Low expansion alloys

Claim 2

A metallic cast article adapted to be employed under stress at temperatures in excess of ambient temperature and having enhanced utility by virtue of dimensional stability over the temperature range from ambient temperature to at least 300°C and high strength and consisting of an alloy having an as-cast and age-hardened microstructure, said microstructure being characterized by a Ni 3 Ti precipitate and by substantial segregation of elemental constituents within the as-cast structure but, on the average consisting essentially, in percent by weight, of about 27% to about 47% nickel, about 1% to about 4% uncombined titanium, up to about 16% cobalt, up to about 1.5% niobium, up to about 0.1% carbon, with the balance, except for impurities and incidental elements being essentially iron, to provide in said as-cast plus age-hardened alloy a linear thermal expansion coefficient between 20°C and 300°C of less than about 6 × 10 - 6 /°C and a 0.2% proof stress at 20°C greater than about 350 N/mm 2 .

Claim 3

A metallic cast article according to claim 1, wherein the alloy contains up to about 0.3% silicon, up to about 0.4% manganese, up to about 0.3% aluminum, and up to about 0.2% magnesium.

Claim 4

A metallic cast article according to claim 1, wherein the alloy contains about 29% to about 47% nickel and the nickel, cobalt, titanium and niobium contents are correlated such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] - 2 (%Ti)/(%Ti + %Nb) = 37 to 40.

Claim 5

A metallic cast article according to claim 1, wherein the nickel content is about 29% to about 44%, and the nickel, cobalt, titanium and niobium contents are correlated such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] - 2 (%Ti)/(%Ti + %Nb) = 37 to 39, and wherein said alloy has a linear thermal coefficient of expansion between 20° and 300°C. of less than about 5 × 10 - 6 /°C.

Claim 6

A metallic cast article adapted to be employed under stress at temperatures in excess of ambient temperature and having enhanced utility by virtue of dimensional stability over the temperature range from ambient temperature to at least 300°C. and high strength and consisting of an alloy having an as-cast and age-hardened microstructure, said microstructure being characterized by a Ni 3 Ti precipitate and by substantial segregation of elemental constituents within the as-cast structure but on the average consisting essentially, in percent by weight, of about 32% to about 38% nickel, from above 1.75% to about 2.7% uncombined titanium, from about 7 to about 14% cobalt, up to about 1.5% niobium, up to about 0.04% carbon, with the balance, except for impurities and incidental elements being essentially iron, said nickel, cobalt, titanium and niobium contents being correlated such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] - 2 (%Ti)/(%Ti + Nb) = 37 to 39, hydrocarbon combustion to provide in said as-cast age-hardened alloy a linear thermal expansion coefficient between 20°C and 300°C of less than about 5 × 10 - 6 /°C and a 0.2% proof stress at 20°C greater than about 350 N/mm 2 .

Claim 7

A metallic cast article adapted to be employed under stress at temperatures in excess of ambient temperature and having enhanced utility by virtue of dimensional stability over the temperature range from ambient temperature to at least 300°C. and high strength and consisting of an alloy having an as-cast and age-hardened microstructure, said microstructure being characterized by a Ni 3 Ti precipitate and by substantial segregation of elemental constituents within the as-cast structure but on the average consisting essentially, in percent by weight, of about 32% to about 38% nickel, from above 1.75% to about 2.7% uncombined titanium, from about 7 to about 14% cobalt, up to about 1.5% niobium, up to about 0.04% carbon, with the balance, except for impurities and incidental elements being essentially iron, said nickel, cobalt, titanium and niobium contents being correlated such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] - 2 (%Ti)/(%Ti + Nb) = 37 to 39, hydrocarbon combustion to provide in said as-cast age-hardened alloy a linear thermal expansion coefficient between 20°C and 300°C of less than about 5 × 10 - 6 /°C and a 0.2% proof stress at 20°C greater than about 350 N/mm 2 .

Claim 8

A metallic cast article according to claim 5, wherein the alloy contains up to about 0.3% silicon, up to about 0.3% manganese, up to about 0.3% aluminum and up to about 0.1% magnesium.

Claim 9

A metallic cast article according to claim 5, wherein the alloy contains from about 36.5% to about 38% nickel, about 7.5% to about 8.5% cobalt, from about 1.9% to about 2.2% uncombined titanium, and about 0.3% to about 0.6% niobium.

Claim 10

A metallic cast article according to claim 7, wherein the alloy contains from about 36.5% to about 37.5% nickel.

Claim 11

A metallic cast article according to claim 8, wherein the alloy contains about 8% cobalt, about 2% uncombined titanium, and up to about 0.002% carbon.

Claim 12

A metallic cast article according to claim 9, wherein the alloy contains about 0.5% niobium.

Claim 13

A metallic cast article according to claim 5, wherein the alloy contains about 32.5% to about 34.5% nickel, about 2.5% uncombined titanium, and about 13.5% cobalt.

Claim 14

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 32% to about 38% nickel, from above 1.75% to about 2.7% uncombined titanium, from about 7% to about 16% cobalt, up to about 1.5% niobium, up to about 0.04% carbon, up to about 0.3% silicon, up to about 0.3% manganese, up to about 0.3% aluminum, up to about 0.1% magnesium, and the balance, apart from impurities and incidental constituents, being essentially iron, and said alloy having in the as-cast, age-hardened condition an expansivity of less than about 5 × 10 - 6 /°C. over a temperature range of 20° to 300°C. and a 0.2% proof stress at 20°C. higher than about 350 N/mm 2 .

Claim 15

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 32% to about 38% nickel, from above 1.75% to about 2.7% uncombined titanium, from about 7% to about 16% cobalt, up to about 1.5% niobium, up to about 0.04% carbon, up to about 0.3% silicon, up to about 0.3% manganese, up to about 0.3% aluminum, up to about 0.1% magnesium, and the balance, apart from impurities and incidental constituents, being essentially iron, and said alloy having in the as-cast, age-hardened condition an expansivity of less than about 5 × 10 - 6 /°C. over a temperature range of 20° to 300°C. and a 0.2% proof stress at 20°C. higher than about 350 N/mm 2 .

Claim 16

A precision cast rotor according to claim 12, wherein the alloy contains about 36.5% to about 38% nickel, 7.5% to about 8.5% cobalt, from about 1.9% to about 2.2% titanium, and about 0.3% to about 0.6% niobium, up to about 0.1% silicon, and up to about 0.2% aluminum.

Claim 17

A shaped casting made of an alloy consisting essentially of, by weight, from about 29% to about 47% nickel, from about 1% to about 4% titanium, up to about 16% cobalt, up to about 1.5% niobium, and the balance, apart from impurities and incidental constituents, being essentially iron, and said contents of nickel, cobalt, titanium and niobium being such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] 2 (%Ti)/(%Ti + %Nb) = 37 to 40, said shaped casting being prepared by forming the alloy into a shaped casting and subjecting said casting directly to age-hardening conditions to obtain a shaped casting having in the as-cast age-hardened condition a thermal coefficient of expansion between about 20°C to about 300°C of less than about 6 × 10 - 6 /°C and a 0.2% proof stress at 20°C greater than about 350 N/mm 2 .

Claim 18

A shaped casting made of an alloy consisting essentially of, by weight, from about 29% to about 47% nickel, from about 1% to about 4% titanium, up to about 16% cobalt, up to about 1.5% niobium, and the balance, apart from impurities and incidental constituents, being essentially iron, and said contents of nickel, cobalt, titanium and niobium being such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] 2 (%Ti)/(%Ti + %Nb) = 37 to 40, said shaped casting being prepared by forming the alloy into a shaped casting and subjecting said casting directly to age-hardening conditions to obtain a shaped casting having in the as-cast age-hardened condition a thermal coefficient of expansion between about 20°C to about 300°C of less than about 6 × 10 - 6 /°C and a 0.2% proof stress at 20°C greater than about 350 N/mm 2 .

Claim 19

A shaped casting according to claim 14 wherein the contents of nickel, cobalt, titanium and niobium are such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.3 (%Nb)] - 2 (%Ti)/(%Ti + %Nb) = 37 to 39, and wherein said thermal coefficient of expansion in the as-cast age-hardened condition is less than 5 × 10 - 6 /°C.

Claim 20

A shaped casting according to claim 14 wherein the cobalt content of the alloy is from above 5% to about 16%.

Claim 21

A shaped casting according to claim 14 wherein the nickel content of the alloy is about 32% to about 38%.

Claim 22

A shaped casting according to claim 14 wherein the titanium content of the alloy is from above 1.75% to about 2.7%.

Claim 23

A shaped casting according to claim 17 wherein the alloy contains about 7.5% to about 8.5% cobalt, about 1.9% to about 2.2% titanium, and about 0.3 to about 0.6% niobium.

Claim 24

A shaped casting according to claim 14 wherein the alloy contains up to about 0.3% Si, up to about 0.4% manganese, up to about 0.3% aluminum, and not more than about 0.1% carbon.

Claim 25

A shaped casting according to claim 14 wherein the age-hardening treatment is carried out in the temperature range of about 550° to about 700°C.

Claim 26

A shaped casting according to claim 14 wherein the alloy is investment cast to form the shaped casting and the investment casting is subjected directly to an age-hardening treatment at a temperature in the range of 550°C to 700°C.

Claim 27

A shaped casting made of an alloy consisting essentially of, by weight, about 29 to about 43% nickel, from about 1% to about 4% titanium, from above 5% to about 16% cobalt, up to about 1.5% niobium, and the balance, apart from impurities and incidental constituents, being essentially iron and said contents of nickel, cobalt, titanium and niobium being such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] - 2 (%Ti)/(%Ti + %Nb) = 37 to 40, said shaped casting being prepared by forming the alloy into a shaped casting at a casting temperature of about 1500° to about 1550°C and subjecting said casting directly to age-hardening conditions at a temperature of about 550° to about 700°C to obtain a shaped casting having in the as-cast age-hardened conditions condition a microstructure characterized by a Ni 3 Ti precipitate and by substantial segregation of elemental constituents within the as-cast structure and said as-cast age-hardened alloy having a linear thermal coefficient of expansion between about 20°C to about 300°C of less than about 6 × 10 - 6 /°C and a 0.2% proof stress at 20°C greater than about 350 N/mm 2 .

Claim 28

A shaped casting made of an alloy consisting essentially of, by weight, about 29 to about 43% nickel, from about 1% to about 4% titanium, from above 5% to about 16% cobalt, up to about 1.5% niobium, and the balance, apart from impurities and incidental constituents, being essentially iron and said contents of nickel, cobalt, titanium and niobium being such that: %Ni + 0.7 (%Co) - 1.25 [%Ti + 0.35 (%Nb)] - 2 (%Ti)/(%Ti + %Nb) = 37 to 40, said shaped casting being prepared by forming the alloy into a shaped casting at a casting temperature of about 1500° to about 1550°C and subjecting said casting directly to age-hardening conditions at a temperature of about 550° to about 700°C to obtain a shaped casting having in the as-cast age-hardened conditions condition a microstructure characterized by a Ni 3 Ti precipitate and by substantial segregation of elemental constituents within the as-cast structure and said as-cast age-hardened alloy having a linear thermal coefficient of expansion between about 20°C to about 300°C of less than about 6 × 10 - 6 /°C and a 0.2% proof stress at 20°C greater than about 350 N/mm 2 .