Method of forming pressure pad or other flexible element for use during cure of composite materials

Patent metadata

Field	Value
Publication number	US-2017225409-A1
Application number	US-201615264136-A
Country	US
Kind code	A1
Filing date	Sep 13, 2016
Priority date	Sep 14, 2015
Publication date	Aug 10, 2017
Grant date	—

Abstract

A method of manufacturing a flexible element configured for pressing against composite material received on a mold surface of a mold during cure, including placing a porous material over the mold surface, forming a sealed enclosure containing the mold surface and the porous material, infusing a curable liquid material such as silicone in liquid form into the enclosure under vacuum and through the porous material, curing the liquid material to form the flexible element, and opening the enclosure and disengaging the flexible element from the mold. In a particular embodiment, the flexible element is a pressure pad.

First claim

1 . A method of manufacturing a pressure pad configured for pressing against composite material received on a mold surface of a mold during cure, the method comprising:
placing a porous material over the mold surface; forming a sealed enclosure containing the mold surface and the porous material; with the sealed enclosure under vacuum, infusing a curable liquid material into the enclosure and through the porous material; curing the liquid material under vacuum to form the pressure pad; and opening the enclosure and disengaging the pressure pad from the mold.

2 . The method according to claim 1 , further comprising trimming excess material from the pressure pad after disengaging the pressure pad from the mold.

3 . The method according to claim 1 , wherein the porous material is placed with at least a portion thereof spaced apart from the mold so as to define a cavity between the mold and the portion of the porous material, and wherein placing the porous material includes removably connecting the porous material to the mold so that the portion remains spaced apart from the mold under vacuum.

4 . The method according to claim 1 , wherein the porous material is a first porous material, the method further comprising, before infusing the curable liquid material, placing at least one second porous material over the first porous material to overlap predetermined areas of the mold.

5 . The method according to claim 4 , wherein the first porous material is shaped under vacuum against the mold surface before placing the at least one second porous material over the first porous material.

6 . The method according to claim 1 , further comprising, before forming the enclosure, placing a protective material on the porous material over selected features of the mold, the protective material being more tear resistant than the porous material.

7 . The method according to claim 6 , wherein the protective material is a polytetrafluoroethylene tape.

8 . The method according to claim 1 , wherein the liquid material is cured at ambient temperature.

9 . The method according to claim 1 , wherein the curable liquid material includes silicone.

10 . The method according to claim 1 , wherein the porous material includes a polyester breather fabric.

11 . The method according to claim 1 , further comprising adjusting a level of the vacuum during the infusion.

12 . A method of manufacturing a flexible element configured for pressing against composite material received on a mold surface of a mold during cure, the method comprising:
placing a porous material over the mold surface; placing the mold and the porous material in a sealed enclosure under vacuum; infusing silicone in liquid form into the enclosure through the porous material; curing the silicone in the sealed enclosure under vacuum to form the flexible element with the porous material being embedded therein; and disengaging the flexible element from the sealed enclosure and from the mold.

13 . The method according to claim 12 , wherein the flexible element is shaped for use as bagging material during the cure of the composite material.

14 . The method according to claim 12 , wherein the flexible element is shaped for use as a pressure pad received inside a sealed enclosure also containing the composite material during the cure of the composite material.

15 . The method according to claim 12 , wherein the porous material is placed with at least a portion thereof spaced apart from the mold so as to define a cavity between the mold and the portion of the porous material, and wherein placing the porous material includes removably connecting the porous material to the mold so that the portion remains spaced apart from the mold under vacuum.

16 . The method according to claim 12 , wherein the porous material is a first porous material, the method further comprising, before infusing the curable liquid material, placing at least one second porous material over the first porous material to overlap predetermined areas of the mold.

17 . The method according to claim 16 , wherein the first porous material is shaped under vacuum against the mold surface before placing the at least one second porous material over the first porous material.

18 . The method according to claim 12 , further comprising, before forming the enclosure, placing a protective material on the porous material over selected features of the mold, the protective material being more tear resistant than the porous material.

19 . The method according to claim 12 , wherein the liquid material is cured at ambient temperature.

20 . The method according to claim 12 , wherein the porous material includes a polyester breather fabric.

Assignees

• Bell Helicopter Textron Inc
• Nat Res Council Canada

Inventors

• Lauzon Marc
• Dupré Patrick
• Octeau Marc-André
• Forget Pascal
• Roy Steven

Classifications

• B29C33/3842

  Manufacturing moulds, e.g. shaping the mould surface by machining · CPC title

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29C70/443 Primary

  and impregnating by vacuum or injection · CPC title

• B29C70/10

  characterised by the structure of fibrous reinforcements {, e.g. hollow fibres} · CPC title

• B29C70/549

  Details of caul plates, e.g. materials or shape · CPC title