Invention Grant
US08721277B2 Unit for locking ring sectors on a turbomachine casing, comprising radial passages for gripping it 有权
用于在涡轮机壳体上锁定环形部分的单元,包括用于夹紧的径向通道

  • Patent Title: Unit for locking ring sectors on a turbomachine casing, comprising radial passages for gripping it
  • Patent Title (中): 用于在涡轮机壳体上锁定环形部分的单元,包括用于夹紧的径向通道
  • Application No.: US12990913
    Application Date: 2009-05-14
  • Publication No.: US08721277B2
    Publication Date: 2014-05-13
  • Inventor: Alain Dominique Gendraud
  • Applicant: Alain Dominique Gendraud
  • Applicant Address: FR Paris
  • Assignee: SNECMA
  • Current Assignee: SNECMA
  • Current Assignee Address: FR Paris
  • Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
  • Priority: FR0853182 20080516
  • International Application: PCT/EP2009/055811 WO 20090514
  • International Announcement: WO2009/138443 WO 20091119
  • Main IPC: F01D9/04
  • IPC: F01D9/04 F01D25/28
Unit for locking ring sectors on a turbomachine casing, comprising radial passages for gripping it
Abstract:
A unit locking a ring sector attachment device onto an aircraft turbomachine casing, the unit including two clamping arms connected to each other at their aft ends by a connecting arm extending approximately parallel to the general direction between the two clamping arms. The unit also includes a passage enabling gripping of the unit on each side of a fictitious median plane orthogonal to the circumferential direction, each passage being formed in the connecting arm, extending along a direction line approximately parallel to the direction between the arms.
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