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1. 发明授权

US06634597B2 Method and apparatus for controlling aircraft airflow 失效
标题翻译：用于控制飞机气流的方法和装置
公开(公告)号：US06634597B2
公开(公告)日：2003-10-21
申请号：US10044517
申请日：2002-01-11
申请人： Richard N. Johnson , Paul E. Nelson
发明人： Richard N. Johnson , Paul E. Nelson
IPC分类号： B64D1302
CPC分类号： B64D13/00 , B64D2013/0625
摘要： A method and apparatus for controlling aircraft airflow. An apparatus in accordance with an embodiment of the invention can include an air scoop having an inlet and an outlet and configured to mount to the aircraft and be movable relative to at least a portion of the aircraft between a first position and a second position. The air scoop can be oriented to capture air when in the second position. The outlet can be configured to be coupled in fluid communication with a pressurized portion of the aircraft when the air scoop is in the second position to convey air from the inlet to the pressurized portion. The air scoop can be configured to significantly increase the drag of the aircraft from a first value when the air scoop is in the first position to a second value when the air scoop is in the second position.
摘要翻译：一种用于控制飞行器气流的方法和装置。根据本发明的实施例的装置可以包括具有入口和出口并被配置为安装到飞行器并且可以相对于飞行器的至少一部分在第一位置和第二位置之间移动的空气铲斗。空气勺可以定向成在处于第二位置时捕获空气。当空气铲斗处于第二位置以将空气从入口传送到加压部分时，出口可以构造成与飞行器的加压部分流体连通地联接。当空气铲斗处于第二位置时，空气铲斗可以构造成在空气铲斗处于第一位置时显着增加飞行器从第一值的阻力。

2. 发明授权

US5121806A Power wheelchair with torsional stability system 失效
标题翻译：电动轮椅具有扭转稳定系统
公开(公告)号：US5121806A
公开(公告)日：1992-06-16
申请号：US664674
申请日：1991-03-05
申请人： Richard N. Johnson
发明人： Richard N. Johnson
IPC分类号： A61G5/04 , B60K1/04
CPC分类号： B60K1/04 , A61G5/1051 , A61G5/045 , A61G5/1072 , Y10S180/907 , Y10S297/04
摘要： An improved power wheelchair is provided that provides exceptional maneuverability, stability and directional tracking characteristics. The wheelchair includes a torsional frame and a rigid stability frame. Two main wheels and a pivoting drive wheel are coupled to the torsional frame. At least two freely rotating casters are coupled to the stability frame. The torsional frame and stability frame interact to provide automatic compensation for directional tracking errors caused by shifts in the mass center of an occupant. The wheelchair can be equipped with either manual or power steering. A unique three-point battery mounting assembly also permits easy replacement of batteries.
摘要翻译：提供了一种改进的动力轮椅，提供卓越的机动性，稳定性和定向跟踪特性。轮椅包括扭力框架和刚性稳定框架。两个主轮和枢转驱动轮联接到扭转框架。至少两个自由旋转的脚轮联接到稳定框架。扭转框架和稳定框架相互作用，为乘员身体中心移动引起的定向跟踪误差提供自动补偿。轮椅可配备手动或动力转向。独特的三点电池安装组件也可以轻松更换电池。

3. 发明授权

US06860726B2 Dual drive for hydraulic pump and air boost compressor 有权
标题翻译：双驱动液压泵和增压压缩机
公开(公告)号：US06860726B2
公开(公告)日：2005-03-01
申请号：US10068234
申请日：2002-02-05
申请人： Howard Carter III , Richard N. Johnson , Michael John Provost , John David Brown
发明人： Howard Carter III , Richard N. Johnson , Michael John Provost , John David Brown
IPC分类号： B64D41/00 , F02C7/32 , F04D25/02 , F04D25/06 , F04B17/03
CPC分类号： B64D41/00 , F02C7/32 , F04D25/02 , F04D25/06 , Y02T50/44 , Y02T50/671 , Y10T74/19172
摘要： A dual drive system for a hydraulic pump and an air boost compressor is provided. Reversible power is transmitted to a shaft connected to clockwise and counterclockwise over-running clutches connected to different vehicle or equipment subsystems. Reversing the drive allows power to be alternately transmitted to one or the other of the subsystems. The invention includes utilizing the dual drive for hydraulic and air conditioning systems for an aircraft, with the provision of an additional drive motor providing constant power to one or more of the subsystems.
摘要翻译：提供了一种用于液压泵和增压压缩机的双驱动系统。可逆动力被传递到连接到连接到不同车辆或设备子系统的顺时针和逆时针超跑离合器的轴。驱动器的反转允许电力被交替传送到一个或另一个子系统。本发明包括利用用于飞机的液压和空调系统的双驱动器，其中提供额外的驱动马达为一个或多个子系统提供恒定的功率。

4. 发明授权

US5619205A Microarc chaff 失效
标题翻译： Microarc谷壳
公开(公告)号：US5619205A
公开(公告)日：1997-04-08
申请号：US797390
申请日：1985-09-25
申请人： Richard N. Johnson
发明人： Richard N. Johnson
IPC分类号： H01Q15/14 , H04K3/00 , G01S7/38
CPC分类号： H01Q15/145
摘要： An improved chaff in which a plurality of metallic or metallic coated elets are joined as chain links that, when deployed, produce microarcs when the link elements make and break contact with each other in an electromagnet field such as that created by a high power radar transmitter. These microarcs will then in turn create current spikes that will reflect a radar signal that has a wider bandwidth than conventional chaff, so as to make it more difficult to distinguish the chain link chaff from a fast moving target such as an aircraft.
摘要翻译：一种改进的谷壳，其中多个金属或金属涂层元件作为链节连接，当部署时，当连接元件在诸如由大功率雷达发射器产生的电磁场中形成和断开接触时，产生微弧。然后，这些微型计算机又将产生电流尖峰，其将反映具有比常规谷壳更宽带宽的雷达信号，以便使链式谷壳与诸如飞机的快速移动目标更加难于区分。

5. 发明授权

US4295334A Parametric energy converter 失效
标题翻译：参数能量转换器
公开(公告)号：US4295334A
公开(公告)日：1981-10-20
申请号：US99368
申请日：1979-12-03
申请人： Richard N. Johnson
发明人： Richard N. Johnson
IPC分类号： F01K11/04 , F01K11/02
CPC分类号： F01K11/04
摘要： A method and apparatus for converting thermal energy into mechanical energy by parametric pumping of rotary inertia. In a preferred embodiment, a modified Tesla turbine rotor is positioned within a rotary boiler along its axis of rotation. An external heat source, such as solar radiation, is directed onto the outer casing of the boiler to convert the liquid to steam. As the steam spirals inwardly toward the discs of the rotor, the moment of inertia of the mass of steam is reduced to thereby substantially increase its kinetic energy. The laminar flow of steam between the discs of the rotor transfers the increased kinetic energy to the rotor which can be coupled out through an output shaft to perform mechanical work. A portion of the mechanical output can be fed back to maintain rotation of the boiler.
摘要翻译：一种通过旋转惯性的参数泵送将热能转换为机械能的方法和装置。在优选实施例中，改进的特斯拉涡轮机转子沿其旋转轴线定位在旋转锅炉内。诸如太阳辐射的外部热源被引导到锅炉的外壳上以将液体转化为蒸汽。随着蒸汽向内朝向转子的盘旋转，蒸汽质量的惯性矩减小，从而显着增加其动能。转子盘之间的蒸汽层流将转动的动能传递给转子，动力可以通过输出轴耦合出来进行机械作业。机械输出的一部分可被反馈以保持锅炉的旋转。

6. 发明授权

US08123163B2 Aircraft kinetic landing energy conversion system 有权
标题翻译：飞机动能降落能量转换系统
公开(公告)号：US08123163B2
公开(公告)日：2012-02-28
申请号：US12106135
申请日：2008-04-18
申请人： William R. McCoskey , Michael M. Vander Wel , Richard N. Johnson
发明人： William R. McCoskey , Michael M. Vander Wel , Richard N. Johnson
IPC分类号： B64C25/42
CPC分类号： B64C25/42 , B60L7/10 , B60L11/182 , B60L2200/26 , B64C25/36 , B64C25/405 , Y02T10/7005 , Y02T10/7072 , Y02T50/823 , Y02T90/122 , Y02T90/14
摘要： A kinetic energy system which transfers the kinetic landing into recoverable electric energy for an aircraft. The system incorporates at least one wheel supporting the aircraft for landing and takeoff coupled with a dynamic functioning motor/generator mounted to and operated by rotation of the wheel to create electrical energy from kinetic energy. An induction shoe structurally connected to the aircraft and electrically connected to the motor/generator, which shoe draws the converted energy from the generator which supplies the load created by the inductively coupled induction shoe to the an ancillary load provided by the resistive heat sink on by the capacitor storage bank. This provides the generator circuit for conversion of the rotational energy of the wheel to electrical energy and creates braking drag. In exemplary embodiments, the system employs an energy storage system acting as the load to store electrical potential energy created by the generator. Additionally, the generator is employable as a motor, receiving energy from the storage system for traction power to the associated aircraft wheel. An induction grid or a surface mounted conductive layer mounted into or onto a runway is employed for transferring energy to and from the motor/generator.
摘要翻译：将动能着陆转变为飞机可恢复电能的动能系统。该系统包括至少一个支撑飞机的轮子，用于着陆和起飞，其与通过轮的旋转安装到其上并由动能产生电能的动态功能马达/发电机相结合。一种结构上连接到飞行器并与电动机/发电机电连接的感应瓦，该滑靴将来自发电机的转换的能量从电感耦合感应靴产生的负载拉到由电阻散热器所提供的辅助负载上电容器存储库。这提供了用于将车轮的旋转能量转换为电能并且产生制动阻力的发电机电路。在示例性实施例中，系统采用充当负载的能量存储系统来存储由发电机产生的电势。此外，发电机可用作电动机，从存储系统接收能量以用于牵引力到相关的飞行器轮。安装在跑道中或导轨上的感应电网或表面安装的导电层用于将电能传送到电动机/发电机。

7. 发明授权

US07578469B2 Terminal docking port for an operational ground support system 有权
标题翻译：终端对接端口，用于操作地面支持系统
公开(公告)号：US07578469B2
公开(公告)日：2009-08-25
申请号：US11164467
申请日：2005-11-23
申请人： William R. McCoskey , Richard N. Johnson
发明人： William R. McCoskey , Richard N. Johnson
IPC分类号： B64C9/00
CPC分类号： B64F1/305 , B64C25/405 , B64F1/31 , B64F1/36 , Y02T50/82 , Y02T50/823
摘要： A terminal (14) for an airport (13) includes multiple servicing levels (82, 102). A ground support service sub-system is coupled to the servicing levels (82, 102) and is configured to mate with a service opening (26) of the aircraft (12). The ground support service sub-system provides services to the aircraft (12) through the service opening (26) and on the servicing levels (82, 102).
摘要翻译：机场（13）的终端（14）包括多个服务等级（82,102）。地面支持服务子系统耦合到维修水平（82,102），并被配置为与飞行器（12）的服务开口（26）配合。地面支援服务子系统通过维修口（26）和服务水平（82,102）向飞机（12）提供服务。

8. 发明授权

US07275715B2 Operational ground support system 有权
标题翻译：操作地面支援系统
公开(公告)号：US07275715B2
公开(公告)日：2007-10-02
申请号：US10711610
申请日：2004-09-28
申请人： William R. McCoskey , Richard N. Johnson , W. James Renton
发明人： William R. McCoskey , Richard N. Johnson , W. James Renton
IPC分类号： B64C9/00
CPC分类号： B64F1/36 , B64C25/405 , B64F1/305 , B64F1/31 , Y02T50/82 , Y02T50/823
摘要： An integrated operational ground mobility and support system (10) that includes an aircraft (12) having one or more service openings on a side of the aircraft (12). The integrated support system (10) may have an airport interface terminal docking port (14) that has a ground support service sub-system. The docking port (14) mates with the aircraft (12) at the service openings and has multiple service levels. The ground support service sub-system provides services to the aircraft (12) through the service openings and on the service levels. The integrated support system (10) may have in addition to or in replacement of the interface terminal docking port an aircraft loader/unloader. The loader/unloader has ground support service sub-systems and mates with the aircraft (12) at one or more of the service openings. The service sub-systems of the loader/unloader include a passenger ingress/egress system (62) and provide services to the aircraft (12).
摘要翻译：一种综合的操作地面机动和支援系统（10），包括在飞机（12）一侧具有一个或多个服务开口的飞机（12）。集成支撑系统（10）可以具有具有地面支撑服务子系统的机场接口终端对接端口（14）。对接端口（14）在服务口处与飞机（12）配合，并具有多个服务级别。地面支援服务子系统通过服务开放和服务水平向飞机（12）提供服务。集成支持系统（10）可以具有除了接口终端对接端口或替代飞行器装载机/卸载机的附加或替代。装载机/卸载机具有地面支持服务子系统，并且在一个或多个服务开口处与飞机（12）配合。装载机/卸载机的服务子系统包括乘客入口/出口系统（62）并向飞行器（12）提供服务。

9. 发明授权

US4204198A Radar analog to digital converter 失效
标题翻译：雷达模数转换器
公开(公告)号：US4204198A
公开(公告)日：1980-05-20
申请号：US862319
申请日：1977-12-20
申请人： Andree N. Filipov , Richard N. Johnson , Christopher N. Winslow
发明人： Andree N. Filipov , Richard N. Johnson , Christopher N. Winslow
IPC分类号： H03M1/00 , H03K13/02
CPC分类号： H03M1/48 , H03M1/182
摘要： An analog-to-digital converter is disclosed providing high speed operationor high resolution analog signal data. The converter utilizes the repetitive nature of the data by converting a portion of the signal corresponding to the changing component of the data. A smaller number of bits of information is thus converted from analog-to-digital form than is needed to represent the data. In addition to savings in hardware, a significant saving in conversion time is provided. The cancellation of static components of a radar signal moreover provides, within the system, a clutter-free signal.
摘要翻译：公开了提供用于高分辨率模拟信号数据的高速操作的模数转换器。转换器通过转换对应于数据的变化分量的信号的一部分来利用数据的重复性质。因此，从数字形式转换比信息数据少的数字比数据更少。除了节省硬件外，还提供了显着的转换时间节省。雷达信号的静态分量的消除还在系统内提供无杂波信号。

10. 发明授权

US07549607B2 Aircraft having a dual floor servicing system associated with an operational ground support system 有权
标题翻译：具有与操作性地面支持系统相关联的双层维修系统的飞机
公开(公告)号：US07549607B2
公开(公告)日：2009-06-23
申请号：US11164463
申请日：2005-11-23
申请人： William R. McCoskey , Richard N. Johnson
发明人： William R. McCoskey , Richard N. Johnson
IPC分类号： B64C9/00
CPC分类号： B64F1/305 , B64C1/22 , B64C25/405 , B64F1/31 , B64F1/36 , Y02T50/82 , Y02T50/823
摘要： An aircraft (12) includes a servicing opening (26) and multiple service levels (82, 102). The service levels (82, 102) include a noncargo-based service level (82). The service levels (82, 102) are accessible through the service opening (26). An aircraft onboard primary servicing system (66) includes a primary service sub-system (151). An aircraft primary service coupler (154) is configured to attach to a corresponding terminal primary service coupler (152). The aircraft primary service coupler (154) and the terminal primary service coupler (152) providing at least one primary service therethrough.
摘要翻译：飞机（12）包括维修开口（26）和多个服务水平（82,102）。服务级别（82,102）包括基于非基于服务级别的服务级别（82）。服务级别（82,102）可通过服务开口（26）访问。主机服务系统（66）的飞机包括主服务子系统（151）。飞机主服务耦合器（154）被配置为附接到相应的终端主服务耦合器（152）。飞行器主要服务耦合器（154）和终端主要服务耦合器（152）通过其提供至少一个主要服务。

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