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1. 发明申请

US20190202543A1 Blade or Wing 审中-公开
公开(公告)号：US20190202543A1
公开(公告)日：2019-07-04
申请号：US16297126
申请日：2019-03-08
申请人： Brunel University London
发明人： Alvin Gatto
IPC分类号： B64C3/52 , B64C3/18 , B64C13/40 , F03D1/06
CPC分类号： B64C3/52 , B64C3/187 , B64C3/48 , B64C13/40 , B64C2003/445 , B64C2003/543 , F01D5/00 , F03D1/0633 , F03D1/0675 , F05B2240/31 , F05B2250/02 , Y02T50/14
摘要： A blade or wing element includes a plurality of ribs (20) rotatable and/or slidable with respect to one another whereby to vary the aerodynamic configuration of the blade or wing element by causing a twist thereof. A blade or wing or blade or wing assembly, including such a blade or wing element is disclosed, as well as an aerodynamic apparatus such as an aircraft, or a wind turbine. A method of assembling a blade or wing element is also disclosed.

2. 发明授权

US08342447B2 Morphing control surface transition 有权
标题翻译：变形控制面过渡
公开(公告)号：US08342447B2
公开(公告)日：2013-01-01
申请号：US12816372
申请日：2010-06-15
申请人： Keith A. Etling
发明人： Keith A. Etling
IPC分类号： B64C9/00 , B64C5/10
CPC分类号： B64C7/00 , B64C9/00 , B64C2003/543 , Y10T74/20207
摘要： A transition section forms a continuous contour across a gap between a pair of structures. The transition section comprises at least one rib mounted within the gap and being pivotable relative to the structures. A tip may be mounted to an aft end of the rib and may be rotatable about a tip axis. A skin panel may extend between the structures and may at least partially cover the tip. The skin panel may be deformable during pivoting of the rib such that the tip may rotate into substantial alignment with the skin panel.
摘要翻译：过渡部分跨越一对结构之间的间隙形成连续轮廓。过渡部分包括安装在间隙内的至少一个肋，并且可相对于结构枢转。尖端可以安装到肋的后端并且可以围绕尖端轴线旋转。皮肤面板可以在结构之间延伸并且可以至少部分地覆盖尖端。皮肤面板可以在肋的枢转期间变形，使得尖端可以旋转成与皮肤面板基本对准。

3. 发明授权

US09975622B2 Morphing foil or wing 有权
公开(公告)号：US09975622B2
公开(公告)日：2018-05-22
申请号：US14660184
申请日：2015-03-17
申请人： Blue Bear Systems Research Limited
发明人： Michael Snook
IPC分类号： B64C3/54 , B64C3/40 , B64C39/02
CPC分类号： B64C3/546 , B64C3/40 , B64C3/54 , B64C39/024 , B64C2003/543 , B64C2201/102 , Y02T50/14
摘要： Embodiments of the present invention relate to an adaptable wing having a variable geometry for influencing aerodynamic performance, the wing comprising a jointed leading edge having a main pivot, and a wrist joint, with a wing arm therebetween, and a distal wing hand depending from the wrist joint; the wing being reciprocally actuable, via the main pivot and wrist joint, between a first state having an extended wing planform and a second state having a tucked wing planform.

4. 发明申请

US20170021918A1 STRUCTURAL HEALTH MONITORING SENSORY SYSTEM INTEGRATED TO A SELF-ADAPTING MORPHING SYSTEM 审中-公开
标题翻译：结构健康监测系统集成到自适应变形系统
公开(公告)号：US20170021918A1
公开(公告)日：2017-01-26
申请号：US14808142
申请日：2015-07-24
申请人： Embraer S.A.
发明人： Paulo Anchieta DA SILVA , Tomaz LAZANHA , Ricardo Pinheiro RULLI , Fernando DOTTA
IPC分类号： B64C23/06 , A61B5/053 , B64F5/00 , G01M99/00
CPC分类号： A61B5/053 , B64C23/072 , B64C2003/445 , B64C2003/543 , B64D2045/0085 , B64F5/60 , F03D7/022 , F05B2240/31 , G01M5/0016 , G01M5/0033 , G01M5/0041 , G01M99/00 , Y02T50/164
摘要： A system and method for damage detection and for evaluating the real operation conditions for structural platforms using structural health monitoring is integrated to a system and method that permits for the platform to provide a flexible geometric control considering a self-adapting morphing which is capable of providing better operating structural platform performance.
摘要翻译：使用结构健康监测的结构平台的损伤检测和实际操作条件的评估系统和方法被集成到一个允许平台提供灵活几何控制的系统和方法，该自适应变形能够提供能够提供更好的操作结构平台性能。

5. 发明授权

US11760465B2 Aircraft wing control 有权
公开(公告)号：US11760465B2
公开(公告)日：2023-09-19
申请号：US17595649
申请日：2020-05-28
申请人： Stellar Advanced Concepts Ltd
发明人： Michael Newsam
IPC分类号： B64C3/54 , B64C3/42 , B64C39/02 , B63G8/18 , B64U30/12 , B64U101/15
CPC分类号： B64C3/546 , B64C3/42 , B64C39/024 , B63G8/18 , B64C2003/543 , B64U30/12 , B64U2101/15
摘要： A vehicle comprising a morphing wing and a body is disclosed. The aircraft is configured to transform from a first configuration into a second configuration for ascent or descent of the aircraft. The drag force and lift force on the aircraft in the second configuration are less than in the first configuration. Transforming from the first to the second configuration comprises: contracting the wing within a geometric plane defined by the wing, and rotating the outer edge of the wing downwards, out of the geometric plane.

6. 发明授权

US09856012B2 Morphing wing for an aircraft 有权
公开(公告)号：US09856012B2
公开(公告)日：2018-01-02
申请号：US14408722
申请日：2013-06-21
申请人： BOMBARDIER INC.
发明人： Fengfeng Xi , Allan Daniel Finistauri , Amin Moosavian
IPC分类号： B64C3/38 , B64C3/44 , B64C3/54 , B64C3/52 , B64C3/40
CPC分类号： B64C3/38 , B64C3/385 , B64C3/40 , B64C3/44 , B64C3/52 , B64C3/54 , B64C2003/445 , B64C2003/543 , Y02T50/14
摘要： A morphing wing for an aircraft includes first and second structural ribs with four active members and four passive members connected therebetween. First and second active members and third and fourth active members attach at first and second positions. The first and third active members and the second and fourth active members attach at third and fourth positions. A first passive member connects between third and fifth positions. A second passive member connects between second and seventh positions. A third passive member connects between fourth and sixth positions. A fourth passive member connects between first and eighth positions. Adjustment of the four active members morphs the wing from a first configuration to a second configuration. The first and second positions are at corners of a first quadrilateral diagonally opposite to one another. The four passive members attach to the first structural rib at the corners of the first quadrilateral.

7. 发明申请

US20170291683A1 DEPLOYABLE WING FOR AN AIRCRAFT 审中-公开
公开(公告)号：US20170291683A1
公开(公告)日：2017-10-12
申请号：US15096998
申请日：2016-04-12
申请人： THOMAS E. KEAVNEY , JOHN C. RUFINO
发明人： THOMAS E. KEAVNEY , JOHN C. RUFINO
IPC分类号： B64C3/30 , B64C3/54
CPC分类号： B64C3/30 , B64C3/54 , B64C2003/543 , B64D17/80
摘要： An apparatus for selectively increasing a wing area of an aircraft having a fuselage with an interior space includes an inflatable wing moveable between a stowed condition located in the interior space and a deployed condition located outside the interior space. A plurality of reels is secured to the aircraft. A plurality of suspension lines connects the wing to the reels. At least one reel is operable to unwind a corresponding suspension line to allow the wing to inflate to the deployed condition exclusively by ram air generated by movement of the aircraft. A method of use for a deployable wing is also provided.

8. 发明申请

US20160176502A1 Morphing Foil or Wing 有权
标题翻译：变形箔或翼
公开(公告)号：US20160176502A1
公开(公告)日：2016-06-23
申请号：US14660184
申请日：2015-03-17
申请人： Blue Bear Systems Research Limited
发明人： Michael SNOOK
IPC分类号： B64C3/54 , B64C39/02 , B64C3/40
CPC分类号： B64C3/546 , B64C3/40 , B64C3/54 , B64C39/024 , B64C2003/543 , B64C2201/102 , Y02T50/14
摘要： Embodiments of the present invention relate to an adaptable wing having a variable geometry for influencing aerodynamic performance, the wing comprising a jointed leading edge having a main pivot, and a wrist joint, with a wing arm therebetween, 5 and a distal wing hand depending from the wrist joint; the wing being reciprocally actuable, via the main pivot and wrist joint, between a first state having an extended wing planform and a second state having a tucked wing planform.
摘要翻译：本发明的实施例涉及一种具有可变几何形状以用于影响空气动力学性能的适应翼，所述机翼包括具有主枢轴的接合前缘和在其间具有翼臂的腕关节5，以及远侧翼手从腕关节; 所述机翼通过主枢轴和腕关节在具有延伸机翼平面图的第一状态和具有卷起的机翼平面图的第二状态之间可往复地起动。

9. 发明申请

US20150151830A1 MORPHING WING FOR AN AIRCRAFT 有权
标题翻译：飞机的飞行员
公开(公告)号：US20150151830A1
公开(公告)日：2015-06-04
申请号：US14408722
申请日：2013-06-21
申请人： BOMBARDIER INC.
发明人： Fengfeng Xi , Allan Daniel Finistauri , Amin Moosavian
IPC分类号： B64C3/38 , B64C3/54 , B64C3/40
CPC分类号： B64C3/38 , B64C3/385 , B64C3/40 , B64C3/44 , B64C3/52 , B64C3/54 , B64C2003/445 , B64C2003/543 , Y02T50/14
摘要： A morphing wing for an aircraft includes a top surface, a bottom surface, a leading edge, a trailing edge, a tip, and a root. A plurality of structural ribs is disposed between the root and tip so that they extend between the top surface and the bottom surface and intersect with a lateral axis thereof. At least one active member connects between two adjacent structural ribs along or at a first angle to the lateral axis. The active member is actively adjustable. At least one passive member connects between the two adjacent structural ribs along or at a second angle to the lateral axis. The passive member is passively adjustable. Adjustment of at least one active member moves the adjacent structural ribs with respect to one another, thereby morphing the wing from a first configuration to a second configuration.
摘要翻译：用于飞机的变形翼包括顶表面，底表面，前缘，后缘，尖端和根部。多个结构肋设置在根部和尖端之间，使得它们在顶表面和底表面之间延伸并与其横向轴线相交。至少一个有源构件沿着或相对于横向轴线以第一角度连接在两个相邻结构肋之间。活动构件可以主动调节。至少一个无源构件沿着或相对于横向轴线的第二角度在两个相邻的结构肋之间连接。被动元件被动调节。至少一个活动构件的调节使相邻的结构肋相对于彼此移动，从而使机翼从第一构型变形到第二构型。

10. 发明公开

US20240286730A1 MORPHING WING, FLIGHT CONTROL DEVICE, FLIGHT CONTROL METHOD, AND PROGRAM 审中-公开
公开(公告)号：US20240286730A1
公开(公告)日：2024-08-29
申请号：US18575216
申请日：2022-07-06
申请人： Japan Aerospace Exploration Agency
发明人： Daichi WADA
IPC分类号： B64C3/54 , G05D1/654 , G05D101/15 , G05D109/22
CPC分类号： B64C3/546 , G05D1/654 , B64C2003/543 , G05D2101/15 , G05D2109/23
摘要： A morphing wing (140) of the present invention includes a link mechanism configured to be deployed in a first direction and retracted in a second direction opposite to the first direction, a plurality of front wing covers (180) mounted on a front side which is one side of the link mechanism perpendicular to the first direction, and a plurality of flight feathers (160) mounted on a rear side which is the other side of the link mechanism perpendicular to the first direction, wherein the front wing covers (180) and the flight feathers (160) are streamlined from the front side toward the rear side, and when the link mechanism is retracted, the flight feathers (160) are retracted inside the adjacent flight feathers (160).

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