Method of making composite wire mesh seal
AssigneeMetex Corporation
InventorPeter P. Usher
Life of this patent
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Abstract
A high temperature seal, particularly suitable for use in vehicle engine exhaust systems, is 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.
Claims9
A method of producing a substantially coherent high temperature composite seal comprising the steps of constructing a preform comprising flexible refractory sheet material aligned against flexible knitted wire mesh by convoluting of strip of refractory material with one or more overlying pieces of knitted wire mesh to form a generally cylindrical preform, 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 composite 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 composite seal and to cause said refractory material to substantially fill the openings in said wire mesh and to become firmly interlocked with said mesh.
A method of producing a 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 preform by convoluting a strip of flexible refractory sheet material with one or more overlying pieces of flexible 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.
Dependencies are inferred from the claim text.