DE602007007454D1 - Kontinuierlich und kontrolliert verformt werden kann - Google Patents

Kontinuierlich und kontrolliert verformt werden kann

Info

Publication number
DE602007007454D1
DE602007007454D1 DE602007007454T DE602007007454T DE602007007454D1 DE 602007007454 D1 DE602007007454 D1 DE 602007007454D1 DE 602007007454 T DE602007007454 T DE 602007007454T DE 602007007454 T DE602007007454 T DE 602007007454T DE 602007007454 D1 DE602007007454 D1 DE 602007007454D1
Authority
DE
Germany
Prior art keywords
deformed
profile
controlled
envelope
continuous
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
DE602007007454T
Other languages
English (en)
Inventor
Georges Meyer
Fabrice Laurent
Cedric Maupoint
Herve Drobez
Hostis Gildas L
Bernard Durand
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.)
CETIM CERMAT ASS
Original Assignee
CETIM CERMAT ASS
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 CETIM CERMAT ASS filed Critical CETIM CERMAT ASS
Publication of DE602007007454D1 publication Critical patent/DE602007007454D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16—Blades
    • B64C11/20—Constructional features
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/148—Blades with variable camber, e.g. by ejection of fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06—Rotors
    • F03D1/065—Rotors characterised by their construction elements
    • F03D1/0675—Rotors characterised by their construction elements of the blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/31—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape
    • F05B2240/311—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape flexible or elastic
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Prostheses (AREA)
  • Laminated Bodies (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Moulding By Coating Moulds (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Control Of El Displays (AREA)
  • Braking Arrangements (AREA)
DE602007007454T 2006-03-27 2007-03-01 Kontinuierlich und kontrolliert verformt werden kann Active DE602007007454D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0651048A FR2898865B1 (fr) 2006-03-27 2006-03-27 Profil aerodynamique ou hydrodynamique pouvant etre deforme de maniere continue et controlee
PCT/FR2007/050866 WO2007110518A1 (fr) 2006-03-27 2007-03-01 Profil aerodynamique ou hydrodynamique pouvant être deforme de maniere continue et controlee

Publications (1)

Publication Number Publication Date
DE602007007454D1 true DE602007007454D1 (de) 2010-08-12

Family

ID=37460436

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007007454T Active DE602007007454D1 (de) 2006-03-27 2007-03-01 Kontinuierlich und kontrolliert verformt werden kann

Country Status (14)

Country Link
US (1) US20100051752A1 (de)
EP (1) EP2001739B1 (de)
JP (1) JP2009531222A (de)
CN (1) CN101410293A (de)
AT (1) ATE472471T1 (de)
AU (1) AU2007231272A1 (de)
BR (1) BRPI0710228A2 (de)
CA (1) CA2647164A1 (de)
DE (1) DE602007007454D1 (de)
FR (1) FR2898865B1 (de)
MA (1) MA30334B1 (de)
TN (1) TNSN08368A1 (de)
WO (1) WO2007110518A1 (de)
ZA (1) ZA200809193B (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8454318B2 (en) 2006-12-15 2013-06-04 Bladena Aps Reinforced aerodynamic profile
ES2496167T3 (es) 2007-01-16 2014-09-18 Bladena Aps Pala reforzada para aerogenerador
DK2108083T3 (da) 2007-01-25 2013-02-04 Bladena Aps Forstærket vindmøllevinge
ES2383061T3 (es) 2008-06-24 2012-06-18 Bladena Aps Paleta de turnina eólica reforzada
WO2010000263A2 (en) * 2008-07-01 2010-01-07 Danmarks Tekniske Universitet A reinforced blade for a wind turbine
GB2467945B (en) * 2009-02-20 2014-03-05 Westland Helicopters Device which is subject to fluid flow
EP2330294B1 (de) 2009-12-02 2013-01-16 Bladena ApS Verstärkter, flügelförmiger Körper
EP2526287B1 (de) * 2010-01-21 2016-07-06 Vestas Wind Systems A/S Windturbinenrotorblatt mit knickaustrittskante
CN112550663B (zh) * 2020-12-08 2022-11-11 中国空气动力研究与发展中心设备设计及测试技术研究所 一种基于智能驱动装置的变形机翼
CN115675832B (zh) * 2022-12-27 2023-03-17 成都航空职业技术学院 一种多段式空间四边形机翼骨架及仿生飞行器

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3893639A (en) * 1973-08-22 1975-07-08 Jr Thomas L Croswell Airplane wing camber control
JP2605696B2 (ja) * 1986-09-14 1997-04-30 株式会社島津製作所 誘導飛翔体の操舵装置
US5150864A (en) * 1991-09-20 1992-09-29 Georgia Tech Research Corporation Variable camber control of airfoil
US5367970A (en) * 1993-09-27 1994-11-29 The United States Of America As Represented By The Secretary Of The Navy Controllable camber fin
DE19707392A1 (de) * 1997-02-25 1998-08-27 Deutsch Zentr Luft & Raumfahrt Aerodynamisches Bauteil, wie Landeklappe, Tragflügel, Höhen- oder Seitenleitwerk, mit veränderbarer Wölbung
DE19742314C2 (de) * 1997-09-25 2000-06-21 Daimler Chrysler Ag Tragende Struktur
DE69916360T3 (de) 1998-05-21 2008-06-05 Mcdonnell Douglas Corp. Flügelprofil
DE29817162U1 (de) * 1998-09-24 1999-01-07 Homann, Werner M., Dipl.-Ing. (FH), 82449 Uffing Einrichtung bei einem Tragflügel eines Luftfahrzeuges zur Veränderung der Flügelform
DE19852944C1 (de) * 1998-11-17 2000-02-10 Daimler Chrysler Ag Adaptiver Strömungskörper
JP3609770B2 (ja) * 2001-09-27 2005-01-12 株式会社東芝 揺動アクチュエータ装置
DE10304530B4 (de) 2003-02-04 2005-09-15 Eads Deutschland Gmbh Verformbares aerodynamisches Profil
US7059664B2 (en) * 2003-12-04 2006-06-13 General Motors Corporation Airflow control devices based on active materials
FR2867102B1 (fr) * 2004-03-02 2006-06-23 Cetim Cermat Materiau composite a deformation continue et controlee
JP4568906B2 (ja) * 2004-12-16 2010-10-27 独立行政法人 宇宙航空研究開発機構 飛行体用翼、飛行体用翼複合材およびその製造方法

Also Published As

Publication number Publication date
EP2001739A1 (de) 2008-12-17
ZA200809193B (en) 2009-06-24
JP2009531222A (ja) 2009-09-03
CN101410293A (zh) 2009-04-15
CA2647164A1 (fr) 2007-10-04
WO2007110518A1 (fr) 2007-10-04
EP2001739B1 (de) 2010-06-30
MA30334B1 (fr) 2009-04-01
BRPI0710228A2 (pt) 2011-08-02
ATE472471T1 (de) 2010-07-15
TNSN08368A1 (fr) 2009-12-29
FR2898865B1 (fr) 2008-05-30
FR2898865A1 (fr) 2007-09-28
AU2007231272A1 (en) 2007-10-04
US20100051752A1 (en) 2010-03-04

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