IP Library Granted Patent US 9,731,373
Granted Patent B2
US 9,731,373 · App. 14/347,565 · Granted Aug 15, 2017

Method for welding and for hard surface deposition of metal parts made of aluminium by a MIG method with pulsed current and filler wire

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Quick Facts
Patent No.
US 9,731,373
App. No.
14/347,565
Granted
Aug 15, 2017
Kind
B2
Abstract

A method for hard surface deposition on aluminum metal parts of a turbine engine using MIG welding equipment which includes a pulsed current generator and pulsed filler metal wire feed, wherein the deposition is achieved using a filler metal wire whose composition is of the same nature as the composition of the aluminum alloy of the part to undergo hard surface deposition, with the pulsed metal wire feed and speed of deposition on the metal part of the turbine engine being adapted to carry out deposition without hot fissuring.

Claims (14)

1. A method for hard surface deposition on an aluminium alloy metal part of a turbine engine, the method comprising:

depositing an aluminium alloy on said aluminium alloy metal part using a MIG welding equipment which includes a pulsed current generator and pulsed filler metal wire feed, said depositing using a filler metal wire of said aluminium alloy, the aluminium alloy of said filler metal wire and the aluminium alloy of the metal part to undergo said hard surface deposition being the same aluminium alloy, with said pulsed metal wire feed and speed of deposition on the aluminium alloy metal part of the turbine engine being selected so that said deposition is carried out without hot fissuring said aluminium alloy metal part.

2. The hard surface deposition method according to claim 1 , comprising performing a heat treatment.

3. The hard surface deposition method according to claim 1 , further comprising reconstructing the aluminium alloy metal part made of aluminium alloy of grade 6061 with the deposition speed between 50 cm/min and 120 cm/min.

4. The hard surface deposition method according to claim 1 , further comprising welding mechanical parts made of aluminium alloy of grade 6061, with hard surface deposition of filler metal, and with a welding speed between 40 cm/min and 100 cm/min.

5. The hard surface deposition method according to claim 1 , comprising performing a heat treatment of the metal undergoing hard surface deposition so as to optimise mechanical characteristics of the part that has undergone hard surface deposition.

6. The hard surface deposition method according to claim 5 , wherein said heat treatment consists of:

a first solution sub-step:

a second hyper-tempering sub-step:

a third tempering sub-step.

7. A repair method for a retaining housing of a turbine engine which includes at least one mounting flange to be repaired, said method successively including:

shaving the mounting flange to be repaired:

reconstructing said mounting flange by a hard surface deposition method according to claim 1 ;

machining said deposited metal in order to achieve a final geometry of said mounting flange.

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, 2014
From: MOTTIN, JEAN-BAPTISTE; BENOIT, ALEXANDRE YANN MICHEL; CASTAGNE, JEAN-FRANCOIS; BAUDIN, THIERRY; PAILLARD, PASCAL
To: SNECMA; CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (CNRS); UNIVERSITE PARIS SUD (UPS); UNIVERSITE DE NANTES
Reel/Frame 032533/0892 →