GB8824723D0 - Fuselage - Google Patents

Fuselage

Info

Publication number
GB8824723D0
GB8824723D0 GB888824723A GB8824723A GB8824723D0 GB 8824723 D0 GB8824723 D0 GB 8824723D0 GB 888824723 A GB888824723 A GB 888824723A GB 8824723 A GB8824723 A GB 8824723A GB 8824723 D0 GB8824723 D0 GB 8824723D0
Authority
GB
United Kingdom
Prior art keywords
fuselage
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.)
Granted
Application number
GB888824723A
Other versions
GB2224000A (en
GB2224000B (en
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.)
Katyrev I Y
Original Assignee
Katyrev I Y
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 Katyrev I Y filed Critical Katyrev I Y
Publication of GB8824723D0 publication Critical patent/GB8824723D0/en
Publication of GB2224000A publication Critical patent/GB2224000A/en
Application granted granted Critical
Publication of GB2224000B publication Critical patent/GB2224000B/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/12—Construction or attachment of skin panels
GB8824723A 1988-11-10 1988-10-21 Aircraft fuselage or other pressure vessel. Expired - Lifetime GB2224000B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8814714A FR2638708B1 (en) 1988-11-10 1988-11-10 IMPROVEMENT TO A FUSELAGE

Publications (3)

Publication Number Publication Date
GB8824723D0 true GB8824723D0 (en) 1988-11-30
GB2224000A GB2224000A (en) 1990-04-25
GB2224000B GB2224000B (en) 1992-05-27

Family

ID=9371782

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8824723A Expired - Lifetime GB2224000B (en) 1988-11-10 1988-10-21 Aircraft fuselage or other pressure vessel.

Country Status (3)

Country Link
DE (1) DE3900167A1 (en)
FR (1) FR2638708B1 (en)
GB (1) GB2224000B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2935722B2 (en) * 1990-02-28 1999-08-16 富士重工業株式会社 Aircraft fuselage structure and molding method thereof
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
GB2279930B (en) * 1993-06-18 1997-03-26 Royal Ordnance Plc The protection of aircraft structures
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7503368B2 (en) 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
DE102008012282A1 (en) 2008-03-03 2009-09-17 Airbus Deutschland Gmbh Hull structure for airplane
DE102010018932B4 (en) * 2010-04-30 2013-06-13 Airbus Operations Gmbh Perimeter stiffening for an aircraft fuselage
US10745104B2 (en) * 2018-03-02 2020-08-18 The Boeing Company Stringer transition through a common base charge

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR845332A (en) * 1938-10-28 1939-08-18 Henschel Flugzeugwerke Ag Device for stiffening smooth sheets
GB534810A (en) * 1940-02-26 1941-03-19 David Henderson Sandilands Stressed skin panels
GB555496A (en) * 1942-02-20 1943-08-25 Henry Kremer Improvements in or relating to structures built up of plywood or other light-weight laminated material
GB559954A (en) * 1942-09-07 1944-03-13 Vultee Aircraft Inc Airplane structures

Also Published As

Publication number Publication date
DE3900167A1 (en) 1990-07-12
FR2638708B1 (en) 1994-05-06
FR2638708A1 (en) 1990-05-11
GB2224000A (en) 1990-04-25
GB2224000B (en) 1992-05-27

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19931021