RU2357892C2 - Шпангоут каркаса фюзеляжа летательного аппарата - Google Patents

Шпангоут каркаса фюзеляжа летательного аппарата Download PDF

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Publication number
RU2357892C2
RU2357892C2 RU2007122393/11A RU2007122393A RU2357892C2 RU 2357892 C2 RU2357892 C2 RU 2357892C2 RU 2007122393/11 A RU2007122393/11 A RU 2007122393/11A RU 2007122393 A RU2007122393 A RU 2007122393A RU 2357892 C2 RU2357892 C2 RU 2357892C2
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RU
Russia
Prior art keywords
frame
lower arc
fuselage
transverse beam
bulkhead
Prior art date
Application number
RU2007122393/11A
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English (en)
Russian (ru)
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RU2007122393A (ru
Inventor
Брюно КАКСИАГЕРРА (FR)
Брюно КАКСИАГЕРРА
Original Assignee
Эрбюс Франс
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.)
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Publication date
Application filed by Эрбюс Франс filed Critical Эрбюс Франс
Publication of RU2007122393A publication Critical patent/RU2007122393A/ru
Application granted granted Critical
Publication of RU2357892C2 publication Critical patent/RU2357892C2/ru

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    • 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
    • B64C1/18—Floors
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • 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)
  • Rod-Shaped Construction Members (AREA)
  • Body Structure For Vehicles (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Holders For Apparel And Elements Relating To Apparel (AREA)
  • Package Frames And Binding Bands (AREA)
  • Ladders (AREA)
  • Greenhouses (AREA)
  • Tents Or Canopies (AREA)
  • Compressor (AREA)
RU2007122393/11A 2004-11-15 2005-11-07 Шпангоут каркаса фюзеляжа летательного аппарата RU2357892C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0452622A FR2877916B1 (fr) 2004-11-15 2004-11-15 Cadre de structure de fuselage d'aeronef
FR0452622 2004-11-15

Publications (2)

Publication Number Publication Date
RU2007122393A RU2007122393A (ru) 2008-12-20
RU2357892C2 true RU2357892C2 (ru) 2009-06-10

Family

ID=34951041

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007122393/11A RU2357892C2 (ru) 2004-11-15 2005-11-07 Шпангоут каркаса фюзеляжа летательного аппарата

Country Status (11)

Country Link
US (1) US7874516B2 (https=)
EP (1) EP1812288B1 (https=)
JP (1) JP4524313B2 (https=)
CN (1) CN100546872C (https=)
AT (1) ATE403598T1 (https=)
BR (1) BRPI0517861A (https=)
CA (1) CA2585869C (https=)
DE (1) DE602005008765D1 (https=)
FR (1) FR2877916B1 (https=)
RU (1) RU2357892C2 (https=)
WO (1) WO2006051235A1 (https=)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2519301C1 (ru) * 2013-02-18 2014-06-10 Иван Сергеевич Рыбкин Шпангоут переменной жесткости
RU2607894C2 (ru) * 2011-12-01 2017-01-11 Эйрбас Оперейшнз С.Л. Высоконагруженный шпангоут фюзеляжа летательного аппарата со стенкой решетчатой конструкции
RU2715525C2 (ru) * 2011-05-19 2020-02-28 Зе Боинг Компани Структура самолета для обеспечения высокой устойчивости к оттягиванию композитного стрингера

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DE102006026170B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026169B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026168A1 (de) * 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006029231B4 (de) * 2006-06-26 2013-09-26 Airbus Operations Gmbh Druckschott für einen Rumpf für die Luft- und Raumfahrt
US9611029B2 (en) * 2006-10-11 2017-04-04 The Boeing Company Floor beam support assembly, system, and associated method
GB2477882B (en) * 2006-12-08 2011-10-19 Boeing Co Energy absorbing structure for aircraft
US8376275B2 (en) * 2006-12-08 2013-02-19 The Boeing Company Energy absorbing structure for aircraft
US7954760B2 (en) * 2007-06-11 2011-06-07 The Boeing Company Cargo floor, system, and method
DE102007030026A1 (de) * 2007-06-29 2009-01-02 Airbus Deutschland Gmbh Strukturbauteil mit Spant- und Querträgerelement
DE102008007838B4 (de) * 2008-02-07 2013-07-18 Airbus Operations Gmbh Fußbodensystem für eine Rumpfzelle eines Flugzeugs
DE102008010197B4 (de) * 2008-02-20 2012-03-22 Airbus Operations Gmbh Verfahren zum Verbinden von zwei Rumpfsektionen unter Schaffung eines Querstoßes sowie Querstoßverbindung
FR2933065B1 (fr) 2008-06-30 2011-08-26 Airbus France Procede d'assemblage d'un plancher dans une structure de coque prealablement constituee d'un troncon de fuselage d'aeronef
DE102008038806A1 (de) * 2008-08-13 2010-02-25 Airbus Deutschland Gmbh Vormontage und Integration von Flugzeugkabinen
DE102008042036A1 (de) * 2008-09-12 2010-03-25 Airbus Deutschland Gmbh Stange zur Abstützung von Bauteilen innerhalb einer Rumpfzellenstruktur eines Flugzeugs
US8336820B2 (en) * 2008-10-27 2012-12-25 Embraer S.A. Aircraft cabin floor structures, systems and methods
DE102009012424B4 (de) * 2009-03-10 2014-03-20 Telair International Gmbh Frachtraumboden für einen Frachtraum eines Flugzeugs sowie Verfahren zur Montage eines solchen
FR2947524B1 (fr) * 2009-07-02 2011-12-30 Airbus Operations Sas Procede de fabrication d'un aeronef comprenant un plancher
DE102009049007A1 (de) 2009-10-09 2011-04-21 Airbus Operations Gmbh Druckrumpf eines Flugzeuges mit heckseitiger Druckkalotte
DE102010014302B4 (de) * 2010-04-09 2014-12-04 Premium Aerotec Gmbh Luftfahrzeug und Befestigungsanordnung für eine Fußbodenstruktur in einem Luftfahrzeug
DE102010014638B4 (de) * 2010-04-12 2019-08-01 Airbus Defence and Space GmbH Luftfahrzeug mit einer integrierten energieaufnehmenden Verformungsstruktur und Luftfahrzeug mit einem derartigen Rumpf
DE102010045588B4 (de) 2010-09-16 2017-04-06 Airbus Operations Gmbh Rumpfsegment für ein Luftfahrzeug
DE102010062018B4 (de) * 2010-11-26 2015-05-13 Airbus Operations Gmbh Stützstab zur Stützung einer Fussbodenstruktur eines Flugzeugs
ES2401517B1 (es) * 2011-05-31 2014-06-18 Airbus Operations S.L. Cuaderna de aeronave en material compuesto.
FR2979896A1 (fr) 2011-09-08 2013-03-15 Airbus Operations Sas Element de cadre de fuselage d'aeronef
DE102012005353A1 (de) * 2012-03-16 2013-09-19 Airbus Operations Gmbh Flugzeugrumpfstruktur mit Querprofilen und Fachwerkstruktur
US9505354B2 (en) 2013-09-16 2016-11-29 The Boeing Company Carbon fiber reinforced polymer cargo beam with integrated cargo stanchions and c-splices
EP2876042B1 (en) * 2013-11-20 2018-01-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Helicopter airframe
PL2905228T3 (pl) * 2014-02-06 2018-05-30 Airbus Helicopters Deutschland GmbH Płatowiec kadłubowy i zbiornik
EP2907743A1 (en) * 2014-02-13 2015-08-19 Airbus Operations GmbH Stiffening element, method for coupling the same, and shell component for an aircraft or spacecraft
FR3021624B1 (fr) * 2014-05-30 2017-12-22 Airbus Operations Sas Liaison coulissante entre la structure plancher et la structure de coque d'un aeronef.
US10625844B2 (en) * 2014-11-10 2020-04-21 The Boeing Company Fuselage with structural and non-structural stanchions
FR3035070B1 (fr) * 2015-04-20 2017-05-05 Airbus Operations Sas Aeronef a section courante simplifiee
US10745098B2 (en) * 2017-09-05 2020-08-18 The Boeing Company Energy-absorbing under-floor airframe
US11383817B2 (en) * 2019-07-19 2022-07-12 The Boeing Company Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and MEl'hods of assembling modular fuselage assemblies
FR3124487A1 (fr) * 2021-06-29 2022-12-30 Airbus Operations Élément de liaison entre un premier et un deuxième élément structurel de fuselage d’un aéronef permettant une dissipation améliorée des efforts.
FR3128938A1 (fr) * 2021-11-10 2023-05-12 Airbus Operations Ensemble structurel pour un aéronef
US20250368312A1 (en) * 2024-05-29 2025-12-04 The Boeing Company Stanchion for aircraft structure
EP4667351A1 (en) * 2024-06-20 2025-12-24 Airbus Operations, S.L.U. An aircraft fuselage section
US12534176B1 (en) * 2024-09-30 2026-01-27 Civil Aviation University Of China Fuselage sub-floor structure with aircraft components having corrugated C-channel

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US1803494A (en) * 1928-12-20 1931-05-05 Emboutissage Et De Const Mecan Hollow-frame assembly
SU708102A1 (ru) * 1977-08-02 1980-01-05 Предприятие П/Я А-3611 Соединение оболочек из композиционных материалов
DE4017978A1 (de) * 1990-06-05 1991-12-12 Dornier Luftfahrt Herstellung profilierter stringer
SU1726691A1 (ru) * 1990-08-29 1992-04-15 Центральный научно-исследовательский институт специального машиностроения Опорный шпангоут из композиционного материала
US5171510A (en) * 1988-06-08 1992-12-15 Aerospatiale Societe Nationale Industrielle Method of producing a frame made of a composite material, especially for the fuselage of an aircraft
US5752673A (en) * 1994-05-10 1998-05-19 Daimler-Benz Aerospace Airbus Gmbh Passenger aircraft with increased passenger capacity

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US1963416A (en) * 1932-03-07 1934-06-19 Boeing Co Airplane structural elements
US2412778A (en) * 1944-12-18 1946-12-17 Cons Vultee Aircraft Corp Suspension type flooring for aircraft
US4308703A (en) * 1980-01-18 1982-01-05 James Knowles Metal connector struts for truss-type beams
DE3141869C2 (de) * 1981-10-22 1984-02-02 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Fußbodenkonstruktion für den oberen Laderaum eines Luftfahrzeuges
US5072895A (en) * 1990-07-05 1991-12-17 Mark Camus Cargo platform assembly mounted to a helicopter
US5560102A (en) * 1992-10-13 1996-10-01 The Boeing Company Panel and fuselage assembly
CN1153500A (zh) * 1994-04-06 1997-07-02 波音公司 半刚性、轻型玻璃纤维/聚酰亚胺泡沫夹层绝缘层片
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GB0113916D0 (en) * 2001-06-07 2001-08-01 Bae Systems Plc Adding glass to composite bonding surfaces
CN2507779Y (zh) * 2001-07-30 2002-08-28 罗专予 半圆形飞机水密封舱
DE10145276B4 (de) * 2001-09-14 2008-04-10 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugzeug, insbesondere Passagierflugzeug, mit einem Rumpf, der eine tragende Primärstruktur und einen Frachtraum umfasst

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1803494A (en) * 1928-12-20 1931-05-05 Emboutissage Et De Const Mecan Hollow-frame assembly
SU708102A1 (ru) * 1977-08-02 1980-01-05 Предприятие П/Я А-3611 Соединение оболочек из композиционных материалов
US5171510A (en) * 1988-06-08 1992-12-15 Aerospatiale Societe Nationale Industrielle Method of producing a frame made of a composite material, especially for the fuselage of an aircraft
DE4017978A1 (de) * 1990-06-05 1991-12-12 Dornier Luftfahrt Herstellung profilierter stringer
SU1726691A1 (ru) * 1990-08-29 1992-04-15 Центральный научно-исследовательский институт специального машиностроения Опорный шпангоут из композиционного материала
US5752673A (en) * 1994-05-10 1998-05-19 Daimler-Benz Aerospace Airbus Gmbh Passenger aircraft with increased passenger capacity

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2715525C2 (ru) * 2011-05-19 2020-02-28 Зе Боинг Компани Структура самолета для обеспечения высокой устойчивости к оттягиванию композитного стрингера
RU2607894C2 (ru) * 2011-12-01 2017-01-11 Эйрбас Оперейшнз С.Л. Высоконагруженный шпангоут фюзеляжа летательного аппарата со стенкой решетчатой конструкции
RU2519301C1 (ru) * 2013-02-18 2014-06-10 Иван Сергеевич Рыбкин Шпангоут переменной жесткости

Also Published As

Publication number Publication date
EP1812288A1 (fr) 2007-08-01
DE602005008765D1 (de) 2008-09-18
JP4524313B2 (ja) 2010-08-18
CA2585869A1 (fr) 2006-05-18
BRPI0517861A (pt) 2008-10-21
RU2007122393A (ru) 2008-12-20
WO2006051235A1 (fr) 2006-05-18
US7874516B2 (en) 2011-01-25
FR2877916B1 (fr) 2008-04-25
FR2877916A1 (fr) 2006-05-19
CN101056796A (zh) 2007-10-17
ATE403598T1 (de) 2008-08-15
CN100546872C (zh) 2009-10-07
CA2585869C (fr) 2013-12-24
US20080093503A1 (en) 2008-04-24
JP2008519730A (ja) 2008-06-12
EP1812288B1 (fr) 2008-08-06

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Legal Events

Date Code Title Description
PC43 Official registration of the transfer of the exclusive right without contract for inventions

Effective date: 20120221

MM4A The patent is invalid due to non-payment of fees

Effective date: 20191108