US2004101433A1PendingUtilityA1
Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
Priority: Oct 20, 2000Filed: Sep 13, 2001Published: May 27, 2004
Est. expiryOct 20, 2020(expired)· nominal 20-yr term from priority
C22C 19/05C22C 19/055
31
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Claims
Abstract
The invention relates to an austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy, comprising (in mass %): carbon: 0.05 to 0.10%; chromium: 21 to 23%; cobalt: 10 to 15%; molybdenum: 10 to 11%; aluminium: 1.0 to 1.5%; tungsten: 5.1 to 8.0%; yttrium: 0.01 to 0.10%; boron: 0.001 to 0.010%; titanium: max. 0.50%; silicon: max. 0.50%; iron: max. 2%; manganese: max. 0.5%; nickel: remainder; including unavoidable impurities caused by the smelting process.
Claims
exact text as granted — not AI-modified1 . Austenitic nickel-chrome-cobalt-molybdenum-tungsten alloy consisting of (in % by mass):
carbon:
0.05 to 0.10%
chrome:
21 to 23%
cobalt:
10 to 15%
molybdenum:
10 to 11%
aluminium:
1.0 to 1.5%
tungsten:
5.1 to 8.0%
yttrium:
0.01 to 0.10%
boron:
0.001 to 0.010%
titanium:
max. 0.50%
silicium:
max. 0.50%
iron:
max. 2%
manganese:
max. 0.5%
nickel:
remainder
including unavoidable impurities caused by the smelting process.
2 . Austenitic nickel-chrome-cobalt-molybdenum-tungsten alloy consisting of (in % by mass):
carbon:
0.05 to 0.10%
chrome:
21 to 23%
cobalt:
12 to 13%
molybdenum:
10 to 11%
aluminium:
1.0 to 1.5%
tungsten:
5.1 to 7.0%
yttrium:
0.04 to 0.07%
boron:
0.001 to 0.005%
titanium:
max. 0.50%
silicium:
max. 0.50%
iron:
max. 2%
manganese:
max. 0.5%
nickel:
remainder
including unavoidable impurities caused by the smelting process.
3 . Use of an austenitic nickel-chrome-cobalt-molybdenum-tungsten alloy according to claim 1 or 2 , in particular for combustion chambers of stationary or flying gas turbines.
4 . Use of an austenitic nickel-chrome-cobalt-molybdenum-tungsten alloy according to claim 1 or 2 , in particular for compressors and turbo-superchargers of combustion engines.
5 . Use of an austenitic nickel-chrome-cobalt-molybdenum-tungsten alloy according to claim 1 or 2 , in particular for steam turbines.
6 . Use of an austenitic nickel-chrome-cobalt-molybdenum-tungsten alloy according to claim 1 or 2 , in particular for shafts, roots and blades of high temperature ventilators.
7 . Use of an austenitic nickel-chrome-cobalt-molybdenum-tungsten alloy according to claim 1 or 2 for gas and steam turbine power stations, in particular combustion chamber walls, blades, tubes, boiler walls, membrane walls, collectors or the like.Join the waitlist — get patent alerts
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