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

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 9/00 (2006.01) B64C 11/50 (2006.01) B64D 31/00 (2006.01) B64D 31/12 (2006.01) F02C 9/42 (2006.01)

Patent

CA 2364647

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.

Affiliated with

Also associated with

Rating

Method for the control of aero gas turbine engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method for the control of aero gas turbine engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method for the control of aero gas turbine engines will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1693085