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Invention Grant
US08418593B2 Deformable rear disc for missile container, including a downstream bearing frame 有权
用于导弹集装箱的可变形后盘，包括下游轴承架

  • Patent Title: Deformable rear disc for missile container, including a downstream bearing frame
  • Patent Title (中): 用于导弹集装箱的可变形后盘，包括下游轴承架
  • Application No.: US12735379
    Application Date: 2009-01-08
  • Publication No.: US08418593B2
    Publication Date: 2013-04-16
  • Inventor: Pierre Jacques Truyman
  • Applicant: Pierre Jacques Truyman
  • Applicant Address: FR Paris
  • Assignee: DCNS
  • Current Assignee: DCNS
  • Current Assignee Address: FR Paris
  • Agency: Jacobson Holman PLLC
  • Priority: FR0850162 20080111
  • International Application: PCT/FR2009/050020 WO 20090108
  • International Announcement: WO2009/092938 WO 20090730
  • Main IPC: F41F3/04
  • IPC: F41F3/04
Deformable rear disc for missile container, including a downstream bearing frame
Abstract:
The invention relates to an improved deformable downstream disc (56; 156; 256) to be fitted on the bottom of a container (15) for a missile (16) and including a stack of elastic blades (63) clamped between at least an upstream and a downstream thermal protection membrane and sealing membrane (70, 71, 72, 73), and maintained between an upstream bearing frame (61) and a downstream bearing frame (64), characterised in that the downstream bearing frame includes an inner edge (80) having an extension so as to provide the disc with an abutment means defining a position of maximum deformation of the elastic blades.
Abstract(Chinese):

本发明涉及一种改进的可变形的下游盘（56; 156; 256），其被装配在用于导弹（16）的容器（15）的底部，并且包括一堆弹性叶片（63），其夹在至少一个上游 和下游的热保护膜和密封膜（70,71,72,73），并且保持在上游轴承框架（61）和下游轴承框架（64）之间，其特征在于，所述下游轴承框架包括内边缘 80）具有延伸部，以便为盘提供限定弹性片的最大变形位置的邻接装置。

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