JP6159409B2 - 航空機胴体フレームをウィングボックスに取り付ける方法及び装置 - Google Patents

航空機胴体フレームをウィングボックスに取り付ける方法及び装置 Download PDF

Info

Publication number
JP6159409B2
JP6159409B2 JP2015536842A JP2015536842A JP6159409B2 JP 6159409 B2 JP6159409 B2 JP 6159409B2 JP 2015536842 A JP2015536842 A JP 2015536842A JP 2015536842 A JP2015536842 A JP 2015536842A JP 6159409 B2 JP6159409 B2 JP 6159409B2
Authority
JP
Japan
Prior art keywords
wing box
aircraft
fuselage
aircraft fuselage
wing
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.)
Active
Application number
JP2015536842A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015533111A (ja
JP2015533111A5 (enExample
Inventor
トーマス、グラント、ブライアン
リン、チュン—リアン
リン、チュン―リアン
アンドリューズ、フランシス、イー・
チョイ、ウェンデル、シー・ケイ・
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of JP2015533111A publication Critical patent/JP2015533111A/ja
Publication of JP2015533111A5 publication Critical patent/JP2015533111A5/ja
Application granted granted Critical
Publication of JP6159409B2 publication Critical patent/JP6159409B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26Attaching the wing or tail units or stabilising surfaces
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49622Vehicular structural member making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Toys (AREA)
  • Automatic Assembly (AREA)
JP2015536842A 2012-10-16 2013-10-08 航空機胴体フレームをウィングボックスに取り付ける方法及び装置 Active JP6159409B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/652,975 2012-10-16
US13/652,975 US8857765B2 (en) 2012-10-16 2012-10-16 Method and apparatus for attaching an aircraft fuselage frame to a wing box
PCT/US2013/063913 WO2014062423A1 (en) 2012-10-16 2013-10-08 Method and apparatus for attaching an aircraft fuselage frame to a wing box

Publications (3)

Publication Number Publication Date
JP2015533111A JP2015533111A (ja) 2015-11-19
JP2015533111A5 JP2015533111A5 (enExample) 2016-07-07
JP6159409B2 true JP6159409B2 (ja) 2017-07-05

Family

ID=49385426

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015536842A Active JP6159409B2 (ja) 2012-10-16 2013-10-08 航空機胴体フレームをウィングボックスに取り付ける方法及び装置

Country Status (5)

Country Link
US (1) US8857765B2 (enExample)
EP (1) EP2909085B1 (enExample)
JP (1) JP6159409B2 (enExample)
CN (1) CN104603007B (enExample)
WO (1) WO2014062423A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU225507U1 (ru) * 2024-01-10 2024-04-23 Акционерное общество "Термостойкие изделия и инженерные разработки" (АО "ТИИР") Фрикционная накладка

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2998868B1 (fr) * 2012-11-30 2016-02-05 Airbus Operations Sas Dispositif de fixation intermediaire entre un fuselage d'aeronef et un train d'atterrissage d'aeronef
US9828083B2 (en) 2014-11-14 2017-11-28 The Boeing Company Methods and components for wing-to-fuselage integration
US10106240B2 (en) 2015-07-13 2018-10-23 The Boeing Company Pinned fuselage-to-wing connection
US10275565B2 (en) 2015-11-06 2019-04-30 The Boeing Company Advanced automated process for the wing-to-body join of an aircraft with predictive surface scanning
DE102017117314A1 (de) 2017-07-31 2019-01-31 Airbus Operations Gmbh Befestigungseinheit zum beweglichen Befestigen einer Luftfahrzeugkomponente an einer Tragstruktur eines Luftfahrzeugs
US10712730B2 (en) 2018-10-04 2020-07-14 The Boeing Company Methods of synchronizing manufacturing of a shimless assembly
US11136107B2 (en) * 2018-10-05 2021-10-05 The Boeing Company Method and apparatus for attaching a fuselage frame to a wing box
US11174042B2 (en) 2018-10-09 2021-11-16 The Boeing Company Wing join system and method for a wing assembly
CN109774964A (zh) * 2019-01-28 2019-05-21 陕西智翔航空科技发展有限公司 复合材料机身对合型架
BR102021017320A2 (pt) * 2020-11-03 2022-07-26 The Boeing Company Sistema e método para prender uma porção de uma fuselagem de uma aeronave a uma porção de uma asa da aeronave
KR20240148479A (ko) * 2023-04-04 2024-10-11 현대자동차주식회사 동체의 날개 하중 지지구조

Family Cites Families (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1865964A (en) 1926-09-27 1932-07-05 Rohrbach Patents Corp Monoplane
US2001260A (en) 1932-07-20 1935-05-14 Martin James Construction and arrangement of aeroplane wings
US2211089A (en) * 1938-03-29 1940-08-13 Curtiss Wright Corp Wing and fuselage construction
US2370801A (en) 1941-05-14 1945-03-06 Cons Vultee Aireraft Corp Airplane wing structure
US2412778A (en) 1944-12-18 1946-12-17 Cons Vultee Aircraft Corp Suspension type flooring for aircraft
US2779558A (en) 1952-04-09 1957-01-29 Sncase Fuselage of aerodynes
US2749061A (en) 1954-06-18 1956-06-05 Wesley A Franz Airplane wing stress compensating structure assembly
US3018985A (en) 1956-12-31 1962-01-30 Martin Marietta Corp Swept wing with unswept spar
US3942746A (en) * 1971-12-27 1976-03-09 General Dynamics Corporation Aircraft having improved performance with beaver-tail afterbody configuration
US4120998A (en) * 1977-02-03 1978-10-17 Northrop Corporation Composite structure
DE2932667C2 (de) 1979-08-11 1982-07-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Hauptanschluß für den Tragflügel eines Luftfahrzeuges
US4417708A (en) 1982-05-12 1983-11-29 Grumman Aerospace Corporation Interchangeable wing aircraft
US4893964A (en) * 1989-02-06 1990-01-16 Grumman Aerospace Corporation Interlocking structural members utilizing overlying composite strips
US5332178A (en) * 1992-06-05 1994-07-26 Williams International Corporation Composite wing and manufacturing process thereof
JP4128626B2 (ja) * 1996-03-22 2008-07-30 ザ・ボーイング・カンパニー 決定的な翼アセンブリ
CA2444869A1 (en) * 2002-10-21 2004-04-21 The Boeing Company Method and apparatus for actuating movable components, including canards, over multiple ranges
FR2873347B1 (fr) * 2004-07-22 2006-11-17 Airbus France Sas Dispositif d'eclissage d'elements de structure composite avec des elements de structure metallique
FR2883548B1 (fr) * 2005-03-23 2007-06-15 Airbus France Sas Dispositif et procede d'eclissage mixte carbone-metal dissymetrique
DE102005034891B4 (de) * 2005-07-26 2007-06-14 Airbus Deutschland Gmbh Querkraftanschluss
US8142126B2 (en) * 2005-09-02 2012-03-27 The Boeing Company Multi-piece fastener with self-indexing nut
US9359061B2 (en) * 2005-10-31 2016-06-07 The Boeing Company Compliant stiffener for aircraft fuselage
US7398586B2 (en) * 2005-11-01 2008-07-15 The Boeing Company Methods and systems for manufacturing a family of aircraft wings and other composite structures
GB0525896D0 (en) * 2005-12-20 2006-02-01 Airbus Uk Ltd A joint for use in aircraft construction
US7501814B2 (en) * 2006-09-07 2009-03-10 Southwest Research Institute Apparatus and method for second-layer through-bushing inspection of aircraft wing attachment fittings using electric current perturbation
US7546979B1 (en) * 2006-09-15 2009-06-16 The Boeing Company Trapezoidal panel pin joint allowing free deflection between fuselage and wing
DE102006051572B4 (de) * 2006-11-02 2010-01-21 Airbus Deutschland Gmbh Flügel-Rumpf-Verbindung eines Flugzeugs
US7721992B2 (en) * 2007-03-07 2010-05-25 The Boeing Company Aircraft floor to fuselage attachment
FR2913400B1 (fr) * 2007-03-07 2009-11-20 Airbus France Plancher d'aeronef et fuselage muni d'un tel plancher.
US8016236B2 (en) * 2007-04-04 2011-09-13 The Boeing Company Method and apparatus for attaching a wing to a body
FR2915173B1 (fr) * 2007-04-17 2009-10-23 Airbus Sa Sa Dispositif de fixation d'un organe de sustentation au fuselage d'un avion.
US7887009B2 (en) * 2007-12-05 2011-02-15 The Boeing Company Methods and systems for attaching aircraft wings to fuselages
GB0803692D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Fitting for pivotally connecting aerodynamic control element to aircraft structure
US7975965B2 (en) * 2008-05-13 2011-07-12 The Boeing Company Wing tip joint in airfoils
CN100577512C (zh) * 2008-06-24 2010-01-06 北京航空航天大学 一种民用大型飞机机翼机身连接接头
GB0901228D0 (en) 2009-01-26 2009-03-11 Airbus Uk Ltd Aircraft joint
US8061655B1 (en) * 2009-03-25 2011-11-22 The Boeing Company Aircraft configuration utilizing fuselage, wing, empennage, and exhaust flow control devices
ES2378702B1 (es) * 2009-04-21 2013-02-28 Airbus Operations, S.L. Herrajes para la cogida del estabilizador vertical de cola de una aeronave.
FR2948099B1 (fr) * 2009-07-16 2012-05-11 Airbus Operations Sas Procede de fabrication d'un aeronef a voilure fixe
ES2372849B1 (es) * 2010-03-25 2012-12-13 Airbus Operations, S.L. Estructura de unión de cajones de torsión en una aeronave mediante un herraje triforme de materiales compuestos no metálicos.
DE102010013370B8 (de) * 2010-03-30 2013-12-12 Eads Deutschland Gmbh Wandbauteil für ein Luftfahrzeug
GB201009922D0 (en) * 2010-06-14 2010-07-21 Airbus Uk Ltd Aircraft wing box joint
US8333345B2 (en) * 2010-08-26 2012-12-18 The Boeing Company Composite aircraft joint
FR2970463B1 (fr) 2011-01-17 2013-02-15 Airbus Operations Sas Dispositif d'eclissage a tenue mecanique amelioree.
FR2970942B1 (fr) * 2011-01-28 2013-02-22 Airbus Operations Sas Raccordement des cadres de raidissage entre un fuselage d'aeronef et un caisson de voilure
FR2972997B1 (fr) * 2011-03-25 2013-05-10 Airbus Operations Sas Raccordement d'un fuselage a une voilure d'aeronef
US8777158B2 (en) * 2011-03-25 2014-07-15 The Boeing Company Joint sealing system
US9878772B2 (en) * 2012-01-10 2018-01-30 Gulfstream Aerospace Corporation Mounting assembly and method for mounting a sound-deadening body to a fuselage of an aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU225507U1 (ru) * 2024-01-10 2024-04-23 Акционерное общество "Термостойкие изделия и инженерные разработки" (АО "ТИИР") Фрикционная накладка

Also Published As

Publication number Publication date
CN104603007B (zh) 2016-08-10
JP2015533111A (ja) 2015-11-19
EP2909085A1 (en) 2015-08-26
WO2014062423A1 (en) 2014-04-24
US20140103162A1 (en) 2014-04-17
US8857765B2 (en) 2014-10-14
CN104603007A (zh) 2015-05-06
EP2909085B1 (en) 2018-08-29

Similar Documents

Publication Publication Date Title
JP6159409B2 (ja) 航空機胴体フレームをウィングボックスに取り付ける方法及び装置
US9889943B2 (en) Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon
US10272759B2 (en) Structural enhancements of an electric vehicle
US10112470B2 (en) Structural enhancements of an electric vehicle
EP2018316B1 (en) Floor structure for a fuselage
US9926017B1 (en) Structural enhancements of an electric vehicle
US8177166B2 (en) Tail structure for an aircraft or spacecraft
US9862497B2 (en) Assembly for an aircraft, comprising an engine attachment body partially produced in one piece with an internal stiffening rib of an attachment pylon box section
KR101972404B1 (ko) 회전익기용 일체형 선체를 지닌 서브플로어 구조물
US20180194211A1 (en) Structural enhancements of an electric vehicle
KR20150007202A (ko) 항공기의 복합재료 구조를 연결하기 위한 장치 및 방법
JP7280137B2 (ja) 胴体フレームを翼ボックスに取り付けるための方法および装置
CN102015442A (zh) 航空器地板组件的固定方法
US20170066518A1 (en) Aircraft rear portion comprising a vertical stabilizer having a box-section structure including a lower portion accommodated in the fuselage
US9180956B1 (en) Methods and apparatus for attaching an aircraft wing assembly to an aircraft body
US8894010B2 (en) Aircraft fuselage frame element
CN101472794A (zh) 飞行器机身组装原理
US10214091B2 (en) Underbody for the co-installation of an electric engine and a heat engine
US12162601B2 (en) Fittings for connecting structures
KR20240141356A (ko) 동체의 배터리 하중 지지구조
CN205203395U (zh) 一种开剖面行李舱支撑结构
CN118651400A (zh) 集成的门框单元

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20160516

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20160516

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20170223

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20170228

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20170330

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20170606

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20170609

R150 Certificate of patent or registration of utility model

Ref document number: 6159409

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250