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

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-001/06
  • B64C-001/12
출원번호 US-0174477 (1993-12-28)
발명자 / 주소
  • Roseburg Lawrence E. (Bellevue WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 93  인용 특허 : 0

초록

An aircraft construction which enables visual inspection of critical body skin/stringer circumferential splice failure lines from the interior of an aircraft comprises a bulkhead member with an alternating shear tie foot pattern such that in alternating stringer bays the critical failure path along

대표청구항

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 anot

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