发明名称 |
MANUFACTURE OF HOLLOW BLADE OF TURBINE ENGINE AND STEPWISE HOT TWIST DEVICE USED THEREIN |
摘要 |
PROBLEM TO BE SOLVED: To provide a manufacturing method for a hollow blade of a turbine engine, and a stepwise hot twist device used in its manufacturing method. SOLUTION: A manufacturing method of a hollow blade for a turbine engine includes a stepwise hot twist work of a manufacturing element l of an impeller by hot twist of the element l made of titanium alloy of a TA6V type at a temperature of 700 deg.C or more, by action of a plurality of bars 5 operated by rotary motion around a twist shaft, acting on collar which is beforehand fixed on the element 1 arranged according to twist formula which is set beforehand. An allocation and the number of the collars are decided so as to obtain a linear change of twist between the collars. A specified device is used for carrying out work. |
申请公布号 |
JPH1089008(A) |
申请公布日期 |
1998.04.07 |
申请号 |
JP19970226380 |
申请日期 |
1997.08.22 |
申请人 |
SOC NATL ETUD CONSTR MOT AVIAT <SNECMA>;ETAB 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):F01D5/18 |
主分类号 |
F01D5/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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