JP6039175B2 - 多機能頂部を用いる胴体とその作製方法 - Google Patents

多機能頂部を用いる胴体とその作製方法 Download PDF

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Publication number
JP6039175B2
JP6039175B2 JP2011245427A JP2011245427A JP6039175B2 JP 6039175 B2 JP6039175 B2 JP 6039175B2 JP 2011245427 A JP2011245427 A JP 2011245427A JP 2011245427 A JP2011245427 A JP 2011245427A JP 6039175 B2 JP6039175 B2 JP 6039175B2
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Japan
Prior art keywords
fuselage
composite
skin
duct
aircraft
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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.)
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Application number
JP2011245427A
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English (en)
Japanese (ja)
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JP2012101787A (ja
JP2012101787A5 (enExample
Inventor
ハーラン グリース ケニース
ハーラン グリース ケニース
イー． ジョージソン ゲアリー
イー． ジョージソン ゲアリー
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Boeing Co
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Boeing Co
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Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of JP2012101787A publication Critical patent/JP2012101787A/ja
Publication of JP2012101787A5 publication Critical patent/JP2012101787A5/ja
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • 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
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • 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
    • 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

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Tents Or Canopies (AREA)
JP2011245427A 2010-11-11 2011-11-09 多機能頂部を用いる胴体とその作製方法 Active JP6039175B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/944,113 2010-11-11
US12/944,113 US8752791B2 (en) 2010-11-11 2010-11-11 Fuselage employing multifunctional crown and method of making the same

Publications (3)

Publication Number Publication Date
JP2012101787A JP2012101787A (ja) 2012-05-31
JP2012101787A5 JP2012101787A5 (enExample) 2014-11-27
JP6039175B2 true JP6039175B2 (ja) 2016-12-07

Family

ID=44905700

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011245427A Active JP6039175B2 (ja) 2010-11-11 2011-11-09 多機能頂部を用いる胴体とその作製方法

Country Status (4)

Country Link
US (1) US8752791B2 (enExample)
EP (1) EP2452872B1 (enExample)
JP (1) JP6039175B2 (enExample)
CN (1) CN102530234B (enExample)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007050422B4 (de) * 2007-10-22 2012-03-08 Airbus Operations Gmbh Flugzeugkomponentenmontagesystem
USD732459S1 (en) * 2013-05-21 2015-06-23 Airbus Corporate Jet Centre Aircraft cabin
EP2979975B1 (en) * 2014-07-30 2017-09-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An aircraft with a framework structure that comprises at least one hollow frame.
CA2979158A1 (en) * 2015-03-23 2016-09-29 Bombardier Inc. Simulation of loads on aerostructures during aircraft assembly
WO2018061281A1 (ja) 2016-09-29 2018-04-05 株式会社Ｓｕｂａｒｕ 複合材構造体及び複合材構造体の製造方法
CN106596003B (zh) * 2016-11-29 2019-04-23 中国航空工业集团公司沈阳飞机设计研究所 一种复合材料飞机机身段充压试验方法
DE102017112594A1 (de) * 2017-06-08 2018-12-13 Airbus Operations Gmbh Luftverteilungssystem für eine Flugzeugkabine
US11220353B2 (en) * 2019-04-18 2022-01-11 The Boeing Company Method of fabricating a composite structure
US11866200B2 (en) * 2020-11-18 2024-01-09 The Boeing Company Pulsed line fabrication for a fuselage using work stations
US11872780B2 (en) 2022-06-02 2024-01-16 The Boeing Company Methods and tool for cutting an uncured composite material
DE102022133280A1 (de) * 2022-12-14 2024-06-20 Airbus Operations Gmbh Bauteil mit Hohlleiter, Datenübertragungssystem und Luftfahrzeug

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04329125A (ja) * 1991-04-30 1992-11-17 Mitsubishi Heavy Ind Ltd 複合材料一体成形方法
JPH1016085A (ja) * 1996-07-04 1998-01-20 Mitsubishi Heavy Ind Ltd 航空機の胴体外板の製造方法
JP4318381B2 (ja) * 2000-04-27 2009-08-19 本田技研工業株式会社 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体
DE10154063B4 (de) * 2001-11-02 2013-11-28 Airbus Operations Gmbh Doppelwandiger Kernverbund, vorzugsweise Faserverbund
US7380752B2 (en) * 2003-10-17 2008-06-03 The Boeing Company Aircraft interior architecture
US7252267B2 (en) 2003-10-17 2007-08-07 The Boeing Company Aircraft archway architecture
US7228611B2 (en) * 2003-11-18 2007-06-12 The Boeing Company Method of transferring large uncured composite laminates
US7166251B2 (en) * 2004-12-01 2007-01-23 The Boeing Company Segmented flexible barrel lay-up mandrel
USD539210S1 (en) 2005-04-28 2007-03-27 The Boeing Company Modular archway for an aircraft
JP4800672B2 (ja) * 2005-06-09 2011-10-26 株式会社竹中工務店 経路構造
DE102005043898A1 (de) * 2005-09-14 2007-03-22 Airbus Deutschland Gmbh Fenster-Anordnung zum Einrichten größerer Flugzeugfenster
US9359061B2 (en) * 2005-10-31 2016-06-07 The Boeing Company Compliant stiffener for aircraft fuselage
DE102005054869A1 (de) * 2005-11-17 2007-05-31 Airbus Deutschland Gmbh Verfahren zur Herstellung einer Rumpfzelle eines Luftfahrzeugs
DE102006002248B4 (de) * 2006-01-17 2008-01-03 Airbus Deutschland Gmbh Strukturgebende Konstruktion für einen Flugzeugrumpf
JP2008028549A (ja) * 2006-07-19 2008-02-07 Taisei Corp 通信波搬送導波管
DE102006039292B4 (de) * 2006-08-22 2010-07-22 Airbus Deutschland Gmbh Rahmenelement, Flugzeugklimatisierungssystem sowie Verfahren zur Montage eines Rahmenelements in einem Flugzeug
US7735779B2 (en) * 2006-11-02 2010-06-15 The Boeing Company Optimized fuselage structure
US7861970B2 (en) 2006-11-02 2011-01-04 The Boeing Company Fuselage structure including an integrated fuselage stanchion
DE102007003277B4 (de) * 2007-01-23 2012-08-02 Airbus Operations Gmbh Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen
DE102007049926A1 (de) * 2007-10-18 2009-04-23 Airbus Deutschland Gmbh System und Verfahren zur Klimatisierung zumindest eines Teilbereichs eines Flugzeugs
US7879276B2 (en) * 2007-11-08 2011-02-01 The Boeing Company Foam stiffened hollow composite stringer
US8040243B2 (en) 2008-11-18 2011-10-18 The Boeing Company RFID-based corrosion and moisture detection
US8421692B2 (en) * 2009-02-25 2013-04-16 The Boeing Company Transmitting power and data
US8500066B2 (en) * 2009-06-12 2013-08-06 The Boeing Company Method and apparatus for wireless aircraft communications and power system using fuselage stringers
US8570152B2 (en) * 2009-07-23 2013-10-29 The Boeing Company Method and apparatus for wireless sensing with power harvesting of a wireless signal

Also Published As

Publication number Publication date
EP2452872A3 (en) 2017-10-04
CN102530234A (zh) 2012-07-04
CN102530234B (zh) 2015-04-29
JP2012101787A (ja) 2012-05-31
US8752791B2 (en) 2014-06-17
US20120119028A1 (en) 2012-05-17
EP2452872A2 (en) 2012-05-16
EP2452872B1 (en) 2019-08-28

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