Invention Grant
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

  • Patent Title: Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor
  • Patent Title (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
  • Application No.: US13060708
    Application Date: 2009-09-03
  • Publication No.: US08662838B2
    Publication Date: 2014-03-04
  • Inventor: Laurent FerrerClaude Marcel Mons
  • Applicant: Laurent FerrerClaude Marcel Mons
  • Applicant Address: FR Paris
  • Assignee: SNECMA
  • Current Assignee: SNECMA
  • Current Assignee Address: FR Paris
  • Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
  • Priority: FR0855959 20080905
  • International Application: PCT/EP2009/061382 WO 20090903
  • International Announcement: WO2010/026180 WO 20100311
  • Main IPC: F01D11/12
  • IPC: F01D11/12
Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor
Abstract:
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.
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