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US4516782A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of producing high temperature composite seal

Assignee: Metex Corp USA
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Filing: 1983-08-29
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Granted: 1985-05-14
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Expires: 2003-08-29
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Abstract

Abstract A high temperature seal, particularly suitable for use in vehicle engine exhaust systems, formed of a composite structure including refractory sheet material and wire mesh. In a typical application, the seal is disposed between confronting ends of an engine exhaust manifold pipe and an exhaust tail pipe, and permits relative rotation of the pipes without impairment of the effectiveness of the seal, thereby preventing leakage of high temperature exhaust gases passing through the joined pipes.

Inventors

  • 👤 Peter P. Usher

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 17:22
CPC Classifications
F; F01; F01N; F01N13/00; F01N13/18; F01N13/1805; F01N13/1827; F16; F16J; F16J15/00; F16J15/02; F16J15/06; F16J15/10; F16J15/12; F16L; F16L27/00; F16L27/02; F16L27/04; F16L27/053; F16L27/06; F16L27/073; Y; Y10; Y10S; Y10S285/00; Y10S285/91

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 163 words
A method of producing substantially coherent high temperature exhaust seal adapted to sealingly engage confronting surfaces on pipes and flanges to be joined to one another to form a flexible joint comprising the steps of constructing a generally cylindrical preform by convoluting a strip of flexible refractory sheet material with one or more overlaying pieces of flexbile knitted wire mesh said wire mesh being formed of wire and having voids of given size between said wires, disposing said preform in a compression die, said die having a cavity size and shape which is substantially the same as the desired exhaust seal, and applying an axial load to said preform, said load being of sufficient force to collapse said preform to substantially the size and shape of said exhaust seal and to cause said refractory material to substantially fill the openings in said wire mesh and substantially all other air voids within said exhaust seal and to become firmly interlocked with said wire mesh.
Claim 2
Independent Claim 163 words
A method of producing substantially coherent high temperature exhaust seal adapted to sealingly engage confronting surfaces on pipes and flanges to be joined to one another to form a flexible joint comprising the steps of constructing a generally cylindrical preform by convoluting a strip of flexible refractory sheet material with one or more overlaying pieces of flexbile knitted wire mesh said wire mesh being formed of wire and having voids of given size between said wires, disposing said preform in a compression die, said die having a cavity size and shape which is substantially the same as the desired exhaust seal, and applying an axial load to said preform, said load being of sufficient force to collapse said preform to substantially the size and shape of said exhaust seal and to cause said refractory material to substantially fill the openings in said wire mesh and substantially all other air voids within said exhaust seal and to become firmly interlocked with said wire mesh.
Claim 3
Dependent Claim 22 words
The method of claim 1 wherein the length of wire mesh corresponds to two or more circumferential lengths of the finished seal.
Claim 4
Dependent Claim 22 words
The method of claim 1 wherein the width of the mesh is two or more times the height of the finished seal.

References Cited (Backward Citations)

US2400533A Cited
US2398210A Cited
US2676823A Cited
US2924471A Cited
US3044922A Cited
GB972650A Cited
US3404061A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-05-13 1988-11-12 1989-05-14 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-05-13 1992-11-12 1993-05-14 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-05-13 1996-11-12 1997-05-14 $7700.00 Window Closed / Lapsed

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