GB620462A - Improvements in and relating to aeroplanes - Google Patents

Improvements in and relating to aeroplanes

Info

Publication number
GB620462A
GB620462A GB1753/47A GB175347A GB620462A GB 620462 A GB620462 A GB 620462A GB 1753/47 A GB1753/47 A GB 1753/47A GB 175347 A GB175347 A GB 175347A GB 620462 A GB620462 A GB 620462A
Authority
GB
United Kingdom
Prior art keywords
sections
fuselage
ring
aeroplanes
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
GB1753/47A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB1753/47A priority Critical patent/GB620462A/en
Publication of GB620462A publication Critical patent/GB620462A/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
    • 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
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite 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)
  • Joints Allowing Movement (AREA)

Abstract

620,462. Aircraft framework HEENAN, J. N. D. Jan. 20, 1947 No. 1753. [Class 4] An aeroplane fuselage of the kinc which is built up from two or more separate longitudinal sections adapted to be secured together in endwise relationship to form a complete fuselage is characterisec in that the opposed joint-forming edges of the sections 4, 4a are re leasably held together by an interna locking ring 2 which is expandec by hand levers 8 to lock the twc sections together. The ring 2 may have a wedging engagement with the flanges 4, 4a.
GB1753/47A 1947-01-20 1947-01-20 Improvements in and relating to aeroplanes Expired GB620462A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1753/47A GB620462A (en) 1947-01-20 1947-01-20 Improvements in and relating to aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1753/47A GB620462A (en) 1947-01-20 1947-01-20 Improvements in and relating to aeroplanes

Publications (1)

Publication Number Publication Date
GB620462A true GB620462A (en) 1949-03-24

Family

ID=9727385

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1753/47A Expired GB620462A (en) 1947-01-20 1947-01-20 Improvements in and relating to aeroplanes

Country Status (1)

Country Link
GB (1) GB620462A (en)

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