发明名称 КОРПУС С ТУРБИНЫ С ТУГОПЛАВКИМИ СКОБАМИ, ИЗГОТОВЛЕННЫЙ СПОСОБОМ ПОРОШКОВОЙ МЕТАЛЛУРГИИ
摘要 A turbine stator casing comprising a jacket and fastener hooks for fastening a turbine distributor nozzle, the hooks projecting from the inside face of the jacket, said jacket being made of a first alloy by hot isostatic compression using metal powder, said fastener hooks being made out of a second alloy that is more refractory than the first, and being secured to said jacket by diffusion welding during the hot isostatic compression. The casing also comprises inserts passing through the fastener hooks and through said jacket. These inserts, which are likewise secured to the jacket by diffusion welding, serve during manufacture of the casing to fasten the hooks to a mold portion inside which the jacket is formed. The invention is applicable to the turbines of airplane turbojets.
申请公布号 RU2005109763(A) 申请公布日期 2006.10.10
申请号 RU20050109763 申请日期 2005.04.04
申请人 СНЕКМА МОТЕР (FR) 发明人 ИМБУРГ Себастьен Ален (FR);МОН Клод Марсель (FR);ПАБИОН Филипп Жан-Пьер (FR);СУПИЗОН Жан-Люк (FR)
分类号 B22F3/14;B22F3/15;B22F3/24;B22F5/00;B22F7/06;B22F7/08;F01D9/00;F01D9/04;F01D25/14;F01D25/24;F02C7/00 主分类号 B22F3/14
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