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1. 发明授权

US5860620A Ram wing vehicle 失效
标题翻译：拉姆翼车
公开(公告)号：US5860620A
公开(公告)日：1999-01-19
申请号：US679351
申请日：1996-07-10
申请人： Barnaby Sam Wainfan , Douglas E. Shultz , Jeffry Scott Philhower
发明人： Barnaby Sam Wainfan , Douglas E. Shultz , Jeffry Scott Philhower
IPC分类号： B60V1/22 , B64C21/04
CPC分类号： B60V1/22
摘要： A ram wing vehicle comprises a main structure extending between a nose end and a tail end, including an aerodynamic lifting body having an aspect ratio less than approximately 1.0 and extending between a leading edge and a trailing edge. The ratio of the thickness of the lifting body intermediate the leading edge and the trailing edge to the length of the chord thereof is greater than approximately 1:8. A propulsion source is provided adjacent the nose end for generating an efflux and for directing the efflux beyond the tail end in a direction away from the nose end. A directional control mechanism is positioned adjacent the nose end for turning the vehicle about the yaw axis into a curve having a center and so vectoring the efflux from the propulsion source as to direct the efflux to the outside of the turn and the nose end toward the center of the curve. The directional control mechanism includes a yaw control mechanism for vectoring the efflux from the propulsion means about the yaw axis and a pitch control mechanism for vectoring the efflux from the propulsion means about the pitch axis of the main structure. The vehicle has significant cargo carrying capacity and is capable of operating either in ground effect, over terrain, or on water.
摘要翻译：一种公升翼车辆包括在鼻端和尾端之间延伸的主结构，包括具有小于约1.0的纵横比并且在前缘和后缘之间延伸的空气动力提升体。提升体在前缘和后缘之间的厚度与弦的长度之比大于约1:8。在鼻端附近提供推进源，用于产生外排，并用于在远离鼻端的方向上引导超出尾端的外流。方向控制机构位于鼻端附近，用于将车辆绕偏转轴线转动成具有中心的曲线，并且因此对来自推进源的流出进行矢量化，以将外流引导到转向的外侧，将鼻端朝向曲线中心。方向控制机构包括偏航控制机构，用于对来自推进装置的绕偏转轴线的流出进行矢量化;以及俯仰控制机构，用于对来自推进装置的推进装置围绕主结构的俯仰轴线进行矢量化。该车具有重要的货物承载能力，能够在地面作用，地形或水上运行。

2. 发明授权

US6138950A Aircraft engine air intake system 有权
标题翻译：飞机发动机进气系统
公开(公告)号：US6138950A
公开(公告)日：2000-10-31
申请号：US167209
申请日：1998-10-06
申请人： Barnaby Sam Wainfan , Yu Ping Liu , Daniel R. Rihn , Douglas William Leggett , Martin James Georges , Jeffry Scott Philhower , Douglas Ellwood Shultz , Charles Boccados
发明人： Barnaby Sam Wainfan , Yu Ping Liu , Daniel R. Rihn , Douglas William Leggett , Martin James Georges , Jeffry Scott Philhower , Douglas Ellwood Shultz , Charles Boccados
IPC分类号： B64D33/02 , F02C7/05 , F02C7/055 , B64B1/24 , B01D39/00 , B64D27/00
CPC分类号： F02C7/05 , B64D33/02 , F02C7/055 , B64D2033/022 , B64D2033/026 , Y02T50/672
摘要： In accordance with the present invention, there is provided an aircraft engine air intake cover for use with an air intake which is characterized by an air velocity profile therewithin. The air intake cover is provided with an air induction plate which disposed across at least a portion of the air intake. The air intake cover is further provided with a multitude of air induction ducts. The induction ducts are disposed about and extend through the air induction plate. Each induction duct has a duct inlet, a duct outlet and a duct body interposed between the duct inlet and the duct outlet. The duct inlets each respectively define an effective inlet diameter. The duct bodies each respectively define a duct body length which is greater than the associated effective duct inlet diameter. The duct outlets each respectively define an effective outlet diameter greater than the effective inlet diameter for increasing the cohesiveness of the air velocity profile within the air intake.
摘要翻译：根据本发明，提供了一种与进气口一起使用的飞机发动机进气盖，其特征在于其中的空气速度分布。吸气罩设置有空气感应板，其设置在进气口的至少一部分的两侧。进气盖还设有多个空气导入管。导入管围绕并延伸通过空气感应板。每个感应管道具有管道入口，管道出口和插入管道入口和管道出口之间的管道体。管道入口各自分别限定有效入口直径。导管体各自分别限定了大于相关联的有效管道入口直径的管道本体长度。导管出口分别限定大于有效入口直径的有效出口直径，以增加空气入口内的空气速度分布的内聚性。

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