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US4546737A Expired / Lapsed US ⏱️ 0.0 years remaining

Valve-seat insert for internal combustion engines

Assignee: Sumitomo Electric Industries Ltd
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Filing: 1984-06-29
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Granted: 1985-10-15
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Expires: 2004-06-29
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Abstract

Abstract A valve-seat insert for internal combustion engines comprises a double layered, sintered alloy composed of a valve-seat layer on which a valve is seated, and a base layer integrated with the valve-seat layer and adapted to be seated in a cylinder head of an engine. The valve-seat layer is composed of a sintered alloy of a high heat resistance and a high wear resistance having a composition comprising, by weight, 4 to 8% Co, 0.6 to 1.6% Cr, 4 to 8% Mo, 1 to 3% Ni, 0.3 to 1.5% C, 0.2 to 0.6% Ca, and the balance being substantially Fe, the additives, Co, Cr and Mo being present mainly in a form of a Co-Cr-Mo hard alloy and a hard Fe-Mo alloy dispersed in the Fe matrix. The base layer is composed of a sintered alloy of a higher heat resistance and a higher wear resistance than those of the valve-seat layer and having a composition comprising, by weight, 11 to 15% Cr, 0.4 to 2.0% Mo, 0.05 to 0.3% C, balance substantially Fe. The sintered alloy for the base layer may have a compositions further including 2 to 4% Cu.

Inventors

  • 👤 Koji Kazuoka
  • 👤 Testuya Suganuma
  • 👤 Naoki Motooka
  • 👤 Nobuhito Kuroishi

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 11:46
CPC Classifications
F; F01; F01L; F01L3/00; F01L3/22; B; B22; B22F; B22F7/00; B22F7/06; C; C22; C22C; C22C33/00; C22C33/02; C22C33/0257; C22C33/0278; C22C33/0285; F02; F02B; F02B1/00; F02B1/02; F02B1/04

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 138 words
A valve-seat insert for internal combustion engines comprising a double layered, sintered alloy composed of a valve-seat layer on which a valve is seated, and a base layer integrated with the valve-seat layer and adapted to be seated in a cylinder head of the engine, said valve-seat layer being composed of a sintered alloy of a high heat resistance and a high wear resistance, said base layer being composed of a sintered alloy having a radial crushing strength which is higher than that of the valve-seat layer and not less than 100 kgf/mm 2 at room temperature, but not less than 80 kgf/mm 2 at 500° C., said sintered alloy of the base layer comprising, by weight, 11 to 15% or Cr, 0.4 to 2.0% of Mo, 0.05 to 0.3% of C, and the balance being substantially Fe.
Claim 2
Dependent Claim 138 words
A valve-seat insert for internal combustion engines comprising a double layered, sintered alloy composed of a valve-seat layer on which a valve is seated, and a base layer integrated with the valve-seat layer and adapted to be seated in a cylinder head of the engine, said valve-seat layer being composed of a sintered alloy of a high heat resistance and a high wear resistance, said base layer being composed of a sintered alloy having a radial crushing strength which is higher than that of the valve-seat layer and not less than 100 kgf/mm 2 at room temperature, but not less than 80 kgf/mm 2 at 500° C., said sintered alloy of the base layer comprising, by weight, 11 to 15% or Cr, 0.4 to 2.0% of Mo, 0.05 to 0.3% of C, and the balance being substantially Fe.
Claim 3
Dependent Claim 22 words
A valve-seat insert according to claim 1, wherein the sintered alloy of said base layer further comprises 2 to 4% of Cu.
Claim 4
Dependent Claim 83 words
A valve-seat insert according to claim 1, wherein the sintered alloy of said valve-seat layer comprises, by weight, 4 to 8% of Co, 0.6 to 1.5% of Cr, 4 to 8% of Mo, 1 to 3% of Ni, 0.3 to 1.5% of C, 0.2 to 0.6% of Ca, and the balance substantially Fe, said Co, Cr and Mo being present mainly in a form of a Co-Cr-Mo hard alloy and a Fe-Mo hard alloy dispersed in the Fe matrix of the valve-seat layer.
Claim 5
Dependent Claim 209 words
A valve-seat insert for internal combustion engines comprising a double layered, sintered alloy composed of a valve-seat layer on which a valve is seated, and a base layer intergrated with said valve-seat layer and adapted to be seated in a cylinder head of an engine, said valve-seat layer being composed of a sintered alloy of a high heat resistance and a high wear resistance, the sintered alloy of said valve-seat layer consisting esstentially of, by weight, 4 to 8% Co, 0.6 to 1.5% Cr, 4 to 8% Mo, 1 to 3% Ni, 0.3 to 1.5% C, 0.2 to 0.6% Ca, and the balance substantially Fe, said Co, Cr and Mo being present mainly in a form of a Co-Cr-Mo hard alloy and a Fe-Mo hard alloy dispersed in the Fe matrix of the valve-seat layer, said base layer being composed of a sintered alloy having a radial crushing strength which is higher than that of the valve-seat layer and not less than 100 kgf/mm 2 at room temperature, but not less than 80 kgf/mm 2 at 500° C., the sintered alloy of said base layer consisting essentially of, by weight, 11 to 15% Cr, 0.4 to 2.0% Mo, 0.05 to 0.3% C and the balance consisting substantially of Fe.
Claim 6
Dependent Claim 209 words
A valve-seat insert for internal combustion engines comprising a double layered, sintered alloy composed of a valve-seat layer on which a valve is seated, and a base layer intergrated with said valve-seat layer and adapted to be seated in a cylinder head of an engine, said valve-seat layer being composed of a sintered alloy of a high heat resistance and a high wear resistance, the sintered alloy of said valve-seat layer consisting esstentially of, by weight, 4 to 8% Co, 0.6 to 1.5% Cr, 4 to 8% Mo, 1 to 3% Ni, 0.3 to 1.5% C, 0.2 to 0.6% Ca, and the balance substantially Fe, said Co, Cr and Mo being present mainly in a form of a Co-Cr-Mo hard alloy and a Fe-Mo hard alloy dispersed in the Fe matrix of the valve-seat layer, said base layer being composed of a sintered alloy having a radial crushing strength which is higher than that of the valve-seat layer and not less than 100 kgf/mm 2 at room temperature, but not less than 80 kgf/mm 2 at 500° C., the sintered alloy of said base layer consisting essentially of, by weight, 11 to 15% Cr, 0.4 to 2.0% Mo, 0.05 to 0.3% C and the balance consisting substantially of Fe.

References Cited (Backward Citations)

US3856478A Cited
US3982905A Cited
JPS5228407A Cited
US4035159A Cited
GB2016046A Cited
US4346684A Cited
JPS563654A Cited
JPS5620146A Cited
JPS56169750A Cited
US4424953A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-10-14 1989-04-15 1989-10-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-10-14 1993-04-15 1993-10-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-10-14 1997-04-15 1997-10-15 $7700.00 Window Closed / Lapsed

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