HEADLINER AND METHOD OF PRODUCING SAME
20200061886 ยท 2020-02-27
Inventors
- Paul Alan Forgette (Brownstown, MI, US)
- Amy M. Boardman (Garden City, MI, US)
- John Andrew Stakoe (Bloomfield Hills, MI, US)
- Anna Miller Hill (Belleville, MI, US)
- Robert Ralph Armitage, Jr. (Howell, MI, US)
Cpc classification
B29C51/02
PERFORMING OPERATIONS; TRANSPORTING
B29C45/1418
PERFORMING OPERATIONS; TRANSPORTING
B29C2045/14188
PERFORMING OPERATIONS; TRANSPORTING
B29C51/165
PERFORMING OPERATIONS; TRANSPORTING
B29C2045/14286
PERFORMING OPERATIONS; TRANSPORTING
B29C51/12
PERFORMING OPERATIONS; TRANSPORTING
B29C51/268
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C45/14
PERFORMING OPERATIONS; TRANSPORTING
B29C51/12
PERFORMING OPERATIONS; TRANSPORTING
B60R13/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A headliner includes a unitary body having a substrate with an A-surface and a B-surface, a secondary component carried on the B-surface and a laminated surface covering on the A-surface. That method of producing that headliner with a unitary body is also provided.
Claims
1. A headliner, comprising: a unitary body including (a) a substrate having an A-surface and a B-surface, (b) a secondary component carried on said B-surface and (c) a laminated surface covering on said A-surface.
2. The headliner of claim 1, wherein said secondary component is a side air curtain deployment feature.
3. The headliner of claim 1, wherein said secondary component is an integral attachment feature.
4. The headliner of claim 3, wherein said integral attachment feature is a bracket.
5. The headliner of claim 4, wherein said bracket includes a receiver adapted to receive and hold a magnetic fastener.
6. The headliner of claim 1, wherein said secondary component is an integral reinforcement.
7. The headliner of claim 6, wherein said integral reinforcement is a plurality of ribs.
8. The headliner of claim 1, wherein said secondary component is an integral energy absorbing feature.
9. The headliner of claim 1, wherein said secondary component is a trim ring.
10. The headliner of claim 9, wherein said trim ring includes a receiver adapted to receive a sun roof assembly.
11. A method of producing a headliner with a unitary body, comprising: thermoforming a blank into a headliner substrate; simultaneously injection molding a secondary component onto said headliner substrate wherein said secondary component is selected from a group consisting of a side air curtain deployment feature, an integral attachment feature, a bracket, a bracket including a receiver adapted to receive and hold a magnetic fastener, an integral reinforcement, a plurality of ribs, a trim ring, an integral energy absorbing feature and combinations thereof; and laminating a surface covering to said headliner substrate.
12. The method of claim 11, including heating said blank prior to thermoforming and injection molding.
13. The method of claim 12, including loading said blank into a combined thermoforming and injection molding apparatus following said heating.
14. The method of claim 13, including trimming said headliner substrate following said thermoforming and injection molding and before laminating.
15. The method of claim 14, including transferring said headliner substrate from said combined thermoforming and injection molding apparatus into a laminating press for said laminating.
Description
BRIEF DESCRIPTION OF THE DRAWING FIGURES
[0013] The accompanying drawing figures incorporated herein and forming a part of the specification, illustrate several aspects of the method together with the description serve to explain certain principles thereof.
[0014]
[0015]
[0016]
[0017]
[0018]
[0019]
[0020]
[0021] Reference will now be made in detail to the present preferred embodiments of the headliner and the method, examples of which are illustrated in the accompanying drawing figures.
DETAILED DESCRIPTION
[0022] As noted above, this document relates to a method of producing a headliner 10 having a unitary body 12. As illustrated in
[0023] More particularly, as will be described in greater detail below, the substrate 14 may be formed from a polypropylene glass matte technology (PP/GMT) blank. The secondary component 20 may be made from any appropriate plastic composite material suitable for injection molding and adapted for fusing with the PP/GMT material used to form the substrate. For purposes of this document it should be understood that the terminology unitary body means produced as a single integral component not requiring assembly from separate parts or components.
[0024] In the embodiment of the headliner 10 illustrated in
[0025] In the embodiment of the headliner 10 illustrated in
[0026]
[0027]
[0028]
[0029] Any of the headliners 10 illustrated in
[0030] This is then followed by the step of thermoforming the blank 48 into a headliner substrate 14 (note box 58) and simultaneously injection molding the secondary component 20 onto the B surface 18 of the headliner substrate (note box 60). Toward this end, the combined thermoforming and injection molding apparatus 100 of the illustrated embodiment includes a stationary platen 102 and a cooperating displaceable platen 104 to complete the thermoforming and compression molding of the blank 48 into the substrate 14. A clamping cylinder 106 displaces the displaceable platen 104 in the desired manner.
[0031] The combined thermoforming and injection molding apparatus 100 also includes an injection molding section having a feed hopper 108, for receiving plastic material in the form of pellets or the like, a feed screw or auger 110 for delivering the plastic material 112 toward the injection molding nozzle 114, a drive motor 116 for turning the feed screw and a cylinder 118 for reciprocating the feed screw through the barrel 120.
[0032] The secondary component 20 injection molded to the B surface 18 of the headliner substrate 14 may be selected from a group of secondary components consisting of the side air curtain deployment feature illustrated in
[0033] The method also includes the step of curing the headliner substrate 14 following thermoforming and injection molding and before laminating (note box 62) as well as the step of trimming the headliner substrate following thermoforming and injection molding and before laminating (note box 64). The trimming may be performed during the curing. Further, it should be appreciated that the trimming may include cutting any necessary holes in the headliner substrate 14 as required for the particular motor vehicle application for which the headliner is to be used.
[0034] As further illustrated, the method also includes the step of transferring the headliner substrate 14 from the combined thermoforming and injection molding apparatus 100 to a laminating press 200 (note box 68). This is then followed by the step of laminating the surface covering 22 to the A surface 16 of the headliner substrate 14 (note box 70).
[0035] That surface covering may comprise any appropriate material suited for the intended purpose including, for example, cloth, felt, alcantara or other appropriate material. The embodiment of the method illustrated in
[0036] More particularly, the broader method may include heating the blank prior to the thermoforming and injection molding and then loading the preheated blank into a combined thermoforming and injection molding apparatus following heating. Further, the method may include trimming the component substrate following the thermoforming and injection molding and before laminating. In addition, the method may include transferring the component substrate from the combined thermoforming and injection molding apparatus into a laminating press for the laminating process.
[0037] Numerous benefits and advantages result from the method of producing a headliner 10 with a unitary body 12 as described herein. The new method allows for the reduction of engineering and design inefficiencies. The method reduces component part proliferation by providing an integral unitary body thereby reducing both the piece cost and mass of the headliner 10 or overhead system.
[0038] Significantly, the method allows for a reduction in component tooling, assembly tooling and assembly capital equipment investment. Further, the method allows for directing indirect labor reduction while also eliminating the need for many different adhesives and mechanical fasteners thereby simplifying assembly processes. The method also results in reduced shipping requirements thereby eliminating any fuel and shipping container expenses. The above should be considered to be an exemplary list of the benefits and advantages provided by the method rather than an exhaustive recitation of those benefits and advantages.
[0039] The foregoing has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the embodiments to the precise form disclosed. Obvious modifications and variations are possible in light of the above teachings. All such modifications and variations are within the scope of the appended claims when interpreted in accordance with the breadth to which they are fairly, legally and equitably entitled.