IP Library Granted Patent US 7,448,280
Granted Patent B2
US 7,448,280 · App. 11/833,628 · Granted Nov 11, 2008

Method for evaluating the fatigue strength of welded joints

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Quick Facts
Patent No.
US 7,448,280
App. No.
11/833,628
Granted
Nov 11, 2008
Kind
B2
Abstract

Method for evaluating the fatigue strength of welded joints produced by melting an alloy using a specified welding technique, which method comprises the following steps: a statistically significant number N of specimens are produced with a welded joint using said welding technique; each of the specimens is subjected to cyclic fatigue tests, with an alternating stress a, until failure; the size of the relevant defect appearing in the fracture plane of the specimens is measured by fractography; a range of defect dimensions for which the probability of measuring by fractography a defect outside the range is less than a predetermined level of probability t is determined from the measured sizes; and the lowest stress σ min liable to cause the specimen to fail with a level of probability t is determined from this range.

Claims (10)

1. A method for evaluating the fatigue strength of welded joints produced by melting an alloy using a specified welding technique, which method comprises the following steps:

a statistically significant number N of specimens are produced with a welded joint using said welding technique;

each of the specimens is subjected to cyclic fatigue tests, with an alternating stress σ, until failure;

the size of the relevant defect appearing in the fracture plane of the specimens is measured by fractography;

a range of defect dimensions for which the probability of measuring by fractography a defect outside the range is less than a predetermined level of probability t is determined from the measured sizes; and

the lowest stress σ min liable to cause the specimen to fail with a level of probability t is determined from this range.

2. The method as claimed in claim 1 , wherein welded joints are produced on the specimens, the volume of which is between 10% and 100% of the welded joints on one of the parts to be assembled.

3. The method as claimed in claim 1 , applied to evaluating the fatigue behavior of a titanium alloy assembly, the number of specimens of which is between 35and 45, preferably 40.

4. The method as claimed in one of the preceding claims, the level of probability t of which is less than 1%.

5. The method as claimed in one of the preceding claims, the welding technique of which employs a laser beam to melt the alloy.

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 Aug 6, 2007
From: MONS, CLAUDE MARCEL
To: SNECMA
Reel/Frame 019648/0560 →