发明授权
US07316372B2 Fuselage spar for aircraft and central sparbox provided with such a spar 有权
飞机和中央翼型架的机身翼梁提供了这样的翼梁

  • 专利标题: Fuselage spar for aircraft and central sparbox provided with such a spar
  • 专利标题(中): 飞机和中央翼型架的机身翼梁提供了这样的翼梁
  • 申请号: US11070648
    申请日: 2005-03-02
  • 公开(公告)号: US07316372B2
    公开(公告)日: 2008-01-08
  • 发明人: Bruno Sarpy
  • 申请人: Bruno Sarpy
  • 申请人地址: FR Toulouse
  • 专利权人: Airbus France
  • 当前专利权人: Airbus France
  • 当前专利权人地址: FR Toulouse
  • 代理机构: Patterson, Thuente, Skaar & Christensen, P.A.
  • 优先权: FR0450452 20040304
  • 主分类号: B64C1/00
  • IPC分类号: B64C1/00
Fuselage spar for aircraft and central sparbox provided with such a spar
摘要:
A fuselage spar for aircraft is vertically mounted between an upper surface panel and a lower surface panel of the fuselage at the junction between a first wing structure spar and a second wing structure spar symmetrical with the first wing structure spar relative to the fuselage, and comprises peripheral zones and a central zone. This fuselage spar comprises a hollowed-out portion in the central zone, the peripheral zones of the spar providing for a draining of the normal loads conveyed by the wing structure spars. Also disclosed is a central spar box comprising such a spar.
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