IP Library Granted Patent US 8,047,466
Granted Patent B2
US 8,047,466 · App. 12/300,065 · Granted Nov 1, 2011

Yoke with notched arm roots

Assignee: Bell Helicopter Textron Inc.
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Quick Facts
Patent No.
US 8,047,466
App. No.
12/300,065
Granted
Nov 1, 2011
Kind
B2
Abstract

A yoke for a rotary wing aircraft rotor system has a plurality of arms, each arm having a root. Each root has a notched portion configured to allow passage of a portion of a blade-pitch control system through the notched portion.

Claims (20)

1. A yoke for a rotary-wing aircraft, the yoke comprising:

a plurality of arms extending from a central portion, each arm having a root; and

a notch formed in a leading edge or a trailing edge of each root and adapted to allow positioning of a portion of a blade-pitch control system within each notch.

2. The yoke according to claim 1 , wherein the yoke is formed from a composite material.

3. The yoke according to claim 1 , wherein each notch comprises a notch envelope defined by an imaginary continuation of the corresponding edge toward the central portion.

4. The yoke according to claim 1 , wherein the yoke has four arms.

5. A rotor system for a rotary-wing aircraft, the rotor system comprising:

a yoke having a plurality of arms extending from a central portion, each arm having a root;

a blade-pitch control system; and

a notch formed in a leading edge or a trailing edge of each root and configured to allow positioning of a portion of the blade-pitch control system within each notch.

6. The rotor system according to claim 5 , wherein the yoke is formed from a composite material.

7. The rotor system according to claim 5 , wherein each notch comprises a notch envelope defined by an imaginary continuation of the corresponding edge toward the central portion.

8. The rotor system according to claim 5 , wherein the yoke has four arms.

9. A rotary-wing aircraft, comprising:

at least one rotor system having a yoke with arms extending from a central portion, each arm having a notch in an arm root and a blade rotatably attached to the arm for allowing adjustable pitch of each blade; and

a blade-pitch control system;

wherein a portion of the blade-pitch control system is positioned within each notch.

10. The aircraft according to claim 9 , wherein the yoke is formed from a composite material.

11. The aircraft according to claim 9 , wherein each notch comprises a notch envelope defined by an imaginary continuation of a corresponding leading edge or trailing edge toward the central portion.

12. The aircraft according to claim 9 , wherein the yoke has four arms.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 27, 2016
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 039862/0274 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 25, 2008
From: STAMPS, FRANK B.; RAUBER, RICHARD E.; CAMPBELL, THOMAS C.; DONOVAN, TOM; TISDALE, PATRICK R.; BRASWELL, JAMES L., JR.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 021891/0354 →
Continuity (1)
Related Publication 20090179107A1 · Jul 16, 2009