公开(公告)号：WO2008073069A2

公开(公告)日：2008-06-19

申请号：PCT/US2006032280

申请日：2006-08-18

Applicant: CYBER DEFENSE SYSTEMS INC ,  ALMAN JAMES

Inventor： ALMAN JAMES

IPC: B64C5/04

CPC classification number: B64C39/024 ,  B64C15/12 ,  B64C29/0066 ,  B64C29/0075 ,  B64C39/12 ,  B64C2201/021 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/126

Abstract: An unmanned aerial vehicle includes a fuselage, a horizontal stabilizer assembly, a wing assembly, a forward propulsion device, and at least one rear propulsion device. The fuselage has a forward end portion and a rearward portion. The horizontal stabilizer assembly has a left wing and a right wing. The wing assembly has a wing substantially aligned with and parallel to the horizontal stabilizer assembly. Upon activation, the forward propulsion device operates to provide thrust to assist in lifting the unmanned aerial vehicle. Upon activation, the at least one rear propulsion device is selectively rotatable ninety degrees so as to direct the thrust from the at least one rear propulsion device in one of a downward direction and a rearward direction. The forward propulsion device and the at least one rear propulsion device cooperate to provide a downward thrust resulting in the lifting of the unmanned aerial vehicle.

Abstract translation: 无人驾驶飞行器包括机身，水平稳定器组件，翼组件，前推推动装置和至少一个后推进装置。 机身具有前端部和后方部。 水平稳定器组件具有左翼和右翼。 机翼组件具有与水平稳定器组件基本对准并平行的翼。 在启动时，前进推进装置操作以提供推力以辅助提升无人驾驶飞行器。 在激活时，至少一个后推进装置可选择性地旋转90度，以便将来自至少一个后推进装置的推力引导到向下方向和向后方向之一。 前进推进装置和至少一个后部推进装置协作以提供导致无人驾驶飞行器的提升的向下推力。

公开(公告)号：WO2006073750A3

公开(公告)日：2006-12-28

申请号：PCT/US2005045715

申请日：2005-12-16

Applicant: ALMAN JAMES

Inventor： ALMAN JAMES

IPC: B64C3/38

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203

Abstract: An unmanned aerial vehicle (UAV) having a design for optimum stowability and low cost. The UAV having a collapsible wing section which can be easily removed from the fuselage, allowing for quick assembly and disassembly and ease of portability. The unmanned aerial vehicle includes a primary wing assembly, a fuselage, a means for propelling the unmanned aerial vehicle , and means for remotely controlling the unmanned aerial vehicle. The primary wing assembly includes a wing having a center spar and two outwardly diverging side spars. The wing also has a pliable flexible material supported by the center spar and the at least two outwardly diverging side spars. The pylon is connected to the wing and supports the wing. The fuselage is connected to the pylon such that the pylon extends away from the fuselage and spaces the wing a distance from the fuselage. The fuselage includes a tail having a rudder located along a trailing edge and elevators located along the trailing edge.

Abstract translation: 无人飞行器（UAV）具有最佳的可收藏性和低成本的设计。 无人机具有可折叠的机翼部分，可以方便地从机身中移除，从而实现快速组装和拆卸，便于携带。 无人飞行器包括主翼组件，机身，用于推动无人驾驶飞行器的装置，以及用于远程控制无人驾驶飞行器的装置。 主翼组件包括具有中心翼梁和两个向外发散的侧翼的翼。 机翼还具有由中心翼梁和至少两个向外发散的侧翼支撑的柔韧的柔性材料。 塔架连接到机翼并支撑机翼。 机身连接到挂架，使得吊架远离机身延伸，并将机翼与机身隔开一段距离。 机身包括尾部，尾部沿着后缘设有方向舵，沿着后缘设有电梯。

公开(公告)号：WO2008051175A2

公开(公告)日：2008-05-02

申请号：PCT/US2005045424

申请日：2005-12-16

Applicant: ALMAN JAMES

Inventor： ALMAN JAMES

IPC: B64B1/02

CPC classification number: B64B1/06 ,  B64B1/32

Abstract: A lighter than air semi-rigid air vehicle utilizing two or more spherical chambers with composite fairings in between to reduce drag. The vehicle also may utilize a reverse ballonet or conventional ballonet system for the lift gas control (Helium, Hot Air, Hydrogen or any other lift gas). The power plants may use reversible pitch propellers to enhance maneuverability.

Abstract translation: 比空气半刚性的空气车辆更轻，利用两个或多个具有复合整流罩的球形腔，以减少阻力。 车辆还可以使用用于提升气体控制（氦气，热空气，氢气或任何其它提升气体）的反向气球或常规气球系统。 发电厂可以使用可逆螺距螺旋桨来提高机动性。