IP Library Granted Patent US 10,137,640
Granted Patent B2
US 10,137,640 · App. 15/101,754 · Granted Nov 27, 2018

Method for adhering parts and device for implementing said method

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Quick Facts
Patent No.
US 10,137,640
App. No.
15/101,754
Granted
Nov 27, 2018
Kind
B2
Abstract

A method is provided of bonding together at least two parts. The method includes assembling together at least two parts and at least one adhesive layer, the adhesive being configured so that its adhesive power increases on heating as a result of it polymerizing, at least one of the parts being made of composite material or of metal, the adhesive layer being present, after assembly, between the parts, the assembled together parts and the adhesive being present in a chamber defined by a wall, the wall having an inside face situated facing a first part present between the adhesive layer and the wall, the first part being intended to be bonded to a second part and only a fraction of the second part being present inside the chamber; and applying a liquid against the wall on its side opposite from the chamber.

Claims (19)

1. A method of bonding together at least two parts, the method comprising:

assembling together at least two parts and at least one adhesive layer, the adhesive being configured so that its adhesive power increases on heating as a result of it polymerizing, at least one of the parts being made of composite material or of metal, the adhesive layer being present, after assembly, between the parts, the assembled together parts and the adhesive being present in a chamber defined by a wall, the wall having an inside face situated facing a first part present between the adhesive layer and the wall, the first part being intended to be bonded to a second part and only a fraction of the second part being present inside the chamber;

applying a hydrostatic pressure on the parts by contacting a stationary liquid with a side of the wall opposite from the chamber, the wall being configured so that, at least after application of the hydrostatic pressure, its inside face has the same shape as the first part; and

bonding the parts with the hydrostatic pressure applied thereto.

2. The method according to claim 1 , wherein the inside face of the wall conserves its shape during application of the liquid.

3. The method according to claim 1 , wherein the shape of the inside face of the wall is modified during application of the liquid.

4. The method according to claim 1 , further comprising the step of heating the adhesive layer.

5. The method according to claim 4 , wherein a heater member performing heating is present in a cavity into which the liquid is inserted.

6. The method according to claim 1 , wherein the chamber is defined between the wall and a support defining a cavity into which the liquid is inserted.

7. The method according to claim 1 , wherein a plurality of adhesive layers are present on at least one of the parts, the adhesive layers not being in contact with one another and each adhesive layer being present between two parts for bonding together.

8. The method according to claim 1 , wherein the wall moves and in that the movement of all or part of the wall is controlled by a member for limiting the movement of the wall.

9. The method according to claim 1 , wherein the parts are made of composite material and comprise fiber reinforcement together with a matrix.

10. The method according to claim 1 , wherein the first part is made of metal and a second part to which the first part is to be bonded is made of composite material and comprises fiber reinforcement together with a matrix.

11. The method according to claim 1 , wherein the parts are made of metal.

12. The method according to claim 1 , wherein the first part is an element for constituting, once bonded, a leading edge or a trailing edge, and a second part onto which the first part is to be bonded is a turbine engine blade.

13. A device comprising:

a wall defining a chamber, the chamber defining an inside volume in which at least two parts are to be bonded together by means of at least one adhesive layer; and

a liquid injection device configured to apply a liquid against the wall,

the device being configured so that applying the liquid against the wall does not modify the shape of the inside face of the wall situated beside the chamber and generates sufficient pressure on the wall to move the wall and reduce the inside volume of the chamber, wherein the device further includes a heater member, the heater member being present in a cavity in which the liquid is to be inserted.

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 27, 2016
From: GODON, THIERRY; SCHNEIDER, JULIEN; VARIN, FRANCK BERNARD LEON
To: SNECMA
Reel/Frame 039865/0264 →
Cited By (1)
US 12,285,884