发明名称 Turbine engine vane plate seal
摘要 A plate closes the main part of a vane in two parts. An internal cavity is closed by the plate. Around a bearing surface of the plate, a groove receives an elastic seal, and the outer edge of the plate extends over the groove to compress the seal and to establish excellent leak proofing. The position of the plate may be guaranteed by centring pins penetrating into holes adjacent to the seal and which it fills when the pins have been removed, which completes the closing of the cavity. The plate has application in particular to stationary gas guide vanes in turbine engines.
申请公布号 US9556745(B2) 申请公布日期 2017.01.31
申请号 US201214233549 申请日期 2012.07.17
申请人 SNECMA 发明人 Papin Thierry Georges Paul;Lacroix Lise;Raulin Dominique
分类号 F04D29/38;F01D9/02;F01D5/14;F01D9/04;F04D29/54 主分类号 F04D29/38
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 turbine engine vane, comprising: a main part containing a cavity and ribs extending into the cavity; and a plate joined to the main part while closing the cavity and while resting on the ribs, wherein the plate is joined to the main part while resting on a bearing surface of the main part, the bearing surface is set back with respect to an outer face of the main part that surrounds the main part, by a region adjacent to an outer edge of the plate, and wherein the outer edge of the plate extends above a groove of the main part which surrounds the bearing surface and is filled by a seal made of elastic material, the seal being compressed by the outer edge.
地址 Paris FR