FR2638708B1 - Perfectionnement a un fuselage - Google Patents

Perfectionnement a un fuselage

Info

Publication number
FR2638708B1
FR2638708B1 FR8814714A FR8814714A FR2638708B1 FR 2638708 B1 FR2638708 B1 FR 2638708B1 FR 8814714 A FR8814714 A FR 8814714A FR 8814714 A FR8814714 A FR 8814714A FR 2638708 B1 FR2638708 B1 FR 2638708B1
Authority
FR
France
Prior art keywords
fuselage
improvement
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 - Fee Related
Application number
FR8814714A
Other languages
English (en)
Other versions
FR2638708A1 (fr
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 IGOR
NOVOZHILOV GENRIKH
Original Assignee
KATYREV IGOR
NOVOZHILOV GENRIKH
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
Priority to GB8824723A priority Critical patent/GB2224000B/en
Application filed by KATYREV IGOR, NOVOZHILOV GENRIKH filed Critical KATYREV IGOR
Priority to FR8814714A priority patent/FR2638708B1/fr
Priority to DE3900167A priority patent/DE3900167A1/de
Publication of FR2638708A1 publication Critical patent/FR2638708A1/fr
Application granted granted Critical
Publication of FR2638708B1 publication Critical patent/FR2638708B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064Stringers; Longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12Construction or attachment of skin panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8814714A 1988-11-10 1988-11-10 Perfectionnement a un fuselage Expired - Fee Related FR2638708B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB8824723A GB2224000B (en) 1988-11-10 1988-10-21 Aircraft fuselage or other pressure vessel.
FR8814714A FR2638708B1 (fr) 1988-11-10 1988-11-10 Perfectionnement a un fuselage
DE3900167A DE3900167A1 (de) 1988-11-10 1989-01-05 Luftfahrzeugrumpf

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8814714A FR2638708B1 (fr) 1988-11-10 1988-11-10 Perfectionnement a un fuselage

Publications (2)

Publication Number Publication Date
FR2638708A1 FR2638708A1 (fr) 1990-05-11
FR2638708B1 true FR2638708B1 (fr) 1994-05-06

Family

ID=9371782

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8814714A Expired - Fee Related FR2638708B1 (fr) 1988-11-10 1988-11-10 Perfectionnement a un fuselage

Country Status (3)

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

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2935722B2 (ja) * 1990-02-28 1999-08-16 富士重工業株式会社 航空機の胴体構造およびその成形方法
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 (de) 2008-03-03 2009-09-17 Airbus Deutschland Gmbh Rumpfstruktur für Flugzeug
DE102010018932B4 (de) * 2010-04-30 2013-06-13 Airbus Operations Gmbh Umfangsversteifung für einen Luftfahrzeugrumpf
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 (fr) * 1938-10-28 1939-08-18 Henschel Flugzeugwerke Ag Dispositif pour le raidissage de tôles lisses
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
FR2638708A1 (fr) 1990-05-11
GB2224000B (en) 1992-05-27
GB8824723D0 (en) 1988-11-30
DE3900167A1 (de) 1990-07-12
GB2224000A (en) 1990-04-25

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Legal Events

Date Code Title Description
ST Notification of lapse