ARC-TYPE WING EQUIPPED WITH ADJUSTABLE JUNCTION SYSTEM OF BRIDLES
    21.
    发明申请
    ARC-TYPE WING EQUIPPED WITH ADJUSTABLE JUNCTION SYSTEM OF BRIDLES 审中-公开
    具有可调式连接系统的弧型

    公开(公告)号:WO2015107556A1

    公开(公告)日:2015-07-23

    申请号:PCT/IT2014/000315

    申请日:2014-11-26

    CPC classification number: B63B35/7976 B64C31/06

    Abstract: An arc-type wing (1) is described, connected to at least one pair of power ropes (2) through at least two pairs of control bridles, each one of such pairs being composed of at least one front bridle (21) and of at least one rear bridle (22), such wing (1) being composed of at least one section of central arc (13) laterally connected to each pair of bridles (21, 22) by interposing at least one respective shoulder (14), each one of such shoulders (14) comprising at least one adjustable junction system of an attack point (P) at least of such respective rear bridles (22) with respect to such wing (1).

    Abstract translation: 描述了弧形翼(1),通过至少两对控制桥与至少一对电力绳(2)连接,这些对中的每一对由至少一个前桥(21)和 至少一个后桥(22),所述翼(1)由至少一个中心弧(13)的部分组成,所述至少一个中心弧(13)通过插入至少一个相应的肩部(14)横向地连接到每对桥梁(21,22) 这些肩部(14)中的每一个至少包括相对于这种翼(1)的至少一个相应的后桥(22)的攻击点(P)的可调节的连接系统。

    METHOD FOR SETTING UP AN ARC-TYPE WING
    23.
    发明申请
    METHOD FOR SETTING UP AN ARC-TYPE WING 审中-公开
    用于设置弧型的方法

    公开(公告)号:WO2015037025A1

    公开(公告)日:2015-03-19

    申请号:PCT/IT2014/000232

    申请日:2014-09-04

    Inventor: IPPOLITO MASSIMO

    CPC classification number: F03D5/00 B64C2031/065 Y02E10/70

    Abstract: A method is described for real-time determining the shape of an arc-type wing (1) with high aerodynamic efficiency, wherein the wing (1) is composed of a central arc section (13) connected to pairs of bridles (11,12) through a pair of shoulders (14), and comprising a detecting system (4,5) adapted to measure the difference of meaningful heights (dl-dl'), (d2-d2' ) for determining in real time the shape of the wing (1), the detecting system (4,5) being housed in panels (2) fastened to each shoulder (14).

    Abstract translation: 描述了一种用于实时确定具有高空气动力学效率的弧形翼(1)的形状的方法,其中翼(1)由连接到成对的蹄(11,12)的中心弧段(13)组成 )通过一对肩部(14),并且包括适于测量有意义的高度差(d1-d1')的检测系统(4,5),(d2-d2'),用于实时确定 翼(1),检测系统(4,5)容纳在固定到每个肩部(14)的面板(2)中。

    SYSTEM FOR MEASURING THE WIND SPEED AT A CERTAIN HEIGHT
    24.
    发明申请
    SYSTEM FOR MEASURING THE WIND SPEED AT A CERTAIN HEIGHT 审中-公开
    用于测量一定风速的风速系统

    公开(公告)号:WO2014199405A1

    公开(公告)日:2014-12-18

    申请号:PCT/IT2014/000129

    申请日:2014-05-13

    CPC classification number: G01P5/00

    Abstract: A system is described, for measuring the wind speed at a certain height, comprising at least one unmanned aircraft (1) immersed in a field of motion (2) determined by such wind, such unmanned aircraft (1) being equipped with first on-board processing means adapted to operatively interact on a propulsion system and/or on a flying guiding system of such aircraft (1) to modify its flight attitude depending on external perturbations exerted by such wind present in such field of motion (2) to keep a centring of such aircraft (1) along at least one reference flying trajectory (3) passing through one or more following flight attitudes (l,i l,m, l,f) corresponding with different flight heights above a reference level (S), and detect attitude data related to such attitudes (l,i, l,m, l,f) at such relative flight heights.

    Abstract translation: 描述了一种用于测量在一定高度处的风速的系统,包括至少一个浸没在由这种风决定的运动场(2)中的无人驾驶飞机(1),这种无人驾驶飞机(1) 板处理装置,其适于在这种飞机(1)的推进系统和/或飞行引导系统上可操作地相互作用,以根据由这种运动场(2)中存在的这种风施加的外部扰动来修改其飞行姿态,以保持 沿着沿着参考水平(S)以上的不同飞行高度的一个或多个跟随飞行姿态(l,il,m,l,f)的至少一个参考飞行轨迹(3)将这种飞机(1)定心,以及 在这样的相对飞行高度处检测与这种态度(l,i,l,m,l,f)有关的态度数据。

    SYSTEM FOR PERFORMING THE AUTOMATIC CONTROL OF THE FLIGHT OF KITES
    25.
    发明申请
    SYSTEM FOR PERFORMING THE AUTOMATIC CONTROL OF THE FLIGHT OF KITES 审中-公开
    执行THE THE飞行自动控制系统

    公开(公告)号:WO2008072269A1

    公开(公告)日:2008-06-19

    申请号:PCT/IT2007/000834

    申请日:2007-11-30

    Abstract: A system (10) is described for performing the automatic control of the flight of at least one kite (11) controlled and driven by cables (13) comprising at least one first actuating motor (12) adapted to exert an unwinding-rewinding action of such cables (13) on respective winches (14a, 14b) and at least one second actuating motor (15) adapted to perform a differential control action of such cables ( 13).

    Abstract translation: 描述了一种用于执行由电缆(13)控制和驱动的至少一个风筝(11)的飞行的自动控制的系统(10),所述风筝包括至少一个第一致动马达(12),所述至少一个第一致动马达(12)适于施加退绕 - 相应的绞盘(14a,14b)上的这种电缆(13)和适于执行这种电缆(13)的差动控制动作的至少一个第二致动马达(15)。

    AUTOMATIC CONTROL SYSTEM AND PROCESS FOR THE FLIGHT OF KITES
    26.
    发明申请
    AUTOMATIC CONTROL SYSTEM AND PROCESS FOR THE FLIGHT OF KITES 审中-公开
    自动控制系统及飞镖程序

    公开(公告)号:WO2007135701A2

    公开(公告)日:2007-11-29

    申请号:PCT/IT2007/000325

    申请日:2007-05-03

    Abstract: An automatic control system (1) is described for the flight of at least one kite (2), in order to generate electric or mechanical energy, such kite (2) being controlled by a driving unit (4) equipped with two winches to which the kite (2) is connected through two respective driving cables (6), comprising first detecting means (3) on board the kite (2) adapted to detect first pieces of information regarding at least a position and an orientation in the space of such kite (2) and accelerations to which the kite (2) is subjected; second detecting means (5) on the ground adapted to detect second pieces of information regarding at least an amount of a tension on the driving cables (6) of such kite (2) and their relative position, a direction and an intensity of a wind current W inside which the kite (2) is immersed; processing and controlling means (7) of such first and second pieces of information (P), adapted to transform the contents of such information (P) into a mechanical command related to a control function (U) operating on the winches of the driving unit (4) for driving the kite (2) along a flight trajectory maximising an amount of kinetic energy subtracted to the wind current W; and a transmitting system of the first pieces of information to the processing and controlling means (7). An automatic control process for the flight of kites is further described, adapted to perform a control function (U) through a predictive control methodology based on a flight dynamics model of such kite (2) starting from such information (P).

    Abstract translation: 描述了用于至少一个风筝(2)的飞行的自动控制系统(1),以便产生电力或机械能量,这种风筝(2)由配备有两个绞盘的驱动单元(4)控制,至此, 风筝(2)通过两个相应的驱动电缆(6)连接,包括在风筝(2)上的第一检测装置(3),适于检测关于这样的空间中的至少一个位置和取向的第一信息 风筝(2)和风筝(2)所经受的加速度; 地面上的第二检测装置(5),其适于检测关于这种风筝(2)的驱动电缆(6)上的至少一定张力的第二信息及其相对位置,风向的方向和强度 放置风筝(2)的电流W; 这些第一和第二信息(P)的处理和控制装置(7)适于将这种信息(P)的内容变换成与在驱动单元的绞盘上操作的控制功能(U)有关的机械命令 (4),用于沿着飞行轨迹驱动风筝(2),最大化减去风向W的动能量; 以及将第一信息的发送系统发送到处理和控制装置(7)。 进一步描述了用于风筝飞行的自动控制过程,其适于通过基于从这种信息(P)开始的这种风筝(2)的飞行动力学模型的预测控制方法来执行控制功能(U)。

    APPARATUS FOR CONVERTING MECHANICAL ENERGY INTO ELECTRIC ENERGY
    27.
    发明申请
    APPARATUS FOR CONVERTING MECHANICAL ENERGY INTO ELECTRIC ENERGY 审中-公开
    将机械能量转换为电能的装置

    公开(公告)号:WO2015181841A1

    公开(公告)日:2015-12-03

    申请号:PCT/IT2015/000057

    申请日:2015-03-05

    Inventor: IPPOUTO Massimo

    Abstract: A kite powered wind generator comprising two independently controlled outer rotor-type electric motor generators axially aligned on a single central support, each rotor carrying a winch pulley in contact with a section of a tether holding the kite; both rotors and pulleys are coaxially connected to a single hub (30), said hub (30) is supported and journaled by a single central bearing (40) between the two rotors.

    Abstract translation: 一种风筝动力风力发电机,包括两个独立控制的外转子式电动发电机,其轴向对准在单个中央支撑件上,每个转子承载与保持风筝的系绳的一部分接触的绞车滑轮; 两个转子和滑轮同轴连接到单个轮毂(30),所述轮毂(30)由两个转子之间的单个中心轴承(40)支承和支承。

    ARC-SHAPED WING WITH DIFFERENTIATED WING PROFILES
    28.
    发明申请
    ARC-SHAPED WING WITH DIFFERENTIATED WING PROFILES 审中-公开
    具有差异化型号的弧形形状

    公开(公告)号:WO2015083189A1

    公开(公告)日:2015-06-11

    申请号:PCT/IT2014/000296

    申请日:2014-11-07

    CPC classification number: B64C31/06 B64C3/14

    Abstract: An arc-shaped wing (1) with differentiated wing profiles is described, composed of a section of central arc (11) and two lateral shoulders (12), wherein such central arc (11) is composed of a first wing profile (2) and each one of such shoulders (12) is composed of a second wing profile (3).

    Abstract translation: 描述了具有不同翼型的弧形翼(1),其由中心弧(11)和两个侧肩(12)组成,其中这种中心弧由第一翼型(2)组成, 并且这些肩部(12)中的每一个由第二翼型材(3)构成。

    KITE WIND ENERGY COLLECTOR
    29.
    发明申请
    KITE WIND ENERGY COLLECTOR 审中-公开
    风筝能量收集器

    公开(公告)号:WO2014199407A1

    公开(公告)日:2014-12-18

    申请号:PCT/IT2014/000155

    申请日:2014-06-05

    CPC classification number: F03D5/06 F03D5/00 F03D13/20 Y02E10/70

    Abstract: A wing with bi-mode operation is described, for passing from an arc shape to an undistorted plane shape and vice versa, composed of three or more power wing airfoils (1-1, 1-2, 1-3) connected in series and mutually articulated through at least one articular joint (2, 3) interposed between at least one pair of such adjacent power wing airfoils (1-1, 1-2, 1-3).

    Abstract translation: 描述了具有双模操作的翼,从弧形通过到未失真的平面形状,反之亦然,由三个或更多个串联连接的功率翼型(1-1,1-2,3-3)组成, 通过插入在至少一对这样的相邻的动力翼型(1-1,1-2,1-3)之间的至少一个关节(2,3)相互铰接。

    SYSTEM AND PROCESS FOR STARTING THE FLIGHT OF POWER WING AIRFOILS, IN PARTICULAR FOR WIND GENERATOR
    30.
    发明申请
    SYSTEM AND PROCESS FOR STARTING THE FLIGHT OF POWER WING AIRFOILS, IN PARTICULAR FOR WIND GENERATOR 审中-公开
    启动风力发电机飞行器的系统和过程,特别是风力发电机

    公开(公告)号:WO2014199406A1

    公开(公告)日:2014-12-18

    申请号:PCT/IT2014/000154

    申请日:2014-06-05

    Inventor: IPPOLITO Massimo

    Abstract: 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).

    Abstract translation: 描述了用于开始动力翼型(7)的飞行的系统(1),特别是用于风力发电机(5)的飞行,该风力发电机包括通过控制拉杆(9)可操作地连接的至少一个翼型材(7) 至少一个自适应运输飞行矢量(11),适于通过可分离的连接装置(13)连接到至少一个机翼轮廓(7);以及 在飞行中运输这种翼型(7)。 进一步描述了通过这种系统(1)开始这种动力翼型件(7)的飞行的过程。

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