ES2193644T3 - Actuador superfiial para deformar una estructura superficial elastica. - Google Patents

Actuador superfiial para deformar una estructura superficial elastica.

Info

Publication number
ES2193644T3
ES2193644T3 ES99120185T ES99120185T ES2193644T3 ES 2193644 T3 ES2193644 T3 ES 2193644T3 ES 99120185 T ES99120185 T ES 99120185T ES 99120185 T ES99120185 T ES 99120185T ES 2193644 T3 ES2193644 T3 ES 2193644T3
Authority
ES
Spain
Prior art keywords
surface structure
deform
actuator
elastic
actuator elements
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 - Lifetime
Application number
ES99120185T
Other languages
English (en)
Inventor
Lucio Flavio Dr Campanile
Markus Kleineberg
Ralf Keimer
Rainer Uckermann
Stefan Dr Seelecke
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
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 Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Application granted granted Critical
Publication of ES2193644T3 publication Critical patent/ES2193644T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts 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
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/06—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like
    • F03G7/061—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element
    • F03G7/0614—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using expansion or contraction of bodies due to heating, cooling, moistening, drying or the like characterised by the actuating element using shape memory elements
    • F03G7/06143—Wires
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C2003/148—Aerofoil profile comprising protuberances, e.g. for modifying boundary layer flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
  • Micromachines (AREA)

Abstract

Actuador superficial con una estructura superficial (1) elástica y anisótropa y varios elementos actuadores (2) formados por un material activable, alojados en la estructura superficial (1), para deformar la estructura superficial (1) en dirección normal respecto a la superficie de la estructura superficial (1), caracterizado porque entre los elementos actuadores (2), en los bordes laterales de la estructura superficial, se prevén ranuras en la dirección de acción de los elementos actuadores (2).
ES99120185T 1999-10-09 1999-10-09 Actuador superfiial para deformar una estructura superficial elastica. Expired - Lifetime ES2193644T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP99120185A EP1090835B1 (de) 1999-10-09 1999-10-09 Flächenaktuator zum Verformen einer federnden Flächenstruktur

Publications (1)

Publication Number Publication Date
ES2193644T3 true ES2193644T3 (es) 2003-11-01

Family

ID=8239172

Family Applications (1)

Application Number Title Priority Date Filing Date
ES99120185T Expired - Lifetime ES2193644T3 (es) 1999-10-09 1999-10-09 Actuador superfiial para deformar una estructura superficial elastica.

Country Status (3)

Country Link
EP (1) EP1090835B1 (es)
DE (1) DE59905478D1 (es)
ES (1) ES2193644T3 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10155119B4 (de) * 2001-11-09 2006-12-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aktuator
US6588709B1 (en) * 2002-03-20 2003-07-08 The Boeing Company Apparatus for variation of a wall skin
GB0312505D0 (en) * 2003-05-31 2003-07-09 Rolls Royce Plc Engine nozzle
DE102006037650B4 (de) 2006-02-09 2018-09-13 Otto Egelhof Gmbh & Co. Kg Linearbewegungsaktuator
DE102006040316B4 (de) 2006-08-29 2012-07-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Piezokeramischer Flächenaktuator und Verfahren zur Herstellung eines solchen
WO2009006318A1 (en) 2007-06-29 2009-01-08 Artificial Muscle, Inc. Electroactive polymer transducers for sensory feedback applications
EP2239793A1 (de) 2009-04-11 2010-10-13 Bayer MaterialScience AG Elektrisch schaltbarer Polymerfilmaufbau und dessen Verwendung
WO2012118916A2 (en) 2011-03-01 2012-09-07 Bayer Materialscience Ag Automated manufacturing processes for producing deformable polymer devices and films
TW201250288A (en) 2011-03-22 2012-12-16 Bayer Materialscience Ag Electroactive polymer actuator lenticular system
WO2013142552A1 (en) 2012-03-21 2013-09-26 Bayer Materialscience Ag Roll-to-roll manufacturing processes for producing self-healing electroactive polymer devices
KR20150031285A (ko) 2012-06-18 2015-03-23 바이엘 인텔렉쳐 프로퍼티 게엠베하 연신 공정을 위한 연신 프레임
US9590193B2 (en) 2012-10-24 2017-03-07 Parker-Hannifin Corporation Polymer diode
CN103171757B (zh) * 2013-04-13 2015-07-29 哈尔滨工业大学 一种运用压电纤维复合材料的自适应后缘驱动装置
DE102015016436A1 (de) * 2015-12-17 2017-06-22 Diehl Defence Gmbh & Co. Kg Flugkörper

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5367970A (en) * 1993-09-27 1994-11-29 The United States Of America As Represented By The Secretary Of The Navy Controllable camber fin
US5662294A (en) * 1994-02-28 1997-09-02 Lockheed Martin Corporation Adaptive control surface using antagonistic shape memory alloy tendons
US5700337A (en) * 1996-03-01 1997-12-23 Mcdonnell Douglas Corporation Fabrication method for composite structure adapted for controlled structural deformation
US5931422A (en) * 1997-06-09 1999-08-03 Mcdonnell Douglas Active reinforced elastomer system
DE19742314C2 (de) * 1997-09-25 2000-06-21 Daimler Chrysler Ag Tragende Struktur
DE19804308C2 (de) * 1997-09-30 2003-10-30 Deutsch Zentr Luft & Raumfahrt Profil

Also Published As

Publication number Publication date
EP1090835B1 (de) 2003-05-07
EP1090835A1 (de) 2001-04-11
DE59905478D1 (de) 2003-06-12

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