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1. 发明授权

US08602348B2 Flying-wing aircraft 有权
标题翻译：飞翼飞机
公开(公告)号：US08602348B2
公开(公告)日：2013-12-10
申请号：US12865429
申请日：2009-02-02
申请人： Ashley Christopher Bryant
发明人： Ashley Christopher Bryant
IPC分类号： B64C15/12 , B64C29/00 , B64C39/10
CPC分类号： B64C29/0033 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/088 , B64C2201/162 , B64C2201/165
摘要： A vertical take-off and landing flying-wing aircraft has a pair of thrust-vectoring propulsion units mounted fore and aft of the aircraft pitch axis on strakes at opposite extremities of the wing-structure, with the fore unit below, and the aft unit above, the wing-structure. The propulsion units are pivoted to the strakes, either directly or via arms, for individual angular displacement for thrust-vectored maneuvering of the aircraft in yaw, pitch and roll and for hover and forward and backward flight. When arms are employed, the arms of fore and aft propulsion units are intercoupled via chain drives or linkages. The wing-structure may have fins, slats and flaps and other aerodynamic control-surfaces, and enlarged strakes may incorporate rudder surfaces. Only one propulsion unit may be mounted at each extremity and additional fan units may be used.
摘要翻译：垂直起飞和着陆的飞翼飞机具有一对推力矢量推进装置，其在机翼结构的相对两端的前翼和后部单元的前后悬架的飞机俯仰轴上前后安装以上，翼结构。推进单元直接或经由臂枢转到斜面，用于单独的角位移，用于以偏航，俯仰和滚动以及用于悬停和向前和向后飞行的推力向导操纵飞行器。当使用武器时，前后推进单元的臂通过链条驱动器或连杆相互联接。机翼结构可以具有翅片，板条和翼片以及其它空气动力学控制表面，并且扩大的履带可以包括舵面。每个末端只能安装一个推进装置，也可以使用额外的风扇装置。

2. 发明申请

US20110001001A1 FLYING-WING AIRCRAFT 有权
标题翻译：飞行飞机
公开(公告)号：US20110001001A1
公开(公告)日：2011-01-06
申请号：US12865429
申请日：2009-02-02
申请人： Ashley Christopher Bryant
发明人： Ashley Christopher Bryant
IPC分类号： B64C29/00 , B64C39/10
CPC分类号： B64C29/0033 , B64C39/024 , B64C39/10 , B64C2201/028 , B64C2201/088 , B64C2201/162 , B64C2201/165
摘要： A vertical take-off and landing (VTOL) flying-wing aircraft has a pair of thrust-vectoring propulsion units (2, 3; 4, 5) mounted fore and aft of the aircraft pitch axis (PA) on strakes (6, 7) at opposite extremities of the wing-structure (1), with the fore unit (2; 4) below, and the aft unit (3; 5) above, the wing-structure (1). The propulsion units (2-5) are pivoted to the strakes (6, 7), either directly or via arms (56), for individual angular displacement for thrust-vectored maneuvering of the aircraft in yaw, pitch and roll and for hover and forward and backward flight. When arms (56) are employed, the arms (56) of fore and aft propulsion units (52,54; 53,55) are intercoupled via chain drives (57-60) or linkages (61). The wing-structure (1; 51 ; 78) may have fins (47;84), slats (81) and flaps (82) and other aerodynamic control-surfaces, and enlarged strakes (84) may incorporate rudder surfaces (80). Only one propulsion unit (21) may be mounted at each extremity and additional fan units (48,83) may be used.
摘要翻译：垂直起降（VTOL）飞翼飞机具有一对推进矢量推进单元（2,3; 4,5），其安装在飞行器俯仰轴线（PA）的前后，位于横梁（6,7））在机翼结构（1）的相对两端，前部单元（2; 4）和下方的后部单元（3; 5），机翼结构（1）。推进单元（2-5）直接地或经由臂（56）枢转到斜面（6,7），用于单独的角位移，用于偏航，俯仰和滚动中的推进向导操纵的飞行器，并且用于悬停和向前和向后飞行当使用臂（56）时，前后推进单元（52,54; 53,55）的臂（56）通过链条驱动器（57-60）或连杆（61）相互配合。机翼结构（1; 51; 78）可以具有翅片（47; 84），板条（81）和翼片（82）和其它空气动力学控制表面，并且扩大的横条（84）可以包括舵表面（80）。每个末端只安装一个推进单元（21），并且可以使用附加的风扇单元（48,83）。

3. 发明授权

US07581381B2 Ducted air power plant 失效
标题翻译：管道空气发电厂
公开(公告)号：US07581381B2
公开(公告)日：2009-09-01
申请号：US10519526
申请日：2003-06-27
申请人： Ashley Christopher Bryant
发明人： Ashley Christopher Bryant
IPC分类号： F02K1/00 , B64C29/00
CPC分类号： F02K3/025 , A63H27/00 , B64C11/001 , B64C15/02 , B64C29/0025 , B64C39/024 , B64C2201/162 , F02K1/004 , Y02T50/672
摘要： A ducted air power plant, comprising a motor driven fan (7) situated in a duct (4), the fan (7) having an air intake side and in operation providing a high pressure air stream in the duct, and the fan being located adjacent air splitter mechanism (18), the air splitter mechanism (18) being arranged to divert the air stream into two or more subsidiary streams for delivery to respective jet nozzles (9) of the plant. The plant may be used in a vehicle such as an aircraft in order to provide a vertical take-off and hover capability as well a level flight power source.
摘要翻译：一种管道空气动力装置，包括位于管道（4）中的电机驱动风扇（7），所述风扇（7）具有进气侧并且在所述管道中提供高压气流，并且所述风扇位于相邻的空分机机构（18），空分机机构（18）被布置成将空气流转移到两个或更多个辅助流中，以便输送到设备的相应的喷嘴（9）。该工厂可用于诸如飞行器的车辆中，以提供垂直起飞和悬停能力以及水平飞行动力源。

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