CN101365579A - 制造复合材料飞行器机身的方法 - Google Patents
制造复合材料飞行器机身的方法 Download PDFInfo
- Publication number
- CN101365579A CN101365579A CNA2006800476609A CN200680047660A CN101365579A CN 101365579 A CN101365579 A CN 101365579A CN A2006800476609 A CNA2006800476609 A CN A2006800476609A CN 200680047660 A CN200680047660 A CN 200680047660A CN 101365579 A CN101365579 A CN 101365579A
- Authority
- CN
- China
- Prior art keywords
- inner frame
- tool housing
- shell
- framework
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 47
- 239000002131 composite material Substances 0.000 title claims abstract description 22
- 238000010276 construction Methods 0.000 claims description 27
- 239000007787 solid Substances 0.000 claims description 26
- 239000000463 material Substances 0.000 claims description 15
- 239000000835 fiber Substances 0.000 claims description 9
- 239000011347 resin Substances 0.000 claims description 7
- 229920005989 resin Polymers 0.000 claims description 7
- 238000009434 installation Methods 0.000 claims description 6
- 239000000853 adhesive Substances 0.000 claims description 3
- 230000001070 adhesive effect Effects 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 16
- 239000004744 fabric Substances 0.000 description 13
- 239000002184 metal Substances 0.000 description 7
- 230000000694 effects Effects 0.000 description 5
- 238000006116 polymerization reaction Methods 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000008719 thickening Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 241001074085 Scophthalmus aquosus Species 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000002344 fibroplastic effect Effects 0.000 description 1
- 238000009432 framing Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Images
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
- B29C70/32—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 on a rotating mould, former or core
-
- 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
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
-
- 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
- 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
- B64C1/068—Fuselage sections
- B64C1/0683—Nose cones
-
- 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
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Reduction Rolling/Reduction Stand/Operation Of Reduction Machine (AREA)
- Rolls And Other Rotary Bodies (AREA)
Abstract
Description
Claims (16)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0553972A FR2894869B1 (fr) | 2005-12-20 | 2005-12-20 | Procede de fabrication d'un fuselage d'aeronef en materiau composite |
FR0553972 | 2005-12-20 | ||
PCT/FR2006/051385 WO2007071879A2 (fr) | 2005-12-20 | 2006-12-19 | Procede de fabrication d'un fuselage d'aeronef en materiau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101365579A true CN101365579A (zh) | 2009-02-11 |
CN101365579B CN101365579B (zh) | 2012-05-02 |
Family
ID=37074135
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2006800476609A Expired - Fee Related CN101365579B (zh) | 2005-12-20 | 2006-12-19 | 制造复合材料飞行器机身的方法 |
Country Status (11)
Country | Link |
---|---|
US (1) | US8220154B2 (zh) |
EP (1) | EP1963079B1 (zh) |
JP (1) | JP5222151B2 (zh) |
CN (1) | CN101365579B (zh) |
AT (1) | ATE484376T1 (zh) |
BR (1) | BRPI0620206A2 (zh) |
CA (1) | CA2632913C (zh) |
DE (1) | DE602006017584D1 (zh) |
FR (1) | FR2894869B1 (zh) |
RU (1) | RU2412859C2 (zh) |
WO (1) | WO2007071879A2 (zh) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102596547A (zh) * | 2009-10-01 | 2012-07-18 | 空中客车运营简化股份公司 | 用于自动生产干纤维预成型件的方法及设备 |
CN102666052A (zh) * | 2009-12-18 | 2012-09-12 | 空中客车德国运营有限责任公司 | 用于制造用于飞行器的由纤维复合材料制成的机身壳体的装置 |
CN102686381A (zh) * | 2009-12-07 | 2012-09-19 | 空中客车德国运营有限责任公司 | 用于制造用于飞行器的由纤维复合材料制成的机身外壳的装置和方法 |
CN103221200A (zh) * | 2010-11-19 | 2013-07-24 | 西姆佩尔坎普机械设备制造有限责任公司和两合公司 | 制造圆柱形大型结构的方法和设备 |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
DE102006026170B4 (de) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
FR2921295A1 (fr) | 2007-09-24 | 2009-03-27 | Airbus France Sas | Dispositif pour la fabrication d'une piece en materiau composite integrant un systeme de drainage |
FR2921898B1 (fr) * | 2007-10-08 | 2009-12-11 | Airbus France | Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage |
FR2927013B1 (fr) | 2008-01-31 | 2010-02-19 | Airbus France | Dispositif pour la fabrication d'une piece en materiau composite comprenant des toles de lissage a jonctions glissantes et procede de fabrication de toles de lissage a jonctions glissantes |
ES2357489B1 (es) * | 2008-05-19 | 2012-03-05 | Airbus Operations, S.L. | Procedimiento y útil de montaje de cajones de torsión para uso aeron�?utico. |
FR2946024B1 (fr) * | 2009-05-27 | 2011-07-22 | Airbus France | Installation de realisation d'un troncon de fuselage d'aeronef. |
FR2952579B1 (fr) | 2009-11-17 | 2013-05-17 | Airbus Operations Sas | Machine pour le drapage de pieces composites cylindriques |
US8585856B1 (en) | 2010-05-13 | 2013-11-19 | Textron Innovations Inc. | Process for fabricating aircraft parts using an integrated form |
EP3141380A1 (de) | 2010-12-22 | 2017-03-15 | MAGNA STEYR Fahrzeugtechnik AG & Co KG | Fahrgastzelle mit einer hohlen positivform und einer aussenhülle aus faserverstärktem kunststoff und deren herstellung |
US8776375B2 (en) * | 2011-05-19 | 2014-07-15 | The Boeing Company | Aircraft structure for high capacity pull off |
GB201116476D0 (en) * | 2011-09-26 | 2011-11-09 | Rolls Royce Plc | Mandrel for forming a component |
US9302455B1 (en) | 2012-02-08 | 2016-04-05 | Textron Innovations, Inc. | Fast cure process |
US9545757B1 (en) | 2012-02-08 | 2017-01-17 | Textron Innovations, Inc. | Composite lay up and method of forming |
US9051062B1 (en) | 2012-02-08 | 2015-06-09 | Textron Innovations, Inc. | Assembly using skeleton structure |
US9649820B1 (en) | 2012-02-08 | 2017-05-16 | Textron Innovations, Inc. | Assembly using skeleton structure |
US9050757B1 (en) | 2012-02-08 | 2015-06-09 | Textron Innovations, Inc. | System and method for curing composites |
US10265915B2 (en) | 2014-01-17 | 2019-04-23 | Sikorsky Aircraft Corporation | Composite bonded repair method |
US10112713B2 (en) * | 2015-06-26 | 2018-10-30 | Nelson Tyler | Back mounted flight machine |
US10005267B1 (en) | 2015-09-22 | 2018-06-26 | Textron Innovations, Inc. | Formation of complex composite structures using laminate templates |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3341564A1 (de) | 1983-11-17 | 1985-05-30 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung |
JPS61169394A (ja) * | 1985-01-21 | 1986-07-31 | 日立造船株式会社 | 飛行機の胴体成形方法 |
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 |
FR2766407B1 (fr) * | 1997-07-22 | 1999-10-15 | Aerospatiale | Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs |
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 |
-
2005
- 2005-12-20 FR FR0553972A patent/FR2894869B1/fr not_active Expired - Fee Related
-
2006
- 2006-12-19 CA CA2632913A patent/CA2632913C/fr not_active Expired - Fee Related
- 2006-12-19 DE DE602006017584T patent/DE602006017584D1/de active Active
- 2006-12-19 RU RU2008129665/11A patent/RU2412859C2/ru not_active IP Right Cessation
- 2006-12-19 JP JP2008546552A patent/JP5222151B2/ja not_active Expired - Fee Related
- 2006-12-19 WO PCT/FR2006/051385 patent/WO2007071879A2/fr active Application Filing
- 2006-12-19 BR BRPI0620206-3A patent/BRPI0620206A2/pt not_active IP Right Cessation
- 2006-12-19 AT AT06847175T patent/ATE484376T1/de not_active IP Right Cessation
- 2006-12-19 CN CN2006800476609A patent/CN101365579B/zh not_active Expired - Fee Related
- 2006-12-19 US US12/158,214 patent/US8220154B2/en active Active
- 2006-12-19 EP EP06847175A patent/EP1963079B1/fr not_active Not-in-force
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102596547A (zh) * | 2009-10-01 | 2012-07-18 | 空中客车运营简化股份公司 | 用于自动生产干纤维预成型件的方法及设备 |
CN102596547B (zh) * | 2009-10-01 | 2014-12-03 | 空中客车运营简化股份公司 | 用于自动生产干纤维预成型件的方法及设备 |
CN102686381A (zh) * | 2009-12-07 | 2012-09-19 | 空中客车德国运营有限责任公司 | 用于制造用于飞行器的由纤维复合材料制成的机身外壳的装置和方法 |
CN102666052A (zh) * | 2009-12-18 | 2012-09-12 | 空中客车德国运营有限责任公司 | 用于制造用于飞行器的由纤维复合材料制成的机身壳体的装置 |
US8746315B2 (en) | 2009-12-18 | 2014-06-10 | Airbus Operations Gmbh | Apparatus for the production of an aircraft fuselage shell consisting of a fibre composite |
CN102666052B (zh) * | 2009-12-18 | 2014-10-01 | 空中客车德国运营有限责任公司 | 用于制造用于飞行器的由纤维复合材料制成的机身壳体的装置 |
CN103221200A (zh) * | 2010-11-19 | 2013-07-24 | 西姆佩尔坎普机械设备制造有限责任公司和两合公司 | 制造圆柱形大型结构的方法和设备 |
CN103221200B (zh) * | 2010-11-19 | 2015-07-15 | 辛北尔康普机器及成套设备有限责任公司 | 制造圆柱形大型结构的方法和设备 |
Also Published As
Publication number | Publication date |
---|---|
FR2894869A1 (fr) | 2007-06-22 |
BRPI0620206A2 (pt) | 2011-11-01 |
CA2632913A1 (fr) | 2007-06-28 |
JP2009519860A (ja) | 2009-05-21 |
RU2008129665A (ru) | 2010-01-27 |
JP5222151B2 (ja) | 2013-06-26 |
DE602006017584D1 (de) | 2010-11-25 |
EP1963079A2 (fr) | 2008-09-03 |
RU2412859C2 (ru) | 2011-02-27 |
ATE484376T1 (de) | 2010-10-15 |
US20090020645A1 (en) | 2009-01-22 |
CN101365579B (zh) | 2012-05-02 |
FR2894869B1 (fr) | 2009-10-09 |
US8220154B2 (en) | 2012-07-17 |
CA2632913C (fr) | 2015-05-05 |
WO2007071879A2 (fr) | 2007-06-28 |
WO2007071879A3 (fr) | 2007-08-23 |
EP1963079B1 (fr) | 2010-10-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C53 | Correction of patent of invention or patent application | ||
CB02 | Change of applicant information |
Address after: France Toulouse Applicant after: Airbus Operations S.A.S. Address before: France Toulouse Applicant before: Airbus France Address after: France Toulouse Applicant after: Airbus France Address before: France Toulouse Applicant before: Airbus France |
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COR | Change of bibliographic data |
Free format text: CORRECT: APPLICANT; FROM: AIRBUS FRANCE TO: AIRBUS OPERATIONS S.A.S. |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120502 Termination date: 20201219 |