发明名称 Process for manufacturing a hollow turbomachine blade and progressive hot twisting apparatus for use in said process
摘要 A process for manufacturing a hollow turbomachine blade made from a titanium alloy of the TA6V type includes a hot twisting step in which an element of the blade is twisted progressively at a temperature above 700 DEG C. by a plurality of bars which are rotated about the twist axis and act on collars previously fixed to the element, the distribution and number of collars being determined according to the desired twist to be imparted and such as to obtain a linear twist development between each collar. Hot twisting apparatus for use in carrying out the operation is also described.
申请公布号 US5933952(A) 申请公布日期 1999.08.10
申请号 US19970914186 申请日期 1997.08.19
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA";ETABLISSEMENTS ROBERT CREUZET 发明人 BICHON, MATHIEU PHILIPPE ALBERT;COSTEPLANE, BERNARD ARMAND RENE;LORIEUX, ALAIN GEORGES HENRI
分类号 F01D5/18;B21D11/14;B21D53/78;C22F1/00;C22F1/18;F01D5/28;F02C7/00;(IPC1-7):B23P15/00 主分类号 F01D5/18
代理机构 代理人
主权项
地址