发明名称 Process for the vapor phase aluminization of a turbomachine metal part and donor liner and turbomachine vane comprising such a liner
摘要 An aluminization process by vapor phase deposition for high-temperature oxidation protection of a metal turbomachine part. The part including a cavity into which a metal component is introduced and assembled from an opening in the part. A halide is formed by reaction between a halogen and a metal donor containing aluminum, then the halide is transported by a carrier gas in order to come into contact with the metal part, wherein the metal component has first, before the implementation of the process, been surface-enriched with aluminum in order to serve as an aluminum donor.
申请公布号 US9157142(B2) 申请公布日期 2015.10.13
申请号 US201213473200 申请日期 2012.05.16
申请人 SNECMA 发明人 Carlin Maxime Francois Roger;Lanciaux Lucie Marie Ida
分类号 F01D9/06;C23C10/48;F01D5/18;C23C10/08;C23C16/04;C23C16/12;C23C16/448;F01D5/28 主分类号 F01D9/06
代理机构 Oblon, McClelland, Maier & Neustadt, L.L.P. 代理人 Oblon, McClelland, Maier & Neustadt, L.L.P.
主权项 1. A hollow turbomachine vane including a liner for distributing cooling air, the liner being cylindrical, the liner including a first end which is welded or brazed to a coolant supplying opening of the vane and a second end which is introduced into and not welded to a housing which communicates with an outlet of the vane, and a surface of the liner being coated, at least partially, with a layer of at least 15 weight percent of aluminum, wherein a thickness of the layer of aluminum is determined so as to have a sufficient amount of aluminum to react with a halogen to form a vapor-phase halide during an aluminization operation of an internal surface of the vane, and wherein the internal surface of the vane is free of a coating comprising aluminum.
地址 Paris FR