IP Library Granted Patent US 7,273,346
Granted Patent B2
US 7,273,346 · App. 11/383,277 · Granted Sep 25, 2007

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

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Quick Facts
Patent No.
US 7,273,346
App. No.
11/383,277
Granted
Sep 25, 2007
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 on the follower member and being connected to the casing by a wheel sliding in a slot secured to the casing.

Claims (5)

1. A control system for controlling two stages of variable-pitch stator vanes in 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 respective levers, the control system including 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 on the follower member and being connected to the casing by a wheel sliding in a slot secured to the casing.

2. A control system according to claim 1 , in which the slot presents a shape and a direction that are determined so as to compensate for path differences between a desired pitch relationship and a nominal pitch relationship.

3. A control system according to claim 1 , in which the additional pivot member has a first arm connected to the second control ring via a first control rod, and a second arm connected to the casing via said wheel.

4. A control system according to claim 1 , in which the follower member has a first arm pivotally connected to the additional pivot member and a second arm connected to one end of the synchronization bar.

5. A control system according to claim 4 , in which the leader member has 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 that is opposite from its end connected to the follower member, and a third arm connected to the drive element.

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 Jun 14, 2006
From: BOURU, MICHEL ANDRE
To: SNECMA
Reel/Frame 017994/0537 →