Methods of joining and repairing composite components

Patent metadata

Field	Value
Publication number	US-11813802-B2
Application number	US-202117397435-A
Country	US
Kind code	B2
Filing date	Aug 9, 2021
Priority date	Apr 8, 2019
Publication date	Nov 14, 2023
Grant date	Nov 14, 2023

Abstract

A first thermoplastic component and a second thermoplastic component including a first joint portion and a second joint portion, respectively, are provided. A least a portion of a surface area of each of the first and second joint portions include a respective first and second mating surface. The first and second mating surfaces of the respective first and second joint portions are positioned in contact with one another. The first and second joint portions are fusion joined. Fusion joining the first and second joint portions forms a fused unitary portion of the first and second thermoplastic components.

First claim

What is claimed is:

1. A method for joining fiber-reinforced thermoplastic composite components, the method comprising:
providing a first fiber-reinforced thermoplastic composite component and a second fiber-reinforced thermoplastic composite component comprising a first joint portion and a second joint portion, respectively, at least a portion of a surface area of each of the first and second joint portions comprising a respective first and second mating surface;
positioning the first and second mating surfaces of the respective first and second joint portions in contact with one another;
consolidating the first and second joint portions with a press system; and
joining the first and second joint portions by applying heat and pressure to the first and second joint portions with the press system,
wherein the press system forms a first interface with a first surface of at least one of the first and second joint portions and a second interface with a second surface of at least one of the first and second joint portions opposite the first and second joint portions from the first interface and wherein the first and second surfaces are different than the first and second mating surfaces, and
wherein joining the first and second joint portions comprises melting an entire volume of the first and second joint portions to form a fused unitary portion of the first and second fiber-reinforced thermoplastic composite components.

2. The method of claim 1 , wherein the unitary portion is a homogenous portion.

3. The method of claim 1 , wherein the first and second mating surfaces have a load bearing joint configuration.

4. The method of claim 3 , wherein the load bearing joint configuration is a step configuration.

5. The method of claim 3 , wherein the load bearing joint configuration is a scarf configuration.

6. The method of claim 1 , wherein the step of joining the first and second joint portions includes applying a heat and a pressure to the first and second joint portions simultaneously.

7. The method of claim 6 , wherein the heat applied to the first and second joint portions is in a range of 600 to 800 T.

8. The method of claim 1 , wherein a thickness of the first and second joint portions disposed between the first and second interfaces is greater than 1.5 inches.

9. The method of claim 1 , wherein a first material of the first component and a second material of the second component each include at least one ply having a plurality of reinforcing fibers.

10. The method of claim 9 , wherein the plurality of reinforcing fibers of the at least one ply in each of the first material and the second material have a unidirectional fiber orientation.

11. The method of claim 1 , wherein the first mating surface and the second mating surface each extend from the first surface to the second surface.

12. The method of claim 1 , wherein the first component is a skin panel and the second component is a stiffener.

13. The method of claim 1 , wherein the press system includes a first tooling portion and a second tooling portion, the first tooling portion forming the first interface with the first surface and the second tooling portion forming the second interface with the second surface and wherein the one or both of the first interface and the second interface are non-planar, the method further comprising:
tailoring one or both of the first tooling portion and the second tooling portion to a specific geometry of the first component and the second component at the respective first interface and second interface.

14. A method for joining fiber-reinforced thermoplastic composite components, the method comprising:
providing a first fiber-reinforced thermoplastic composite component and a second fiber-reinforced thermoplastic composite component comprising a first joint portion and a second joint portion, respectively, the first and second joint portions comprising a volume of the respective first and second thermoplastic components and at least a portion of a surface area of each of the first and second joint portions comprising a respective first and second mating surface;
positioning the first and second mating surfaces of the respective first and second joint portions in contact with one another;
consolidating the first and second joint portions with a press system; and
joining the first and second joint portions,
wherein joining the first and second joint portions comprises melting an entire volume of the first and second joint portions to form a fused unitary portion of the first and second fiber-reinforced thermoplastic composite components which is a homogenous portion.

15. The method of claim 14 , wherein the first and second mating surfaces have a load bearing joint configuration.

16. The method of claim 15 , wherein the load bearing joint configuration is a step configuration.

17. The method of claim 15 , wherein the load bearing joint configuration is a scarf configuration.

18. The method of claim 14 , wherein a first material of the first fiber-reinforced thermoplastic composite component and a second material of the second fiber-reinforced thermoplastic composite component each include at least one ply having a plurality of reinforcing fibers.

19. The method of claim 14 , wherein the step of joining the first and second joint portions includes applying heat and pressure to the first and second joint portions with the press system, and wherein the heat applied to the first and second joint portions is in a range of 600 to 800° F.

20. The method of claim 14 , wherein the press system forms a first interface with a first surface of at least one of the first and second joint portions and a second interface with a second surface of at least one of the first and second joint portions opposite the first and second joint portions from the first interface and wherein the first and second surfaces are different than the first and second mating surfaces; and
wherein the press system includes a first tooling portion and a second tooling portion, the first tooling portion forming the first interface with the first surface and the second tooling portion forming the second interface with the second surface and wherein the one or both of the first interface and the second interface are non-planar, the method further comprising:
tailoring one or both of the first tooling portion and the second tooling portion to a specific geometry of the first component and the second component at the respective first interface and second interface.

Assignees

• Rohr Inc

Inventors

• Salah Lamia
• Bahramshahi Noushin
• Ursenbach Daniel O

Classifications

• B64C1/00

  Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like · CPC title

• B29C65/18 Primary

  using heated tools · CPC title

• B29C66/1162

  Single bevel to bevel joints, e.g. mitre joints · CPC title

• B29C66/12822

  comprising at least three overlap joint-segments · CPC title

• B29C66/12861

  comprising at least two bevelled joint-segments · CPC title