Composite material molding jig, composite material molding method, ultrasonic test system, ultrasonic test method and aircraft structural object

Patent metadata

Field	Value
Publication number	US-10416121-B2
Application number	US-201715451792-A
Country	US
Kind code	B2
Filing date	Mar 7, 2017
Priority date	Mar 24, 2016
Publication date	Sep 17, 2019
Grant date	Sep 17, 2019

Abstract

According to one implementation, a composite material molding jig includes a rigid portion and a convex portion for forming a groove for inserting an optical fiber sensor. The rigid portion has a surface for laminating prepreg sheets. The convex portion is formed in a surface side of the rigid portion. Further, according to one implementation, a composite material molding method is a method for molding a composite material, on which the groove for inserting the optical fiber sensor has been formed, by heating and curing a laminated body of the prepreg sheets laminated on the above-mentioned composite material molding jig.

First claim

What is claimed is:

1. A composite material molding method, comprising:
placing one or more plies of prepreg sheets on a molding jig, the molding jig comprising a rigid portion having a surface for laminating prepreg sheets, and a convex portion for forming a groove for insertion of an optical fiber sensor, the convex portion being formed in a surface side of the rigid portion, and
heating and curing a laminated body of the prepreg sheets laminated on the molding jig, the groove for inserting the optical fiber sensor having been formed in the one or more prepreg sheets, wherein
each of the one or more prepreg sheets is, prior to curing, a glass fiber reinforced plastic or a carbon fiber reinforced plastic, and
placing one or more plies of prepreg sheets on the molding jig comprises disposing one or more plies of prepreg sheets on each of both sides of the convex portion for forming the groove, with a length direction of fibers of the disposed one or more plies of prepreg sheets being a length direction of the convex portion.

2. The composite material molding method according to claim 1 ,
wherein the convex portion has a height of one ply of a prepreg sheet.

3. The composite material molding method according to claim 1 ,
wherein a height of the convex portion and a width of a cross section of the convex portion are not less than 125 μm and not more than 150 μm, respectively.

4. The composite material molding method according to claim 1 ,
wherein the convex portion has a length not more than 10 m in a longitudinal direction of the convex portion.

5. The composite material molding method according to claim 1 ,
wherein the groove has a depth corresponding to one ply of a prepreg sheet.

6. The composite material molding method according to claim 1 , further comprising:
inserting an optical fiber sensor into the groove formed in the composite material and applying an adhesive between the groove and the optical fiber sensor; and
hardening the adhesive to produce a composite material integrated with the optical fiber sensor.

7. The composite material molding method according to claim 1 ,
wherein at least one of both end portions of the groove in a length direction is made to have a shape of which a depth and a width of a cross section gradually decrease.

8. A composite material molding method comprising:
producing a laminated body of prepregs, which has a groove for inserting an optical fiber sensor, each of the prepregs, prior to curing, being a glass fiber reinforced plastic or a carbon fiber reinforced plastic; and
molding a composite material with the prepregs by curing the laminated body of the prepregs, the prepregs having the groove,
wherein the groove is formed without cutting fibers of the prepregs, a length direction of the groove being a length direction of the fibers, the groove being formed by disposing one or more plies of prepreg sheets on each of both sides of a convex portion for forming the groove, the convex portion being formed on a surface of a rigid composite material molding jig, a length direction of fibers of the disposed one or more plies of prepreg sheets being a length direction of the convex portion.

9. The composite material molding method according to claim 8 ,
wherein the groove has a depth corresponding to one ply of a prepreg sheet.

10. The composite material molding method according to claim 8 , further comprising:
inserting an optical fiber sensor into the groove formed in the composite material and applying an adhesive between the groove and the optical fiber sensor; and
hardening the adhesive to produce a composite material integrated with the optical fiber sensor.

11. The composite material molding method according to claim 8 ,
wherein at least one of both end portions of the groove in a length direction is made to have a shape of which a depth and a width of a cross section gradually decrease.

Assignees

• Fuji Heavy Ind Ltd
• Subaru Corp

Inventors

• Takahashi Kohei

Classifications

• B29L2031/3082

  Fuselages · CPC title

• B29K2105/06

  containing reinforcements, fillers or inserts · CPC title

• B29C2043/5808

  pressure or compressing force · CPC title

• B29C2033/0094

  Means for masking a part of the moulding surface · CPC title

• B29C70/42

  for producing articles of definite length, i.e. discrete articles · CPC title