GB157265A - Improvements relating to the construction of hollow bodies for aircraft - Google Patents

Improvements relating to the construction of hollow bodies for aircraft

Info

Publication number
GB157265A
GB157265A GB1159/21A GB115921A GB157265A GB 157265 A GB157265 A GB 157265A GB 1159/21 A GB1159/21 A GB 1159/21A GB 115921 A GB115921 A GB 115921A GB 157265 A GB157265 A GB 157265A
Authority
GB
United Kingdom
Prior art keywords
members
aircraft
construction
hollow bodies
improvements relating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1159/21A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zeppelin GmbH
Original Assignee
Zeppelinwerke GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zeppelinwerke GmbH filed Critical Zeppelinwerke GmbH
Publication of GB157265A publication Critical patent/GB157265A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

157,265. Zeppelin-Werk Lindau Ges., and Dornier, C. May 4, 1917, [Convention date]. Fuselages; framework. -A sheet-metal body for aircraft, especially adapted for use as a hull, comprises open longitudinal members B and annular members C, D all connected together by the envelope A. The members C are composed of pairs of flanged rings secured back to back; or they may be single members of open profile. The members D are corrugated. The members B and C, D may be secured together at their points of intersection. In long hulls, the metal envelope A may be in sections threaded over the bars B.
GB1159/21A 1917-05-04 1921-01-10 Improvements relating to the construction of hollow bodies for aircraft Expired GB157265A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE157265X 1917-05-04

Publications (1)

Publication Number Publication Date
GB157265A true GB157265A (en) 1922-04-10

Family

ID=5678490

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1159/21A Expired GB157265A (en) 1917-05-04 1921-01-10 Improvements relating to the construction of hollow bodies for aircraft

Country Status (1)

Country Link
GB (1) GB157265A (en)

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