IP Library Granted Patent US 10,933,986
Granted Patent B2
US 10,933,986 · App. 16/016,280 · Granted Mar 2, 2021

Blade fold method and apparatus for a tilt rotor hub

Inventors: Jared Mark Paulson (Fort Worth, TX); Ken Shundo (Keller, TX)
Assignee: Bell Helicopter Textron Inc.
B64C27/50F16H37/122B64C29/0033
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Quick Facts
Patent No.
US 10,933,986
App. No.
16/016,280
Granted
Mar 2, 2021
Kind
B2
Abstract

A folding rotor blade assembly includes a blade fold support and a blade-fold actuator system coupled to the blade fold support. The blade-fold actuator system includes a motor, a tab configured to selectively prevent rotation of a blade tang of a rotor blade, and a cam connected to the blade fold support and coupled to the motor, the cam configured to move the tab between a locked position that prevents rotation of the blade tang and an unlocked position that permits rotation of the blade tang.

Claims (54)

1. A folding rotor blade assembly comprising:

a blade fold support; and

a blade-fold actuator system coupled to the blade fold support and comprising:

a motor;

a tab rotatably coupled to a shaft of the blade-fold actuator system and configured to rotate into and out of engagement with a blade tang of a rotor blade to selectively prevent rotation of the blade tang;

a cam connected to the blade fold support and coupled to the motor, the cam configured to rotate the tab between a locked position that prevents rotation of the blade tang and an unlocked position that permits rotation of the blade tang, wherein the tab comprises a tapered face that contacts the blade tang in the locked position;

a track; and

a track linkage comprising a first end coupled to the track and a second end connected to the blade fold support.

2. The folding rotor blade assembly of claim 1 , further comprising:

a second blade fold support; and

wherein the blade-fold actuator system further comprises:

a second tab configured to rotate into and out of engagement with a second blade tang of the rotor blade; and

a second cam connected to the second blade fold support and coupled to the cam via a linkage, the second cam configured to rotate the second tab of the blade-fold actuator system between a second locked position that prevents rotation of the second blade tang and a second unlocked position that permits rotation of the second blade tang.

3. The folding rotor blade assembly of claim 2 , wherein the blade-fold actuator system further comprises an arm connected to the blade tang.

4. The folding rotor blade assembly of claim 2 , further comprising a pitch lock pin coupled to the second cam and configured to lock a pitch of the rotor blade when the second tab is in the second unlocked position.

5. The folding rotor blade assembly of claim 4 , further comprising a guide configured to receive the pitch lock pin.

6. The folding rotor blade assembly of claim 1 , wherein the track is configured to allow the track linkage to move therethrough for a range of motion before the motor begins to rotate the rotor blade.

7. The folding rotor blade assembly of claim 1 , wherein the blade fold support comprises a slot configured to accommodate the blade tang.

8. A folding rotor blade system comprising:

a yoke;

a grip coupled to the yoke via an inboard bearing assembly;

a rotor blade coupled to the grip via an outboard bearing assembly;

a blade fold support connected to the grip; and

a blade-fold actuator system coupled to the blade fold support and comprising:

a motor;

a tab rotatably coupled to a shaft of the blade-fold actuator system and configured to rotate into and out of engagement with a blade tang of the rotor blade to selectively prevent rotation of the blade tang;

a cam connected to the blade fold support and coupled to the motor, the cam configured to rotate the tab between a locked position that prevents rotation of the blade tang and an unlocked position that permits rotation of the blade tang, wherein the tab comprises a tapered face that contacts the blade tang in the locked position;

a track; and

a track linkage comprising a first end coupled to the track and a second end connected to the blade fold support.

9. The folding rotor blade system of claim 8 , further comprising:

a second blade fold support; and

wherein the blade-fold actuator system comprises:

a second tab; and

a second cam connected to the second blade fold support and coupled to the cam via a linkage, the second cam configured to rotate the second tab of the blade-fold actuator system between a second locked position that prevents rotation of a second blade tang and a second unlocked position that permits rotation of the second blade tang.

10. The folding rotor blade system of claim 9 , further comprising a pitch lock pin coupled to the second cam and configured to lock a pitch of the rotor blade when the second tab is in the second unlocked position.

11. The folding rotor blade system of claim 10 , further comprising a guide configured to receive the pitch lock pin.

12. The folding rotor blade system of claim 9 , wherein the blade-fold actuator system further comprises an arm connected to the blade tang.

13. The folding rotor blade system of claim 8 , wherein the track is configured to allow the track linkage to move therethrough for a range of motion before the motor begins to rotate the rotor blade.

14. A folding rotor blade assembly comprising:

a first blade fold support;

a second blade fold support; and

a blade-fold actuator system coupled to the first blade fold support and comprising:

a motor;

a first tab rotatably coupled to a shaft of the blade-fold actuator system and configured to rotate into and out of engagement with a first blade tang of a rotor blade to selectively prevent rotation of the first blade tang;

a first cam connected to the first blade fold support and coupled to the motor, the first cam configured to rotate the first tab between a locked position that prevents rotation of the first blade tang and an unlocked position that permits rotation of the first blade tang;

a second tab configured to rotate into and out of engagement with a second blade tang of the rotor blade;

a second cam connected to the second blade fold support and coupled to the first cam via a linkage, the second cam configured to rotate the second tab of the blade-fold actuator system between a second locked position that prevents rotation of the second blade tang and a second unlocked position that permits rotation of the second blade tang;

a track; and

a track linkage comprising a first end coupled to the track and a second end connected to the first blade fold support.

15. The folding rotor blade assembly of claim 14 , wherein the track is configured to allow the track linkage to move therethrough for a range of motion before the motor begins to rotate the rotor blade.

16. The folding rotor blade assembly of claim 14 , wherein the blade-fold actuator system further comprises an arm connected to the first blade tang.

17. The folding rotor blade assembly of claim 14 , further comprising a pitch lock pin coupled to the second cam and configured to lock a pitch of the rotor blade when the second tab is in the second unlocked position.

18. The folding rotor blade assembly of claim 17 , further comprising a guide configured to receive the pitch lock pin.

19. The folding rotor blade assembly of claim 14 , wherein the first blade fold support comprises a slot configured to accommodate the first blade tang.

Assignments (5)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE NAME OF THE RECEIVING PARTY PREVIOUSLY RECORDED AT REEL: 059970 FRAME: 0231. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Jul 29, 2022
From: BELL HELICOPTER TEXTRON INC.
To: BELL HELICOPTER RHODE ISLAND INC.
Reel/Frame 061003/0869 →
CORRECTIVE ASSIGNMENT TO CORRECT THE THE SPELLING IN THE ASSIGONR'S NAME PREVIOUSLY RECORDED AT REEL: 059758 FRAME: 0819. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded May 12, 2022
From: BELL HELICOPTER TEXTRON INC.
To: BELL TEXTRON RHODE ISLAND INC.
Reel/Frame 059970/0231 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 28, 2022
From: BELL HELICOTPTER TEXTRON INC.
To: BELL TEXTRON RHODE ISLAND INC.
Reel/Frame 059758/0819 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 28, 2022
From: BELL HELICOPTER RHODE ISLAND INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 059765/0361 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 22, 2018
From: PAULSON, JARED MARK; SHUNDO, KEN
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 046182/0243 →
Continuity (1)
Related Publication 20190389569A1 · Dec 26, 2019
Cited By (1)
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