发明名称 Process for fabricating multi-alloy components
摘要 A component, such as a turbine disk, made from a metal or metal alloy which has been processed to display superplastic properties at elevated temperatures, is diffusion bonded to a component or components, such as turbine blades, made from another metal or metal alloy, by disposing the components in a press with the surfaces to be bonded in mating contact. Moisture and oxygen are removed from between the surfaces. Heat and pressure are then applied, such as by forging at an elevated temperature or by hot isostatic pressing, to cause superplastic deformation of at least one of the components at the bonding surfaces. The heat and pressure are held sufficiently long to diffusion bond the surfaces. The new integral assembly is then heat treated to obtain desired properties. Consistently good diffusion bonds are achieved by this method.
申请公布号 US4529452(A) 申请公布日期 1985.07.16
申请号 US19840635782 申请日期 1984.07.30
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WALKER, BRYANT H.
分类号 B23K20/00;B22F5/04;B22F7/06;B23K20/02;B23K20/22;B23K20/227;B23P15/00;C22F1/00;C22F1/10;F01D5/28;F01D5/34;(IPC1-7):B22F5/04;B23P15/04 主分类号 B23K20/00
代理机构 代理人
主权项
地址