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公开(公告)号：EP4433343A1
公开(公告)日：2024-09-25
申请号：EP22761849.3
申请日：2022-08-10
申请人： Regent Craft Inc.
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公开(公告)号：EP3898316A1
公开(公告)日：2021-10-27
申请号：EP19849042.7
申请日：2019-12-18
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公开(公告)号：EP3812227A1
公开(公告)日：2021-04-28
申请号：EP19275103.0
申请日：2019-10-22
申请人： BAE SYSTEMS plc
摘要： The present disclosure relates to a control system for a vehicle, comprising: at least one compressor arranged to generate compressed fluid having a massflow rate; at least one fluidic control effector in fluidic communication with the at least one compressor and arranged to change the direction of travel of the vehicle when the compressed fluid is incident on the at least one fluidic control effector; a dump duct for expelling excess compressed fluid not delivered to the at least one fluidic control effector out of the vehicle; a dump valve for controlling the massflow rate of compressed fluid delivered to the dump duct; and a controller electrically coupled to the dump valve and configured to adjust the dump valve. The present disclosure also relates to an aircraft having the control system and a method of controlling a vehicle.
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公开(公告)号：EP3006287B1
公开(公告)日：2019-03-20
申请号：EP15189119.9
申请日：2015-10-09
申请人： Goodrich Corporation
发明人： Himmelmann, Richard
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公开(公告)号：EP2851251A1
公开(公告)日：2015-03-25
申请号：EP14185541.1
申请日：2014-09-19
发明人： Durham, Michael , Macey, Paul
CPC分类号： B64C25/001 , B60V1/043 , B60V1/06 , B60V1/16 , B60V3/08 , B64B2201/00
摘要： An air cushioned landing system for an air vehicle comprises an inflatable and deflatable skirt (113) in the form of a tube having inner (101) and outer (100) walls. The inner wall defines a central plenum (116) within the skirt, the skirt including gas pockets (130) arranged to stiffen one or more regions of at least one of the inner (101) and outer (100) walls during deflation of the skirt.
摘要翻译： 用于空中交通工具的气垫着陆系统包括具有内（101）和外（100）壁的管形式的可充气和可放气的裙部（113）。 所述内壁在所述裙部内限定中央增压室（116），所述裙部包括气囊（130），所述气囊布置成在所述裙部（112）的通气期间加强所述内部（101）和外部（100）壁中的至少一个的一个或多个区域 。
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公开(公告)号：EP1951567A4
公开(公告)日：2013-04-17
申请号：EP06809824
申请日：2006-11-01
发明人： YOELI RAPHAEL
IPC分类号： B64C15/00 , B60V3/08 , B64C1/00 , B64C1/14 , B64C1/22 , B64C3/00 , B64C3/40 , B64C23/00 , B64C27/08 , B64C27/20 , B64C29/00 , B64C39/00
CPC分类号： B64C1/1415 , B60V3/08 , B64C1/22 , B64C3/40 , B64C27/08 , B64C27/20 , B64C29/0025 , B64C29/0033 , Y02T50/145
摘要： A ducted air flow vehicle including a fuselage having a longitudinal axis, a first cockpit on one side of the longitudinal axis, a center portion adjacent and below the first cockpit, a first air flow duct mounted in the fuselage and including a first prime air mover to force surrounding air flow through the first air flow duct, and a second air flow duct mounted in the fuselage and including a second prime air mover to force surrounding air flow through the second duct, where outer upper and lower surfaces of the center portion are aerodynamically shaped to enhance production of aerodynamic lift forces by air flowing over the center portion and reduce resistance to air flow exiting the first airflow duct.
摘要翻译： 一种管道空气流动车辆，包括具有纵向轴线的机身，在纵向轴线的一侧上的第一驾驶舱，与第一驾驶舱相邻并且在其下方的中心部分，安装在机身中的第一气流管道，并且包括第一主要空气推进器 以迫使周围的空气流过第一空气流动管道，以及第二气流管道，其安装在机身中并且包括第二原始空气移动器，以迫使周围的空气流过第二管道，其中中心部分的外部上表面和下表面是 空气动力学形状，以通过在中心部分流动的空气来增强空气动力提升力的产生，并降低抵抗离开第一气流管道的气流的阻力。
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公开(公告)号：EP2353955A1
公开(公告)日：2011-08-10
申请号：EP11250146.5
申请日：2011-02-09
发明人： Fox, Jeremy Wilfred
摘要： A ground effect transport system comprising a plenum roof platform (27) for location beneath a load carrying means, a skirt (13) depending from the platform (27) to form a plenum chamber (11) with the platform (27), fan means on or in the platform for supplying air to the plenum chamber (11), wherein the skirt (13) extends downwardly towards the ground surface (43) and has a ground engaging support member (44) for supporting the bottom of the skirt (13) above the ground surface and a separate detachable sealing member (52) for providing a seal between the bottom of the skirt (13) and the ground surface (43).
摘要翻译： 一种地面运输系统，包括用于位于承载装置下方的增压室顶部平台（27），从所述平台（27）悬垂以形成具有所述平台（27）的增压室（11）的裙部（13），风扇装置 在所述平台中或在所述平台中用于向所述通风室（11）供应空气，其中所述裙部（13）向下延伸朝向所述地面（43）并具有用于支撑所述裙部（13）的底部的接地支撑构件（44） ）和用于在裙部（13）的底部和地面（43）之间提供密封的单独的可拆卸密封构件（52）。
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10.发明公开Retracting Air Cushioned Landing System for Air Vehicles 有权Einfahrbares Landesystem mit LuftkissenfürLuftfahrzeuge
公开(公告)号：EP2143610A2
公开(公告)日：2010-01-13
申请号：EP09164336.1
申请日：2009-07-01
发明人： Morehead, John , Greiner, Douglas , Pasman, Renee , Boyd, Robert
IPC分类号： B60V3/08
CPC分类号： B60V3/08 , B64B1/06 , B64B1/32 , B64B2201/00
摘要： A hybrid air vehicle (100) is disclosed in which a cover is provided for a plurality of air cushioned landing pads (206) to reduce drag when airborne. The pad is inflatable to provide an air cushioned during touchdown and deflatable during flight of the air vehicle. The cover can include a first cover portion and a second cover portion. A first cover roller of the first cover portion and a matching second cover roller of the second cover portion abut to cover the corresponding pad. The first cover roller and the second cover roller, which are separate and free from a physical linkage there between, are separable in an eyelid fashion to expose the corresponding pad. A separation gap between the first cover roller and the second cover roller is increased or decreased by roller straps to cover or expose the corresponding pad.
摘要翻译： 公开了一种混合动力飞行器（100），其中为多个气垫着陆垫（206）设置盖，以减少空降时的阻力。 该垫是可充气的，以提供在着陆期间缓冲的气垫，并在空中飞行器的飞行期间可放气。 盖可以包括第一盖部分和第二盖部分。 第一盖部分的第一覆盖辊和第二盖部分的匹配的第二盖辊邻接以覆盖相应的垫。 第一覆盖辊和第二覆盖辊分离并且不存在于其间的物理连接，可以以眼睑的方式分离以暴露相应的垫。 第一覆盖辊和第二覆盖辊之间的分离间隙由辊带增加或减小以覆盖或暴露相应的垫。
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