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Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices

  • US 5,518,208 A
  • Filed: 12/28/1993
  • Issued: 05/21/1996
  • Est. Priority Date: 12/28/1993
  • Status: Expired due to Term
First Claim
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1. An aircraft fuselage bulkhead member comprising:

  • a central web member adapted for placement within an aircraft transverse to the longitudinal axis of the aircraft, said central web member having a forward and an aft face;

    at least two first shear tie members positioned in spaced relation to one another and extending a substantial extent only away from the forward face of said central web member; and

    at least two second shear tie members positioned in spaced relation to one another and extending away from the aft face of said central web member, wherein the longitudinal alignment of a particular first shear tie member is offset from the longitudinal alignment of a corresponding second shear tie member.

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