Low expansion alloys

Claim 2

A dimensionally stable casting being in the as-cast heat treated condition and made from a high-strength, low expansion carbidic alloy consisting essentially of, by weight, from about 21 to about 43% nickel, up to about 18% cobalt, from about 0.3 to about 1.0% carbon, from about 0.1 to about 1% chromium, from about 0.2 to about 1.2% vanadium, up to about 2% molybdenum, up to about 0.5% aluminum, up to about 0.5% silicon, up to about 2% manganese, up to about 2% zirconium, up to about 2% niobium, up to about 2% tungsten, up to about 0.1% magnesium, up to about 0.05% calcium and up to about 0.2% in total of at least one of the group consisting of yttrium, lanthanum and the lanthanides, with the provisos that the sum of the chromium, molybdenum, vanadium, zirconium, niobium and tungsten contents is in the range of from 1 to 4, the sum of %Ni + 0.75 (%Co) = 31.5 to 43 and the nickel to iron ratio is equal to or greater than 0.4:1, the balance, apart from impurities, being essentially iron, said casting exhibiting at room temperature a predominantly austenitic structure and having a 0.2% proof stress at 500°C greater than 200 N/mm 2 and a coefficient of thermal expansion over the temperature range 20° to 250°C not greater than 6.5 × 10 - 6 /° c.

Claim 3

A dimensionally stable casting being in the as-cast, heat treated condition and made from a high-strength low expansion carbidic alloy consisting essentially of, by weight, from about 21 to about 35 nickel, from about 5 to about 18% cobalt, from about 0.3 to about 2.5% carbon, up to about 3% chromium, from about 0.2 to about 1.2% vanadium, up to about 3% molybdenum, up to about 0.5% aluminum, up to about 0.5% silicon, up to about 2% manganese, up to about 2% zirconium, up to about 2% niobium, up to about 2% tungsten, up to about 0.1% magnesium, up to about 0.05% calcium, and up to about 0.2% in total of at least one of the group consisting of yttrium, lanthanum and the lanthanides, with the provisos that the sum of the chromium, molybdenum, vanadium, zirconium, niobium and tungsten contents is in the range of from 1 to 4, the sum of % Ni + 0.75 (%Co) = 30.5 to 55, and the nickel to iron ratio is equal to or greater than 0.4:1, the balance, apart from impurities, being essentially iron and said casting exhibiting at room temperature a predominantly austenitic structure.

Claim 4

A dimensionally stable casting being in the as-cast, heat treated condition and made from a high-strength low expansion carbidic alloy consisting essentially of, by weight, from about 21 to about 35 nickel, from about 5 to about 18% cobalt, from about 0.3 to about 2.5% carbon, up to about 3% chromium, from about 0.2 to about 1.2% vanadium, up to about 3% molybdenum, up to about 0.5% aluminum, up to about 0.5% silicon, up to about 2% manganese, up to about 2% zirconium, up to about 2% niobium, up to about 2% tungsten, up to about 0.1% magnesium, up to about 0.05% calcium, and up to about 0.2% in total of at least one of the group consisting of yttrium, lanthanum and the lanthanides, with the provisos that the sum of the chromium, molybdenum, vanadium, zirconium, niobium and tungsten contents is in the range of from 1 to 4, the sum of % Ni + 0.75 (%Co) = 30.5 to 55, and the nickel to iron ratio is equal to or greater than 0.4:1, the balance, apart from impurities, being essentially iron and said casting exhibiting at room temperature a predominantly austenitic structure.

Claim 5

A dimensionally stable casting according to claim 2, wherein said casting has been subjected directly to a heat treatment at a temperature in the range of from about 500° to about 900°C for a period of from about 1 to about 24 hours.

Claim 6

A dimensionally stable casting according to claim 2, having in the as-cast age hardened condition a 0.2% proof stress at 500°C greater than 200 N/mm 2 and a coefficient of thermal expansion over the temperature range 20° to 350°C not greater than 6.5 × 10 - 6 /°C, said casting being made from an alloy in which the sum of % Ni + 0.75 (% Co) is from 31.5 to 43, the chromium content is from about 0.1% to about 1%, the maximum carbon content is about 1%, and the maximum molybdenum content is about 2%.

Claim 7

A dimensionally stable casting according to claim 4 comprising at least about 0.8% molybdenum.

Claim 8

A dimensionally stable casting according to claim 4, in which the alloy contains from about 26.5% to about 28.5% nickel, from about 13% to about 15% cobalt, from about 0.5% to about 1% chromium, from about 0.45% to about 0.55% carbon, from about 0.4% to about 0.6% vanadium, from about 0.8% to about 1.2% molybdenum, not more than about 0.3% manganese, less than about 0.3% silicon, and up to about 0,25% aluminum.

Claim 9

A dimensionally stable casting according to claim 3 having in the as-cast heat-treated condition a 0.2% proof stress at 500°C greater than 200 N/mm 2 and a coefficient of thermal expansion over the temperature range 20° to 250°C not greater than 6.5 × 10 - 6 /°C, said casting being made from an alloy, the sum of % Ni + 0.75 (% Co) is from 31.5 to 43, the chromium content is at least 1%, the maximum carbon content is about 1%, and the maximum molybdenum content is about 2%.

Claim 10

A dimensionally stable casting according to claim 4 for use over the temperature range of about 20° to about 200°C, in which the sum of % Ni + 0.75 (% Co) is in the range of from 34.1 to 37.1.

Claim 11

A dimensionally stable casting according to claim 4 for use over the temperature range of about 20° to about 200°C, in which the sum of % Ni + 0.75 (% Co) is in the range of from 35.4 to 38.4.

Claim 12

A dimensionally stable casting according to claim 4 for use over the temperature range of about 20° to about 300°C, in which the sum of % Ni + 0.75 (% Co) is in the range of from 36.6 to 39.6.

Claim 13

A dimensionally stable casting according to claim 4 for use over the temperature range of about 20° to about 350°C, in which the sum of % Ni + 0.75 (% Co) is in the range of from 37 to 40.

Claim 14

A dimensionally stable casting according to claim 4 for use over the temperature range of about 20° to about 450°C, in which the sum of % Ni + 0.75 (% Co) is in the range of from 38 to 41.

Claim 15

A dimensionally stable casting according to claim 7, containing about 0.6% carbon, about 2% chromium, about 0.5% vanadium, about 0.3% silicon, about 10% cobalt, and about 30% nickel.

Claim 16

A dimensionally stable casting according to claim 7, containing about 26% nickel, about 14.5% cobalt, about 0.47% carbon, about 1.97% chromium, about 1.01% molybdenum, about 0.49% vanadium.

Claim 17

A precision cast rotor having adjoining thick and thin sections which are resistant to hot tearing at the junctures, said rotor being subjected in use to high centrifugal stresses, thermal cycling, temperature gradients, and simultaneously to oxidizing and hydrocarbon combustion product atmospheres, said rotor being made of a low expansion alloy cast at elevated temperatures and cooled, the alloy having a composition consisting essentially of, by weight, from about 21% to about 43% nickel, up to about 18% cobalt, from about 0.3 to about 2.5% carbon, up to about 3% chromium, from about 0.2 to about 1.2% vanadium, up to about 3% molybdenum, up to about 0.5% aluminum, up to about 0.5% silicon, up to about 2% manganese, up to about 2% zirconium, up to about 2% niobium, up to about 2% tungsten, up to about 0.1% magnesium, up to about 0.05% calcium, and up to about 0.2% in total of at least one of the group consisting of yttrium, lanthanum and the lanthanides, with the provisos that the sum of the chromium, molybdenum, vanadium, zirconium, niobium and tungsten contents is in the range of from 1 to 4, the sum of % Ni + 0.75 (% Co) = 30.5 to 55, and the nickel to iron ratio is equal to or greater than 0.4:1, the balance, apart from impurities, being essentially iron.

Claim 18

A precision cast rotor having adjoining thick and thin sections which are resistant to hot tearing at the junctures, said rotor being subjected in use to high centrifugal stresses, thermal cycling, temperature gradients, and simultaneously to oxidizing and hydrocarbon combustion product atmospheres, said rotor being made of a low expansion alloy cast at elevated temperatures and cooled, the alloy having a composition consisting essentially of, by weight, from about 21% to about 43% nickel, up to about 18% cobalt, from about 0.3 to about 2.5% carbon, up to about 3% chromium, from about 0.2 to about 1.2% vanadium, up to about 3% molybdenum, up to about 0.5% aluminum, up to about 0.5% silicon, up to about 2% manganese, up to about 2% zirconium, up to about 2% niobium, up to about 2% tungsten, up to about 0.1% magnesium, up to about 0.05% calcium, and up to about 0.2% in total of at least one of the group consisting of yttrium, lanthanum and the lanthanides, with the provisos that the sum of the chromium, molybdenum, vanadium, zirconium, niobium and tungsten contents is in the range of from 1 to 4, the sum of % Ni + 0.75 (% Co) = 30.5 to 55, and the nickel to iron ratio is equal to or greater than 0.4:1, the balance, apart from impurities, being essentially iron.

Claim 19

A dimensionally stable casting according to claim 3, wherein the sum of %Ni + 0.75(%Co) is from 31.5 to 43, the chromium content is from about 0.1% to about 1%, the maximum carbon content is about 1% and the maximum molybdenum content is about 2%, said casting having in the as-cast heat-treated condition a 0.2% proof stress at 500°C greater than 200 N/mm 2 and a coefficient of thermal expansion over the temperature range 20 to 350°C not greater than 6.5 × 10 - 6 /°C.

Claim 20

A dimensionally stable casting according to claim 16 comprising at least about 0.8% molybdenum.

Claim 21

A dimensionally stable casting according to claim 16, wherein the alloy contains from about 26.5% to about 28.5% nickel, from about 13% to about 15% cobalt, from about 0.5% to about 1% chromium, from about 0.45% to about 0.55% carbon, from about 0.4% to about 0.6% vanadium, from about 0.8% to about 1.2% molybdenum, not more than about 0.3% manganese, less than about 0.3% silicon, and up to about 0.25% aluminum.

Claim 22

A dimensionally stable casting according to claim 18, wherein the alloy contains about 0.5% carbon, about 0.75% chromium, about 0.5% vanadium, about 1% molybdenum, about 14% cobalt and about 28% nickel.

Claim 23

A precision cast rotor according to claim 15, comprising at least about 0.8% molybdenum.

Claim 24

A precision cast rotor according to claim 15, in which the maximum nickel content is about 43%, the sum of % Ni - 0.75 (% Co) is from 31.5 to 43, the chromium content is from about 0.1% to about 1%, the maximum carbon content is about 1%, and the maximum molybdenum content is about 2%, said alloy having in the as-cast heat treated condition a 0.2% proof stress at 500°C greater than 200 N/ mm 2 and a coefficient of thermal expansion over the temperature range 20° to 350°C not greater than 6.5 × 10 - 6 /°C.

Claim 25

A precision cast rotor according to claim 21, containing from about 26.5% to about 28.5% nickel, from about 13% to about 15% cobalt, from about 0.5% to about 1% chromium, from about 0.45% to about 0.55% carbon, from about 0.4% to about 0.6% vanadium, from about 0.8% to about 1.2% molybdenum, up to about 0.3% manganese, up to about 0.3% silicon, and up to about 0.25% aluminum.

Claim 26

A precision cast rotor according to claim 22, containing about 0.5% carbon, about 0.75% chromium, about 0.5% vanadium, about 1.0% molybdenum, about 0.3% manganese, about 0.2% aluminum, about 14% cobalt, and about 28% nickel.

Claim 27

A precision cast rotor according to claim 15, in which the maximum nickel content is about 43%, the sum of % Ni + 0.75 (% Co) is from 31.5 to 43, the chromium content is at least about 1%, the maximum carbon content is about 1%, and the maximum molybdenum content is about 2%, said alloy having in the as-cast heat treated condition a 0.2% proof stress at 500°C greater than 200 N/mm 2 and a coefficient of thermal expansion over the temperature range 20° to 250°C not greater than 6.5 × 10 - 6 /°C.