ADJUSTABLE SAIL AND A VESSEL COMPRISING SUCH A SAIL
    1.
    发明申请
    ADJUSTABLE SAIL AND A VESSEL COMPRISING SUCH A SAIL 审中-公开
    可调节的沙滩和包含这样的船的船只

    公开(公告)号:WO2016076727A1

    公开(公告)日:2016-05-19

    申请号:PCT/NO2015/000028

    申请日:2015-11-16

    Inventor: LAMBERG, Vemund

    CPC classification number: B63H9/08 B63H9/0607 B63H9/0657 B63H9/10 B64C31/06

    Abstract: There is disclosed a sail for producing propulsive power or lift in a fluid, where the sail comprises a first layer and a second layer where the first layer and the second layer are connected along at least one corresponding side, and the first layer and the second layer define a cross-sectional shape of the sail substantially perpendicular to a longitudinal direction of the sail. The shape of the first layer is adjustable and/or the shape of the second layer is adjustable such that the cross-sectional shape of the sail is adjustable. There is also disclosed a vessel or a sailboat comprising such a sail.

    Abstract translation: 公开了一种用于在流体中产生推进力或升力的帆,其中帆包括第一层和第二层,其中第一层和第二层沿着至少一个对应的侧面连接,第一层和第二层 层限定了基本上垂直于帆的纵向方向的帆的横截面形状。 第一层的形状是可调节的和/或第二层的形状是可调节的,使得帆的横截面形状是可调节的。 还公开了一种包括这种帆的船只或帆船。

    A KITE
    2.
    发明申请
    A KITE 审中-公开
    风筝

    公开(公告)号:WO2016075461A1

    公开(公告)日:2016-05-19

    申请号:PCT/GB2015/053419

    申请日:2015-11-11

    CPC classification number: B64C31/06 B64D47/02 F03D5/00 Y02E10/70

    Abstract: A kite for use in a system for extracting energy from the wind comprises: a wing (1) having a roll neutral point or zone when the kite is in flight; a tether (4) coupled directly or indirectly to the wing; a rigid spar arrangement (2); tensile couplings (3) from the spar arrangement to multiple locations on the wing; and an actuator linkage arrangement (6, 7, 10,11) having a length dimension that can be controllably adjusted. The spar arrangement has first and second attachments (8, 5) to the tether, at the first attachment (8) the spar arrangement is fixed to the tether at a location that is above a roll neutral point or zone of the wing, and at the second attachment (5) the spar arrangement is attached to the tether by the actuator arrangement (6, 7, 10, 11) at a location that is below the roll neutral point or zone of the wing.

    Abstract translation: 用于从风中提取能量的系统中使用的风筝包括:当风筝在飞行中时具有滚动中性点或区域的翼(1); 连接器(4),直接或间接地连接到机翼上; 刚性翼梁布置(2); 从翼梁装置到机翼上的多个位置的拉伸联轴器(3) 以及具有可被可调节地调节的长度尺寸的致动器联动装置(6,7,10,11)。 翼梁装置在系绳上具有第一和第二附接件(8,5),在第一附接件(8)处,翼梁装置在位于机翼的中立点或区域上方的位置处固定到系绳上,并且在 所述第二附件(5)所述翼梁装置通过所述致动器装置(6,7,10,11)在位于所述翼的中性点或区域下方的位置附接到所述系绳。

    CURVATURE SENSING TETHERED AIRCRAFT
    3.
    发明申请
    CURVATURE SENSING TETHERED AIRCRAFT 审中-公开
    曲轴感应三角飞机

    公开(公告)号:WO2015094641A1

    公开(公告)日:2015-06-25

    申请号:PCT/US2014/068139

    申请日:2014-12-02

    Applicant: GOOGLE INC.

    Abstract: A system (100,400) may include a tether (120,420) connected to a ground station (110). The tether (120,420) may include at least two bridle segments (122,123,124,422,423,424). The system may further include an aerial vehicle (130) connected to the at least two bridle segments (122,123,124,422,423,424). The system (100,400) may also include at least one sensor (160A-D) and a control system. The control system may be configured to: a) receive sensor data from the at least one sensor (160A-D); and b) determine a tether roll angle (450) based on the sensor data. The tether roll angle (450) may represent an angle between the tether (420) and an axis of the aerial vehicle (440). Optionally, the control system may also be configured to determine a curvature of a path (150) of the aerial vehicle (130) based on the tether roll angle (450). The control system may additionally be configured to control at least one control surface of the aerial vehicle (130) based on the curvature of the path (150).

    Abstract translation: 系统(100,400)可以包括连接到地面站(110)的系绳(120,420)。 系绳(120,420)可以包括至少两个线段(122,123,124,422,423,424)。 所述系统还可以包括连接到所述至少两个线段(122,123,124,422,423,424)的航空器(130)。 系统(100,400)还可以包括至少一个传感器(160A-D)和控制系统。 所述控制系统可以被配置为:a)从所述至少一个传感器(160A-D)接收传感器数据; 以及b)基于所述传感器数据确定系绳侧倾角(450)。 系绳侧倾角(450)可以表示系绳(420)与飞行器(440)的轴线之间的角度。 可选地,控制系统还可以被配置为基于系绳滚动角度(450)来确定空中飞行器(130)的路径(150)的曲率。 控制系统还可以被配置为基于路径(150)的曲率来控制空中飞行器(130)的至少一个控制表面。

    ARC-TYPE WING WITH IMPROVED SHOULDERS
    4.
    发明申请
    ARC-TYPE WING WITH IMPROVED SHOULDERS 审中-公开
    具有改进的肩膀的弧型

    公开(公告)号:WO2015037026A1

    公开(公告)日:2015-03-19

    申请号:PCT/IT2014/000233

    申请日:2014-09-04

    CPC classification number: B64C31/06 B64C9/323

    Abstract: An arc-type wing (1) with high aerodynamic efficiency is described, composed of a central arc section (13) connected to pairs of bridles (11, 12) through a pair of shoulders (14, 15); each shoulder (14, 15) supports a panel (2) equipped with an air brake (21), and the panel (2) houses on board sensors, electric energy accumulators, micro- turbines, and a card for collecting data emitted by the sensors.

    Abstract translation: 描述了具有高空气动力效率的弧形翼(1),其通过一对肩部(14,15)连接到一对桁条(11,12)的中心弧形部分(13)。 每个肩部(14,15)支撑配备有空气制动器(21)的面板(2),并且面板(2)容纳在板上的传感器,蓄电池,微型涡轮机和用于收集由 传感器。

    QUICK-DISCONNECTING DEVICE, IN PARTICULAR FOR KITE- SURF
    5.
    发明申请
    QUICK-DISCONNECTING DEVICE, IN PARTICULAR FOR KITE- SURF 审中-公开
    快速断开设备,特别适用于KITE-SURF

    公开(公告)号:WO2013111169A1

    公开(公告)日:2013-08-01

    申请号:PCT/IT2013/000005

    申请日:2013-01-09

    Abstract: A quick-disconnecting device (1), in particular for kite-surf, comprising a fixed element (3) and a moving element (5) having an operating connecting position in which the moving element (5) is kept integral with the fixed element (3) by interposing a blocking system (7), and an operating disconnecting position in which the moving element (5) is disengaged from the fixed element (3) by actuating the blocking system (7), such moving element (5) being equipped with a first connecting end (9), of a terminal (21) of a connecting element to by actuating the blocking system (7), such moving element (5) cooperating with the fixed element (3) through a lever-type dynamics around a fulcrum point (F) interposed between the moving element (5) and the fixed element (3),. such device (1) further comprising an automatic fastening system (40) of the moving element (5) to the connecting element.

    Abstract translation: 一种快速断开装置(1),特别是用于风筝冲浪的装置,包括具有操作连接位置的固定元件(3)和移动元件(5),移动元件(5)与固定元件 (3)通过插入阻挡系统(7)以及通过致动所述阻塞系统(7)使所述移动元件(5)从所述固定元件(3)脱离的操作断开位置,所述移动元件(5)是 配备有连接元件的端子(21)的第一连接端(9),以通过致动所述阻塞系统(7),所述移动元件(5)通过杠杆式动力学与所述固定元件(3)配合 围绕位于移动元件(5)和固定元件(3)之间的支点(F)。 这种装置(1)还包括移动元件(5)到连接元件的自动紧固系统(40)。

    KITE GROUND STATION AND SYSTEM USING SAME
    6.
    发明申请
    KITE GROUND STATION AND SYSTEM USING SAME 审中-公开
    风筝地台和系统使用相同

    公开(公告)号:WO2013096345A1

    公开(公告)日:2013-06-27

    申请号:PCT/US2012/070424

    申请日:2012-12-18

    Abstract: A kite system with a ground station adapted for airborne power generation. The kite system may include a kite which comprises one or more airfoils which have mounted thereon a plurality of turbine driven generators. The turbine driven generators may also function as motor driven propellers in a powered flight mode, which may be used during take -off, which may include aspects of vertical take-off and landing. A perch adapted to facilitate the take-off and landing may be used as part of the system. The perch may pivot such that the pivot is oriented towards the tension direction of the tether.

    Abstract translation: 具有适用于机载发电的地面站的风筝系统。 风筝系统可以包括风筝,其包括一个或多个已经安装有多个涡轮驱动发电机的翼型件。 涡轮驱动发电机还可以以动力飞行模式用作电动机驱动的螺旋桨,其可以在起飞期间使用,其可以包括垂直起飞和着陆的方面。 适用于起飞和着陆的栖息处可用作系统的一部分。 鲈鱼可以枢转,使得枢轴朝向系绳的张力方向定向。

    DRACHEN MIT VERÄNDERLICHEM PROFIL
    7.
    发明申请
    DRACHEN MIT VERÄNDERLICHEM PROFIL 审中-公开
    具有可变轮廓DRAGON

    公开(公告)号:WO2012143058A1

    公开(公告)日:2012-10-26

    申请号:PCT/EP2011/056450

    申请日:2011-04-21

    Inventor: AHRENS, Uwe

    CPC classification number: B63B35/7979 B64C31/06 B64D2013/0674

    Abstract: Die vorliegende Erfindung betrifft einen Strömungskörper (2), insbesondere einen Staudruckströmungskörper, insbesondere einen Drachen, der insbesondere als Zugströmungskörper ausgebildet ist, sowie ein Verfahren zum Fliegen eines Strömungskörpers, aufweisend Steuerleinenbefestigungsvorrichtungen (8) zur Befestigung von, insbesondere unabhängig voneinander beweglichen, Steuerleinen (6) und/oder, insbesondere unabhängig voneinander bewegliche, Steuerleinen, wobei die mindestens eine Strömungsfläche relativ zueinander bewegliche Strömungsflächenabschnitte (9) aufweist und wobei Leinenbefestigungsvorrichtungen und/oder Steuerleinen mit den relativ zueinander bewegliche Strömungsflächenabschnitten gekoppelt sind, dadurch gekennzeichnet, dass mehr als vier Leinenbefestigungsvorrichtungen und/oder Steuerleinen vorgesehen sind und jeweils mit einem der relativ zueinander beweglichen Strömungsflächenabschnitten gekoppelt sind.

    Abstract translation: 本发明涉及一种流量主体(2),特别是背压流体,特别是风筝,其被设计特别是作为Zugströmungskörper,和飞行的流体,其包括控制线附连装置的方法(8)紧固,尤其是彼此独立地可移动的,该控制线(6 )和/或,尤其是彼此独立地可移动的,控制线,其特征在于,表面相对于彼此可移动的翼型件部分的所述至少一个流(9),并且其中所述电缆连接装置和/或控制线耦合到所述相对移动的翼型件部分,其特征在于,四个以上的线附连装置和 设置/或控制线,并且各自耦合到所述相对移动的翼面区段中的一个。

    INFLATABLE KITE WITH LEADING EDGE SWEPT FORWARDS AT WINGTIP
    8.
    发明申请
    INFLATABLE KITE WITH LEADING EDGE SWEPT FORWARDS AT WINGTIP 审中-公开
    有魅力的风筝与领先的边缘在WINGTIP

    公开(公告)号:WO2012103643A1

    公开(公告)日:2012-08-09

    申请号:PCT/CA2012/000115

    申请日:2012-02-01

    Inventor: HARRINGTON, Ross

    CPC classification number: B64C31/06 B63B35/7976

    Abstract: An inflatable kite has a continuous leading edge tube that is swept forward at its left and right wingtip ends so that bridle lines attaching the canopy to the user are forward of the centre of effort of the kite.

    Abstract translation: 充气风筝具有连续的前缘管,其在其左侧和右侧翼尖端向前扫掠,使得将冠层连接到使用者的襟翼线在风筝的中心之前。

    BIMODAL KITE SYSTEM
    10.
    发明申请
    BIMODAL KITE SYSTEM 审中-公开
    双体筝系统

    公开(公告)号:WO2009035492A1

    公开(公告)日:2009-03-19

    申请号:PCT/US2008/008791

    申请日:2008-07-18

    CPC classification number: B64C31/06 F03D5/00 Y02E10/70

    Abstract: A kite is disclosed. The kite comprises a first control element coupled to the kite in a first tether-force configuration, wherein the first control element is used to maintain controlled flight of the kite in the first tether- force configuration during a power generating phase. The kite further comprises a second control element coupled to the kite in a second tether-force configuration, wherein the second control element is used to maintain controlled flight of the kite in the second tether-force configuration during a recovery phase, and wherein during the recovery phase a tether force associated with the second tether-force configuration is reduced as compared to the tether force associated with the first tether-force configuration during the power generating phase

    Abstract translation: 风筝被披露。 风筝包括以第一系绳力构造耦合到风筝的第一控制元件,其中第一控制元件用于在发电阶段期间保持风筝在第一系绳力配置中的受控飞行。 风筝还包括以第二系绳力构造耦合到风筝的第二控制元件,其中第二控制元件用于在恢复阶段期间将风筝的控制飞行保持在第二系绳力构造中,并且其中在 与在发电阶段期间与第一系绳力构造相关联的系绳力相比,恢复阶段与第二系绳力构造相关联的系绳力减小

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