IP Library Granted Patent US 7,281,892
Granted Patent B2
US 7,281,892 · App. 11/045,264 · Granted Oct 16, 2007

Control lever for the pitch angle of a blade in a turbomachine

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,281,892
App. No.
11/045,264
Granted
Oct 16, 2007
Kind
B2
Abstract

A control lever for the pitch angle of a blade in a turbomachine, said lever having a first end intended to be mounted on a blade pivot so as to rotate it and a second end comprising a cylindrical peg for mounting on a control annulus, this peg being fixed by crimping of one of its ends in an orifice of the second end of the lever and comprising an annular flange to which is applied the second end of the lever, wherein stress distribution means are interposed between the second end of the lever and the crimped end of the peg.

Claims (15)

1. A control lever for the pitch angle of a blade in a turbomachine, said lever comprising:

a first end configured to be mounted on a blade pivot so as to rotate it and a second end carrying a cylindrical peg configured to mount on a control annulus, this peg being fixed by crimping of one of its ends in an orifice of the second end of the lever and including an annular flange to which is applied the second end of the lever, wherein stress distribution means are sandwiched between the second end of the lever and the crimped end of the peg.

2. The control lever as claimed in claim 1 , wherein the stress distribution means comprise a washer.

3. The control lever as claimed in claim 2 , wherein the washer is made of a more flexible material than that of the control lever.

4. The control lever as claimed in claim 3 , wherein the washer is made of polymer.

5. The control lever as claimed in claim 2 , wherein the washer is made of a harder material than that of the control lever.

6. The control lever as claimed in claim 5 , wherein the washer is made of polymer or of metal.

7. The control lever as claimed in claim 5 , wherein the washer comprises a substantially plane annular surface applied to the second end of the lever and exhibiting a convex or chamfered annular edge at its outer periphery.

8. The control lever as claimed in claim 2 , wherein the thickness of the washer is about one millimeter.

9. The control lever as claimed in claim 2 , wherein the washer has an outer diameter equal to or slightly less than that of the flange of the peg.

10. The control lever as claimed in claim 2 , wherein a first side of the washer is in direct contact with a first surface of the lever, and a second surface of the lever opposite the first surface of the lever is in direct contact with the annular flange.

11. The control lever as claimed in claim 10 , wherein a second side of the washer opposite the first side of the washer is in direct contact with the crimped end of the peg.

12. The control lever as claimed in claim 2 , wherein the crimped end of the peg contacts the washer along a surface of the crimped end extending in a direction perpendicular to an axis of the peg.

13. The control lever as claimed in claim 1 , wherein the lever is made of titanium and the peg is made of steel.

14. The control lever as claimed in claim 1 , wherein an inner surface of the orifice in the second end of the lever is in direct contact with the peg.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →