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.