IP Library Granted Patent US 7,241,961
Granted Patent B2
US 7,241,961 · App. 11/130,140 · Granted Jul 10, 2007

TIG welding method

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Quick Facts
Patent No.
US 7,241,961
App. No.
11/130,140
Granted
Jul 10, 2007
Kind
B2
Abstract

A TIG welding method of welding a first part with a first wall and an end edge to a second part with a second wall and an edge along a junction surface between said edges and along which the first wall forms a salient angle with the second wall. The TIG welding electrode is moved along the junction surface to weld the first part to the second part. The electrode being aligned on the side of the salient angle at an angle (β) with respect to the first wall smaller than 180° and with the longitudinal axis of the electrode running through the re-entrant angle associated with the salient angle.

Claims (16)

1. A TIG welding method comprising the steps of:

providing a spark plug guide, said spark plug guide including a guide wall terminating in an end edge;

providing a combustion chamber jacket of a gas turbine motor, said combustion chamber jacket including a jacket wall having an orifice, said orifice having an edge;

providing a TIG welding electrode having a longitudinal axis;

aligning the end edge of the spark plug guide to the edge of the orifice of the combustion chamber jacket to thereby define an intersection portion of the spark plug guide with the combustion chamber jacket, the intersection portion lying in a jointing plane;

aligning the TIG welding electrode at an angle with respect to the guide wall smaller than 180° and with the longitudinal axis of the TIG welding electrode running through the intersection portion of the jointing plane; and

moving the TIG welding electrode to weld the spark plug guide to the combustion chamber jacket without using any external filler.

2. The method according to claim 1 , wherein sufficient welding energy is applied to form a fillet.

3. The method according to claim 1 , wherein the guide wall is cylindrical.

4. The method according to claim 1 , wherein the TIG welding electrode is positioned within the orifice of the combustion chamber jacket during the step of moving the TIG welding electrode to weld the spark plug guide to the combustion chamber jacket.

5. The method according to claim 1 , wherein the jacket wall forms a projection along the intersection portion of the jointing plane before welding.

6. The method according to claim 1 , wherein the jacket wall has a countersink against which the end edge of the guide wall rests before welding.

7. The method according to claim 1 , wherein displacement speed and intensity of current are varied during movement of the TIG welding electrode.

8. The method according to claim 1 , wherein the TIG welding electrode provides direct heat to one of said guide wall or said jacket wall and provides only indirect heat to the other of said guide wall or said jacket wall.

9. The method according to claim 1 , wherein the intersection portion lying in the jointing plane forms an acute angle with said guide wall.

10. The method according to claim 1 , wherein the end edge forms an acute angle with said guide wall.

Assignments (4)
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 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 17, 2005
From: DURET, JEAN-MICHEL; GUERNIOU, PASCAL
To: SNECMA MOTEURS
Reel/Frame 016572/0946 →