Blade pitch change control system
AssigneeUnited Technologies Corporation
InventorsRobert J. Lampeter, Jerome G. Duchesneau
Life of this patent
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AssigneeUnited Technologies Corporation
InventorsRobert J. Lampeter, Jerome G. Duchesneau
Estimating the term…
A pitch change actuation system is disclosed for adjusting the pitch of a variable pitch propeller blades (120) operatively connected for pitch change to a pitch change actuator piston (140). A pitch change control system (10) is operatively connected to the pitch change actuator piston (140) for selectively pressuring the pitch change actuator piston to effectuate a desired change in the pitch of the propeller blades (120). The pitch change control system (10) comprises a primary electrohydraulic valve (30), a protection valve (60), an electronic controller (20) and a protection solenoid (50). During normal operation, the primary electrohydraulic valve (30) is modulated under control of the electronic controller (20) to effect pitch change. In the event of failure of the electronic controller (20), the protection solenoid (50) is operative to activate the protection valve (60) to assume pitch change authority over the primary electrohydraulic valve (30) thereby providing emergency feathering capability, overspeed protection, low pitch stop limit protection, and in place pitchlock despite failure of the electronic controller.
A pitch change control system for use in a pitch change actuation system for adjusting the pitch of a blade of a variable pitch propeller, the blade rotatively mounted to a hub of the propeller, said pitch change actuation system having a pitch change actuator piston operatively connected to the blade and said pitch change control system operatively connected to the pitch change actuator piston for selectively pressuring the pitch change actuator piston to effectuate a desired change in the pitch of the blade, said pitch change control system comprising:
Dependencies are inferred from the claim text.