公开(公告)号：EP1711399A4

公开(公告)日：2012-08-08

申请号：EP04791846

申请日：2004-10-27

申请人： YOELI RAPHAEL ,  URBAN AERONAUTICS LTD

发明人： YOELI RAPHAEL

IPC分类号： B64C29/00 ,  B60V1/04 ,  B64C20060101 ,  B64C1/14 ,  B64C1/22 ,  B64C3/40 ,  B64C27/08 ,  B64C27/20 ,  B64D7/00 ,  B64D17/80

CPC分类号： B64C27/08 ,  B60V1/043 ,  B64C1/1415 ,  B64C1/22 ,  B64C3/40 ,  B64C27/20 ,  B64C29/0025 ,  B64C29/0033 ,  B64D7/00 ,  B64D17/80 ,  Y02T50/145

摘要： A vehicle including a fuselage having a longitudinal axis and a transverse axis, two Ducted Fan lift-producing propellers carried by the fuselage on each side of the transverse axis, a pilot's compartment formed in the fuselage between the lift-producing propellers and substantially aligned with one side of the fuselage, a payload bay formed in the fuselage between the lift-producing propellers and opposite the pilot's compartment, and two pusher fans located at the rear of the vehicle. Many variations are described enabling the vehicle to be used not only as a VTOL vehicle, but also as a multi-function utility vehicle for performing many diverse functions including hovercraft and ATV functions. Also described is an Unmanned version of the vehicle. Also described are unique features applicable in any single or multiple ducted fans and VTOL vehicles.

公开(公告)号：EP1951567A4

公开(公告)日：2013-04-17

申请号：EP06809824

申请日：2006-11-01

申请人： URBAN AERONAUTICS LTD

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。

公开(公告)号：EP2234883A4

公开(公告)日：2016-06-29

申请号：EP08863181

申请日：2008-12-15

申请人： URBAN AERONAUTICS LTD

发明人： YOELI RAPHAEL

IPC分类号： B64C27/20 ,  B64C29/00

CPC分类号： B64C29/0025 ,  B64C27/20

公开(公告)号：EP2318273A4

公开(公告)日：2017-09-06

申请号：EP09811177

申请日：2009-08-28

申请人： URBAN AERONAUTICS LTD

发明人： YOELI RAPHAEL

IPC分类号： B64C27/08 ,  B64C27/20 ,  B64C29/00

CPC分类号： B64C27/20 ,  B64C29/0033

摘要： A VTOL vehicle includes a forward rotor, an aft rotor and a fuselage, the forward and aft rotor lying in a longitudinal axis of the vehicle, with the fuselage located axially between the forward and aft rotors. The vehicle has an in-flight configuration wherein the forward rotor is tilted downwardly at a negative tilt angle relative to the fuselage and the aft rotor is tilted upwardly at a positive tilt angle relative to the fuselage.

摘要翻译： VTOL车辆包括前转子，后转子和机身，前后转子位于车辆的纵向轴线上，其中机身位于前转子和后转子之间。 该车辆具有飞行中构型，其中前转子相对于机身以负倾角向下倾斜，并且后转子相对于机身以正倾角向上倾斜。