IP Library Granted Patent US 7,891,073
Granted Patent B2
US 7,891,073 · App. 11/279,811 · Granted Feb 22, 2011

Method of assembling two parts, at least one of which is made of a composite, and insert for carrying out the assembly

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Quick Facts
Patent No.
US 7,891,073
App. No.
11/279,811
Granted
Feb 22, 2011
Kind
B2
Abstract

A method for bonding a first part made of a composite to a second part to a predetermined dimension is disclosed. The method includes placing an insert into the first part, a first surface of the insert protruding beyond the predetermined dimension; machining the insert until the first surface is at the predetermined dimension; placing the second part on the insert; and fastening the second part via the insert. The use of an insert makes it possible to produce, with high precision, a reproducible assembly, which can still be dismantled.

Claims (16)

1. A method for bonding a first part made of a ceramic matrix composite to a second part to create an assembly, the method comprising:

drilling a hole in said first part;

placing an insert into said first part along an axis of the hole, a first surface of said insert protruding beyond a predetermined dimension between the first surface of the insert and a first surface of the first part in a direction parallel to the axis of the hole;

machining the first surface of the insert until a distance between the first surface of the insert and the first surface of the first part in the direction parallel to the axis of the hole is the predetermined dimension;

placing the second part on the first surface of the insert; and

fastening the second part via the insert.

2. The method as claimed in claim 1 , wherein the insert includes a cylindrical portion and a portion with a shoulder, the cylindrical portion of the insert is placed in the hole such that the shoulder abuts a second surface of the first part, the second surface of the first part is opposite the first surface of the first part, and the insert is fastened by a washer that is brazed to the first surface of the first part.

3. The method as claimed in claim 2 , wherein the brazing temperature is above the operating temperature of the assembly so that the insert pinches on the first part.

4. The method as claimed in claim 2 , wherein at least one of the portion of the insert with the shoulder or the cylindrical portion of the insert is machined.

5. The method as claimed in claim 2 , wherein the second part is fastened to the first part by a rivet, a welded stud or a bolt passing through the insert along an axis of the cylindrical portion.

6. The method as claimed in claim 2 , wherein the insert comprises a first part of defined thickness is bonded to a second part to a defined dimension, wherein the cylindrical portion is of greater height than the thickness of the first part, the shoulder having a protrusion that can be machined off.

7. The method as claimed claim 6 , wherein the insert further comprises a central bore passing through the cylindrical portion and the shoulder.

8. The method as claimed in claim 1 , further comprising assembling a third part via the insert.

9. The method as claimed in claim 2 , wherein the shoulder includes a clamping means for immobilizing the insert during the machining operation.

10. The method as claimed in claim 2 , further comprising machining two flaps that are parallel to each other on the shoulder of the insert.

11. The method as claimed in claim 2 , further comprising machining two notches in the shoulder of the insert.

Assignments (2)
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 →