Propeller pitch control system and apparatus
AssigneeThe Boeing Company
InventorsHenry J. Miyatake, Seiya Sakurai
Life of this patent
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AssigneeThe Boeing Company
InventorsHenry J. Miyatake, Seiya Sakurai
Estimating the term…
A plurality of propeller blades are mounted to an axially elongated tubular propeller hub (H1). Each blade is rotatable in position about a radial axis. An electromechanical linear actuator (A1) is housed within the hub for rotating the blades to change their pitch. The actuator includes a rod member (R1) fixed in position relative to the hub, a casing (C1) which can extend and retract relative to the rod member, a rotary electric motor (M1), and a planetary screw drive (SD1). The screw drive (SD1) drivingly interconnects the electric motor (M1) with the casing (C1) for causing the casing to move axially in response to operation of the motor. The actuator (A1) is connected to the propeller (P1) by a linkage (L1) so that movement of the casing causes the propellers to change their pitch. A second actuator (A2) may be housed within the hub (H1) and connected to the first actuator (A1) for providing redundancy in the event of failure of the first actuator.
An adjustable pitch propeller, comprising:
An apparatus for adjusting the pitch of a propeller, the apparatus being housed within a propeller hub that rotates about a center axis, said apparatus comprising:
The apparatus of claim 16, wherein said rod member outer surface includes at least one axially extending spline, and including a guide member connected to said casing, said guide member having a portion shaped for sliding engagement with said spline, such portion of said guide member cooperating with said spline to permit said casing to move axially relative to said rod member but preventing rotation of said rod member and said casing relative to each other.
An electromechanical actuator connected between a support and a member to be moved relative to said support, said actuator comprising:
Dependencies are inferred from the claim text.