IP Library Granted Patent US 9,835,049
Granted Patent B2
US 9,835,049 · App. 14/427,723 · Granted Dec 5, 2017

Turbomachine distributor comprising a thermal protection sheet with a radial stop, and associated thermal protection sheet

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 9,835,049
App. No.
14/427,723
Granted
Dec 5, 2017
Kind
B2
Abstract

A distributor of a turbomachine configured to be mounted in a housing, including: a plurality of segments; a plurality of anti-rotation pins, mounted both on a segment of the distributor and on the housing; and a thermal protection sheet, including at least one axial tab configured to radially abut against an inner face of a first anti-rotation pin, and at least one radial tab configured to axially abut against an upstream face of a second anti-rotation pin.

Claims (9)

1. A distributor for a turbomachine, or a low-pressure distributor, to be mounted in a housing, comprising:

a plurality of segments circumferentially distributed around an axis of rotation of the turbomachine;

a plurality of anti-rotation pins, each of which is mounted both on a segment of the distributor and on the housing; and

a thermal protection metal sheet, positioned between the housing and the segments of the distributor, comprising a plurality of tabs, each tab bearing against an anti-rotation pin;

wherein the plurality of tabs of the thermal protection metal sheet comprises at least one axial tab radially abutting against a radially inward face of a first anti-rotation pin, and at least one radial tab axially abutting against an upstream face of a second anti-rotation pin.

2. The distributor according to claim 1 , wherein the thermal protection metal sheet comprises a plurality of the axial tabs and the radial tabs.

3. The distributor according to claim 1 , wherein the number of the radial tabs and the number of the axial tabs is equal.

4. The distributor according to claim 1 , wherein the radial tabs and the axial tabs alternate along the thermal protection metal sheet, around the axis of rotation of the turbomachine, and are separated by an indentation, or with removal of material.

5. The distributor according to claim 1 , wherein the at least one axial tab is at a distance from the first anti-rotation pin when the turbomachine is at rest.

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 Mar 12, 2015
From: ARNOULD, JULIEN
To: SNECMA
Reel/Frame 035148/0826 →