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US4195478A Expired / Lapsed US ⏱️ 0.0 years remaining

Low cost insertable type port liner

Assignee: Ford Motor Co
•
Filing: 1977-11-09
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Granted: 1980-04-01
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Expires: 1997-11-09
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Abstract

Abstract A method and apparatus for insulating the exhaust passage of an internal combustion engine is disclosed. A three-zone liner assembly is provided with an outer zone comprised of a room temperature vulcanizing silicone sleeve, an inner zone comprised of a stamped and seam welded high strength Al--Cr--steel alloy, and an intermediate zone consisting of a ceramic wool mat. The liner assembly is supported or enclosed within a mild carbon sheet metal sleeve which in turn may be bonded to the engine passage wall by use of a room-temperature-vulcanized silicone if of the insert type, or by fusion bonding during casting if of the cast-in-place type.

Inventors

  • 👤 Vemulapalli D. N. Rao
  • 👤 Benjamin T. Howes
  • 👤 Angelo Jaimee

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 22:34
CPC Classifications
B; B32; B32B; B32B15/00; B32B15/04; F; F02; F02B; F02B77/00; F02B77/11; B32B15/06; B32B25/00; B32B25/20; B32B7/00; B32B7/04; B32B7/12; B32B2250/00; B32B2250/03; B32B2307/00; B32B2307/30; B32B2307/304; B32B2307/306; B32B2311/00; B32B2315/00; B32B2315/02; F01; F01N; F01N2310/00; F01N2310/06

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 203 words
For use in an internal combustion engine having a housing mass enclosing a combustion zone in one portion thereof, apparatus for modifying the heat transfer characteristic through the walls of an unlined passage extending through said portion of the mass of said engine, said passage walls defining an outer wall and an interior space, insulating means in said passage conforming substantially to the inner contour of said passage outer wall and having a layered assembly with at least five radially distinct zones, the outermost or first zone of said layered assembly consisting of a room-temperature-curable silicone plastic in the thickness range of 0.02-0.05 inches, a second zone consisting of a plain carbon steel sleeve containing less than 0.6% carbon and having a thickness in the range of 0.015-0.018 inches, a third zone consisting of a coating of room-temperature-curable silicone plastic in a thickness of about 0.01 inches and having a melting temperature greater than 200° F., a fourth zone consisting of an insulating wool or fiber mat in the thickness range of 0.020-0.060 inch providing numerous enclosed trapped air spaces, and a fifth or innermost zone consisting of a temperature resistant and weldable metal alloy, said latter zone having a thickness of 0.020-0.040.
Claim 2
Dependent Claim 203 words
For use in an internal combustion engine having a housing mass enclosing a combustion zone in one portion thereof, apparatus for modifying the heat transfer characteristic through the walls of an unlined passage extending through said portion of the mass of said engine, said passage walls defining an outer wall and an interior space, insulating means in said passage conforming substantially to the inner contour of said passage outer wall and having a layered assembly with at least five radially distinct zones, the outermost or first zone of said layered assembly consisting of a room-temperature-curable silicone plastic in the thickness range of 0.02-0.05 inches, a second zone consisting of a plain carbon steel sleeve containing less than 0.6% carbon and having a thickness in the range of 0.015-0.018 inches, a third zone consisting of a coating of room-temperature-curable silicone plastic in a thickness of about 0.01 inches and having a melting temperature greater than 200° F., a fourth zone consisting of an insulating wool or fiber mat in the thickness range of 0.020-0.060 inch providing numerous enclosed trapped air spaces, and a fifth or innermost zone consisting of a temperature resistant and weldable metal alloy, said latter zone having a thickness of 0.020-0.040.

References Cited (Backward Citations)

US2317018A Cited
US2703355A Cited
US3000433A Cited
US3027252A Cited
US3477869A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-04-01 1983-10-01 1984-04-01 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-04-01 1987-10-01 1988-04-01 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-04-01 1991-10-01 1992-04-01 $7700.00 Window Closed / Lapsed

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