IP Library Granted Patent US 9,566,654
Granted Patent B2
US 9,566,654 · App. 14/566,801 · Granted Feb 14, 2017

Multipurpose electrical discharge machining tool for a ring sector

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Quick Facts
Patent No.
US 9,566,654
App. No.
14/566,801
Granted
Feb 14, 2017
Kind
B2
Abstract

An electrical discharge machining tool of a ring sector for an aircraft turbomachine is provided. The ring sector includes an abradable member and a support element to which the abradable member is fixed; and one or more gripping holes opening on a radially outer surface of a central body of the support element. The machining tool includes at least two machining sets chosen from groove, notch, opening, length-cutting, or abradable element electro-machining sets. The machining tool also has a gripping device for the ring sector by the gripping holes. The gripping device is configured to move the ring sector from one of the electro-machining sets to another of the electro-machining sets.

Claims (22)

1. An electrical discharge machining tool configured to manufacture a ring sector of a turbine for an aircraft turbomachine, the machining tool comprising:

a frame intended to be immersed into a dielectric bath, and

a gripping device configured to grip the ring sector to be machined, wherein the gripping device is configured to grip the ring sector to be machined via gripping holes of the ring sector to be machined,

wherein the frame comprises at least two of the electro-machining sets of the ring sector to be machined, from the following sets:

a length-cutting electro-machine set, configured to correct the circumferential length of the ring sector,

an abradable element electro-machining set, configured to machine an abradable element of the ring sector,

a groove electro-machining set, configured to machine a groove arranged on a circumferential edge of the ring sector, the groove being configured to accommodate at least one inter-sector sealing tab,

a notch electro-machining set, configured to machine a notch located on a downstream rim of a downstream end of a ring sector, the downstream end having the shape of a U opened radially outwards, and

an opening electro-machining set, configured to machine an opening provided in an upstream end of the ring sector, the upstream end having a C-shaped cross-section the opening of which opens into the upstream part of the ring sector,

and wherein the gripping device is movable in relation to the frame in order to move the ring sector to be machined from one of the electro-machining sets to another of the electro-machining sets.

2. The electrical discharge machining tool according to claim 1 , wherein the frame comprises a length-cutting electro-machining set having two length-cutting electro-machining stations configured to correct the circumferential length of the ring sector to be machined, both length-cutting electro-machining stations being intended to be facing each other.

3. The electrical discharge machining tool according to claim 1 , wherein the frame comprises a groove electro-machining set having two groove electro-machining stations configured to electro-machine one or more grooves on a circumferential edge of the ring sector to be machined, both groove electro-machining stations being intended to be facing each other.

4. The electrical discharge machining tool according to claim 2 , wherein the frame comprises an opening electro-machining set, the opening electro-machining set being intended to be arranged in a direction substantially perpendicular to the length-cutting machining set.

5. The electrical discharge machining tool according to claim 3 , wherein the frame comprises an opening electro-machining set, the opening electro-machining set being intended to be arranged in a direction substantially perpendicular to the groove electro-machining set.

6. A method for manufacturing a ring sector for a turbomachine, by an electrical discharge machining tool according to claim 1 , comprising the following steps:

assembling an abradable element on a support element, in order to form the ring sector ready to be machined,

gripping the ring sector, via at least one gripping hole provided on the support element, by the gripping device of the electrical discharge machining tool, and

performing a plurality of electrical discharge machining operations, by means of the electrical discharge machining tool, during which machining operations the ring sector is held on the gripping device.

7. The manufacturing method according to claim 6 , further comprising the following steps:

correcting the circumferential length of the ring sector, using a length-cutting electro-machining set of the machining tool, and then

electrical discharge machining, by a groove electro-machining set of the machining tool, one or more grooves on at least two opposite circumferential edges of the ring sector,

during which one or more grooves are made on one of the circumferential edges, then the ring sector is turned over on the groove electro-machining set, before making one or more grooves on the opposite circumferential edge.

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 26, 2015
From: GIARDINI, BRUNO; MARTY, ANTOINE; TIAN, XI; ARNOULD, JULIEN; CANELLE, ETIENNE; HASCOET, FREDERIC; LEBASTARD, MATTHIEU
To: SNECMA
Reel/Frame 035260/0140 →