IP Library Granted Patent US 9,494,051
Granted Patent B2
US 9,494,051 · App. 14/405,565 · Granted Nov 15, 2016

Counter plate and turbo machine comprising a counter plate

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Quick Facts
Patent No.
US 9,494,051
App. No.
14/405,565
Granted
Nov 15, 2016
Kind
B2
Abstract

A counter plate for a turbo machine, including: a first external surface and a second external surface, which are substantially parallel; the first external surface of the counter plate creates a continuous ring or continuous ring segment and includes a first series of holes through which fasteners can pass; the second external surface of the counter plate including a plurality of surfaces for supporting heads of the fasteners, the support surfaces including a second series of holes, positioned facing the first series of holes, so that the fasteners can pass through the holes in the counter plate.

Claims (14)

1. A turbomachine comprising:

a flange;

a mounting flange to which the flange is mounted;

a counter-plate including a first outer surface and a substantially parallel second outer surface;

the first outer surface of the counter-plate forming a continuous ring, or a continuous ring segment, and including a first series of holes for passage of fastening means;

the second outer surface of the counter-plate including a plurality of support surfaces for heads of fastening means, the support surfaces including a second series of holes, arranged facing the first series of holes, for passage of the fastening means through the holes of the counter-plate;

the first outer surface of the counter-plate including a material allowing prevention of galvanic corrosion which can occur between the flange and the mounting flange; and

the first outer surface separating the flange and the mounting flange.

2. The turbomachine according to claim 1 , wherein the second outer surface of the counter-plate includes a material allowing prevention of galvanic corrosion which can occur between the fastening means and the flange.

3. The turbomachine according to claim 1 , wherein the second outer surface is a continuous surface.

4. The turbomachine according to claim 1 , wherein the second outer surface is a discontinuous surface.

5. The turbomachine according to claim 4 , wherein the second outer surface is a scalloped surface, scallops whereof are a support surface for heads of the fastening means.

6. The turbomachine according to claim 1 , wherein the first and the second outer surfaces are spaced so that the counter-plate grips the flange.

7. The turbomachine according to claim 1 , wherein the flange is mounted on the mounting flange by attachment means passing through holes in the first and in the second outer surfaces of the counter-plate.

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 Jan 15, 2016
From: FILLAUD, NICOLAS
To: SNECMA
Reel/Frame 037501/0237 →