IP Library Granted Patent US 7,322,790
Granted Patent B2
US 7,322,790 · App. 11/383,287 · Granted Jan 29, 2008

System for controlling stages of variable-pitch stator vanes in a turbomachine

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Quick Facts
Patent No.
US 7,322,790
App. No.
11/383,287
Granted
Jan 29, 2008
Kind
B2
Abstract

A system for controlling two stages of variable-pitch stator vanes of a turbomachine, the system comprising a drive element for turning the control ring of one of the stages via a leader member pivotally mounted on the casing, a synchronization bar for transmitting the turning movement of the ring driven by the drive element to the control ring of the other stage via a follower member pivotally mounted on the casing, and an additional pivot member interposed between the follower member and the follower ring, said additional pivot member being pivotally mounted both on the casing and on the follower member.

Claims (8)

1. A system for controlling two stages of variable-pitch stator vanes of a turbomachine, each stage including a plurality of vanes each pivotally mounted on a casing of the turbomachine, and a control ring for each stage surrounding the casing and connected to each of the vanes of the stage via levers, the control system comprising a drive element for turning a first control ring of one of the stages via a leader member pivotally mounted on the casing, and a synchronization bar for transmitting the turning movement of the first control ring driven by the drive element to a second control ring of the other stage via a follower member pivotally mounted on the casing, the system further comprising an additional pivot member interposed between the follower member and the second control ring, said additional pivot member being pivotally mounted both on the casing and on the follower member.

2. A control system according to claim 1 , wherein the additional pivot member has one arm pivotally mounted on a control rod connected to the second control ring, and a guide rod slidably received in a bushing pivotally mounted on the casing.

3. A control system according to claim 1 , wherein the follower member comprises a first arm pivotally connected to the additional pivot member, and a second arm connected to one end of the synchronization bar.

4. A control system according to claim 3 , wherein the pivot point on the casing of the additional pivot member is disposed inside a circle centered on the pivot point on the casing of the follower member, and has as its radius the first arm of said follower member.

5. A control system according to claim 3 , wherein the pivot point on the casing of the additional pivot member is disposed outside a circle centered on the pivot point on the casing of the follower member, and has as its radius the first arm of said follower member.

6. A control system according to claim 3 , wherein the leader member comprises a first arm connected to the first control ring via a second control rod, a second arm connected to the end of the synchronization bar opposite from its end connected to the follower member, and a third arm connected to the drive element.

7. A turbomachine compressor comprising at least one system according to claim 1 .

8. A turbomachine comprising at least one system according to claim 1 .

Assignments (3)
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 17, 2006
From: BOURU, MICHEL ANDRE
To: SNECMA
Reel/Frame 018106/0860 →