公开(公告)号：US20170002449A1

公开(公告)日：2017-01-05

申请号：US15125836

申请日：2015-03-13

申请人： AUBERT & DUVAL

发明人： Coraline CROZET ,  Alexandre DEVAUX

IPC分类号： C22F1/10 ,  B21B1/02 ,  B22D7/00 ,  B21B3/00 ,  C22C30/02 ,  C22C19/05

CPC分类号： C22F1/10 ,  B21B1/026 ,  B21B3/00 ,  B22D7/005 ,  C22C19/055 ,  C22C19/056 ,  C22C30/00 ,  C22C30/02

摘要： A precipitation hardened nickel-base alloy, characterized in that its composition is, in weight percentages: 18%≦Cr≦22%, preferably 18%≦Cr≦20%; 18%≦Co≦22%, preferably 19%≦Co≦21%; 4%≦Mo+W≦8%, preferably 5.5%≦Mo+W≦7.5%; trace amounts≦Zr≦0.06%; trace amounts≦B≦0.03%. preferably trace amounts≦B≦0.01%; trace amounts≦C≦0.1%, preferably trace amounts≦C≦0.06%; trace amounts≦Fe≦1%; trace amounts≦Nb≦0.01%; trace amounts≦Ta≦0.01%; trace amounts≦S≦0.008%; trace amounts≦P≦0.015%; trace amounts≦Mn≦0.3%; trace amounts≦Si≦0.15%; trace amounts≦O≦0.0025%; trace amounts≦N≦0.0030%; the remainder being nickel and impurities resulting from the elaboration, the Al and Ti contents further satisfying the conditions: Ti/Al≦3;  (1) Al+1.2 Ti≧2%;  (2) (0.2 Al−1.25)2−0.5 Ti≧0%;  (3) Ti+1.5 Al≦4.5%.  (4) Part made in this alloy and its manufacturing method.

摘要翻译： 该合金制成的部件及其制造方法。

公开(公告)号：US20210355564A1

公开(公告)日：2021-11-18

申请号：US17273971

申请日：2019-09-13

申请人： AUBERT & DUVAL ,  SAFRAN

发明人： Philippe BELAYGUE ,  Daniel André Jean CORNU ,  Coraline CROZET ,  Rémi GIRAUD ,  Zéline HERVIER ,  Baptiste Romain LARROUY ,  Charlotte MAYER ,  Jacques MONTAGNON

IPC分类号： C22C19/05 ,  B33Y10/00 ,  B33Y40/10 ,  B33Y70/00 ,  B22F10/28 ,  B22F10/64 ,  B22F9/08 ,  C22C1/04 ,  C22F1/08 ,  B23K26/342

摘要： The present invention relates to a nickel-based superalloy with a high γ′ phase content, intended for the manufacture of components by additive manufacturing followed by heat treatment, characterized in that its composition comprises, in percentages by weight of the total composition: Cr: 15.5-16.5; Co: 7.7-11; Mo+W=5.5-7.5; Al: 2.9-4.3; Ti: 2.6-3.2; Ta: 1.5-2.2; Nb: 0.3-1.1; C: 0.01-0.13; B: 0.0005-0.015; Zr: 0.01; Hf: 0.0001-0.5; Si: ≤0.06; Ni: balance, and also the unavoidable impurities.
It further relates to a method for manufacturing superalloy powder and turbine components.