Method and system for attaching a piece of equipment to a structure made from composite material

Patent metadata

Field	Value
Publication number	US-9827639-B2
Application number	US-201314375570-A
Country	US
Kind code	B2
Filing date	Feb 1, 2013
Priority date	Feb 3, 2012
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

A method of placing a fastener plate on a structure made of composite material, the structure being obtained by a technique of injecting resin under a vacuum, the technique including placing a fiber preform in a closed mold, injecting a thermosetting resin into the mold, and polymerizing the resin prior to cooling. The method includes mounting a metal fastener plate against a wall of the mold before putting the fiber preform into place, the fastener plate coming into contact with one of faces of the fiber preform while the fiber preform is being put into place in the mold, and the resin becoming deposited between the fastener plate and the fiber preform while the resin is being injected into the mold. The method may be used in particular for fastening equipment on a composite material fan casing of a gas turbine for an aeroengine.

First claim

The invention claimed is:

1. A method of placing a metal fastener plate on a structure made of composite material, the structure obtained by a technique of injecting resin under a vacuum, the technique including placing a fiber preform in a closed mold, injecting a thermosetting resin into the mold, and polymerizing the resin prior to cooling, the method comprising:
mounting the metal fastener plate against a wall of the mold before putting the fiber preform into place, the fiber preform having a first face facing said wall of the mold and a second face opposite to the first face;
placing the metal fastener plate into contact with the first face of the fiber preform while the fiber preform is being put into place in the mold such that the metal fastener plate is located between said wall of the mold and said first face of the fiber preform; and
depositing the resin between the fastener plate and the fiber preform while the resin is being injected into the mold.

2. A method according to claim 1 , wherein the metal fastener plate is mounted against the wall of the mold by a holding screw and a clamping wedge.

3. A method according to claim 2 , wherein the screw holding the metal fastener plate is withdrawn after the resin has polymerized and before the resin has cooled.

4. A method of fastening equipment on a structure made of composite material, the method comprising:
placing the metal fastener plate against one of the faces of the composite material structure according to claim 1 , the metal fastener plate presenting a tapped hole;
forming an orifice in the composite material structure in alignment with the tapped hole in the metal fastener plate;
applying the equipment for fastening against the face of the composite material structure opposite from the face on which the metal fastener plate is fastened; and
fastening the equipment for fastening on the composite material structure by screwing a screw member through the composite material structure and into the tapped hole in the metal fastener plate.

5. A method according to claim 4 , wherein the tapped hole in the metal fastener plate is formed during a drilling of the composite material structure.

6. A method according to claim 4 , wherein the tapped hole of the metal fastener plate is a same as a hole for passing a holding screw of the metal fastener plate against the wall of the mold.

7. A method according to claim 4 , wherein the composite material structure is a fan casing of a gas turbine for an aeroengine.

Assignees

• Snecma

Inventors

• Mathon Richard
• Phelippeau Antoine

Classifications

• B29L2031/7504

  Turbines · CPC title

• B29C70/885

  with incorporated metallic wires, nets, films or plates (as lost heating elements B29C35/0272, B29C61/0625) · CPC title

• B29C70/48 Primary

  and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title

• B29C70/68 Primary

  by incorporating or moulding on preformed parts, e.g. inserts or layers {, e.g. foam blocks (mould constructions therefor B29C33/12; joining preformed parts by moulding B29C65/70)} · CPC title

• Y10T29/53687

  by rotation of work part · CPC title