Thermoplastic composite support structures with integral fittings and method

Patent metadata

Field	Value
Publication number	US-9302434-B2
Application number	US-201314095531-A
Country	US
Kind code	B2
Filing date	Dec 3, 2013
Priority date	Dec 3, 2013
Publication date	Apr 5, 2016
Grant date	Apr 5, 2016

Abstract

A compression molded composite structure includes an elongated thermoplastic composite part having integral thermoplastic composite fittings.

First claim

What is claimed is:

1. A method of making a composite part having at least one integral fitting, comprising:
placing a compression cylinder on a mold having a part cavity and at least one fitting cavity;
relatively moving the compression cylinder and the mold along a length of the part;
placing a charge of fiber reinforced resin flakes in the cylinder;
melting resin in the flakes to form a flowable mixture of resin and fibers; and
compressing the flowable mixture into the part cavity and into the fitting cavity as the compression cylinder and the mold move relative to each other along the length of the part.

2. The method of claim 1 , wherein relatively moving the compression cylinder and the mold is performed by continuously moving the mold relative to the compression cylinder.

3. The method of claim 1 , wherein relatively moving the compression cylinder and the mold is performed by intermittently moving the mold relative to the compression cylinder.

4. The method of claim 1 , further comprising:
placing a charge of fiber reinforced resin flakes in each of a plurality of compression cylinders; and
placing each of the compression cylinders on the mold at different locations to respectively form different regions of the part.

5. The method of claim 1 , wherein compressing the flowable mixture is performed by forcing a piston through the cylinder.

6. The method of claim 1 , wherein the resin is a thermoplastic resin.

7. The method of claim 1 , wherein each of the fibers has a length greater than approximately 0.25 inches.

8. The method of claim 1 , wherein each of the fibers has a length of approximately 0.5 inches.

9. A method of making an elongated, fiber reinforced thermoplastic structure having an integral fitting, comprising:
forming a fiber reinforced thermoplastic part by continuous compression molding;
placing a compression cylinder on the part;
compression molding a thermoplastic fitting on the fiber reinforced thermoplastic part using the compression cylinder to compress a flowable mixture of thermoplastic resin and randomly oriented reinforcing fibers onto the part; and
moving the part relative to the compression cylinder along a length of the part to various regions along the length of the part to successively form each of a plurality of fittings on the part.

10. The method of claim 9 , further comprising:
melting together areas of the part with the flowable resin.

11. The method of claim 9 , wherein compression molding a thermoplastic fitting includes:
positioning each of a plurality of molds on the part, and
using the compression cylinder to compress a flowable mixture of thermoplastic resin and fibers into each of the molds and against the part.

12. The method of claim 11 , further comprising:
introducing a charge of thermoplastic prepreg flakes into the compression cylinder; and
melting the resin in the prepreg flakes by heating the charge within the compression cylinder.

Assignees

• Boeing Co

Inventors

• Griffing James Scott

Classifications

• Y10T428/24132

  including grain, strips, or filamentary elements in different layers or components parallel · CPC title

• B29C45/02 Primary

  Transfer moulding, i.e. transferring the required volume of moulding material by a plunger from a "shot" cavity into a mould cavity · CPC title

• Y10T428/31721

  Of polyimide · CPC title

• B29C70/081

  Combinations of fibres of continuous or substantial length and short fibres · CPC title

• B29C45/0408 Primary

  involving at least a linear movement (B29C45/0433 takes precedence) · CPC title