ASSEMBLY OF SUB-COMPONENTS BY COMPRESSION MOLDING

Abstract

A thermoplastic composite component assembly and method of manufacturing the thermoplastic composite component assembly is disclosed. The thermoplastic composite component assembly is manufactured by first performing a molding step to form individual assembly features as discrete assembly feature components, and separately forming a thermoplastic composite component using a first compression molding step. Then, a reprocessing step is performed where the discrete assembly feature components are integrated with the thermoplastic composite component using a second compression molding step. The reprocessing step essentially welds the discrete assembly feature components to the thermoplastic composite component at each of a plurality of desired assembly feature sites.

Claims

1. A method of manufacturing a thermoplastic composite component assembly, the method comprising: a. manufacturing a discrete assembly feature component; b. manufacturing a discrete thermoplastic composite component; c. aligning the assembly feature component with an assembly feature site on the thermoplastic composite component; and d. applying heat and compression to bond the assembly feature component to the thermoplastic composite component at the assembly feature site to form the thermoplastic composite component assembly.

2. The method of claim 1 wherein manufacturing the thermoplastic composite component comprises performing a compression molding process to a thermoplastic composite material.

3. The method of claim 2 wherein the compression molding process comprises applying heat and compression to the thermoplastic composite material.

4. The method of claim 3 wherein the thermoplastic composite component has a molded shape.

5. The method of claim 2 wherein the thermoplastic composite component comprises a plurality of thermoplastic composite layers, and manufacturing the thermoplastic composite component further comprises performing a pre-consolidation process to form laminated thermoplastic composite layers, and performing the compression molding process comprises performing the compression molding process to the laminated thermoplastic composite layers to form the thermoplastic composite component.

6. The method of claim 5 wherein each thermoplastic composite layer comprises a thermoplastic material and a fibrous reinforcement.

7. The method of claim 1 wherein applying heat and compression comprises applying a compression molding process.

8. The method of claim 7 wherein the assembly feature component includes a thermoplastic layer at a distal end, and aligning the assembly feature component with the assembly feature site on the thermoplastic composite component comprises placing the thermoplastic layer at the distal end of the assembly feature component against the thermoplastic composite component, and applying the compression molding process melts the thermoplastic layer to bond the distal end of the assembly feature component with the thermoplastic composite component at the assembly feature site.

9. The method of claim 1 wherein the assembly feature component comprises one of a stud, a fastener, or a threaded insert.

10. The method of claim 1 wherein the assembly feature component comprises a threaded insert, and the threaded insert comprises a thread insert and thermoplastic layer coupled to the thread insert.

11. The method of claim 10 wherein the threaded insert has a threaded hole exposed at a first end of the threaded insert, and the thermoplastic layer forms a cap over a second end of the threaded insert.

12. The method of claim 11 wherein the cap of the threaded insert is positioned against the thermoplastic composite component, and applying heat and pressure melts the cap to bond with the thermoplastic composite component at the assembly feature site.

13. The method of claim 1 further comprising manufacturing a plurality of the discrete assembly feature components, aligning each of the plurality of assembly feature components with a corresponding assembly feature site on the thermoplastic composite component, and applying heat and compression to bond each of the plurality of assembly feature components to the thermoplastic composite component at each of the corresponding assembly feature sites.

14. The method of claim 13 wherein applying heat and compression comprises applying a compression molding process to simultaneously bond each of the plurality of assembly feature components to the thermoplastic composite component at each of the corresponding assembly feature sites.

15. The method of claim 14 wherein aligning each of the plurality of assembly feature components with a corresponding assembly feature site on the thermoplastic composite component comprises positioning each of the plurality of assembly feature components in a corresponding cavity within a compression molding tool and positioning the thermoplastic composite component into a holding location in the compression molding tool.

16. A thermoplastic composite component assembly comprising: a. a thermoplastic composite component; b. an assembly feature component compression molded to the thermoplastic composite component.

17. The thermoplastic composite component assembly of claim 16 wherein the thermoplastic composite component has a molded shape.

18. The thermoplastic composite component assembly of claim 16 wherein the thermoplastic composite component comprises a plurality of thermoplastic composite layers laminated together.

19. The thermoplastic composite component assembly of claim 16 wherein the assembly feature component includes a thermoplastic layer at a distal end, and the thermoplastic layer at the distal end of the assembly feature component is bonded to the thermoplastic composite component at the assembly feature site.

20. The thermoplastic composite component assembly of claim 16 wherein the assembly feature component comprises one of a stud, a fastener, or a threaded insert.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Several example embodiments are described with reference to the drawings, wherein like components are provided with like reference numerals. The example embodiments are intended to illustrate, but not to limit, the invention. The drawings include the following figures:

[0014] FIG. 1 illustrates an exemplary manufacturing process for making a thermoplastic composite component assembly according to some embodiments.

[0015] FIG. 2 illustrates a cut-out side view of the molded threaded insert.

[0016] FIG. 3 illustrates a cut-out side view of the molded thread insert bonded to the thermoplastic composite component.

DETAILED DESCRIPTION OF THE EMBODIMENTS

[0017] Embodiments of the present application are directed to a thermoplastic composite component assembly and method of manufacturing. Those of ordinary skill in the art will realize that the following detailed description of the thermoplastic composite component assembly and method of manufacturing is illustrative only and is not intended to be in any way limiting. Other embodiments of the thermoplastic composite component assembly and method of manufacturing will readily suggest themselves to such skilled persons having the benefit of this disclosure.

[0018] Reference will now be made in detail to implementations of the thermoplastic composite component assembly and method of manufacturing as illustrated in the accompanying drawings. The same reference indicators will be used throughout the drawings and the following detailed description to refer to the same or like parts. In the interest of clarity, not all of the routine features of the implementations described herein are shown and described. It will, of course, be appreciated that in the development of any such actual implementation, numerous implementation-specific decisions must be made in order to achieve the developer's specific goals, such as compliance with application and business related constraints, and that these specific goals will vary from one implementation to another and from one developer to another. Moreover, it will be appreciated that such a development effort might be complex and time-consuming, but would nevertheless be a routine undertaking of engineering for those of ordinary skill in the art having the benefit of this disclosure.

[0019] The thermoplastic composite component assembly includes one or more assembly features integrally formed with the thermoplastic composite component although the one or more assembly features and the thermoplastic composite component are initially manufactured separately as discrete components. An assembly feature is a mounting feature that enables the thermoplastic composite component assembly to be assembled, mounted, connected, joined, attached, or similarly coupled (collectively referred to as assembled) to another discrete component having a complementary assembly feature.

[0020] In the manufacturing process used to make the thermoplastic composite component assembly, the discrete assembly feature components are manufactured separately from the manufacturing of the thermoplastic composite component. The separately manufactured assembly feature components are then integrally combined with the thermoplastic composite component using a compression molding process. FIG. 1 illustrates an exemplary manufacturing process for making a thermoplastic composite component assembly according to some embodiments. A thermoplastic composite component can be made using one or more discrete thermoplastic composite layers combined together. Each thermoplastic composite layer is a combination of thermoplastic material and a reinforcement material of the types previously described. In the exemplary process shown in FIG. 1, N thermoplastic composite layers are used. In some embodiments, each thermoplastic composite layer is made of fabric-thermoplastic prepreg (fibrous reinforcement in the form of a fabric) or unidirectional thermoplastic prepreg (fibrous reinforcement made of individual fibers aligned in a single direction).

[0021] In a step 6, the N thermoplastic composite layers are laminated together through pre-consolidation to form laminated thermoplastic composite layers 8. In a pre-consolidation process, all layers of the composite are not fully pressed together, they just form one loosely attached preform to ease the operation in compression process. In some embodiments, lamination is done using heat and pressure to bond together the N thermoplastic composite layers. At a step 10, a first compression molding process is performed on the laminated thermoplastic composite layers 8, using a first compression molding tool, under suitable pressure and temperature to form a thermoplastic composite component 12 having a molded shape. The pressure is controlled by the molding tool and related machinery, and the temperature is a function of the composite material property. In some embodiments, the first compression molding tool is a different tool than that used for the lamination performed in step 6. Separately from manufacturing the thermoplastic composite component 12, discrete assembly feature components are manufactured. In an exemplary embodiment, one or more of the assembly feature components is a molded thread insert. Subsequent description is based on such a molded thread insert. It is understood that alternative types of assembly feature components can be manufactured and used, such as studs, fasteners, or other types of thread inserts. The molded thread insert can be made by first obtaining a thread insert part 14 and then over-molding the thread insert part 14 with a thermoplastic layer 18, such as by using an injection molding process at a step 16. It is understood that alternative conventional over-molding processes can be used to form the thermoplastic layer 18 over the thread insert 14. The result is a molded thread insert, shown as an assembly feature component 20.

[0022] FIG. 2 illustrates a cut-out side view of the molded thread insert 20. The over-molded thermoplastic layer 18 embeds the thread insert 14. At one end of the thread, a hole of the thread insert 14 is open, and at the other end, there is an extra thermoplastic material 32 that forms a cap. The extra thermoplastic material 32 is a base of the molded thread insert 20, where the base is positioned against an assembly feature site on the thermoplastic composite component. In some embodiments, a thickness of the extra thermoplastic material is in range of 0.5-2 mm. It is understood that thicknesses less than 0.5 mm and greater than 2 mm can be used. To enhance the bonding strength of the base to the underlying thermoplastic composite component 12, the base of the molded thread insert can have a round corner or a chamfer with bigger diameter than the main body.

[0023] Returning to FIG. 1, at a step 22, one or more of the manufactured assembly feature components 20 are positioned on corresponding assembly feature sites of the thermoplastic composite component 12. In some embodiments, a second compression tool is used for bonding the assembly feature components 20 to the thermoplastic composite component 12. The discrete assembly feature components 20 are placed in the second compression tool along with the already formed thermoplastic composite component 12. The second compression tool is configured for the already formed thermoplastic composite component 12 to be positioned in a specific first location and alignment, and with specifically located cavities corresponding to each assembly feature site. Each cavity is configured to receive a corresponding one of the discrete assembly feature components 20. At a step 24, once the second compression tool is loaded with the already formed thermoplastic composite component 12 in the first location and the discrete assembly feature components 20 in the cavities, the second compression tool is heated to a specific temperature, and compression is applied to compress each discrete feature component 20 to the thermoplastic composite component 12 at each assembly feature site. As related to the exemplary molded thread insert 20, the extra thermoplastic material 32 is bonded to the thermoplastic composite component 12. FIG. 3 illustrates a cut-out side view of the molded thread insert 20 bonded to the thermoplastic composite component 12. As shown in FIG. 3, the base of the molded thread insert 20 formed by the extra thermoplastic material 32 is bonded to the thermoplastic composite component 12 at an assembly feature site 34. At each assembly feature site, the thermoplastic material at the interface between each discrete assembly feature component and the thermoplastic composite material used to form the thermoplastic composite component melts, or reflows, which when cooled essentially welds each discrete assembly feature component to the thermoformed thermoplastic composite component. An aspect of this process is to manage the amount of thermoplastic material at each feature site interface to control the welding. Another aspect of this process is to precisely control the temperature applied to the assembly feature components 20 and the thermoplastic composite component 12 to enable bonding of each assembly feature component 20 to the thermoplastic composite component 12 while maintaining the integrity of the thermoplastic composite component 12. To assure the success of the bonding process, the thermoplastic layer of the molded thread insert should have compatibility with the thermoplastic resin matrix of the thermoplastic composite component. The interface area between the molded thread insert and the composite also determines the bonding force. In an exemplary application, nine layers of carbon fiber thermoplastic prepreg are used, the thermoplastic resin matrix of the thermoplastic composite is polycarbonate and the thermoplastic used to over-mold the thread insert is also polycarbonate. The thread insert size of the molded thread insert is ISO M40.7, the outer diameter is 6 mm, and the over-molded thermoplastic layer diameter surrounding the thread insert is 10 mm. Tested bonding force between such a molded thread insert and thermoplastic composite component is higher than 1000 Newton.

[0024] The present application has been described in terms of specific embodiments incorporating details to facilitate the understanding of the principles of construction and operation of the thermoplastic composite component assembly and method of manufacturing. Many of the components shown and described in the various figures can be interchanged to achieve the results necessary, and this description should be read to encompass such interchange as well. As such, references herein to specific embodiments and details thereof are not intended to limit the scope of the claims appended hereto. It will be apparent to those skilled in the art that modifications can be made to the embodiments chosen for illustration without departing from the spirit and scope of the application.