IP Library Granted Patent US 8,097,831
Granted Patent B2
US 8,097,831 · App. 12/204,388 · Granted Jan 17, 2012

Use of an activating flux for the TIG welding of metal parts

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Quick Facts
Patent No.
US 8,097,831
App. No.
12/204,388
Granted
Jan 17, 2012
Kind
B2
Abstract

A method for welding two metal parts, in which: the metal parts are positioned against each other in a welding position, the parts being respectively in surface contact along their welding surfaces, at least one of the parts having at least one extra-thick zone along its welding surface; TIG welding is carried out on the welding surfaces (v) of the metal parts by means of a TIG welding torch, a method in which a penetrating welding flux is applied locally on said extra-thick zone of the metal part prior to the TIG welding step.

Claims (9)

1. A method for welding two metal parts each having a predetermined thickness, in which:

the metal parts are positioned against each other in a welding position, the parts being respectively in surface contact along their welding surfaces, at least one of the parts having at least one extra-thick zone along its welding surface which is substantially thicker than at least one other zone along its welding surface;

TIG welding is carried out on the welding surfaces (v) of the metal parts by means of a TIG welding torch, a method in which

a penetrating welding flux is applied only on said extra-thick zone of the metal part prior to the TIG welding step.

2. The method as claimed in claim 1 , in which the TIG welding torch operates at a constant power during the TIG welding step.

3. The method as claimed in claim 1 , in which a mask is applied to the metal part, arranged so as to allow the penetrating welding flux to be deposited in a precise manner over the extra-thick zone of the metal part.

4. The method as claimed in claim 1 , in which the TIG welding torch is moved at a first speed along the coated zone and at a second speed over zones lacking penetrating welding flux, the first and second speeds being constant.

5. The method as claimed in claim 4 , in which the TIG welding torch is moved at a speed different from said first and second speeds over a transition zone between the coated zone and an adjacent zone lacking the penetrating welding flux.

6. The method as claimed in claim 1 , in which a mechanical scouring step is carried out on the welded parts, scouring enabling any residual trace of penetrating welding flux to be removed.

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 Sep 5, 2008
From: GUEGUEN, MATHIEU; MOREAU, JOHN; SOULLIER, DAVID DANIEL
To: SNECMA
Reel/Frame 021485/0667 →