Invention Grant
US09228449B2 Angular sector of a stator for a turbine engine compressor, a turbine engine stator, and a turbine engine including such a sector 有权
用于涡轮发动机压缩机的定子的角部分,涡轮发动机定子和包括这种扇区的涡轮发动机

  • Patent Title: Angular sector of a stator for a turbine engine compressor, a turbine engine stator, and a turbine engine including such a sector
  • Patent Title (中): 用于涡轮发动机压缩机的定子的角部分,涡轮发动机定子和包括这种扇区的涡轮发动机
  • Application No.: US13805211
    Application Date: 2011-06-16
  • Publication No.: US09228449B2
    Publication Date: 2016-01-05
  • Inventor: Yvon Cloarec
  • Applicant: Yvon Cloarec
  • Applicant Address: FR Paris
  • Assignee: SNECMA
  • Current Assignee: SNECMA
  • Current Assignee Address: FR Paris
  • Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
  • Priority: FR1054849 20100618
  • International Application: PCT/FR2011/051372 WO 20110616
  • International Announcement: WO2011/157956 WO 20111222
  • Main IPC: F01D25/04
  • IPC: F01D25/04 F01D25/06 F04D29/66 F01D5/26 F01D9/04 F01D25/24 F01D5/22
Angular sector of a stator for a turbine engine compressor, a turbine engine stator, and a turbine engine including such a sector
Abstract:
A stator angular sector for a turbine engine compressor including: an outer shroud and an inner shroud, and at least one vane extending radially between the shrouds. The outer shroud includes first and second mounting mechanisms for mounting the stator angular sector on a casing of the engine, which mechanisms are oriented parallel to the axis in opposite directions and connected together by an intermediate portion. The outer shroud includes at least one axial end portion extending from the intermediate portion with which at least one damper-forming insert is configured to come into contact, such that beyond a given value for amplitude of vibration of the end portion, the damper insert and the end portion are configured to move relative to each other to vary total moving mass moving with the end portion, thereby modifying vibratory behavior of the end portion.
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