Propeller blade with relatively movable counterweight

Patent metadata

Field	Value
Publication number	US-9458730-B2
Application number	US-201313735419-A
Country	US
Kind code	B2
Filing date	Jan 7, 2013
Priority date	Jan 7, 2013
Publication date	Oct 4, 2016
Grant date	Oct 4, 2016

Abstract

A propeller rotor has a hub mounting a plurality of blades. A counterweight is movably mounted on the blade. A pitch change mechanism for changing an angle of incidence of an airfoil is associated with each of the blades. The counterweight twists the blades toward an increased pitch direction should the pitch change mechanism fail. A stop member stops rotation of the counterweight as the blade moves to a feather position.

First claim

The invention claimed is:

1. A propeller rotor comprising:
a rotor mounting a plurality of blades, said blades having a root mounted in a hub of said rotor and a counterweight movably mounted on said blades wherein said counterweight is movable relative to said blade;
a pitch change mechanism for changing an angle of incidence of an airfoil associated with said blades, and said counterweight for biasing said blades toward an increased pitch direction should said pitch change mechanism fail;
a stop member for stopping rotation of said counterweight as said blade moves to a feathered position; and
wherein said counterweight moves for a portion of the movement of the blade to the feathered position, but is stopped at some point before the blade reaches the feathered position.

2. The propeller rotor as set forth in claim 1 , wherein said stop member includes a stop pin mounted on said hub.

3. The propeller rotor as set forth in claim 1 , wherein said blade in said feather position includes said airfoils being moved generally parallel to an approaching direction of air.

4. The propeller rotor as set forth in claim 1 , wherein said counterweight is mounted to said blades through an arm, and said arm being connected to a collar which is rotatable about a base of said blade.

5. The propeller rotor as set forth in claim 4 , wherein said collar having a groove with circumferential ends, and said hub including a hub pin, said hub pin contacting one of said ends of said groove such that said counterweight transmits torque to said blade.

6. The propeller rotor as set forth in claim 5 , wherein when said counterweight contacts said stop member, said hub pin is spaced from said circumferential ends.

7. The propeller rotor as set forth in claim 6 , wherein said stop member contacts said arm.

8. The propeller rotor as set forth in claim 7 , wherein said stop member stops further rotation of said arm and said counterweight before said counterweight will cross an envelope of movement of a hub and blade of an adjacent one of said plurality of blades.

9. A method comprising:
mounting a plurality of blades in a hub of a rotor and movably mounting a counterweight on each said blade such that said counterweight is movable relative to said blade;
changing an angle of incidence of an airfoil associated with each of said blades with a pitch change mechanism, and said counterweight twisting said blades toward an increased pitch direction should said pitch change mechanism fail;
stopping rotation of said counterweight when said blade moves to a feather position; and
wherein said counterweight moves for a portion of the movement of the blade to the feathered position, but is stopped at some point before the blade reaches the feathered position.

10. The method as set forth in claim 9 , wherein said moving said blades to said feather position includes moving said airfoils generally parallel to an approaching direction of air.

11. The method as set forth in claim 9 , wherein said counterweight is mounted to said blades through an arm, and said arm being connected to a collar which rotates about a base of said blade.

12. The method as set forth in claim 9 , wherein said collar having a groove with circumferential ends, and said hub including a hub pin, said hub pin contacting one of said ends of said groove such that said counterweight transmits torque to said blade.

13. The method as set forth in claim 9 , wherein when said counterweight contacts said stop member, said hub pin is spaced from said circumferential ends.

14. The method as set forth in claim 13 , wherein said stop member contacts said arm.

15. The method as set forth in claim 14 , wherein said stop member stops further rotation of said arm and said counterweight before said counterweight will cross an envelope of movement of a hub and blade of an adjacent one of said plurality of blades.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Carvalho Paul A

Classifications

• B64C11/385

  comprising feathering, braking or stopping systems · CPC title

• F01D7/00 Primary

  Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title

• B64C11/346

  actuated by the centrifugal force or the aerodynamic drag acting on auxiliary masses or surfaces · CPC title