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    HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND METHOD OF TRANSFORMING SUCH A VEHICLE
    1.
    发明授权
    HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND METHOD OF TRANSFORMING SUCH A VEHICLE 有权
    混合运输车辆用于陆地和空中和方法取得的运输这些车辆的转型

    公开(公告)号：EP2977239B1

    公开(公告)日：2017-04-12

    申请号：EP15184918.9

    申请日：2012-08-22

    申请人： Aeromobil S.r.o.

    发明人： KLEIN, Stefan

    IPC分类号： B60F5/02 ,  B64C37/00 ,  B64C3/56

    CPC分类号： B60F5/02 ,  B60F5/003 ,  B64C3/385 ,  B64C3/54 ,  B64C3/56 ,  B64C25/04 ,  B64C25/54 ,  B64C37/00 ,  B64C2025/003 ,  Y02T50/14

    摘要： Hybrid transportation vehicle for ground and air consisting of a body (4), cabin (6), retractable wings (1), chassis and driving unit (8) with switching of the torque transfer between a propeller (9) situated at the rear of the vehicle and driven wheels (5), the vehicle containing reciprocal transformation mechanisms for transformation into an automobile or into an aircraft, where one or two first reciprocal transformation mechanisms for retraction and expansion of the wings (1) from or to a flying position are situated in the middle of the body (4); each first reciprocal transformation mechanism contains a first actuator and a vertical axis (2) for retraction and expansion of the wing (1) by tilting around the vertical axis between a flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle, and a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle; and two second reciprocal transformation mechanisms for changing the platform outline of the wings, each being situated separately in a wing body (1) and each containing a horizontal axis (3) of the wing and a second actuator, for tilting the rear part of each wing onto the top front part of the wing (1).

    CONVERTIPLANE WITH NEW AERODYNAMIC AND TECHNICAL SOLUTIONS WHICH MAKE THE AIRCRAFT SAFE AND USABLE
    2.
    发明公开
    CONVERTIPLANE WITH NEW AERODYNAMIC AND TECHNICAL SOLUTIONS WHICH MAKE THE AIRCRAFT SAFE AND USABLE 审中-公开
    新的空气动力学和安全性和易用性的技术解决方案可换股PLANE

    公开(公告)号：EP3033272A1

    公开(公告)日：2016-06-22

    申请号：EP14784533.3

    申请日：2014-08-07

    申请人： UNIT 1SRL

    发明人： GIOVENGA, Pietro

    IPC分类号： B64C29/00 ,  B64D27/08 ,  B64C3/38 ,  B64C3/54

    CPC分类号： B64C29/0033 ,  B64C3/385 ,  B64C3/54 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/162 ,  B64D27/08 ,  Y02T50/14

    摘要： A convertiplane has the ability to take off like a helicopter and then fly horizontally like a conventional aircraft. The aircraft includes a variable incidence front wing of variable span located below the fuselage and mounted on a structure in the form of a venturi tube, a rear wing having two propellers for controlling the stability of the vehicle in pitch and roll installed therein, two counter-rotating, pivotally mounted ducted propellers equipped with four flaps orthogonal to each other provided on the sides of the cockpit, engines placed behind the cockpit close to the center of gravity, a static balancing system for controlling the center of gravity of the aircraft consisting of a weight placed in the lower part of the fuselage, self-propelled on the track rack longitudinally to the fuselage, and a digital flight control system.

    VARIABLE GEOMETRY WING
    3.
    发明公开
    VARIABLE GEOMETRY WING 审中-公开
    FLÜGELMIT VARIABLER GEOMETRIE

    公开(公告)号：EP2895388A1

    公开(公告)日：2015-07-22

    申请号：EP13762851.7

    申请日：2013-09-17

    申请人： Blue Bear Systems Research Limited

    发明人： SNOOK, Michael Alexander

    IPC分类号： B64C3/40 ,  B64C3/54 ,  B64C33/02

    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, 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，并且远侧翼手从 腕关节; 所述机翼通过所述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。

    SHAPE-CHANGING STRUCTURE WITH SUPERELASTIC FOAM MATERIAL
    6.
    发明授权
    SHAPE-CHANGING STRUCTURE WITH SUPERELASTIC FOAM MATERIAL 有权
    FORM结构变化超弹性泡沫材料

    公开(公告)号：EP2296963B1

    公开(公告)日：2012-10-24

    申请号：EP09747105.6

    申请日：2009-04-16

    申请人： Raytheon Company

    发明人： SAR, David, R. ,  SANDERSON, Terry, M.

    IPC分类号： B64C3/54 ,  B64C5/02 ,  B64C5/18 ,  F02C7/042 ,  C22F1/18

    CPC分类号： B64C3/54 ,  B64C3/40 ,  B64C5/02 ,  B64C5/18 ,  C22F1/006 ,  C22F1/10 ,  Y02T50/14 ,  Y10T428/12326 ,  Y10T428/12479

    摘要： A shape-changing structure has a superelastic metal foam structural member that changes shape (morphs) to change configuration of the structure. The superelastic metal foam structural member changes shape while maintaining a continuous outer surface, with the continuous metal foam material inside the outer surface expanding, contracting, or otherwise changing shape. The superelastic metal foam material may be heated above a transition temperature to allow it to change shape, and then cooled to cause it to increase in strength, more easily maintaining its new shape. The superelastic metal foam material may be a suitable alloy, for example a nickel titanium alloy, that exhibits superelastic (pseudoelastic) behavior. The superelastic metal foam material may be a shape memory alloy material that returns to a set shape upon moderate heating. The superelastic metal elastic foam structural member may be heated either by an internal heat source or by external heating.

    AILE RIGIDE DE PORTANCE VARIABLE PAR DEPLOIEMENT D'UNE AILE SOUPLE
    8.
    发明授权
    AILE RIGIDE DE PORTANCE VARIABLE PAR DEPLOIEMENT D'UNE AILE SOUPLE 有权
    具有可变BOOST在柔性翼的展开BASIS固定翼

    公开(公告)号：EP1658221B1

    公开(公告)日：2007-03-28

    申请号：EP04767408.0

    申请日：2004-06-22

    申请人： Lisa Airplanes

    发明人： Herzberger, Erick

    IPC分类号： B64C3/54 ,  B64C31/028

    CPC分类号： B64C9/16 ,  B64C3/54 ,  B64C31/02

    摘要： The invention relates to a wing with variable sustentation for small aeroplanes or ULM planes, said wing being characterised in that it has a flexible wing system (3) that can be continuously deployed in the extension of the rigid wing (4) by means of at least one articulated system (5), and in that said flexible wing system (3) and said articulated system (5) are completely incorporated into the rear part of the rigid wing (4) in the configuration of a cruising flight.

    INFLATABLE PROPELLER
    10.
    发明公开
    INFLATABLE PROPELLER 审中-公开
    充气式螺旋桨

    公开(公告)号：EP3309060A1

    公开(公告)日：2018-04-18

    申请号：EP17183531.7

    申请日：2017-07-27

    申请人： The Boeing Company

    发明人： Bernhardt, Roger David ,  Drouin, Donald V.

    IPC分类号： B64C11/20 ,  B64C3/46 ,  B64C3/30 ,  B64C3/54

    CPC分类号： B64C11/18 ,  B64B1/30 ,  B64C3/30 ,  B64C3/46 ,  B64C3/54 ,  B64C11/20 ,  B64C39/10 ,  F03D1/0675 ,  F03D7/022

    摘要： A method and apparatus (110) for controlling movement of an aircraft. An aerodynamic function desired for controlling the movement of the aircraft (106) at a particular altitude is identified. The aerodynamic function identified is part of a group of aerodynamic functions (122) used to control the movement of the aircraft (106) at a number of different altitudes (104). A group of inflatable blades (120) is filled with a fluid (116) to a pressure that corresponds to the aerodynamic function. The group of inflatable blades (120) at the pressure has a shape (208) and a group of dimensions (210) that provide the aerodynamic function.

    摘要翻译： 一种用于控制飞行器的移动的方法和设备（110）。 识别用于控制飞行器（106）在特定高度处的运动所期望的空气动力学功能。 所识别的空气动力学功能是用于控制飞机（106）在多个不同高度（104）处的运动的一组空气动力学功能（122）的一部分。 一组可充气叶片（120）充满流体（116），达到对应于空气动力学功能的压力。 处于压力下的可充气叶片组（120）具有提供空气动力学功能的形状（208）和一组尺寸（210）。