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    • 13. 发明授权
    • Curvature sensing
    • 曲率传感
    • US09056677B1
    • 2015-06-16
    • US14134781
    • 2013-12-19
    • Google Inc.
    • Kenneth JensenDamon Vander Lind
    • G05D1/08G05D1/06G05D1/10B64C31/06
    • B64C31/06B64C39/022B64C2201/148F03D7/02F03D9/25F03D13/20F05B2240/921Y02E10/723Y02E10/728
    • A system may include a tether connected to a ground station. The tether may include at least two bridle segments. The system may further include an aerial vehicle connected to the at least two bridle segments. The system may also include at least one sensor and a control system. The control system may be configured to: a) receive sensor data from the at least one sensor; and b) determine a tether roll angle based on the sensor data. The tether roll angle may represent an angle between the tether and an axis of the aerial vehicle. Optionally, the control system may also be configured to determine a curvature of a path of the aerial vehicle based on the tether roll angle. The control system may additionally be configured to control at least one control surface of the aerial vehicle based on the curvature of the path.
    • 系统可以包括连接到地面站的系绳。 系绳可以包括至少两个绷带段。 该系统可以进一步包括连接到该至少两个线段的航空器。 该系统还可以包括至少一个传感器和控制系统。 所述控制系统可以被配置为:a)从所述至少一个传感器接收传感器数据; 和b)基于传感器数据确定系绳侧倾角。 系绳侧倾角可以表示系绳与飞行器的轴线之间的角度。 可选地,控制系统还可以被配置为基于系绳滚角来确定飞行器的路径的曲率。 控制系统还可以被配置为基于路径的曲率来控制飞行器的至少一个控制表面。
    • 16. 发明申请
    • KITE POWER SYSTEM
    • 风筝动力系统
    • US20150048621A1
    • 2015-02-19
    • US14388402
    • 2013-03-27
    • E-KITE HOLDING B.V.
    • Coenraad, Louis SmeenkAlfred Van Den Brink
    • F03D9/00B65H75/44F03D5/00B64C31/06
    • F03D5/06B64C31/06B65H75/4481F03D5/00F03D9/25F05B2240/231Y02E10/70
    • A kite power system includes a ground control unit with a generator (30), and a kite connected to the generator (30) via at least two main traction cables (10, 11). A rotor part (31) of the generator (30) includes a winch pulley (32, 33) for each of the at least two main traction cables (10, 11), and each of the winch pulleys (32, 33) is indirectly mechanically connected to the generator (30). A further aspect relates to a kite for use in a kite power generation system, having an airfoil shaped body (20) with one or more air filling apertures (23) in a leading edge part of the airfoil shaped body (20). At least two main traction cables (10, 11) are connected to the airfoil shaped body (20), which further includes an additional filling aperture (21) in a side part of the airfoil shaped body (20).
    • 风筝动力系统包括具有发电机(30)的地面控制单元和经由至少两个主牵引电缆(10,11)连接到发电机(30)的风筝。 发电机(30)的转子部分(31)包括用于至少两个主牵引电缆(10,11)中的每一个的绞盘滑轮(32,33),并且每个绞盘滑轮(32,33)间接地 机械地连接到发电机(30)。 另一方面涉及一种用于风筝发电系统的风筝,其具有在机翼形体(20)的前缘部分中具有一个或多个空气填充孔(23)的翼型体(20)。 至少两个主牵引电缆(10,11)连接到翼型体(20),翼形体(20)在翼型体(20)的侧部还包括附加的填充孔(21)。
    • 19. 发明授权
    • Inflatable delta-shaped traction kite
    • 充气三角形牵引风筝
    • US08919701B2
    • 2014-12-30
    • US12525153
    • 2008-01-31
    • Raphael SallesSylvain Peretti
    • Raphael SallesSylvain Peretti
    • A63H27/08B64C31/06F41J9/08B63B35/79B63H9/06
    • B64C31/06B63B35/7976B63B35/7979B63H9/0614
    • Inflatable fraction kite (1) and the system for managing the traction power, the direction and the transient maneuvers thereof, shaped as a negative dihedron, of the type known as ‘C-shape’ or ‘C-kite’, and comprising load-bearing riggers and riggers used to manage the direction and trim, the kite (1) being characterized in that in flight it is designed to be delta-shaped and for this reason its leading edge (10), when laid flat, has a curvature such that, for each half-wing (12, 13) of the kite, the angle (α) formed by the tangent (S) to said central point (A) and the tangent (T) at a given point (B) increases as said given point (B) moves from the forward central point (A) toward the end (14, 15) of the kite (1) and in that, in the first third of said half-wing (12, 13) of the kite, from the forward central point (A) and in the direction of one end (14, 15), said angle (α) is greater than 15°.
    • 膨胀级风筝(1)和用于管理被称为“C形”或“C风筝”的类型的作为负二面体的牵引力,方向和瞬时动作的系统,并且包括负载 - 用于管理方向和装饰的轴承钻机和钻机,风筝(1)的特征在于在飞行中其被设计为三角形,因此,其前缘(10)在平坦时具有如下曲率 对于风筝的每个半翼(12,13),由给定点(B)处的切线(S)到所述中心点(A)和切线(T)形成的角度(α)随着 所述给定点(B)从前向中心点(A)朝向风筝(1)的端部(14,15)移动,并且在所述半风(12,13)的前三分之一的风筝 ,从正向中心点(A)和一端(14,15)的方向,所述角度(α)大于15°。