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81. 发明授权

EP2046644B1 AN UNMANNED AERIAL VEHICLE LAUNCHING AND LANDING SYSTEM 有权
标题翻译： START和着陆系统的无人机
公开(公告)号：EP2046644B1
公开(公告)日：2011-10-05
申请号：EP07736228.3
申请日：2007-04-18
申请人： ELBIT SYSTEMS LTD.
发明人： KARIV, Amnon
IPC分类号： B64F1/02 , B64F1/04 , B64F1/08
CPC分类号： B64F1/06 , B64C2201/084 , B64C2201/182 , B64F1/02
摘要： A system for landing UAV's comprising a slingshot structure (25) that includes a central arm (26) and an axis means (45) installed along the central arm of the structure and wherein it enables the central arm to move around it in addition, the system comprises base means (50) connecting the axis means to a platform (20) at which the system is installable. The system also include a controlled pulling and braking means (55) that connects between lower end of the central arm of the structure and the platform upon which the system is installable and an assembly (35), essentially formed as a substantially 'Y' shape part that is installable unto the top end of the central arm of the structure and a stretchable elastic means (30) installed in a stretched manner at a gap formed between the two arms of the assembly and set to connect with a landing UAV(15). At the landing phase, the controlled pulling and braking means of the system, essentially brakes the motion of the central arm of the structure that is propelled to revolve around the system's axis means, from a time that the UAV forms contact with the elastic means and with it propels the structure to move around the axis means.

82. 发明公开

EP2186728A1 Unmanned air vehicle recovery system 有权
标题翻译： Bergungssystemfürein unbemanntes Luftfahrzeug
公开(公告)号：EP2186728A1
公开(公告)日：2010-05-19
申请号：EP08380317.1
申请日：2008-11-14
申请人： The Boeing Company
发明人： Gomez-Ledesma, Ramon , Kawiecki, Grzegorz
IPC分类号： B64C39/02 , B64F1/02
CPC分类号： B64C39/024 , B64C2201/182 , B64F1/02
摘要： The present invention relates to a recovery system for unmanned air vehicles, namely a system for recovering such air vehicles from flight. The system comprises an unmanned air vehicle (10) and recovery apparatus (30), the air vehicle having first coupling means (20) suspended beneath the air vehicle, and the recovery apparatus comprising second coupling means (32). The first and second coupling means engage. The second coupling means is rotatably mounted (52) so as to allow rotation about a substantially vertical axis upon engagement.
摘要翻译：本发明涉及无人驾驶飞行器的回收系统，即从飞行中回收这种空中客车的系统。该系统包括无人驾驶飞行器（10）和回收装置（30），该空中交通工具具有悬挂在空中车辆下方的第一联接装置（20），该回收装置包括第二联接装置（32）。第一和第二联接装置啮合。第二联接装置可旋转地安装（52），以允许在接合时围绕基本垂直的轴线旋转。

83. 发明公开

EP1633629A2 LOW-PROFILE BRAKE-IN-SPOOL AIRCRAFT ARRESTING SYSTEMS 有权
标题翻译：在集成的制动系统含平面作用的实验研究渔获LOW PROFILE
公开(公告)号：EP1633629A2
公开(公告)日：2006-03-15
申请号：EP04801950.9
申请日：2004-05-18
申请人： Engineered Arresting Systems Corporation
发明人： LOPEZ, Edmond, S.
IPC分类号： B64F1/02
CPC分类号： B60T8/325 , B64F1/02 , F16D2121/02
摘要： Arresting systems (10) attachable to a tail-hook cable (16) or other device for aircraft arrestment may have a total height of one foot, enabling above-ground installation at the edge of a runway. Arresting tapes (66a, 66b) are provided on horizontally positioned dual tape spools in a brake-in-spool configuration. With a friction disk brake assembly (40a, 40b) enclosed within the hub of each horizontal tape spool (60a, 60b)to control tape deployment by braking spool rotation during aircraft arrestment, overall system height is reduced. By use of disposable single-use spools (60a, 60b), requirement for a tape rewind engine and related mechanisms are avoided. Spool hubs can be keyed to the exterior of a rotatable brake assembly (40a, 40b) portion to facilitate slidable tape spool installation and replacement. Pre-tensioned arresting tapes (66a, 66b) on tape spools (60a, 60b) can be employed for improved tape deployment. Computerized hydraulic brake assembly activation can be employed for controlled aircraft arrestment.

84. 发明公开

EP1233905A4 LAUNCH AND RECOVERY SYSTEM FOR UNMANNED AERIAL VEHICLES 有权
标题翻译： START和收集系统无人机
公开(公告)号：EP1233905A4
公开(公告)日：2005-09-28
申请号：EP00952173
申请日：2000-07-24
申请人： ADVANCED AEROSPACE TECHNOLOGIE
发明人： MCDONNELL WILLIAM R
IPC分类号： B64C25/68 , B64C39/02 , B64D3/00 , B64F1/02 , B64F1/04 , B64F1/10
CPC分类号： B64F1/02 , B64C25/68 , B64C39/024 , B64C2201/084 , B64C2201/104 , B64C2201/165 , B64C2201/182 , B64C2201/205 , B64D3/00 , B64F1/04 , B64F1/10
摘要： An improved method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10) is disclosed. The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).

85. 发明公开

EP1044132A1 AIRCRAFT CARRIERS AND METHODS OF OPERATION THEREOF 审中-公开
标题翻译：航母操作方法
公开(公告)号：EP1044132A1
公开(公告)日：2000-10-18
申请号：EP99954149.3
申请日：1999-11-05
申请人： BAE SYSTEMS plc
发明人： ALLEN, P. J. P.,British Aeros. Mil. Airc. and , SEYFANG, G. R.,British Aeros. Mil. Aircraft and
IPC分类号： B64F1/02
CPC分类号： B64F1/00
摘要： An aircraft carrier (10) is provided with an airflow deflection means such as flap (14), an inflatable flap (26) or an airjet curtain (28) such that air passing along the flight deck is provided with an upward component of velocity, thereby to provide an upwash in the airwake behind the aircraft carrier. The upwash persists for a reasonable length downstream of the aircraft carrier and means that, for a given spatial attitude, the angle of angle of attack of the aircraft relative to the airstream is increased. This means that the aircraft may be flown at a reasonably high angle of attack to the airstream on a landing approach without sacrificing the pilot's view of the deck. In addition, the increased angle of attack may be used to facilitate a flare manoeuvre.

86. 发明公开

EP0385784A1 Aircraft arresting elemental net with multiple independent bottom horizontal straps 失效
标题翻译： Flugzeug-Fangnetz mit mehrerenunabhängigenunterenLängsseilen。
公开(公告)号：EP0385784A1
公开(公告)日：1990-09-05
申请号：EP90302208.5
申请日：1990-03-01
申请人： DATRON INC.
发明人： Colarik, David K. , Cripe, Christopher A.
IPC分类号： B64F1/02
CPC分类号： B64F1/02
摘要： An elemental net for a multiple element aircraft arresting net system. The elemental net has a single upper horizontal strap, several vertical straps having top ends and bottom ends, and at least two lower horizontal straps. The top ends of the vertical straps are directly affixed to the upper horizontal strap at spaced intervals along the upper horizontal strap. The bottom ends of the vertical straps are alternatingly affixed to one of the lower horizontal straps so that the lower horizontal straps are free to move relative to each other to a significant degree and so that lifting of one vertical strap will tend to lift only one of the lower horizontal straps in the vicinity of the vertical strap being lifted. The present invention provides a variable window which is free to expand or contract during aircraft engagement, permitting easier penetration of the net by a greater mix of aircraft. The present invention also ensures that only one lower horizontal strap of the elemental net will seat on the nosewheel strut, while at least one lower horizontal is free to move longitudinally under the nosewheel strut to apply arresting force.
摘要翻译：多元素飞机拦截网系统的基本网。元素网具有单个上部水平带，具有顶端和底端的几个垂直带以及至少两个下部水平带。垂直带的顶端沿着上水平带以间隔的间隔直接固定在上水平带上。垂直带的底端交替地固定在下部水平带之一上，使得下部水平带相对于彼此自由地移动很大程度，因此一个垂直带的提升将倾向于仅提升垂直带附近的下水平带被提起。本发明提供了一种可变窗口，其可在飞行器接合期间自由地膨胀或收缩，从而允许通过较大的飞机组合更容易地穿透网。本发明还确保元件网的仅一个下部水平带将位于诺基亚支柱上，同时至少一个下部水平面可在纵向延伸的下方移动以施加止动力。

87. 发明公开

EP0349896A2 Deceleration apparatus and method for stopping a racing vehicle 失效
标题翻译： Verlangsamungsvorrichtung und Verfahren，um Rennfahrzeuge zum Stehen zu bringen。
公开(公告)号：EP0349896A2
公开(公告)日：1990-01-10
申请号：EP89111780.6
申请日：1989-06-28
申请人： Mickey Thompson Entertainment Group
发明人： Thompson, Marion L.
IPC分类号： B64F1/02
CPC分类号： B60T1/12
摘要： A deceleration method and apparatus for stopping a racing vehicle a predetermined distance beyond a race course finish line after a speed run from a standing start. A tether system (9) having an elongated free payout portion (10) is attached to the vehicle (12) at the start line (14). The length of the payout portion (10) approximates the length of the course (28). Energy absorbing apparatus (66) attached to the tether system places the payout portion (10) in tension when it is payed out. The energy absorbing apparatus (66) may be a mechanical friction braking system, or a hydraulic braking system employing rotor vanes rotating past stators in a compartment containing a liquid such as water.
摘要翻译：一种减速方法和装置，用于在从站立开始的速度运行之后使赛车停止预定距离超过跑道终点线。具有细长的自由支出部分（10）的系绳系统（9）在起始线（14）附接到车辆（12）。支付部分（10）的长度近似于课程（28）的长度。安装在系绳系统上的能量吸收装置（66）在付出时使支付部分（10）处于张紧状态。能量吸收装置（66）可以是机械摩擦制动系统，或者采用旋转叶片的液压制动系统，该转子叶片经过定子在包含诸如水的液体的隔间中旋转。

88. 发明公开

EP0292450A2 Arrangement for an arrester device 失效
标题翻译： Einrichtung zur Fanganlage。
公开(公告)号：EP0292450A2
公开(公告)日：1988-11-23
申请号：EP88850152.5
申请日：1988-05-03
申请人： VÄDERSTADVERKEN AB
发明人： Caap, Stig
IPC分类号： B64F1/02
CPC分类号： B64F1/02
摘要： An arrangement for use in conjunction with aircraft arrester devices of the kind which comprise upper and lower, essentially horizontal edge elements (1 and 2), which edge elements are connected together by essentially vertical transverse elements (3) by means of coupling devices (5), for the purpose of protecting the transverse elements against the absorption of moisture, with an associated weight increase and rigidity at sub-zero temperatures.
Each transverse element (3) is enclosed by a hose- or stocking-like protective sleeve (7), which on the one hand is so arranged as to interact in a sealing fashion at its ends with adjacent parts of the arrester device in such a way that water and moisture are prevented from finding their way into the element, and on the other hand is executed from a semi-permeable material of a kind, such as GoreTex®, which is impermeable to water, but allows water vapour to pass through, so that any moisture which, in spite of every precaution, has managed to be absorbed by the transverse element (3), can evaporate into the surroundings.
摘要翻译：一种与包括上部和下部基本上水平的边缘元件（1和2）类型的飞机避雷器装置结合使用的装置，所述边缘元件通过基本垂直的横向元件（3）通过联接装置（5）连接在一起），以保护横向元件免受潮湿的吸收，相关的重量增加和零度以下的刚度。每个横向元件（3）由软管或储存状的保护套（7）包围，其一方面被布置成在其端部以与密封件相反的方式与避雷器装置的相邻部分相互作用防止水分和水分进入元件的方法，另一方面是由一种不渗透水，但允许水蒸汽通过的诸如GoreTex TM的半透性材料，使得尽管有预防措施已经设法被横向元件（3）吸收的任何水分可以蒸发到周围环境中。

89. 发明公开

EP0016126A4 PROGRAMMED AIRCRAFT ARRESTING SYSTEM. 失效
标题翻译：编排的系统停止飞机。
公开(公告)号：EP0016126A4
公开(公告)日：1980-11-14
申请号：EP79900834
申请日：1980-02-25
申请人： ALL AMERICAN ENG CO
发明人： MYHR LARS HALVER
IPC分类号： B64F1/02 , F16D57/04 , G05D17/00
CPC分类号： B64F1/02
摘要： An arresting system which is adaptable to arrest a wide range of aircraft weights and speeds. A variable K factor energy absorber (40) for an aircraft arresting system has a movable control element (32) which is moved into different positions to adjust the K factor. The movement of the control element (32) is programmed during payout of the arresting system in accordance with the speed of the arrested aircraft. The speed is sensed by a pump (17) driven by the arresting gear (40) tape reel. The program is provided by a cam (12, 12A). The control element (32) is moved by a hydraulic drive (15, 16) actuated by an electrical shifting switch (107), which is triggered when the detected speed of the arrested aircraft exceeds the predetermined speed established by a cam (12) during initial and final phases of payout. The control element (32) is thereby moved from an initial low K (A) to an intermediate K (B) position during the initial phase of payout if the predetermined speed established by the cam (12) is exceeded. During the final phase of payout, the switch (10) shifts the control (32) to the high K position (C), if the predetermined speed is exceeded. The cam (12A, 28) also causes the control element (32) to be driven to a high K position (C) at the end of payout if it is not already there. Rewind (35) is accomplished by actuating the drive system (15, 16) to set the control element (32) in the low K position (A) to minimize the required rewind force.

90. 发明公开

EP4294728A1 A DEVICE FOR CATCHING AND LAUNCHING AN UNMANNED AERIAL VEHICLE 审中-实审
公开(公告)号：EP4294728A1
公开(公告)日：2023-12-27
申请号：EP22705606.6
申请日：2022-02-01
申请人： Stepura, Oleksandr Volodymyrovych , Toptun, Mykola Mykolaiovych
发明人： Stepura, Oleksandr Volodymyrovych , Toptun, Mykola Mykolaiovych
IPC分类号： B64F1/02 , B64C39/02

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