JP5694143B2 - 超弾性発泡材料を有する形状変化構造 - Google Patents

超弾性発泡材料を有する形状変化構造 Download PDF

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Publication number
JP5694143B2
JP5694143B2 JP2011509525A JP2011509525A JP5694143B2 JP 5694143 B2 JP5694143 B2 JP 5694143B2 JP 2011509525 A JP2011509525 A JP 2011509525A JP 2011509525 A JP2011509525 A JP 2011509525A JP 5694143 B2 JP5694143 B2 JP 5694143B2
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JP
Japan
Prior art keywords
shape
metal foam
structural member
superelastic metal
changing
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English (en)
Japanese (ja)
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JP2011520688A5 (enExample
JP2011520688A (ja
Inventor
サー、デイビッド・アール．
サンダーソン、テリー・エム．
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Raytheon Co
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Raytheon Co
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Publication of JP2011520688A5 publication Critical patent/JP2011520688A5/ja
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/54—Varying in area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/40—Varying angle of sweep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/18—Stabilising surfaces adjustable in area
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/006—Resulting in heat recoverable alloys with a memory effect
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
    • 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
    • Y02T50/10—Drag 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12326—All metal or with adjacent metals with provision for limited relative movement between components
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12479—Porous [e.g., foamed, spongy, cracked, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Toys (AREA)
  • Laminated Bodies (AREA)
JP2011509525A 2008-05-14 2009-04-16 超弾性発泡材料を有する形状変化構造 Active JP5694143B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/120,275 US7939178B2 (en) 2008-05-14 2008-05-14 Shape-changing structure with superelastic foam material
US12/120,275 2008-05-14
PCT/US2009/040760 WO2009140019A1 (en) 2008-05-14 2009-04-16 Shape-changing structure with superelastic foam material

Publications (3)

Publication Number Publication Date
JP2011520688A JP2011520688A (ja) 2011-07-21
JP2011520688A5 JP2011520688A5 (enExample) 2012-05-24
JP5694143B2 true JP5694143B2 (ja) 2015-04-01

Family

ID=40873374

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011509525A Active JP5694143B2 (ja) 2008-05-14 2009-04-16 超弾性発泡材料を有する形状変化構造

Country Status (5)

Country Link
US (1) US7939178B2 (enExample)
EP (1) EP2296963B1 (enExample)
JP (1) JP5694143B2 (enExample)
AU (1) AU2009246770B2 (enExample)
WO (1) WO2009140019A1 (enExample)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8016249B2 (en) * 2008-05-14 2011-09-13 Raytheon Company Shape-changing structure member with embedded spring
US8382042B2 (en) * 2008-05-14 2013-02-26 Raytheon Company Structure with reconfigurable polymer material
US20100041778A1 (en) * 2008-08-14 2010-02-18 Composite Technology Development, Inc. Reconfigurable polymeric foam structure
US20100148011A1 (en) * 2008-11-12 2010-06-17 Sanderson Terry M Telescoping structure and method
US8262032B2 (en) * 2008-11-13 2012-09-11 Raytheon Company Collapsible wing beams and method
US8056853B2 (en) * 2008-11-25 2011-11-15 Raytheon Company Reconfigurable wing and method of use
US8387536B2 (en) 2008-12-04 2013-03-05 Raytheon Company Interceptor vehicle with extendible arms
US8573535B2 (en) * 2009-03-27 2013-11-05 Raytheon Company Shape-change material and method
US9175702B1 (en) 2011-05-24 2015-11-03 Stephen Lee Bailey Externally supported foil with reversible camber and variable chord length
CN102381467A (zh) * 2011-08-31 2012-03-21 中国航天空气动力技术研究院 一种可变体飞行器机翼变掠方法
DE102011112966A1 (de) * 2011-09-13 2013-03-14 Trw Automotive Gmbh Aktuator mit Stellglied aus Formgedächtnismaterial
US8714476B2 (en) * 2011-10-21 2014-05-06 Raytheon Company Aircraft wing with flexible skins
US8783604B2 (en) * 2011-10-21 2014-07-22 Raytheon Company Aircraft wing with knuckled rib structure
WO2013066439A1 (en) 2011-11-04 2013-05-10 Raytheon Company Chord-expanding air vehicle wings
US8991769B2 (en) 2013-01-28 2015-03-31 Toyota Motor Engineering & Manufacturing North America, Inc. Two-dimensional morphing structure for wing
US9732776B2 (en) * 2014-10-10 2017-08-15 The Boeing Company Marman clamp with a shape memory alloy actuator
US10518908B2 (en) 2015-10-23 2019-12-31 Raytheon Company Spacecraft with shape memory polymer deployment mechanism
US10280904B2 (en) * 2016-03-09 2019-05-07 Northrop Grumman Systems Corporation Electrically activated pivot assembly
US10995859B2 (en) 2018-04-26 2021-05-04 Honda Motor Co., Ltd. Thermally actuated grommet
WO2020177739A1 (zh) * 2019-03-06 2020-09-10 昆明鞘翼科技有限公司 一种用分段倾转底驱式板翼实现垂直起降和水平飞行的航空器及方法
US11591076B2 (en) * 2019-06-26 2023-02-28 Toyota Motor Engineering & Manufacturing North America, Inc. Inflatable drone with shape memory alloy wires
CN110329491B (zh) * 2019-07-29 2020-10-13 吉林大学 基于形状记忆合金驱动的可变形机翼及其变形控制方法
CN114999702B (zh) * 2022-04-14 2023-01-06 哈尔滨工业大学 一种具有形状记忆特性的可多级调控导电性的复合材料的制备方法及应用

Family Cites Families (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2559827A (en) * 1946-10-28 1951-07-10 Northrop Aircarft Inc Means for stabilization of airplanes having highly swept-back wings
JPS60145385A (ja) 1984-01-10 1985-07-31 Waseda Daigaku 形状記憶効果装置
US5082207A (en) * 1985-02-04 1992-01-21 Rockwell International Corporation Active flexible wing aircraft control system
JPH0739506B2 (ja) 1988-09-30 1995-05-01 三菱重工業株式会社 形状記憶ポリマー発泡体
US5181678A (en) * 1991-02-04 1993-01-26 Flex Foil Technology, Inc. Flexible tailored elastic airfoil section
GB9122511D0 (en) 1991-10-23 1991-12-04 Raychem Sa Nv Heat recoverable article
GB9210954D0 (en) 1992-05-22 1992-07-08 Raychem Sa Nv Method of making an electroded laminated article
JPH07205894A (ja) * 1994-01-27 1995-08-08 Mitsubishi Heavy Ind Ltd 航空機のフラッタ抑制装置
US5662294A (en) * 1994-02-28 1997-09-02 Lockheed Martin Corporation Adaptive control surface using antagonistic shape memory alloy tendons
DE19707392A1 (de) * 1997-02-25 1998-08-27 Deutsch Zentr Luft & Raumfahrt Aerodynamisches Bauteil, wie Landeklappe, Tragflügel, Höhen- oder Seitenleitwerk, mit veränderbarer Wölbung
US6056237A (en) * 1997-06-25 2000-05-02 Woodland; Richard L. K. Sonotube compatible unmanned aerial vehicle and system
DE19742314C2 (de) 1997-09-25 2000-06-21 Daimler Chrysler Ag Tragende Struktur
US6264136B1 (en) * 1998-07-27 2001-07-24 Paul H. Weston High efficiency combination wing aircraft
US6482638B1 (en) * 1999-12-09 2002-11-19 3M Innovative Properties Company Heat-relaxable substrates and arrays
US20020195177A1 (en) * 2001-06-21 2002-12-26 The Aerospace Corporation Conductive shape memory metal deployment latch hinge deployment method
ITTO20020134A1 (it) 2002-02-15 2003-08-18 Ferrari Spa Pannello a deformazione comandata.
US6705568B2 (en) * 2002-03-06 2004-03-16 John R. Lee Variable area wing aircraft and method
US6769648B2 (en) * 2002-04-19 2004-08-03 William L. Klima Personal aircraft device
US6989197B2 (en) * 2002-11-04 2006-01-24 The Boeing Company Polymer composite structure reinforced with shape memory alloy and method of manufacturing same
US7567681B2 (en) * 2003-09-03 2009-07-28 Sri International Surface deformation electroactive polymer transducers
US6834835B1 (en) * 2004-03-12 2004-12-28 Qortek, Inc. Telescopic wing system
US20050198904A1 (en) * 2004-03-12 2005-09-15 Browne Alan L. Active seal assemblies for movable windows
DE102004026658A1 (de) 2004-06-01 2005-12-29 Kwd Automotive Group & Co. Kg Hybridgehäuse
US20050274103A1 (en) * 2004-06-10 2005-12-15 United Technologies Corporation Gas turbine engine inlet with noise reduction features
WO2007001392A2 (en) 2004-10-01 2007-01-04 The Regents Of The University Of Michigan Manufacture of shape-memory alloy cellular meterials and structures by transient-liquid reactive joining
AU2006265854A1 (en) * 2005-06-30 2007-01-11 Bell Helicopter Textron Inc. Retractable vortex generator
US7398586B2 (en) * 2005-11-01 2008-07-15 The Boeing Company Methods and systems for manufacturing a family of aircraft wings and other composite structures
DE102005061752A1 (de) * 2005-12-21 2007-07-05 Eads Deutschland Gmbh Dreidimensionales Stapelpiezoelement und piezoelektrischer Aktuator mit einem solchen Stapelpiezoelement
WO2008108881A2 (en) * 2006-09-08 2008-09-12 Steven Sullivan Method and apparatus for mitigating trailing vortex wakes of lifting or thrust generating bodies
GB0624580D0 (en) 2006-12-08 2007-01-17 Imp Innovations Ltd Aerofoil member
US7798443B2 (en) 2006-12-18 2010-09-21 The Boeing Company Composite material for geometric morphing wing
US7777165B2 (en) * 2007-02-02 2010-08-17 Raytheon Company Methods and apparatus for adjustable surfaces
CN100429119C (zh) 2007-03-30 2008-10-29 哈尔滨工业大学 一种可改变机翼后掠角的飞行器
US8382042B2 (en) * 2008-05-14 2013-02-26 Raytheon Company Structure with reconfigurable polymer material
US8016249B2 (en) * 2008-05-14 2011-09-13 Raytheon Company Shape-changing structure member with embedded spring
JP4737281B2 (ja) 2008-12-04 2011-07-27 パナソニック電工株式会社 形状記憶合金アクチュエータ

Also Published As

Publication number Publication date
WO2009140019A1 (en) 2009-11-19
US20090286101A1 (en) 2009-11-19
AU2009246770B2 (en) 2012-04-19
US7939178B2 (en) 2011-05-10
AU2009246770A1 (en) 2009-11-19
EP2296963B1 (en) 2012-10-24
JP2011520688A (ja) 2011-07-21
EP2296963A1 (en) 2011-03-23

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