发明名称 Process for manufacturing a hollow turbine blade and device used for on-going hot twisting
摘要 <p>The procedure consists of forging, machining and welding components made by a computer-aided system, followed by inflation under pressure and superplastic moulding. The required twist in the blade, made from a titanium alloy such as TA6V, is produced by heating the blade to 700 deg C and applying a torsion to it through rotary bars (5) acting on yokes previously attached to the blade. The twisting process can be applied to the individual components of the blade or to assembled blades and uses a cylindrical electric furnace (2) with slits (24) for the bars. The furnace is surrounded by a circular frame (6), and jaws (3, 4) hold the two ends of the blade while it is being twisted.</p>
申请公布号 EP0824981(B1) 申请公布日期 2001.05.02
申请号 EP19970401954 申请日期 1997.08.20
申请人 SNECMA MOTEURS;ETABLISSEMENTS ROBERT CREUZET 发明人 BICHON, MATHIEU PHILIPPE ALBERT;LORIEUX, ALAIN GEORGES HENRI;COSTEPLANE, BERNARD ARMAND RENE
分类号 F01D5/18;B21D11/14;B21D53/78;C22F1/00;C22F1/18;F01D5/28;F02C7/00;(IPC1-7):B21D53/78 主分类号 F01D5/18
代理机构 代理人
主权项
地址