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1. 发明申请

WO2016196831A1 HARDPOINT STRAIN RELIEFS 审中-公开
公开(公告)号：WO2016196831A1
公开(公告)日：2016-12-08
申请号：PCT/US2016/035573
申请日：2016-06-02
申请人： GOOGLE INC.
发明人： CADMAN, Gregor, Boone , VANDER LIND, Damon
IPC分类号： B64C39/02 , B64C31/06
CPC分类号： B64D1/08 , B64C27/04 , B64C31/06 , B64C39/022 , B64C39/024 , B64C39/10 , B64C2201/145 , B64F3/02 , F03D9/255 , F03D9/32
摘要： A hardpoint relief pad (300) is described and includes a base surface (310), a hardpoint overlay (320), and a first stress relief area (330A). The base surface is configured to conform to and be fixedly attached to an interior surface (331) of an aerial vehicle wing. The hardpoint overlay (320) protrudes above adjacent areas of the hardpoint relief pad and is adapted to conform to a hardpoint (323). The hardpoint protrudes from the interior surface of the wing and is configured to carry a load fixed to the hardpoint. The hardpoint overlay includes an oculus (322) that is configured to allow the load to be fixed to the hardpoint through the hardpoint overlay. The first stress relief area (330A) protrudes above adjacent areas of the hardpoint relief pad and also forms a hollow cavity (332) between the first stress relief area and the interior surface of the wing.
摘要翻译：描述了硬点浮雕垫（300），并且包括基面（310），硬点覆盖层（320）和第一应力消除区域（330A）。基座表面构造成符合并固定地连接到飞行器机翼的内表面（331）。硬点覆盖层（320）突出在硬点浮雕垫的相邻区域上方并且适于符合硬点（323）。硬点从机翼的内表面突出并且被配置为承载固定到硬点的负载。硬点覆盖包括一个被配置为允许负载通过硬点覆盖固定到硬点的一个oculus（322）。第一应力消除区域（330A）突出在硬点浮雕垫的相邻区域上方，并且还在第一应力释放区域和机翼的内表面之间形成中空腔（332）。

2. 发明申请

WO2016148870A1 PIVOTING PERCH FOR FLYING WIND TURBINE PARKING 审中-公开
标题翻译：起飞风车停泊
公开(公告)号：WO2016148870A1
公开(公告)日：2016-09-22
申请号：PCT/US2016/019737
申请日：2016-02-26
申请人： GOOGLE INC.
发明人： HACHTMANN, Brian , VANDER LIND, Damon , EVERS, Maaike , SIMONIAN, Michael
IPC分类号： F03D13/20 , F03D1/02 , F03D9/34 , B64D41/00
CPC分类号： F03D7/0268 , B64C31/06 , F03D13/20 , F05B2240/917 , F05B2240/921 , Y02E10/723 , Y02E10/728
摘要： An airborne wind turbine system is provided including an aerial vehicle having a fuselage, an electrically conductive tether having a first end secured to the aerial vehicle and a second end secured to a rotatable drum positioned on a tower onto which the tether is wrapped when the aerial vehicle is reeled in, a perch extending from the tower, one or more perch booms attached to the perch panel and pivotabiv mounted to the tower, wherein when the aerial vehicle is secured to the perch, the aerial vehicle is positionable in a lowered parked position, and wherein the aerial vehicle is movable to a raised parked position caused by rotation of the one or more perch booms with respect to the tower.
摘要翻译：提供了一种机载风力涡轮机系统，其包括具有机身的飞行器，具有固定到飞行器的第一端的导电系绳，以及固定到位于塔架上的可旋转滚筒的第二端，当天线车辆被卷入，从塔架延伸的鲈鱼，一个或多个固定在船尾面板上的鲈鱼吊杆和枢轴安装到塔架上，其中当飞行器固定在鲈鱼上时，飞行器可定位在降低的停放位置，并且其中所述空中飞行器可移动到由所述一个或多个桅杆相对于所述塔的旋转引起的升高的停放位置。

3. 发明申请

WO2016003698A1 SYSTEMS AND METHODS FOR CONTROLLING ROTATION AND TWIST OF A TETHER 审中-公开
标题翻译：用于控制旋转和旋转的系统和方法
公开(公告)号：WO2016003698A1
公开(公告)日：2016-01-07
申请号：PCT/US2015/037091
申请日：2015-06-23
申请人： GOOGLE INC.
发明人： PATTEN, Elias, Wolfgang , VANDER LIND, Damon , GILROYSMITH, Bryan, Christopher , HACHTMANN, Brian
IPC分类号： F03D11/00 , F03D11/04 , F03D9/00 , F03D1/02 , B64F3/00 , B64C39/02
CPC分类号： B64F3/02 , F03D7/02 , F05B2240/921 , Y02E10/723
摘要： A system may include a tether, a slip ring, a tether gimbal assembly, a drive mechanism, a control system. The tether may include a distal tether end coupled to an aerial vehicle, a proximate tether end, and at least one insulated electrical conductor coupled to the aerial vehicle. The slip ring may include a fixed portion and a rotatable portion, where the rotatable portion is coupled to the tether. The tether gimbal assembly may be rotatable about at least one axis and is coupled to the fixed portion of the slip ring. The drive mechanism may be coupled to the slip ring and configured to rotate the rotatable portion of the slip ring. And the control system may be configured to operate the drive mechanism to control twist in the tether.
摘要翻译：系统可以包括系绳，滑环，系绳万向节组件，驱动机构，控制系统。系绳可以包括联接到空中飞行器的远端系绳端，近端系绳端以及耦合到空中飞行器的至少一个绝缘电导体。滑环可以包括固定部分和可旋转部分，其中可旋转部分联接到系绳。系绳万向节组件可以围绕至少一个轴线旋转并且联接到滑环的固定部分。驱动机构可以联接到滑环并且被配置为旋转滑环的可旋转部分。并且控制系统可以被配置为操作驱动机构以控制系绳中的扭转。

4. 发明申请

WO2015160697A1 AIRBORNE RIGID KITE WITH ON-BOARD POWER PLANT FOR SHIP PROPULSION 审中-公开
标题翻译：带有板载动力装置的AIRBORNE RIGID KITE用于船舶推进
公开(公告)号：WO2015160697A1
公开(公告)日：2015-10-22
申请号：PCT/US2015/025553
申请日：2015-04-13
申请人： GOOGLE INC.
发明人： VANDER LIND, Damon , VAN ALSENOY, Thomas , DEVAUL, Richard, Wayne
IPC分类号： B63J3/00 , F03D9/00 , F03D1/00 , B64C31/06 , B64C39/02 , B64F3/00 , B63B35/44
CPC分类号： B64C39/022 , B63H9/00 , B63H9/0685 , B63H21/20 , B63J2003/002 , B63J2003/046 , B64C31/06 , B64C2201/205 , B64D3/00 , B64F1/36 , B64F3/00 , B64F3/02 , C02F1/20 , C02F1/4693 , C02F2101/10 , C25B1/04 , C25B9/00 , F03D5/00 , F03D9/008 , F03D9/25 , F03D9/32 , F05B2240/917 , F05B2240/921 , F05B2240/923 , Y02E10/70 , Y02E10/725 , Y02E10/728 , Y02E60/366 , Y02P20/133 , Y02T70/5209 , Y02T70/5218 , Y02T70/70 , Y02T90/46
摘要： A vehicle-based airborne wind turbine system having an aerial wing, a plurality of rotors each having a plurality of rotatable blades positioned on the aerial wing, an electrically conductive tether secured to the aerial wing and secured to a ground station positioned on a vehicle, wherein the aerial wing is adapted to receive electrical power from the vehicle that is delivered to the aerial wing through the electrically conductive tether; wherein the aerial wing is adapted to operate in a flying mode to harness wind energy to provide a first pulling force through the tether to pull the vehicle; and wherein the aerial wing is also adapted to operate in a powered flying mode wherein the rotors may be powered so that the turbine blades serve as thrust- generating propellers to provide a second pulling force through the tether to pull the vehicle.
摘要翻译：一种具有空中翼面的车载机载风力涡轮机系统，多个转子，每个转子具有位于空中飞翼上的多个可旋转叶片，固定在飞行器上并固定在位于车辆上的地面站的导电系绳，其中所述空中翼适于从通过所述导电系绳传送到所述空中翼的车辆接收电力; 其中所述空中翼适于以飞行模式操作以利用风能以提供穿过所述系绳的第一拉力以拉动所述车辆; 并且其中所述空中翼还适于以动力飞行模式操作，其中所述转子可以被供电，使得所述涡轮机叶片用作推力产生螺旋桨，以提供通过所述系绳拉动所述车辆的第二拉力。

5. 发明申请

WO2015138252A1 RADIATOR CONFIGURATION FOR A FLYING WIND TURBINE THAT PASSIVELY CONTROLS AIRFLOW 审中-公开
标题翻译：用于飞行风控制的飞行风轮的散热器配置
公开(公告)号：WO2015138252A1
公开(公告)日：2015-09-17
申请号：PCT/US2015/019252
申请日：2015-03-06
申请人： GOOGLE INC.
发明人： VANDER LIND, Damon
IPC分类号： F03D11/00 , F03D5/00 , F03D7/02
CPC分类号： F03D80/60 , F03D9/30 , F03D13/20 , F03D80/00 , F05B2240/921 , F05B2260/64 , Y02E10/72
摘要： In order to increase efficiency in aerial wind turbine vehicles, it is desirable to reduce the system drag associated with airflow across radiator in those cases where airflow exceeds the necessary flow to sufficiently cool the motor/generators. Exemplary embodiments herein include passive flow restrictors that can activate under varying flight conditions associated with known states of excessing cooling capacity.
摘要翻译：为了提高空中风力涡轮机车辆的效率，在气流超过必要流量以充分冷却马达/发电机的情况下，期望减少与散热器的气流相关联的系统阻力。本文的示例性实施例包括可在与已知的过剩冷却能力状态相关联的变化的飞行条件下激活的被动流量限制器。

6. 发明申请

WO2015094471A1 PATH BASED POWER GENERATION CONTROL FOR AN AERIAL VEHICLE 审中-公开
标题翻译：基于路径的航空母舰发电控制
公开(公告)号：WO2015094471A1
公开(公告)日：2015-06-25
申请号：PCT/US2014/061386
申请日：2014-10-20
申请人： GOOGLE INC.
发明人： JENSEN, Kenneth , VANDER LIND, Damon
IPC分类号： B64C39/02 , B64B1/50 , F03D9/00
CPC分类号： G05D1/101 , B64C31/06 , B64C39/022 , F03D7/00 , F03D9/007 , F03D9/25 , F03D9/30 , F05B2240/921 , G05D1/0866 , H02S10/12 , Y02E10/723 , Y02E10/725
摘要： Methods and systems described herein relate to power generation control for an aerial vehicle. An example method may include operating an aerial vehicle in a crosswind-flight orientation substantially along a first flight path to generate power. The first flight path may- include a substantially circular path that allows the aerial vehicle to generate the power. While the aerial vehicle is in the crosswind-flight orientation the method may include determining to reduce the power being generated by the aerial vehicle, and responsive to the determination, determining a second flight path that will reduce the power generated by the aerial vehicle when operating on the second flight path. Once determined, the aerial vehicle may operate substantially along the second flight path.
摘要翻译：本文所述的方法和系统涉及用于飞行器的发电控制。示例性方法可以包括以基本上沿着第一飞行路径的侧风飞行方向操作飞行器以产生功率。第一飞行路径可以包括允许航空器产生电力的基本圆形路径。当飞行器处于侧风飞行方向时，该方法可以包括确定以减少由飞行器产生的功率，并且响应于该确定，确定第二飞行路径，其将在运行时减小飞行器产生的功率在第二个飞行路径。一旦确定，飞行器可以基本上沿着第二飞行路径操作。

7. 发明申请

WO2016032881A1 CARBON FIBER MOTOR ROTOR INTEGRATING PROPELLER MOUNT 审中-公开
标题翻译：碳纤维电机转子整合螺旋桨安装
公开(公告)号：WO2016032881A1
公开(公告)日：2016-03-03
申请号：PCT/US2015/046237
申请日：2015-08-21
申请人： GOOGLE INC.
发明人： VANDER LIND, Damon , HOMSY, George, Edward
IPC分类号： F03D1/06 , F03D9/00 , F01D5/02
CPC分类号： F03D9/32 , B64C39/022 , B64C39/024 , B64C2201/021 , B64C2201/12 , B64F3/02 , F03D1/0666 , F03D1/0691 , F03D5/00 , F03D9/25 , F05B2240/921 , F05B2240/923 , F05B2280/10 , F05B2280/6003 , Y02E10/70 , Y02E10/721
摘要： A rotor for use with an airborne wind turbine, wherein the rotor comprises a front flange, a can, a rear flange, and a rigid insert comprising a propeller mount, wherein the front flange, can, and rear flange comprise one of carbon fiber and spun aluminum, wherein a rear end of the front flange is attached to a front end of the can, and the rear flange is mounted to a rear end of the can, wherein the rigid insert is bonded to the front flange; and wherein the rigid insert comprises a tube that axially extends within the rotor to allow for the positioning of a driveshaft therethrough.
摘要翻译：一种与机载风力涡轮机一起使用的转子，其中所述转子包括前凸缘，罐，后凸缘和包括螺旋桨安装件的刚性插入件，其中所述前凸缘可以和所述后凸缘包括碳纤维和其特征在于，所述前凸缘的后端安装在所述罐的前端，所述后凸缘安装在所述罐的后端，其中所述刚性插入件与所述前凸缘接合; 并且其中所述刚性插入件包括在所述转子内轴向延伸以允许驱动轴通过其定位的管。

8. 发明申请

WO2016003580A1 HORIZONTAL TAIL SURFACE 审中-公开
标题翻译：水平尾部表面
公开(公告)号：WO2016003580A1
公开(公告)日：2016-01-07
申请号：PCT/US2015/034023
申请日：2015-06-03
申请人： GOOGLE INC.
发明人： KINNE, Peter , VANDER LIND, Damon , CADMAN, Gregor
IPC分类号： B64C9/08 , B64C5/02 , B64C5/10 , F03D11/00 , B64F3/00
CPC分类号： B64C5/16 , B64C39/022 , F03D5/00 , F05B2240/40 , F05B2240/917 , F05B2240/921 , Y02E10/70 , Y02E10/728
摘要： An aerial vehicle including a fuselage, a main wing attached to the fuselage, a support structure extending upwardly from the fuselage and having a front surface facing the main wing, an overhang positioned on a top of the support structure and extending towards the main wing, one or more rotating actuators positioned on the overhang, a rear elevator attached to the one or more rotating actuators that are configured to move the rear elevator from a flying mode position where a leading edge of the rear elevator faces the main wing to a hover mode position where the major surfaces of the rear elevator faces the main wing, and wherein the major surfaces of the rear elevator remain in front of the front surface of the support structure when the rear elevator is moved from the flying mode position to the hover mode position.
摘要翻译：一种飞行器，包括机身，附接到机身的主翼，从机身向上延伸并且具有面向主翼的前表面的支撑结构，位于支撑结构的顶部上并向主翼延伸的伸出部，一个或多个位于所述伸出部上的旋转致动器，附接到所述一个或多个旋转致动器的后部升降机，所述后部升降机构造成使所述后部升降机从所述后部升降机的前缘面向所述主翼的飞行模式位置移动到悬停模式后升降梯的主表面朝向主翼的位置，并且其中当后电梯从飞行模式位置移动到悬停模式位置时，后电梯的主表面保持在支撑结构的前表面的前面。

9. 发明申请

WO2015138289A1 RADIATOR AND DUCT CONFIGURATION ON AN AIRBORNE WIND TURBINE FOR MAXIMUM EFFECTIVENESS 审中-公开
标题翻译：空气动力涡轮机上的散热器和导管配置，实现最大的有效性
公开(公告)号：WO2015138289A1
公开(公告)日：2015-09-17
申请号：PCT/US2015/019390
申请日：2015-03-09
申请人： GOOGLE INC.
发明人： VANDER LIND, Damon
IPC分类号： F03D11/00 , F03D1/02
CPC分类号： F03D9/30 , F03D13/20 , F03D80/00 , F03D80/60 , F05B2240/921 , F05B2260/221 , Y02E10/72 , Y02E10/722 , Y02T50/675
摘要： In order io maximize cooling while minimizing drag in aerial vehicles of airborne wind turbines, it may be preferable to dissipate the cooling energy of the motors via a radiator in a region with advantageous airflow parameters. Aerial vehicle rotors operating in thrust mode may produce relatively more airflow velocity in certain regions further away from the center of the rotor blades, both radially and longitudinally. Placing a radiator in a rotor-supporting pylon and offset from the center of the rotor blades and aft of the rotor blades may allow for greater cooling while the aerial vehicle while in thrust mode.
摘要翻译：为了最大化冷却，同时最小化机载风力涡轮机的空中飞行器中的阻力，可优选通过具有有利气流参数的区域中的散热器来消散电动机的冷却能量。在推力模式下操作的空中转向架转子可在径向和纵向上在远离转子叶片中心的某些区域中产生相对更多的气流速度。将散热器放置在转子支撑塔中并偏离转子叶片的中心和转子叶片的后部可以允许在空中车辆处于推力模式时更大的冷却。

10. 发明申请

WO2015102855A2 EXTRUDED DRUM SURFACE FOR STORAGE OF TETHER 审中-公开
标题翻译：挤压表面用于储存四周
公开(公告)号：WO2015102855A2
公开(公告)日：2015-07-09
申请号：PCT/US2014/070100
申请日：2014-12-12
申请人： GOOGLE INC.
发明人： VANDER LIND, Damon , HACHTMANN, Brian
IPC分类号： F03D11/00 , F03D3/02 , H02G11/02 , B64C39/02 , B64F1/08 , B65H75/38
CPC分类号： B66D1/30 , B21C23/00 , B21C23/142 , B21C23/145 , B29C47/0004 , B29C47/0023 , B29C47/003 , B29C47/0059 , B29C47/021 , B29C47/8845 , B64C39/022 , B64F3/00 , B65H75/265 , B65H75/4405 , B65H75/4415 , B65H2701/528 , F03D9/25 , F03D9/30 , F05B2240/921 , Y02E10/725 , Y02P70/30 , Y10T29/49002
摘要： A drum for storing an electrically conductive tether having a first end secured to an aerial vehicle and a second end secured to a ground station that includes a drum frame rotatable about a drum axis, a drum surface positioned over the drum frame comprising a spiral extrusion wrapped around the drum frame, wherein the extrusion has a cross-section having an upper surface that is shaped to conform to an outer surface of the electrically conductive tether, and wherein the extrusion is adapted for dissipating heat generated through a transfer of electricity from the aerial vehicle to a ground station through the electrically conductive tether.
摘要翻译：一种用于存储具有固定到飞行器的第一端的导电系绳的滚筒和固定到地面站的第二端，所述第二端包括可围绕鼓轴线旋转的滚筒框架，位于鼓框架上方的滚筒表面包括螺旋挤压包装围绕所述鼓框架，其中所述挤压件具有横截面，所述横截面的上表面被成形为符合所述导电系绳的外表面，并且其中所述挤出件适于消散通过从所述空中传送电而产生的热量车辆通过导电系绳到地面站。

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