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US08662838B2 Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor 有权
压缩机外壳耐钛火，高压压缩机包括这样的外壳和配有这种压缩机的飞机发动机

  • 专利标题： Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor
  • 专利标题（中）： 压缩机外壳耐钛火，高压压缩机包括这样的外壳和配有这种压缩机的飞机发动机
  • 申请号： US13060708
    申请日： 2009-09-03
  • 公开(公告)号： US08662838B2
    公开(公告)日： 2014-03-04
  • 发明人: Laurent Ferrer , Claude Marcel Mons
  • 申请人： Laurent Ferrer , Claude Marcel Mons
  • 申请人地址： FR Paris
  • 专利权人： SNECMA
  • 当前专利权人： SNECMA
  • 当前专利权人地址： FR Paris
  • 代理机构： Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
  • 优先权： FR0855959 20080905
  • 国际申请： PCT/EP2009/061382 WO 20090903
  • 国际公布： WO2010/026180 WO 20100311
  • 主分类号： F01D11/12
  • IPC分类号： F01D11/12
Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor
摘要：
A compressor housing resistant to a titanium fire (burning titanium). A mixed housing is constructed, in which a structure holding stator blades includes a single-cast part made from titanium or titanium alloy, and at least one element forming a shield made from refractory alloy(s), and which is incombustible in presence of burning titanium, where each shield is secured to the single-cast part by fasteners. The fasteners are positioned with each shield so as to define jointly an inner wall demarcating an outer contour of the compressor airstream.
摘要（中）：

耐钛火（耐燃钛）的压缩机外壳。 构成了一种混合的壳体，其中保持定子叶片的结构包括由钛或钛合金制成的单一铸造部件和形成由耐火合金制成的护罩的至少一个元件，并且在存在燃烧时不燃 钛，其中每个护罩通过紧固件固定到单个铸件上。 紧固件与每个护罩一起定位，以便联合地限定压缩机空气流的外轮廓的内壁。

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