GB159351A - Improvements in metal bulkheads for the fuselages or bodies of aircraft - Google Patents

Improvements in metal bulkheads for the fuselages or bodies of aircraft

Info

Publication number
GB159351A
GB159351A GB3066619A GB3066619A GB159351A GB 159351 A GB159351 A GB 159351A GB 3066619 A GB3066619 A GB 3066619A GB 3066619 A GB3066619 A GB 3066619A GB 159351 A GB159351 A GB 159351A
Authority
GB
United Kingdom
Prior art keywords
plates
tube
fixed
flanges
fuselages
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
GB3066619A
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.)
Boulton and Paul Ltd
Original Assignee
Boulton and Paul Ltd
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 Boulton and Paul Ltd filed Critical Boulton and Paul Ltd
Priority to GB3066619A priority Critical patent/GB159351A/en
Publication of GB159351A publication Critical patent/GB159351A/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
    • B64C1/10—Bulkheads
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

159,351. Boulton & Paul, Ltd., and North, J. D. Dec. 8, 1919. Cars and cabins; framework. - Transverse frames of fuselages, nacelles, or bcdies of aircraft are each composed of two sheet-metal plates 1 shaped to conform with the cross-section of the fuselage and rigidly spaced apart by short lengths of tube, tubular rivets, or the like 4, the plates having their edges turned outwards to form flanges 2, to which the covering skin of the fuselage is fixed. In one method of spacing the plates apart there are employed short lengths of tube 4 through each of which passes another tube which has its ends riveted outside the plates. In an alternative method, a single tube has flanges bearing upon the inner sides of the plates 1. Holes 8 are provided for tubular longerons 9, which are carried in sleeves 11 fixed to stiffening-plates 10. The sleeves are formed with ears 12 for the attachment of bracing-wires. The longerons, if formed of bent sheet metal, may be fixed by rivets or other means to the outer flanges of the bulkheads. Spars or other members may be connected so that the two plates 1 are loaded equally by fixing them between the plates 10 or other strengthening- plates. One or more transverse frames may be constructed with members outstanding to facilitate the attachment of fin ribs or tail planes.
GB3066619A 1919-12-08 1919-12-08 Improvements in metal bulkheads for the fuselages or bodies of aircraft Expired GB159351A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3066619A GB159351A (en) 1919-12-08 1919-12-08 Improvements in metal bulkheads for the fuselages or bodies of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3066619A GB159351A (en) 1919-12-08 1919-12-08 Improvements in metal bulkheads for the fuselages or bodies of aircraft

Publications (1)

Publication Number Publication Date
GB159351A true GB159351A (en) 1921-03-03

Family

ID=10311220

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3066619A Expired GB159351A (en) 1919-12-08 1919-12-08 Improvements in metal bulkheads for the fuselages or bodies of aircraft

Country Status (1)

Country Link
GB (1) GB159351A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006026168A1 (en) * 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Aircraft fuselage structure and method for its manufacture
US8534605B2 (en) 2006-06-06 2013-09-17 Airbus Operations Gmbh Aircraft fuselage structure and method for producing it
US8651421B2 (en) 2006-06-06 2014-02-18 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
EP4420974A1 (en) * 2023-02-27 2024-08-28 Airbus Operations GmbH Method for manufacturing a fuselage structural component for a triangular area and a one-piece fuselage structural component

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006026168A1 (en) * 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Aircraft fuselage structure and method for its manufacture
US8534605B2 (en) 2006-06-06 2013-09-17 Airbus Operations Gmbh Aircraft fuselage structure and method for producing it
US8651421B2 (en) 2006-06-06 2014-02-18 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
US8695922B2 (en) 2006-06-06 2014-04-15 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
EP4420974A1 (en) * 2023-02-27 2024-08-28 Airbus Operations GmbH Method for manufacturing a fuselage structural component for a triangular area and a one-piece fuselage structural component

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