Aircraft thrust control

Details Aircraft thrust control Aircraft thrust control

B - Operations, Transporting

64

C

60/142

B64C 11/48 (2006.01) F02C 9/58 (2006.01) F02K 3/072 (2006.01)

Patent

CA 1273211

AIRCRAFT THRUST CONTROL ABSTRACT OF THE DISCLOSURE An integrated control system for coaxial counterrotating aircraft propulsors driven by a common gas turbine engine. The system establishes an engine pressure ratio by control of fuel flow and uses the established pressure ratio to set propulsor speed. Propulsor speed is set by adjustment of blade pitch.

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