Control system for plural engines

Details Control system for plural engines Control system for plural engines

G - Physics

05

D

341/108.1

G05D 15/01 (2006.01) F02C 6/02 (2006.01) F02C 9/42 (2006.01)

Patent

CA 1098997

ABSTRACT OF THE DISCLOSURE Two gas turbine helicopter engines are coupled together for isochronous operation to supply a common load. A control circuit assures that the power delivered to the common load is equally divided between the two engines. The torque of each engine is detected and the torques are compared to established control signals for the engines.

303075

Affiliated with

Also associated with

Rating

Control system for plural 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 Control system for plural engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Control system for plural engines will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-818167