IP Library Granted Patent US 7,850,892
Granted Patent B2
US 7,850,892 · App. 11/876,447 · Granted Dec 14, 2010

Method of fabricating a test blade of composite material

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Quick Facts
Patent No.
US 7,850,892
App. No.
11/876,447
Granted
Dec 14, 2010
Kind
B2
Abstract

A test blade and a method for fabricating the test blade are presented for use in calibrating a tomography system configured to inspect turbomachine blades for defects. The test blade may include a three-dimensional fiber blank and a polymerized resin. The blank may be created by weaving synthetic material fibers. The resin may be configured to be injected into a mold as a liquid where the resin may polymerize around the fiber blank. The test blade may be configured to be modified to include particular defects such as cut fibers and/or cavity defects which are perceived by the tomography system. The dimensions of the cavity defects may be substantially created by pulling two or more fibers apart at a specific distance with a spreading tool.

Claims (15)

1. A method of fabricating a test blade of composite material and calibrating X-ray inspection of similar real blades, the method comprising:

making a three-dimensional blank woven out of synthetic material fibers;

creating cavities at predetermined locations throughout said blank;

inserting said blank into a mold;

injecting a resin under pressure into said mold to obtain said test blade, said test blade being similar in shape and dimensions to the real blades, wherein the cavities are created prior to the inserting said blank into the mold and each of the cavities are completely filled with a clump of resin constituting a test blade defect to be detected when calibrating the X-ray inspection; and

calibrating the X-ray inspection by detecting the test blade defects.

2. A method according to claim 1 , wherein certain strands of fibers are cut at selected locations within a blank perimeter prior to injecting the resin.

3. A method according to claim 2 , wherein the synthetic material fibers are made of carbon fibers.

4. A method according to claim 3 , wherein the resin is an epoxy resin.

5. A method according to claim 3 , wherein the resin is a polyester resin.

6. A method according to claim 3 , wherein the resin is a phenolic resin.

7. A method according to claim 2 , wherein the synthetic material fibers are made of glass fibers.

8. A method according to claim 2 , wherein the synthetic material fibers are made of aramid fibers.

9. A method according to claim 2 , wherein the certain strands of fibers are cut with a pair of scissors.

10. A method according to claim 1 , wherein said creating cavities includes inserting a spreader tool into the woven fibers of said blank and spreading the fibers apart at a first predetermined location and a second predetermined location, wherein the fibers are spread apart at the first predetermined location before the fibers are spread apart at the second predetermined location.

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 Oct 22, 2007
From: ROMERO, JEAN-LOUIS; WOZNIAK, MYRIAM
To: SNECMA
Reel/Frame 019996/0062 →