be addressed in terms of a reduction or avoidance of negative resonances or beats. It also provides an ability to alter thrust from engines of a multi-engined aircraft to reduce rudder trim.

REFERENCES:
patent: 3514055 (1970-05-01), Gregoire et al.
patent: 4009849 (1977-03-01), Eickmann
patent: 5137230 (1992-08-01), Coffinberry
patent: 5939800 (1999-08-01), Artinian et al.
patent: 6127758 (2000-10-01), Murry et al.

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