IP Library Granted Patent US 8,038,387
Granted Patent B2
US 8,038,387 · App. 11/765,693 · Granted Oct 18, 2011

Bearing for variable pitch stator vane

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Quick Facts
Patent No.
US 8,038,387
App. No.
11/765,693
Granted
Oct 18, 2011
Kind
B2
Abstract

A bearing for a turbomachine variable pitch stator vane pivot mounted in a bore of the turbomachine casing is disclosed. The bearing includes an inner bushing secured to the pivot and an outer bushing secured to the bore. An elastomeric material is inserted between the inner bushing and the outer bushing to allow the vane to pivot about its axis and absorb at least some of the flexing of the pivot at right angles to the axis. The design makes it possible to reduce bearing bushing wear.

Claims (7)

1. A bearing for a turbomachine variable pitch stator vane pivot mounted in a bore of the turbomachine casing, comprising:

an inner bushing secured to said pivot, said inner bushing including a first cylindrical element and a second cylindrical element axially spaced from the first cylindrical element along an axis of the pivot, the first cylindrical element and the second cylindrical element being single piece assemblies;

an outer bushing secured to said bore, the outer bushing being a single piece assembly; and

an elastomeric material being inserted between outer diameters of the first and second cylindrical elements of the inner bushing and an inner diameter of the outer bushing and between the first and second cylindrical elements of the inner bushing along the axis of the pivot to allow the vane to pivot about its axis and absorb at least some of the flexing of the pivot at right angles to the axis.

2. A turbomachine stator vane with a pivot intended to be mounted in a bore formed in the turbomachine casing and a journal for attaching to a vane pitch control rod comprising a bearing as claimed in claim 1 positioned at the end of the pivot and the outer bushing of which has a flange.

3. A turbomachine comprising stator vanes with bearings as claimed in claim 1 .

4. The bearing as claimed in claim 1 , wherein the outer bushing includes a transverse flange.

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 →