Aircraft propeller speed control

B - Operations – Transporting – 64 – D

Patent

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341/38.1

B64D 31/06 (2006.01) B64C 11/30 (2006.01) F02C 9/58 (2006.01)

Patent

CA 1305771

13DV-9112 AIRCRAFT PROPELLER SPEED CONTROL ABSTRACT OF THE DISCLOSURE The invention concerns a control for an aircraft propeller. During operation in reverse pitch, as occurs upon thrust reversal during a landing maneuver; the speed of the propeller is controlled by adjusting pitch of the propeller, in order to prevent overspeeding. Further, during the transition period while the propeller is converting from forward pitch to reverse pitch, the propeller presents a light load to the engine. At this time, fuel flow to the engine is limited in order to restrict delivery of energy to the propeller, again, for the purposes of preventing overspeeding.

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