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公开(公告)号：US20170057630A1
公开(公告)日：2017-03-02
申请号：US15119812
申请日：2015-02-17
Inventor： Meinhard Schwaiger
CPC classification number: B64C29/0033 , B64C3/385 , B64C3/56 , B64C27/026 , B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/102 , B64C2201/108 , B64C2201/162 , B64D27/04 , B64D27/24 , B64D2027/026 , B64D2211/00
Abstract: The invention relates to an aircraft comprising a fuselage (1), a plurality of propeller units (3) that can pivot in relation to the fuselage (1), and wings (5) that can pivot at least partially in relation to the fuselage (1) and independently of the propeller units (3).
Abstract translation: 本发明涉及一种飞机，其包括机身（1），可相对于机身（1）枢转的多个螺旋桨单元（3）和能够相对于机身至少部分地枢转的翼（5） 1）并且独立于螺旋桨单元（3）。
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公开(公告)号：US09561843B2
公开(公告)日：2017-02-07
申请号：US14942174
申请日：2015-11-16
Applicant: TUFTS UNIVERSITY
Inventor： Alfram V. Bright , Richard Wlezien
CPC classification number: B64C3/30 , B64C3/56 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/102 , B64C2201/127 , D06M10/001 , D06M10/10 , D06M15/327 , E04H12/00 , F03D13/20 , H05G2/00 , Y02E10/728
Abstract: The present invention provides novel inflatable and rigidizable support elements, and methods of manufacture and use thereof. In particular, the present invention provides inflatable and rigidizable support elements rapidly inflated and rigidized using an acrylic adhesive and UV light generated by combustion, which find use, for example, in rapidly deploying and supporting the wing of an aerial vehicle and wind turbine towers.
Abstract translation: 本发明提供了新颖的可膨胀和可固化的支撑元件，及其制造和使用方法。 特别地，本发明提供了使用丙烯酸粘合剂和由燃烧产生的UV光快速膨胀和刚性化的可膨胀和可固化的支撑元件，其可用于例如快速部署和支撑飞行器和风力涡轮机塔架的机翼。
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公开(公告)号：US09541924B2
公开(公告)日：2017-01-10
申请号：US14737814
申请日：2015-06-12
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： Sergey V. Frolov , John Peter Moussouris , Michael Cyrus
IPC: G05D1/10 , G05D1/00 , G05D1/02 , G05D1/06 , B64C37/02 , B64C3/56 , G08G5/00 , G08G7/02 , B64C29/00
CPC classification number: G05D1/104 , B64C3/56 , B64C29/0016 , B64C37/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/102 , B64C2201/128 , B64C2201/143 , B64C2201/145 , B64D1/02 , G05D1/0022 , G05D1/0027 , G05D1/005 , G05D1/0212 , G05D1/0669 , G05D1/102 , G08G5/0008 , G08G5/0013 , G08G5/0017 , G08G5/0021 , G08G5/003 , G08G5/0065 , G08G5/0069 , G08G5/025 , G08G5/045 , G08G7/02 , Y02T50/14
Abstract: Embodiments of the present invention provide an alternative distributed airborne transportation system. In some embodiments, a method for distributed airborne transportation includes: providing an airborne vehicle with a wing and a wing span, having capacity to carry one or more of passengers or cargo; landing of the airborne vehicle near one or more of passengers or cargo and loading at least one of passengers or cargo; taking-off and determining a flight direction for the airborne vehicle; locating at least one other airborne vehicle, which has substantially the same flight direction; and joining at least one other airborne vehicle in flight formation and forming a fleet, in which airborne vehicles fly with the same speed and direction and in which adjacent airborne vehicles are separated by distance of less than 100 wing spans.
Abstract translation: 本发明的实施例提供了一种替代的分布式机载运输系统。 在一些实施例中，一种用于分布式机载运输的方法包括：向机载车辆提供机翼和机翼跨度，具有携带乘客或货物中的一个或多个的能力; 机载车辆靠近一个或多个乘客或货物并装载至少一个乘客或货物; 起飞和确定机载飞行方向; 至少定位一个具有大致相同的飞行方向的其他机载车辆; 并将至少一个其他机载车辆接入飞行形成并形成一个舰队，其中机载车辆以相同的速度和方向飞行，并且相邻的机载车辆以小于100个翼跨的距离分开。
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公开(公告)号：US09540103B2
公开(公告)日：2017-01-10
申请号：US14313680
申请日：2014-06-24
Applicant: Kitty Hawk Corporation
Inventor： Geoffrey A. Long
CPC classification number: B64C39/024 , B64C27/24 , B64C27/32 , B64C2201/102 , B64C2201/108
Abstract: A vertical takeoff and landing aircraft includes rotors that provide vertical and horizontal thrust. During forward motion, the vertical lift system is inactive. A lift fan mechanism positions the fan blades of the aircraft in a collapsed configuration when the vertical lift system is inactive and positions the fan blades of the aircraft in a deployed configuration when the vertical lift system is active.
Abstract translation: 垂直起降飞机包括提供垂直和水平推力的转子。 在向前运动期间，垂直升降系统不起作用。 当垂直升降系统处于非活动状态时，升降风扇机构将飞行器的风扇叶片定位在折叠构型中，并且当垂直升降系统处于活动状态时将飞行器的风扇叶片定位在展开配置中。
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公开(公告)号：US20160167781A1
公开(公告)日：2016-06-16
申请号：US14944482
申请日：2015-11-18
Applicant: AURORA FLIGHT SCIENCES CORPORATION
Inventor： ROBERT PARKS , ADAM WOODWORTH , TOM VANECK , JUSTIN MCCLELLAN
CPC classification number: B64C37/00 , B60F5/02 , B63G8/001 , B63G8/08 , B63G2008/005 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/08 , B64C2201/102 , B64C2201/127 , B64C2201/165 , B64C2201/167 , F42B15/20
Abstract: A combined submersible vessel and unmanned aerial vehicle preferably includes a body structure, at least one wing structure, at least one vertical stabilizer structure, and at least one horizontal stabilizer structure. A propulsion system is coupled to the body structure and is configured to propel the flying submarine in both airborne flight and underwater operation. Preferably, the propulsion system includes a motor, a gearbox coupled to the motor and configured to receive power generated by the motor and provide variable output power, a drive shaft coupled to the gearbox and configured to transfer the variable output power provided by the gearbox, and a propeller coupled to the drive shaft and configured to accept power transferred to it from the drive shaft. The propeller is further configured to rotate and propel the flying submarine in both an airborne environment and in an underwater environment.
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Patent Agency Ranking
公开(公告)号：US20160122016A1
公开(公告)日：2016-05-05
申请号：US14528024
申请日：2014-10-30
Inventor： Stefano Mintchev , Ludovic Daler , Dario Floreano
IPC: B64C39/02
CPC classification number: B64C39/024 , A63H27/12 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/102 , B64C2201/108 , B64C2201/127
Abstract: An aerial vehicle including self-autonomous deployable arms and methods of deploying the vehicle are disclosed. The arms may include patterns located thereon that allow the arms to transition between wrapped, flat, and deployed configurations autonomously without the need for direct intervention by a user.
Abstract translation: 公开了一种包括自主部署臂的飞行器和部署车辆的方法。 臂可以包括位于其上的图案，其允许臂在包裹的，平坦的和部署的配置之间自主地转换，而不需要用户的直接干预。
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公开(公告)号：US09296270B2
公开(公告)日：2016-03-29
申请号：US13765144
申请日：2013-02-12
Applicant: Aurora Flight Sciences Corporation
Inventor： Robert Parks , Adam Woodworth , Tom Vaneck , Justin McClellan
CPC classification number: B64C37/00 , B60F5/02 , B63G8/001 , B63G8/08 , B63G2008/005 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/08 , B64C2201/102 , B64C2201/127 , B64C2201/165 , B64C2201/167 , F42B15/20
Abstract: A combined submersible vessel and unmanned aerial vehicle preferably includes a body structure, at least one wing structure, at least one vertical stabilizer structure, and at least one horizontal stabilizer structure. A propulsion system is coupled to the body structure and is configured to propel the flying submarine in both airborne flight and underwater operation. Preferably, the propulsion system includes a motor, a gearbox coupled to the motor and configured to receive power generated by the motor and provide variable output power, a drive shaft coupled to the gearbox and configured to transfer the variable output power provided by the gearbox, and a propeller coupled to the drive shaft and configured to accept power transferred to it from the drive shaft. The propeller is further configured to rotate and propel the flying submarine in both an airborne environment and in an underwater environment.
Abstract translation: 组合潜艇和无人驾驶飞行器优选地包括主体结构，至少一个翼结构，至少一个垂直稳定器结构和至少一个水平稳定器结构。 推进系统联接到车身结构并且被构造成在空中飞行和水下操作中推进飞行潜艇。 优选地，推进系统包括电动机，耦合到电动机并被配置为接收由电动机产生的电力并提供可变输出功率的变速箱;耦合到齿轮箱并被配置为传递由变速箱提供的可变输出功率的驱动轴， 以及联接到所述驱动轴并被配置为接受从所述驱动轴传递到其的动力的螺旋桨。 螺旋桨进一步构造成在空中环境和水下环境中旋转和推进飞行潜艇。
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公开(公告)号：US20150360777A1
公开(公告)日：2015-12-17
申请号：US14698803
申请日：2015-04-28
Applicant: Sima MOTTALE
Inventor： Sima MOTTALE
IPC: B64C39/02
CPC classification number: B64C39/024 , B64C27/04 , B64C27/10 , B64C39/08 , B64C2201/024 , B64C2201/042 , B64C2201/066 , B64C2201/102 , B64C2201/108 , B64C2201/126 , B64C2201/146 , B64D47/08 , Y02T50/55
Abstract: The present invention discloses an unmanned aerial vehicle capable of transforming its shape, comprising a) a control apparatus b) one or more propellers being fixed to the control apparatus, c) a multitude of flaps which are foldable reversibly from an open to a closed position, wherein the flaps provide i) in open position about a disc shape which is about in parallel to the plane of the rotating propeller, and ii) in closed position a shuttlecock shape, wherein, at least one of the flaps comprises a battery recharge element, such as a solar panel, photovoltaic element or elements, an electromagnetic harvesting element, a thermoelectric generator and/or a solar thermoelectric generator. The present invention relates also to a rotating disc being suitable for the vehicle, as well as the use of the vehicle and the rotating disc.
Abstract translation: 本发明公开了一种能够转换其形状的无人驾驶飞行器，包括：a）控制装置; b）固定在控制装置上的一个或多个螺旋桨，c）多个襟翼，其可从开放到闭合位置可逆地折叠 ，其中所述翼片提供i）围绕与所述旋转螺旋桨的平面平行的盘形状的打开位置，以及ii）在关闭位置中的羽毛球形状，其中所述翼片中的至少一个包括电池再充电元件 ，例如太阳能电池板，光电元件或元件，电磁收集元件，热电发电机和/或太阳能热电发电机。 本发明还涉及适用于车辆的旋转盘以及车辆和旋转盘的使用。
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249.发明申请SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE 有权长寿命垂直起落架及吊车的系统，装置及方法公开(公告)号：US20150336663A1
公开(公告)日：2015-11-26
申请号：US14507313
申请日：2014-10-06
Applicant: Aurora Flight Sciences Corporation
Inventor： JAMES DONALD PADUANO , PAUL NILS DAHLSTRAND , JOHN BROOKE WISSLER , ADAM WOODWORTH
CPC classification number: B64C27/52 , B64C3/42 , B64C5/02 , B64C9/00 , B64C13/16 , B64C25/10 , B64C29/00 , B64C29/0033 , B64C29/0091 , B64C29/02 , B64C29/04 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102 , B64C2201/108 , B64C2201/162 , B64C2201/187 , B64D27/02 , B64D43/00
Abstract: A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.
Abstract translation: 根据本发明的一个方面的垂直起飞（VTOL）飞机包括机身，具有位于机身尾端的全移动水平稳定器的尾翼，机身具有位于机身的大致中间位置 翼的远端，其中翼被配置成使用位于机身的每一侧上的倾斜铰链在基本上直的机翼构型和倾斜翼结构之间转换。 垂直起落飞行器还可以包括一个或多个可伸缩的弹簧支撑件，其中可伸缩的弹簧支撑构造成从翼的远端中的每一个展开。
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公开(公告)号：US20150284075A1
公开(公告)日：2015-10-08
申请号：US14243540
申请日：2014-04-02
Applicant: Sikorsky Aircraft Corporation
Inventor： Mark R. Alber
CPC classification number: B64C39/024 , B64C29/02 , B64C2201/021 , B64C2201/088 , B64C2201/102
Abstract: A vertical take-off and landing (VTOL) aircraft is provided and includes a fuselage, inboard wings extending from opposite sides of the fuselage to define a support plane and engine nacelles disposed along the wings. Each of the wings includes ground alighting elements and a variable geometry such that a portion of the ground alighting elements are alignable with the support plane during in-flight conditions and displaceable from the support plane.
Abstract translation: 提供垂直起飞和降落（VTOL）飞机，并包括机身，内侧翅膀从机身的相对侧延伸，以限定沿机翼设置的支撑平面和发动机舱。 每个翼包括地面下落元件和可变几何形状，使得地面下落元件的一部分在飞行状态期间与支撑平面对准并且可从支撑平面移位。
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