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US4305348A Expired / Lapsed US ⏱️ 0.0 years remaining

Seal for an internal combustion engine

Assignee: TRW Automotive Products Inc
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Filing: 1978-10-23
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Granted: 1981-12-15
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Expires: 1998-10-23
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Abstract

Abstract The invention relates to an internal combustion engine structure, and addresses the problem of preventing coolant and lubricant from mixing therein. A seal structure is provided for sealing between an engine block 10 and a cylinder liner 34 in an internal combustion engine. The seal structure 40, 42 comprises an annular insert member preferably made of a high temperature resistant resinous material. The insert 100 fits in a recess 136, 134 in the engine block 98 and encircles the cylinder liner 94. A resilient seal member 110, 112, 114 in a groove 104, 106, 108 in the inner surface 130 of the insert 100 seals against the cylinder liner 94.

Inventors

  • 👤 Jon W. Martin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 14:02
CPC Classifications
F; F02; F02F; F02F1/00; F02F1/02; F02F1/10; F02F1/16; F02F1/166; F16; F16J; F16J15/00; F16J15/02; F16J15/021; F16J15/022; F02B; F02B3/00; F02B3/06

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 291 words
Apparatus comprising an engine block having an aperture therein, a cylindrical combustion chamber cylinder liner received in said aperture, said engine block in part defining separate chambers for coolant and lubricant, respectively, a seal structure coacting between said cylinder liner and said engine block to prevent intermixing of coolant and lubricant, said seal structure comprising an annular insert having a conical exterior surface extending between a narrow axial end and a wide axial end of said annular insert, said conical exterior surface engaging a complementary configured conical surface in said engine block, said insert also having an interior surface with is generally cylindrical, said annular insert further having a pair of axial end surfaces which extend parallel to each other and perpendicular to the axis of said interior surface at the opposite ends of said conical surface, said engine block having a ledge surface extending transverse to said axis of said interior surface, the end surface of said annular insert at said wide end of said annular insert engaging said ledge surface, at least one annular resilient seal member in a circumferential seal groove formed in said interior surface for resilient sealing engagement with said cylinder liner, said annular resilient seal member exerting a radially outwardly directed force to enhance the sealing engagement of said conical exterior surface of said annular insert with said configure conical surface in said engine block, the diameter of said aperture and the outer diameter of said annular insert at said narrow end being substantially equal, and said annular insert being resiliently deformable to enable said wide end of said annular insert to be moved through said aperture to position said end surface at the wide end of said insert in engagement with said ledge surface.
Claim 2
Dependent Claim 291 words
Apparatus comprising an engine block having an aperture therein, a cylindrical combustion chamber cylinder liner received in said aperture, said engine block in part defining separate chambers for coolant and lubricant, respectively, a seal structure coacting between said cylinder liner and said engine block to prevent intermixing of coolant and lubricant, said seal structure comprising an annular insert having a conical exterior surface extending between a narrow axial end and a wide axial end of said annular insert, said conical exterior surface engaging a complementary configured conical surface in said engine block, said insert also having an interior surface with is generally cylindrical, said annular insert further having a pair of axial end surfaces which extend parallel to each other and perpendicular to the axis of said interior surface at the opposite ends of said conical surface, said engine block having a ledge surface extending transverse to said axis of said interior surface, the end surface of said annular insert at said wide end of said annular insert engaging said ledge surface, at least one annular resilient seal member in a circumferential seal groove formed in said interior surface for resilient sealing engagement with said cylinder liner, said annular resilient seal member exerting a radially outwardly directed force to enhance the sealing engagement of said conical exterior surface of said annular insert with said configure conical surface in said engine block, the diameter of said aperture and the outer diameter of said annular insert at said narrow end being substantially equal, and said annular insert being resiliently deformable to enable said wide end of said annular insert to be moved through said aperture to position said end surface at the wide end of said insert in engagement with said ledge surface.
Claim 3
Dependent Claim 24 words
Apparatus as defined in claim 1 wherein said annular insert is made of an organic resinous material having a softening point above 300° F.
Claim 4
Dependent Claim 42 words
Apparatus as defined in claim 1 wherein said annular insert has a plurality of axially spaced circumferential seal grooves formed in said interior surface, and an annular resilient seal member is located in each of said plurality of axially spaced circumferential grooves.
Claim 5
Dependent Claim 81 words
Apparatus as defined in claim 1 wherein said ring-shaped body has surfaces defining three parallel circumferential grooves in said interior surface, each of said grooves having an O-ring seal member therein sealingly engaging said body and said cylinder liner, the O-ring in the lower groove being formed from a co-polymer of hexafluoropropene and vinylidene fluoride blended with 5%-10% ethylene-propylene terpolymer rubber, the middle O-ring being formed from Neoprene, and the upper O-ring being formed from a co-polymer of ethylene and propylene.

References Cited (Backward Citations)

DE32483C Cited
US1208744A Cited
GB313033A Cited
GB548682A Cited
US2376017A Cited
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US3853099A 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) 1984-12-14 1985-06-15 1985-12-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-12-14 1989-06-15 1989-12-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-12-14 1993-06-15 1993-12-15 $7700.00 Window Closed / Lapsed

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