CN100410144C - 直升机叶轮整流装置以及制造该装置的方法和设备 - Google Patents

直升机叶轮整流装置以及制造该装置的方法和设备 Download PDF

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Publication number
CN100410144C
CN100410144C CNB2005101320192A CN200510132019A CN100410144C CN 100410144 C CN100410144 C CN 100410144C CN B2005101320192 A CNB2005101320192 A CN B2005101320192A CN 200510132019 A CN200510132019 A CN 200510132019A CN 100410144 C CN100410144 C CN 100410144C
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CN
China
Prior art keywords
preformed
preformed part
sidewall
mould
core
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
CNB2005101320192A
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English (en)
Chinese (zh)
Other versions
CN1810577A (zh
Inventor
L·马耶
L·穆顿
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.)
Kong Kezhishengji
Original Assignee
Eurocopter SA
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 Eurocopter SA filed Critical Eurocopter SA
Publication of CN1810577A publication Critical patent/CN1810577A/zh
Application granted granted Critical
Publication of CN100410144C publication Critical patent/CN100410144C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • 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
    • B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • 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
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
    • B29C33/485—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling cores or mandrels
    • 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
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • 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
    • B29L2031/3088—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8254—Shrouded tail rotors, e.g. "Fenestron" fans
    • 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
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • 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
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Landscapes

  • 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)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
CNB2005101320192A 2004-12-16 2005-12-16 直升机叶轮整流装置以及制造该装置的方法和设备 Expired - Fee Related CN100410144C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0413397 2004-12-16
FR0413397A FR2879496B1 (fr) 2004-12-16 2004-12-16 Procede et dispositif de fabrication d'une carene de rotor d'helicoptere, et carene obtenue

Publications (2)

Publication Number Publication Date
CN1810577A CN1810577A (zh) 2006-08-02
CN100410144C true CN100410144C (zh) 2008-08-13

Family

ID=34951807

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2005101320192A Expired - Fee Related CN100410144C (zh) 2004-12-16 2005-12-16 直升机叶轮整流装置以及制造该装置的方法和设备

Country Status (5)

Country Link
US (1) US7676923B2 (enExample)
EP (1) EP1676775B1 (enExample)
JP (1) JP4236661B2 (enExample)
CN (1) CN100410144C (enExample)
FR (1) FR2879496B1 (enExample)

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FR2924378B1 (fr) * 2007-03-29 2010-01-01 Carbone Forge Procede de fabrication par moulage d'une piece composite thermoplastique.
DE102007015909A1 (de) * 2007-04-02 2008-10-09 Mt Aerospace Ag Verfahren zur Herstellung faserverstärkter Hohlkörper
GB2470087B (en) * 2007-06-07 2010-12-29 Gkn Aerospace Services Ltd Mandrel for use in a method of making composite flange
US8936695B2 (en) * 2007-07-28 2015-01-20 The Boeing Company Method for forming and applying composite layups having complex geometries
US20100279806A1 (en) * 2008-01-03 2010-11-04 Aling Lai Transmission structure improvement for bending tail pipe
CN102019592B (zh) * 2009-09-10 2012-07-04 中国航空工业集团公司北京航空制造工程研究所 一种大尺寸复合材料加筋壁板成形的定位装置
CN101791821B (zh) * 2010-04-08 2011-09-14 中国航空工业集团公司北京航空制造工程研究所 一种大尺寸复合材料长桁的成形装置
US8931731B2 (en) * 2010-11-02 2015-01-13 Groen Brothers Aviation, Inc. Tail jet apparatus and method for low speed yaw control of a rotorcraft
FR2968272B1 (fr) * 2010-12-06 2013-07-12 Eurocopter France Element de structure ameliore d'un giravion pour diminuer la trainee aerodynamique.
ITRM20110626A1 (it) * 2011-11-25 2013-05-26 Aeronautical Service S R L Metodo per la realizzazione di supporti di sostegno per l'avionica.
EP2706009B1 (en) 2012-09-07 2016-04-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An empennage of a helicopter
US9889613B2 (en) 2012-11-01 2018-02-13 Israel Aerospace Industries Ltd. Manufacture of integrated structures formed of composite materials
US8983171B2 (en) 2012-12-26 2015-03-17 Israel Aerospace Industries Ltd. System and method for inspecting structures formed of composite materials during the fabrication thereof
EP2878433B1 (en) * 2013-11-29 2016-04-20 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Shrouded rotary assembly from segmented composite for aircraft and method for its manufacture
EP3061689B1 (en) * 2015-02-27 2017-09-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly
EP3199455B1 (en) * 2016-01-29 2020-04-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotary aircraft with an interface frame joining the fuselage tail boom and the tail cone
US10814971B2 (en) * 2018-04-10 2020-10-27 Textron Innovations Inc. Tail rotor housing
CN109130247B (zh) * 2018-07-20 2021-02-26 菲舍尔航空部件（镇江）有限公司 航空复材c型盒体零件成型方法
KR102215966B1 (ko) * 2019-08-21 2021-02-16 한국항공우주산업 주식회사 헬리콥터용 에프터 콘 핀 제조 장치
GB202020714D0 (en) * 2020-12-30 2021-02-10 Gen Electric Method of joining blade segments using an internal bladder
US20220315212A1 (en) * 2021-04-06 2022-10-06 Bell Textron Inc. Distributed propulsion structure
CN113977984B (zh) * 2021-10-15 2023-07-04 江西洪都航空工业集团有限责任公司 一种管状双曲面复合材料结构件的制备方法
CN115723949B (zh) * 2022-12-09 2025-08-19 哈尔滨飞机工业集团有限责任公司 一种高置涵道式尾部结构及其成型方法
US12097975B1 (en) * 2023-04-26 2024-09-24 James P Gross Tail boom support stand assembly
CN117140995B (zh) * 2023-08-23 2025-06-27 江苏新扬新材料股份有限公司 一种聚酰亚胺复合材料机尾罩的成型方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2556650A1 (fr) * 1983-12-14 1985-06-21 Matra Procede et dispositif de fabrication de corps structural creux en materiau composite, notamment pour missiles
US5158733A (en) * 1986-05-12 1992-10-27 Trimble Brent J Method of making composite cycle frame components
US5251847A (en) * 1991-11-07 1993-10-12 Aerospatiale Societe Nationale Industrielle Tail rotor anti-torque system for a helicopter
US5498129A (en) * 1994-05-04 1996-03-12 Eurocopter France Counter-torque device with ducted tail rotor and ducted flow-straightening stator, for helicopters

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FR2542695B1 (fr) * 1983-03-18 1985-07-26 Aerospatiale Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees
US4594761A (en) * 1984-02-13 1986-06-17 General Electric Company Method of fabricating hollow composite airfoils
FR2699498B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication.
WO1996009159A1 (en) * 1994-09-20 1996-03-28 Viatech, Inc. Method of making internally reinforced composite tubes
FR2740378B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere, et pale a pas variable pouvant etre obtenue par un tel procede
FR2740380B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere
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
US6372176B1 (en) * 1999-03-01 2002-04-16 Kiefel Technologies Inc. System and method for twin sheet forming
US6889937B2 (en) * 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
DE10153875A1 (de) * 2001-11-02 2003-05-15 Bpw Bergische Achsen Kg Bauteil in langgestreckter Bauweise aus einem Faser-Kunststoff-Verbund
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
EP1473131A3 (de) * 2003-04-30 2007-01-03 Airbus Deutschland GmbH Verfahren zum herstellen textiler vorformlinge aus textilen halbzeugen

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2556650A1 (fr) * 1983-12-14 1985-06-21 Matra Procede et dispositif de fabrication de corps structural creux en materiau composite, notamment pour missiles
US5158733A (en) * 1986-05-12 1992-10-27 Trimble Brent J Method of making composite cycle frame components
US5251847A (en) * 1991-11-07 1993-10-12 Aerospatiale Societe Nationale Industrielle Tail rotor anti-torque system for a helicopter
US5498129A (en) * 1994-05-04 1996-03-12 Eurocopter France Counter-torque device with ducted tail rotor and ducted flow-straightening stator, for helicopters

Also Published As

Publication number Publication date
EP1676775B1 (fr) 2015-11-18
CN1810577A (zh) 2006-08-02
US7676923B2 (en) 2010-03-16
JP2006168718A (ja) 2006-06-29
US20060169835A1 (en) 2006-08-03
FR2879496A1 (fr) 2006-06-23
FR2879496B1 (fr) 2008-12-12
JP4236661B2 (ja) 2009-03-11
EP1676775A1 (fr) 2006-07-05

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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
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP01 Change in the name or title of a patent holder

Address after: France Marignane

Patentee after: Kong Kezhishengji

Address before: France Marignane

Patentee before: Eurocopter

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: 20080813

Termination date: 20211216