JP5837579B2 - 形状記憶合金/繊維強化ポリマー複合構造物および形成方法 - Google Patents
形状記憶合金/繊維強化ポリマー複合構造物および形成方法 Download PDFInfo
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Description
表1 CFRPパネルの積層順
また、本願は以下に記載する態様を含む。
(態様1)
少なくとも1層の繊維強化ポリマー層(212)と、
前記少なくとも1層の繊維強化ポリマー層(212)を密接に結合する少なくとも1枚の形状記憶合金板と、
を含む、複合構造物。
(態様2)
前記少なくとも1枚の形状記憶合金板が、約0.002インチから約0.25インチの厚さを有する層を含む、態様1に記載の複合構造物。
(態様3)
前記少なくとも1枚の形状記憶合金板が、少なくとも1層の接着促進層(222)と、層の上面および底面の少なくとも一方に接着剤層(650)と、を有する、態様1に記載の複合構造物。
(態様4)
少なくとも2層の形状記憶合金層と、
前記少なくとも2層の形状記憶合金層の間の少なくとも1層の繊維強化ポリマー層(212)と、
を含む、複合構造物。
(態様5)
前記少なくとも2層の形状記憶合金層は、各々が、約0.002インチから約0.25インチの厚さを有する、態様4に記載の複合構造物。
(態様6)
前記少なくとも2層の形状記憶合金層は、各々が、その上面および底面のうちの1つに少なくとも1層の接着促進層(222)と、接着剤(650)の層と、を有する、態様4に記載の複合構造物。
(態様7)
前記少なくとも1層の繊維強化ポリマー層(212)が、炭素繊維およびガラス繊維からなる群から選択される少なくとも1つの繊維により強化されている、態様4に記載の複合構造物。
(態様8)
前記接着剤(650)の層が、エポキシ接着剤の層である、態様6に記載の複合構造物。
(態様9)
形状記憶合金/繊維強化ポリマー複合構造物を作製するための方法であって、
第1の複数の繊維強化ポリマー層を設ける工程と、
第2の複数の形状記憶合金層を設ける工程と、
前記第2の複数の形状記憶合金層のうちの1層の上面および底面の少なくとも一方を接着剤下塗り層により被覆する工程と、
前記接着剤下塗りにより被覆された形状記憶合金層上を接着剤の層で被覆する工程と、
前記被覆された形状記憶合金層に前記第1の複数の繊維強化ポリマー層の少なくとも2層を挟むことにより、積層体を形成する工程と、
前記積層体を硬化させて、前記形状記憶合金繊維強化ポリマー複合構造物を形成する工程と、
を含む方法。
(態様10)
前記第2の複数の形状記憶合金層は、各々が、約0.002インチから約0.25インチの厚さを有する、態様9に記載の形状記憶合金/繊維強化ポリマー複合構造物を作製するための方法。
(態様11)
約200°Fから約500°Fの温度で、かつ、40PSI以上の圧力で前記積層体を硬化させる工程をさらに含む、態様9に記載の形状記憶合金/繊維強化ポリマー複合構造物を作製するための方法。
(態様12)
複合構造物を変形させるための方法であって、
第1の複数の繊維強化ポリマープリプレグ層(212)を設ける工程と、
各々の上面および底面の少なくとも一方が接着剤により被覆されている第2の複数の形状記憶合金層を設ける工程と、
前記形状記憶合金が第1結晶状態から第2結晶状態へ変態する所定の温度にまで加熱することにより前記複合構造物を変形させる工程と、
を含む、方法。
(態様13)
前記複数の形状記憶合金層をニッケルチタン合金で設ける工程をさらに含む、態様12に記載の複合構造物を変形させるための方法。
(態様14)
前記変形させる工程中に前記複合構造物を110°F以上の温度にまで加熱する工程をさらに含む、態様12に記載の複合構造物を変形させるための方法。
(態様15)
前記変形させる工程中に前記複合構造物を約110°Fから約320°Fの温度にまで加熱する工程をさらに含む、態様12に記載の複合構造物を変形させるための方法。
Claims (4)
- 複合構造物を変形させるための方法であって、
第1の複数の繊維強化ポリマープリプレグ層(212)を設ける工程と、
第2の複数の形状記憶合金シートであって、それぞれのシートが上面および底面の少なくとも一方が接着剤により被覆されている第2の複数の形状記憶合金シートを設ける工程と、
前記第2の複数の形状記憶合金シートを、前記複合構造物を形成する前記第1の複数の繊維強化ポリマープリプレグ層に挟む工程であって、挟むことは前記第1の複数の繊維強化ポリマープリプレグ層の第1の層と第2の層とを用い、第1の層は、第1の方向に実質的に配向した第1の繊維を含み、第2の層は、第2の方向に実質的に配向した第2の繊維を含み、さらに挟むことは第1の方向が第2の方向にほぼ垂直であるように実施される工程と、
第2の複数の形状記憶合金層のそれぞれから前記接着剤のそれぞれへ移行する傾斜層を有する界面を提供する工程であって、前記傾斜層が実質的に繊維が欠けている工程と、
前記形状記憶合金が第1結晶状態から第2結晶状態へ変形する所定の温度にまで加熱することにより前記複合構造物を変形させる工程と、
を含む、方法。 - 前記複数の形状記憶合金層をニッケルチタン合金で設ける工程をさらに含む、請求項1に記載の複合構造物を変形させるための方法。
- 前記変形させる工程中に前記複合構造物を110°F(43.3℃)以上の温度にまで加熱する工程をさらに含む、請求項1または2に記載の複合構造物を変形させるための方法。
- 前記変形させる工程中に前記複合構造物を110°F(43.3℃)から320°F(160℃)の温度にまで加熱する工程をさらに含む、請求項1または2に記載の複合構造物を変形させるための方法。
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US12/917,740 US20110300358A1 (en) | 2010-06-04 | 2010-11-02 | Shape memory alloy/fiber reinforced polymeric composite structures and method for forming |
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Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
US9625361B1 (en) | 2001-08-19 | 2017-04-18 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
GB0807593D0 (en) * | 2008-04-28 | 2008-06-04 | Rolls Royce Plc | A composite article comprising a shape memory material member |
US9522512B2 (en) | 2010-08-17 | 2016-12-20 | The Boeing Company | Methods for making composite structures having composite-to-metal joints |
GB2500699A (en) * | 2012-03-30 | 2013-10-02 | Mbda Uk Ltd | Composite morphing skin for an aircraft |
WO2013144639A1 (en) * | 2012-03-30 | 2013-10-03 | Mbda Uk Limited | Composite material suitable for a morphing skin |
GB201207525D0 (en) * | 2012-04-30 | 2012-06-13 | Airbus Operations Ltd | Morphing aerofoil |
US10661885B2 (en) * | 2012-05-16 | 2020-05-26 | The Boeing Company | Shape memory alloy active spars for blade twist |
DE102012112965A1 (de) | 2012-12-21 | 2014-06-26 | Leibniz-Institut Für Neue Materialien Gemeinnützige Gesellschaft Mit Beschränkter Haftung | Gegenstand mit schaltbarer Adhäsion |
US9253823B2 (en) * | 2013-02-10 | 2016-02-02 | The Boeing Company | Metal matrix composite used as a heating element |
US9610761B2 (en) | 2013-03-12 | 2017-04-04 | The Boeing Company | System and method for use in fabricating a structure |
CN103192528B (zh) * | 2013-04-24 | 2015-05-27 | 哈尔滨飞机工业集团有限责任公司 | 一种钛合金和复合材料件共固化成型的方法 |
CN104339504B (zh) * | 2013-08-05 | 2017-07-25 | 哈尔滨飞机工业集团有限责任公司 | 侧端板前缘r角凹陷的消除方法 |
US9566746B2 (en) * | 2013-11-06 | 2017-02-14 | The Boeing Company | Methods and tools for forming contoured composite structures with shape memory alloy |
JP6434275B2 (ja) * | 2014-01-08 | 2018-12-05 | キヤノン電子株式会社 | 繊維強化積層体及びシャッタ装置並びにカメラ |
US9216814B2 (en) * | 2014-03-02 | 2015-12-22 | Toyota Motor Engineering & Manufacturing North America, Inc. | Stackable wing for an aerocar |
US9719536B2 (en) | 2014-07-03 | 2017-08-01 | The Boeing Company | Assemblies including shape memory alloy fittings and composite structural members |
US10464281B2 (en) * | 2014-08-19 | 2019-11-05 | The Boeing Company | Sandwich composite with shape memory alloy core and method of making same |
DE102014112772A1 (de) * | 2014-09-04 | 2016-03-10 | Thyssenkrupp Steel Europe Ag | Mehrschichtverbundwerkstoff, Verfahren zur Herstellung und Halbzeug mit Formgedächtnismaterial |
DE102014119470A1 (de) | 2014-12-22 | 2016-06-23 | Leibniz-Institut Für Neue Materialien Gemeinnützige Gmbh | Strukturierte Oberfläche mit stufenweise schaltbarer Adhäsion |
US9599983B2 (en) * | 2015-01-21 | 2017-03-21 | The Boeing Company | Systems, methods, and apparatus for automated predictive shimming for large structures |
FR3035938B1 (fr) * | 2015-05-06 | 2017-06-02 | Peugeot Citroen Automobiles Sa | Dispositif de suspension pour vehicule automobile, comprenant des ressorts en materiau composite et en alliage a memoire de forme |
WO2016191118A1 (en) * | 2015-05-22 | 2016-12-01 | 3M Innovative Properties Company | Thermally stable microstructured semi-ipn layer |
WO2017028199A1 (en) * | 2015-08-18 | 2017-02-23 | Hewlett-Packard Development Company, L.P. | Composite material |
WO2017139706A1 (en) * | 2016-02-12 | 2017-08-17 | Massachusetts Institute Of Technology | Shape memory ceramic particles and structures formed thereof |
US10253192B2 (en) * | 2016-08-29 | 2019-04-09 | The Boeing Company | Barrier coating system |
CN106428512B (zh) * | 2016-11-14 | 2018-11-02 | 泉州市泉港区鑫悦盟工业科技有限公司 | 高速变形飞行器 |
KR101903454B1 (ko) * | 2017-01-17 | 2018-10-02 | 한국항공대학교산학협력단 | 키리가미 패턴을 이용한 형상기억 모핑 부재 |
US10919615B2 (en) * | 2017-03-29 | 2021-02-16 | The Boeing Company | Methods and apparatuses for joining titanium and titanium alloy structures to epoxy-containing compounds |
GB2563869B (en) | 2017-06-28 | 2023-05-17 | Qinetiq Ltd | Materials and methods |
CN108648630B (zh) * | 2018-05-31 | 2020-03-17 | 武汉华星光电半导体显示技术有限公司 | 曲面屏贴合装置及贴合方法 |
DE102018129384A1 (de) | 2018-11-22 | 2020-05-28 | Fischerwerke Gmbh & Co. Kg | Faserverbundwerkstoff |
DE102019128494A1 (de) * | 2018-11-22 | 2020-05-28 | Fischerwerke Gmbh & Co. Kg | Spannelement zur Verstärkung eines Bauteils im Bauwesen und Verfahren zur Einleitung einer Druckspannung in ein Bauteil |
CN109760341A (zh) * | 2018-12-29 | 2019-05-17 | 南京航空航天大学 | 双程弯曲的形状记忆合金复合材料、制作方法及驱动方法 |
US10933974B2 (en) | 2019-04-29 | 2021-03-02 | Toyota Motor Engineering & Manufacturing North America, Inc. | Morphable body with shape memory material members |
CN110920864B (zh) * | 2019-10-29 | 2022-06-17 | 南京航空航天大学 | 一种形状记忆合金薄板驱动的双程变体机构及方法 |
US11520355B2 (en) | 2021-02-26 | 2022-12-06 | Toyota Motor Engineering & Manufacturing North America, Inc. | Wing tip control effector |
US12043350B1 (en) * | 2021-03-29 | 2024-07-23 | The United States Of America, As Represented By The Secretary Of The Navy | Implosion-resistant lightweight membrane shell devices for high-pressure applications |
CN114135454B (zh) * | 2021-11-24 | 2024-08-09 | 西安交通大学 | 一种片状柔性sma复合驱动器及其成型工艺 |
US11939055B2 (en) | 2022-04-15 | 2024-03-26 | Toyota Motor Engineering & Manufacturing North America, Inc. | Winglets with passive aeroelastic tailoring |
US11932390B2 (en) | 2022-04-15 | 2024-03-19 | Toyota Motor Engineering & Manufacturing North America, Inc. | Wing shape control |
CN114888533B (zh) * | 2022-06-10 | 2023-02-28 | 清华大学 | 具备温度自传感功能的形状记忆合金软体驱动器的制备方法 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5866272A (en) * | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
US5869141A (en) * | 1996-11-04 | 1999-02-09 | The Boeing Company | Surface pretreatment for sol coating of metals |
US6655218B1 (en) * | 1999-05-28 | 2003-12-02 | Fuji Jukogyo Kabushiki Kaisha | Composite material and method of controlling damage thereto and damage sensor |
JP4338823B2 (ja) * | 1999-05-28 | 2009-10-07 | 富士重工業株式会社 | 複合材の損傷制御方法 |
US6773535B1 (en) * | 2003-03-03 | 2004-08-10 | The United States Of America As Represented By The Secretary Of The Army | Article and method for controlled debonding of elements using shape memory alloy actuators |
JP2004262191A (ja) * | 2003-03-04 | 2004-09-24 | Fuji Heavy Ind Ltd | 複合材及びその製造方法 |
US20050175813A1 (en) * | 2004-02-10 | 2005-08-11 | Wingert A. L. | Aluminum-fiber laminate |
FR2886309B1 (fr) * | 2005-05-31 | 2007-08-17 | Airbus France Sas | Sol pour le revetement par voie sol-gel d'une surface et procede de revetement par voie sol-gel le mettant en oeuvre |
US7958733B2 (en) * | 2006-06-20 | 2011-06-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Jet engine exhaust nozzle flow effector |
US7835130B2 (en) * | 2007-10-05 | 2010-11-16 | The Boeing Company | Method and apparatus for lightning protection of a composite structure |
-
2010
- 2010-11-02 US US12/917,740 patent/US20110300358A1/en not_active Abandoned
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