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1. 发明公开

EP3131811A1 AIRBORNE RIGID KITE WITH ON-BOARD POWER PLANT FOR SHIP PROPULSION 审中-公开
标题翻译： STARRER，IN DER LUFT FLIEGENDER DRACHEN MIT KRAFTWERK AN BORDFÜRSCHIFFSANTRIEB
公开(公告)号：EP3131811A1
公开(公告)日：2017-02-22
申请号：EP15779413.2
申请日：2015-04-13
申请人： X Development LLC
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：一种具有空中翼片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，固定到飞行器架并固定到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所述车辆接收电力; 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牵引力。

2. 发明公开

EP3008332A1 SYSTEM AND PROCESS FOR STARTING THE FLIGHT OF POWER WING AIRFOILS, IN PARTICULAR FOR WIND GENERATOR 有权
标题翻译：系统和方法用于启动电力WINGS配置文件的运行，尤其是用于风力涡轮机
公开(公告)号：EP3008332A1
公开(公告)日：2016-04-20
申请号：EP14748288.9
申请日：2014-06-05
申请人： Kite Gen Research S.R.L.
发明人： IPPOLITO, Massimo
IPC分类号： F03D5/00
CPC分类号： F03D7/06 , F03D5/00 , F05B2240/921 , F05B2240/923 , F05B2260/85 , Y02E10/70
摘要： A system (1) is described, for starting the flight of power wing airfoils (7), in particular for a wind generator (5), comprising at least one wing profile (7), operatively connected through control tie-rods (9), to winches or other control mechanisms of a flight of such wing profile (7), and at least one autonomous transporting flying vector (11) adapted to be connected through disengageable connecting means (13) to at least one wing profile (7) and to transport in flight such wing profile (7). A process is further described, for starting the flight of such power wing airfoils (7) through such system (1).

3. 发明公开

EP3194765A1 CARBON FIBER MOTOR ROTOR INTEGRATING PROPELLER MOUNT 审中-公开
标题翻译：碳纤维电机转子集成螺旋桨座
公开(公告)号：EP3194765A1
公开(公告)日：2017-07-26
申请号：EP15836339.0
申请日：2015-08-21
申请人： X Development LLC
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： 1.一种与空中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座的刚性插入件，其中所述前凸缘罐和后凸缘包括碳纤维和其中所述前凸缘的后端附接到所述罐的前端，并且所述后凸缘安装到所述罐的后端，其中所述刚性插入件结合到所述前凸缘; 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穿过其定位的管。

4. 发明授权

EP2631468B1 System and method for airborne wind energy production 有权
标题翻译：系统和Verfahren zur Herstellung von Windenergie im Fluge
公开(公告)号：EP2631468B1
公开(公告)日：2016-09-07
申请号：EP12157057.6
申请日：2012-02-27
申请人： Ampyx Power B.V.
发明人： Ruiterkamp, Richard, Dr.
IPC分类号： F03D5/00
CPC分类号： B64C39/022 , B64C19/00 , B64C31/02 , B64C39/024 , F03D5/00 , F03D5/02 , F03D9/255 , F03D13/20 , F05B2240/92 , F05B2240/921 , F05B2240/923 , H02G11/02 , Y02E10/70
摘要： The inventions provides for a system for electric power production from wind (50) comprising a glider (10), said glider (10) having an airfoil (14), on-board steering means (20, 22, 24) for pitching, rolling and yawing the glider (10) when airborne, a flight control means (64) for operation of the steering means (20, 22, 24), and a connection means for a tether (44), the system further comprising a ground station (40), said ground station (40) comprising a reel (42) for the tether (44), a rotating electrical machine (46) connected to the reel (42), and a ground station control means (66) for operation of the reel (42) and the rotating electrical machine (46), and the system further comprising a master control means (62) for operation of the system in at least two alternative operation modes, wherein a first operation mode of the system is provided for electric power production with the rotating electrical machine (46) from a rotation of the reel (42) induced by reeling out the tether (44) using a lift force generated upon exposure of the airfoil (14) of the airborne glider (10) to wind (50), and wherein a second operation mode of the system is provided for system recovery by driving the reel (42) with the rotating electrical machine (46), thereby reeling in the tether (44) onto the reel (42). The invention further provides for a method for operation of a system for electric power production from wind (50), for a glider (10) for a system according to the invention and for use of a glider (10) for production of electric power form wind.
摘要翻译：本发明提供了一种用于从包括滑翔机（10）的风（50）的电力生产系统，所述滑翔机（10）具有翼型件（14），车载转向装置（20,22,24），用于俯仰，滚动并且当机载时偏航滑翔机（10），用于操纵转向装置（20,22,24）的飞行控制装置（64）和用于系绳（44）的连接装置，所述系统还包括地面站（ 40），所述地面站（40）包括用于所述系绳（44）的卷轴（42），连接到所述卷轴（42）的旋转电机（46），以及用于操作所述系统的地面站控制装置卷轴（42）和旋转电机（46），并且所述系统还包括主控制装置（62），用于以至少两种替代操作模式操作所述系统，其中所述系统的第一操作模式被提供用于电通过旋转电机（46）从卷轴（42）的旋转而产生的电力产生， 44）使用在机载滑翔机（10）的翼型（14）暴露于风（50）时产生的提升力，并且其中系统的第二操作模式被提供用于通过驱动卷轴（42）与旋转电机（46），从而将系绳（44）卷绕到卷轴（42）上。本发明还提供了一种用于从风（50），用于根据本发明的系统的滑翔机（10）和用于生产电力形式的滑翔机（10）的用于电力生产的系统的操作的方法风。

5. 发明公开

EP1979613A1 A FLYING WIND ENERGY CONVERSION APPARATUS 审中-公开
标题翻译： FLYING WIND能量转换装置
公开(公告)号：EP1979613A1
公开(公告)日：2008-10-15
申请号：EP07704989.8
申请日：2007-01-24
申请人： Goodall, Peter Robert
发明人： Goodall, Peter Robert
IPC分类号： F03D11/04 , B64B1/00 , F03D3/00
CPC分类号： B64B1/00 , F03D1/00 , F03D3/002 , F03D9/255 , F03D13/20 , F03D15/10 , F05B2240/212 , F05B2240/917 , F05B2240/922 , F05B2240/923 , F05B2260/4021 , F05B2260/4031 , Y02E10/728 , Y02E10/74
摘要： A Wind energy conversion apparatus comprising a wind turbine supported by, or integral with, a lighter-than-air structure, the part of the turbine that rotates being rotated by the wind whilst at the same time absorbing substantially all of the force of the wind so that the position of the apparatus can be maintained.

6. 发明公开

EP3386862A1 SYSTEME D'EOLIENNE DE SECOURS COMPRENANT UN DISPOSITIF DE BLOCAGE EN ROTATION DE LA TURBINE 有权
公开(公告)号：EP3386862A1
公开(公告)日：2018-10-17
申请号：EP16819615.2
申请日：2016-12-07
申请人： Safran Electrical & Power
发明人： POLIN, Eric, Joseph, Etienne , GUIRAUD, Julien
IPC分类号： B64D41/00
CPC分类号： F01D21/14 , B64D41/007 , F03D9/32 , F05B2220/10 , F05B2240/92 , F05B2240/923 , F05D2220/34 , Y02E10/728 , Y02T50/671
摘要： The invention relates to an emergency wind turbine system (20) for an aircraft comprising an outer structure (201) in which an opening is made, said emergency wind turbine system (20) comprising an emergency wind turbine (22) comprising: a mast (23) extending along a longitudinal axis (24); a turbine (25) comprising a body (30) which is mounted on the mast (23) such that it rotates about an axis of rotation (26), and a single blade or two blades (32) extending radially from the body (30) between a blade root received in the body (30) and a blade head, the at least one blade root extending along the same blade root axis (35); a locking device (29) designed to lock the rotation of the body (30) of the turbine (25) about the axis of rotation (26), when the emergency wind turbine (22) moves between a so-called retracted position and a so-called deployed position, in a position such that the blade root axis (35) forms an acute and non-null locking angle (α) with an orthogonal projection (24') of the longitudinal axis (24) of the mast (23) over a plane (P) substantially perpendicular to the axis of rotation (26) of the turbine (25) and in which the blade root axis (35) extends, so as to reduce the volume swept by the emergency wind turbine (22) when it moves between the retracted position and the deployed position.

7. 发明公开

EP3348486A1 RELEASE MECHANISM 有权
公开(公告)号：EP3348486A1
公开(公告)日：2018-07-18
申请号：EP17461504.7
申请日：2017-01-14
申请人： Hamilton Sundstrand Corporation
发明人： BOBAK, Jakub Mateusz , KIELCZYKOWSKI, Przemyslaw
IPC分类号： B64D41/00
CPC分类号： B64D41/007 , F03D9/32 , F05B2240/923 , F05D2220/34 , F16H21/26 , F16H21/44
摘要： A toggle release mechanism (100) comprises a base element (102), a toggle element (104) and an actuating rod (142). The toggle element (104) is rotatably mounted at a first end (112) to the base element (102) about a first axis (114) for rotation between a first, locking position and a second, release position. The actuating rod (142) has a central portion (144) extending through the toggle element (104) and first and second end portions (146, 148) projecting on opposed sides thereof for engagement with actuators (154) arranged on opposed sides of the release mechanism (100). The actuating rod (142) further comprises a mounting flange (156) projecting therefrom at a boundary between the central portion (144) and a first end portion (146). The mounting flange (156) has a first hole (158) therein for receiving a first fastener (160). A surface (162) of the toggle element (104) facing the mounting flange (156) has a bore (164) formed therein for receiving the first fastener (160). The mechanism further comprises a mounting element (166) slidably received on the second end (148) of the actuating rod (142). The mounting element (166) has a bore (168) for receiving the second end (148) of the actuator rod (142) and a second hole (170) for receiving a second fastener (176). A surface (174) of the toggle element (104) facing the mounting element (166) having a second bore (176) formed therein for receiving the second fastener (172).

8. 发明公开

EP3131811A4 AIRBORNE RIGID KITE WITH ON-BOARD POWER PLANT FOR SHIP PROPULSION 审中-公开
公开(公告)号：EP3131811A4
公开(公告)日：2017-11-01
申请号：EP15779413
申请日：2015-04-13
申请人： X DEV LLC
发明人： VANDER LIND DAMON , VAN ALSENOY THOMAS , DEVAUL RICHARD WAYNE
IPC分类号： B63J3/00 , B63B35/44 , B64C31/06 , B64C39/02 , B64F3/00 , F03D1/00 , F03D9/00
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 , F03D9/25 , 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.

9. 发明授权

EP2003054B1 Device for supplying electricity 有权
标题翻译：电源设备
公开(公告)号：EP2003054B1
公开(公告)日：2009-12-16
申请号：EP07110337.8
申请日：2007-06-15
申请人： SAAB AB
发明人： Nilsson, Bernt
IPC分类号： B64C11/00 , B64C27/00 , B64D41/00 , F03D11/04
CPC分类号： B64C27/00 , B64C11/00 , B64D41/007 , F03D9/25 , F05B2240/923 , Y02E10/725
摘要： The present invention relates to device (10) for supplying electricity to electrical equipment on a first element (3) drivable for rotating operation with a predetermined rotation rate. Said device (10) comprises an electricity producing means (11) provided with a stator and a rotor that are rotatable in relation to each other. One of the rotor and stator is attached to said first element (3) and the other to a second element (14) provided with at least one braking member (16). In accordance with a predetermined drag coefficient C d , when interacting with a surrounding fluid medium in rotating operation a braking torque T AB is induced, which results in a difference f diff in rotation rate between the first element (3) and said second element (14). An output P G to said electricity producing means (11) is based on the product of said braking torque T AB and said rotation rate difference f diff .

10. 发明公开

EP3194765A4 CARBON FIBER MOTOR ROTOR INTEGRATING PROPELLER MOUNT 审中-公开
公开(公告)号：EP3194765A4
公开(公告)日：2018-05-02
申请号：EP15836339
申请日：2015-08-21
申请人： X DEV LLC
发明人： VANDER LIND DAMON , HOMSY GEORGE EDWARD
IPC分类号： F03D1/06 , F01D5/02 , F03D9/00
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.

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