GB531357A - Improvements in or relating to aircraft fusilages - Google Patents

Improvements in or relating to aircraft fusilages

Info

Publication number
GB531357A
GB531357A GB20986/39A GB2098639A GB531357A GB 531357 A GB531357 A GB 531357A GB 20986/39 A GB20986/39 A GB 20986/39A GB 2098639 A GB2098639 A GB 2098639A GB 531357 A GB531357 A GB 531357A
Authority
GB
United Kingdom
Prior art keywords
girders
fuselage
decks
flanges
aircraft
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
GB20986/39A
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.)
Dornier Werke GmbH
Original Assignee
Dornier Werke 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 Dornier Werke GmbH filed Critical Dornier Werke GmbH
Publication of GB531357A publication Critical patent/GB531357A/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
    • B64C1/061—Frames
    • 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
    • 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
    • B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
    • B64C2001/0027—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged one above the other
    • 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

Abstract

531,357. Aircraft fuselages. DORNIERWERKE GES., and DORNIER, C. July 19, 1939, No. 20986. Convention date, Aug. 26, 1938. '[Class 4] A circular or elliptical fuselage has two or more sheet metal or framework longitudinal girders 26 of the full height of the fuselage and spaced apart to form one or more gangways. The girders have flange members for securing them to the fuselage, and such flanges may form part of the skin of the fuselage. One or more decks 23, 24, 25 may be connected by flanges to the girders. The girders may have passage ways communicating with the decks. Bulkheads forming the walls of rooms may be arranged laterally of the girders.
GB20986/39A 1938-08-26 1939-07-19 Improvements in or relating to aircraft fusilages Expired GB531357A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE531357X 1938-08-26

Publications (1)

Publication Number Publication Date
GB531357A true GB531357A (en) 1941-01-02

Family

ID=6554926

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20986/39A Expired GB531357A (en) 1938-08-26 1939-07-19 Improvements in or relating to aircraft fusilages

Country Status (1)

Country Link
GB (1) GB531357A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5086996A (en) * 1989-07-12 1992-02-11 Airbus Industrie High-capacity fuselage for aircraft
GB2312483A (en) * 1996-04-24 1997-10-29 British Aerospace Joint assembly
EP1614624A1 (en) * 2004-07-08 2006-01-11 AIRBUS France Aircraft floor
WO2008090089A1 (en) 2007-01-23 2008-07-31 Airbus Operations Gmbh Fuselage of an aircraft or spacecraft of crp/metal hybrid construction with a metal framework
US7807005B2 (en) 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
US8333858B2 (en) 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US8491745B2 (en) 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US8691137B2 (en) 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US9102103B2 (en) 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
DE102019102483A1 (en) * 2019-01-31 2020-08-06 Airbus Operations Gmbh Passenger cabin for a vehicle and a vehicle with at least one such cabin
US10821653B2 (en) 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5086996A (en) * 1989-07-12 1992-02-11 Airbus Industrie High-capacity fuselage for aircraft
GB2312483A (en) * 1996-04-24 1997-10-29 British Aerospace Joint assembly
US5944286A (en) * 1996-04-24 1999-08-31 British Aerospace Public Limited Company Joint assemblies
GB2312483B (en) * 1996-04-24 2000-02-23 British Aerospace Joint assemblies
EP1614624A1 (en) * 2004-07-08 2006-01-11 AIRBUS France Aircraft floor
FR2872781A1 (en) * 2004-07-08 2006-01-13 Airbus France Sas FLOOR FOR AIRCRAFT
US7191982B2 (en) 2004-07-08 2007-03-20 Airbus France Floor for aircraft
US8425708B2 (en) 2006-02-02 2013-04-23 The Boeing Company Continuous fabrication of parts using in-feed spools of fiber reinforced thermoplastic
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
US7807005B2 (en) 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
US11524471B2 (en) 2006-02-02 2022-12-13 The Boeing Company Method for fabricating thermoplastic composite parts
US8333858B2 (en) 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
US9511538B2 (en) 2006-02-02 2016-12-06 The Boeing Company Method for fabricating thermoplastic composite parts
US9102103B2 (en) 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US8795457B2 (en) 2006-02-02 2014-08-05 The Boeing Company Fabrication process for thermoplastic composite parts
CN101631715B (en) * 2007-01-23 2013-06-12 空中客车德国有限公司 Fuselage of an aircraft or spacecraft of CRP/metal hybrid construction with a metal framework
JP2010516536A (en) * 2007-01-23 2010-05-20 エアバス・オペレーションズ・ゲーエムベーハー CRP / metal composite aircraft or spacecraft fuselage with metal framework
WO2008090089A1 (en) 2007-01-23 2008-07-31 Airbus Operations Gmbh Fuselage of an aircraft or spacecraft of crp/metal hybrid construction with a metal framework
RU2446076C2 (en) * 2007-01-23 2012-03-27 Эйрбас Оперейшнз Гмбх Aircraft or spacecraft fuselage from hybrid composition of carbon fiber-reinforced plastic/metal with metal frame
US8491745B2 (en) 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US10414107B2 (en) 2007-02-03 2019-09-17 The Boeing Company Method and material efficient tooling for continuous compression molding
US8691137B2 (en) 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US9545761B2 (en) 2009-03-04 2017-01-17 The Boeing Company Tool sleeve for mold die
US10821653B2 (en) 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates
DE102019102483A1 (en) * 2019-01-31 2020-08-06 Airbus Operations Gmbh Passenger cabin for a vehicle and a vehicle with at least one such cabin
US11414192B2 (en) 2019-01-31 2022-08-16 Airbus Operations Gmbh Passenger cabin for a vehicle, and a vehicle having at least one such cabin

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