Claims
- 1. The method of forming heat insulating gasket structures for installation between an automotive engine and a carburetor mounted thereon comprising:
- a. die-cutting a member from a sheet of heat insulating material to form a core;
- b. providing said core with tab-like portions, some of which have a bolt hole therethrough; and
- c. pressing the core only at the tab-like portions to densify and decrease the volume of the core at the tab-like portions, and
- d. applying a gasket layer to at least one side of the core having a density less than that of the core, said gasket structure being thus densified, prior to installation of the gasket structure between said engine and carburetor.
- 2. The method in accordance with claim 1 wherein extra gasket material is provided in the tab-like portion.
- 3. The method in accordance with claim 2 wherein a sealing bead is formed on the outer face of the layer.
- 4. The method in accordance with claim 1 wherein a partial insert member in the form of a washer is inserted.
- 5. The method in accordance with claim 4 wherein a sealing bead is formed on the outer face of the layer.
- 6. The method of forming a heat-insulating gasket structure and the like comprising:
- a. die-cutting from phenolic impregnated asbestos millboard duplicate core parts having a tab-like portion containing a bolt-hole;
- b. interposing between said parts in the area of said tab-like portion a relatively dense substantially non-compressible washer-like member having a bolt-hole therethrough in alignment with the bolt holes provided in said core parts;
- c. placing the said components in a heated pin mold provided with at least one cavity in alignment with and approximately the same configuration as said washer component;
- d. applying heat and pressure to said pin mold to force at least one of the core parts into the mold cavity due to the incompressibility of the washer component to provide the core with a protuberance in the area of said bolt hole; and
- e. curing the composite core.
- 7. The method in accordance with claim 6 wherein a gasket layer is applied to at least one side of the composite core member.
- 8. The method in accordance with claim 7 wherein a sealing bead is formed on the outer face of the gasket layer.
- 9. The method in accordance with claim 8 wherein an additional sealing bead is formed around the periphery of the gasket structure.
- 10. The method in accordance with claim 8 wherein peripheral buttons are formed from such gasket layer.
- 11. The method in accordance with claim 8 wherein said sealing bead and said protuberance in the bolt-hole area are above the surface of the gasket covering.
- 12. The method in accordance with claim 7 wherein said gasket layer is provided with an opening of similar diameter to the outside diameter of said washer-like member into which said protuberance is forced by the application of said heat and pressure.
Parent Case Info
This application is a division of our application Ser. No. 120,526, filed Mar. 3, 1971, which was a continuation-in-part of our application Ser. No. 76,459, filed Sept. 29, 1970 (now U.S. Pat. No. 3,655,210), which was a continuation-in-part of our application Ser. No. 66,958, filed Aug. 26, 1970 (now abandoned).
US Referenced Citations (9)
Divisions (1)
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Number |
Date |
Country |
Parent |
120526 |
Mar 1971 |
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Continuation in Parts (2)
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Number |
Date |
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76459 |
Sep 1970 |
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Parent |
66958 |
Aug 1970 |
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