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Title:
CREEP-RESISTANT, LONG-SERVICE-LIFE, NICKEL-BASED DEFORMATION SUPERALLOY AND METHOD FOR PREPARATION THEREOF AND APPLICATION THEREOF
Document Type and Number:
WIPO Patent Application WO/2022/100169
Kind Code:
A1
Abstract:
Disclosed is a creep-resistant, long-service-life, nickel-based deformation superalloy, comprising: C: 0.04-0.08%; Cr: 18.50-21.50%; Co: 9.00-11.00%; Mo: 8.00-9.00%; Al: 2.00-3.00%; Ti: 1.10-1.49%; Nb: 0.81-2.00%; B: 0.003-0.009%; Sc: 0.001-0.10 %; the remainder is nickel and unavoidable impurities; in terms of mass percentage, the mass percent content of the elements Al, Ti, and Mo in the alloy satisfies the relational expression: 11.59% ≤ Al+Ti+Mo ≤ 13.0%. The nickel-based deformation superalloy of the present invention has excellent creep resistance and long service life, is capable of meeting the requirements for the design and use of advanced aircraft engines and gas turbines, and is suitable for manufacturing precision hot-end components for long-term service in equipment such as advanced aero-engines and gas turbines.

Inventors:
SHU GUOGANG (CN)
WEN XINLI (CN)
DONG JIANXIN (CN)
ZHANG QINGQUAN (CN)
JIANG HE (CN)
LI ZHENRUI (CN)
LIU WEI (CN)
YU ZHIYONG (CN)
PENG JIE (CN)
LIU HAIBO (CN)
WEI RAN (CN)
LI GUOCHAO (CN)
Application Number:
PCT/CN2021/111913
Publication Date:
May 19, 2022
Filing Date:
August 10, 2021
Export Citation:
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Assignee:
CHINA UNITED GAS TURBINE TECH CO LTD (CN)
BEIJING BEIYE FUNCTIONAL MAT CORPORATION (CN)
International Classes:
C22C19/05; C22C1/02; F02C7/00
Foreign References:
CN112575228A2021-03-30
CN110300811A2019-10-01
CN108467972A2018-08-31
CN103160710A2013-06-19
CN201210057737A2005-06-17
CN201910811805A2019-08-30
Other References:
See also references of EP 4245873A4
Attorney, Agent or Firm:
TSINGYIHUA INTELLECTUAL PROPERTY LLC (CN)
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