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公开(公告)号：US5217187A
公开(公告)日：1993-06-08
申请号：US349840
申请日：1989-05-09
申请人： David R. Criswell
发明人： David R. Criswell
摘要： A multi-use launch system comprises a plurality of different modules releasably securable together into a plurality of different possible launch configurations. The modules include an at least partially expendable, unmanned first stage unit which is capable of single-stage-to-orbit operations on its own carrying internal or external payloads, or as part of a multi-stage-to-orbit system for higher payload capacity launches. The first stage unit is demountably securable to other first stage units, unpowered cargo-carrying units, and/or manned space vehicles. The first stage unit may be completely expendable after launch.
摘要翻译： 多用途发射系统包括可释放地固定在一起成多个不同可能的发射配置的多个不同的模块。 这些模块包括至少部分可消耗的无人驾驶的第一级单元，其能够在其自己的承载内部或外部有效载荷上进行单级到轨道操作，或者作为用于更高有效载荷的多级到轨道系统的一部分 容量启动。 第一阶段单元可以安全地安装到其他第一级单元，无动力货物装载单元和/或载人空中飞行器。 第一阶段单元在发射后可能完全消耗。
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公开(公告)号：US20180198320A1
公开(公告)日：2018-07-12
申请号：US15868870
申请日：2018-01-11
申请人： David R. Criswell
CPC分类号： H02J50/23 , H01J25/50 , H01Q9/0435 , H01Q13/02 , H01Q13/0241 , H01Q15/0066 , H01Q15/12 , H01Q19/104 , H01Q19/108 , H02J50/27
摘要： A WPT system and apparatus for the WPT system is provided in the present invention. The apparatus includes: (i) a transmitter, and (ii) a receiver. The transmitter transmits microwave power towards the receiver. The transmitter includes a power generation source, a CP horn and an antenna reflect array aperture. The receiver includes a rectenna array aperture. The rectenna array aperture further includes a sub-array module, a DC power output and a power conditioner circuit. The power conditioner circuit further includes a plurality of rectenna elements. The one or more sub-array module couple to form the rectenna array aperture.
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公开(公告)号：US20120153744A1
公开(公告)日：2012-06-21
申请号：US13323585
申请日：2011-12-12
IPC分类号： H02J17/00
CPC分类号： B64G1/428 , B64G1/44 , H02J17/00 , H02J50/23 , H02J50/27 , H02J50/40 , H02J50/80 , H02J50/90
摘要： A power distribution network is provided comprising ground-based microwave transmitters, receivers and microwave redirectors. The ground-based microwave transmitters have their own directional, focus and amplitude controllers for aiming a focused microwave beam at a microwave redirector. The microwave redirectors each have a receiving antenna and a plurality of transmitting antennae such that the redirectors transmit focused microwave beams to at least two different stations (for example, being either ground-based microwave receivers or other microwave redirectors).
摘要翻译： 提供了一种配电网络，包括地面微波发射器，接收器和微波重定向器。 地面微波发射器具有自己的定向，聚焦和幅度控制器，用于将聚焦微波束瞄准微波重定向器。 微波重定向器每个都具有接收天线和多个发射天线，使得重定向器将聚焦的微波射束发射到至少两个不同的站（例如，基于地面的微波接收器或其他微波重定向器）。
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公开(公告)号：US07900875B2
公开(公告)日：2011-03-08
申请号：US11184158
申请日：2005-07-18
申请人： David R. Criswell
发明人： David R. Criswell
IPC分类号： B64G1/44
摘要： A system and method of generating and distributing power includes one or more microwave power transmitters at locations on Earth adjacent natural fuel or power resources such as natural gas, oil, solid fuel, or geothermal energy. The fuel or energy source is converted into electricity on site, and the electricity is then converted into microwave power beams transmitted from the microwave power transmitter towards a redirector satellite in orbit about the Earth. The redirector satellite then sends one or more microwave beams to rectennas located in consumer nations at appropriate sites for feeding the power grid or to additional redirector satellites for directing to rectennas located on the far side of the Earth.
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公开(公告)号：US5019768A
公开(公告)日：1991-05-28
申请号：US157081
申请日：1988-02-11
CPC分类号： H01Q1/248 , B64G1/428 , B64G1/44 , H01Q1/22 , Y10S343/02
摘要： A system for transmitting microwaves to one or more receiver assemblies comprises an array of separate microwave transmitting assemblies for emitting a plurality of microwave beams, the array being arranged to apparently fill a radiating aperture of predetermined shape and size when viewed from the direction of a receiver assembly, and a phase controlling assembly associated with the microwave transmitting assemblies for controlling the relative phase of the emitted beams to form at least one composite shaped microwave beam directed to at least one receiver assembly. The receiver assembly is located in the near field of the microwave beam. The transmitting assemblies are each associated with separate power sources comprising solar power collecting assemblies. In one arrangement the transmitting system is on the moon and the or each receiver assembly is on Earth.
摘要翻译： 用于将微波传输到一个或多个接收器组件的系统包括用于发射多个微波束的单独的微波发射组件的阵列，所述阵列布置成在从接收器的方向观察时明显地填充预定形状和尺寸的辐射孔 组件以及与微波发射组件相关联的相位控制组件，用于控制发射光束的相对相位，以形成指向至少一个接收器组件的至少一个复合形状的微波光束。 接收器组件位于微波束的近场中。 发射组件各自与包括太阳能收集组件的单独的电源相关联。 在一种布置中，发射系统在月球上，并且每个接收器组件在地球上。
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公开(公告)号：US5016295A
公开(公告)日：1991-05-21
申请号：US553240
申请日：1990-07-16
申请人： David R. Criswell
发明人： David R. Criswell
CPC分类号： E03D1/14 , E03D1/33 , F16K31/18 , Y10T137/7413
摘要： A two position float arm for regulating two water levels in water level control systems that are controlled by a float connected to a inlet water valve by a rod. The rod is replaced by a first member (22) hinged to a second member (28). The first member (22) is screwed into the inlet water valve boss while the second member (28) is screwed into the float boss. A sleeve (34) slides over the hinge, locking the first member (22) and second member (28) in line and establishing a first water level. The sleeve (34) may be slid away from the hinge allowing the second member (28) and the attached float to rise to a higher position relative to the first member (22) and thus establish a second water level. The sleeve (34) is maintained in the locked position by a spring. The sleeve is pulled away from the hinge by a cable attached to a knob or a lever.
摘要翻译： 用于调节水位控制系统中的两个水位的两位浮子臂，其由通过杆连接到入口水阀的浮子控制。 杆被由铰链到第二构件（28）的第一构件（22）代替。 将第一构件（22）拧入入口水阀座中，同时将第二构件（28）拧入浮动凸台。 套筒（34）在铰链上滑动，将第一构件（22）和第二构件（28）锁定在一起并建立第一水位。 套筒（34）可以从铰链滑动，允许第二构件（28）和附着的浮子相对于第一构件（22）上升到更高的位置，从而建立第二水位。 套筒（34）通过弹簧保持在锁定位置。 通过连接到旋钮或杠杆的电缆将套筒从铰链拉出。
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公开(公告)号：US08596581B2
公开(公告)日：2013-12-03
申请号：US13323585
申请日：2011-12-12
IPC分类号： B64G1/44
CPC分类号： B64G1/428 , B64G1/44 , H02J17/00 , H02J50/23 , H02J50/27 , H02J50/40 , H02J50/80 , H02J50/90
摘要： A power distribution network is provided comprising ground-based microwave transmitters, receivers and microwave redirectors. The ground-based microwave transmitters have their own directional, focus and amplitude controllers for aiming a focused microwave beam at a microwave redirector. The microwave redirectors each have a receiving antenna and a plurality of transmitting antennae such that the redirectors transmit focused microwave beams to at least two different stations (for example, being either ground-based microwave receivers or other microwave redirectors).
摘要翻译： 提供了一种配电网络，包括地面微波发射器，接收器和微波重定向器。 地面微波发射器具有自己的定向，聚焦和幅度控制器，用于将聚焦微波束瞄准微波重定向器。 微波重定向器每个都具有接收天线和多个发射天线，使得重定向器将聚焦的微波射束发射到至少两个不同的站（例如，基于地面的微波接收器或其他微波重定向器）。
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公开(公告)号：US08074936B2
公开(公告)日：2011-12-13
申请号：US13013791
申请日：2011-01-25
申请人： David R. Criswell
发明人： David R. Criswell
IPC分类号： B64G1/44
摘要： A system and method of generating and distributing power includes one or more microwave power transmitters at locations on Earth adjacent natural fuel or power resources such as natural gas, oil, solid fuel, or geothermal energy. The fuel or energy source is converted into electricity on site, and the electricity is then converted into microwave power beams transmitted from the microwave power transmitter towards a redirector satellite in orbit about the Earth. The redirector satellite then sends one or more microwave beams to rectennas located in consumer nations at appropriate sites for feeding the power grid or to additional redirector satellites for directing to rectennas located on the far side of the Earth.
摘要翻译： 产生和分配功率的系统和方法包括在地球上与天然气，石油，固体燃料或地热能相邻的天然燃料或电力资源的位置处的一个或多个微波功率发射器。 燃料或能源现场转换为电力，然后将电力转换成从微波功率发射器向围绕地球的轨道卫星转发的微波功率波束。 重定向卫星然后将一个或多个微波波束发送到位于消费国家的适当位置的直角用于馈送电网或用于引导到位于地球远侧的直角的另外的重定向器卫星。
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公开(公告)号：US20110156498A1
公开(公告)日：2011-06-30
申请号：US13013791
申请日：2011-01-25
申请人： David R. Criswell
发明人： David R. Criswell
摘要： A system and method of generating and distributing power includes one or more microwave power transmitters at locations on Earth adjacent natural fuel or power resources such as natural gas, oil, solid fuel, or geothermal energy. The fuel or energy source is converted into electricity on site, and the electricity is then converted into microwave power beams transmitted from the microwave power transmitter towards a redirector satellite in orbit about the Earth. The redirector satellite then sends one or more microwave beams to rectennas located in consumer nations at appropriate sites for feeding the power grid or to additional redirector satellites for directing to rectennas located on the far side of the Earth.
摘要翻译： 产生和分配功率的系统和方法包括在地球上与天然气，石油，固体燃料或地热能相邻的天然燃料或电力资源的位置处的一个或多个微波功率发射器。 燃料或能源现场转换为电力，然后将电力转换成从微波功率发射器向围绕地球的轨道卫星转发的微波功率波束。 重定向卫星然后将一个或多个微波波束发送到位于消费国家的适当位置的直角用于馈送电网或用于引导到位于地球远侧的直角的另外的重定向器卫星。
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10.发明授权Aerospace vehicle having multiple propulsion systems on a relatively rotatable flying wing 失效在相对可旋转的飞翼上具有多个推进系统的航空航天车辆
公开(公告)号：US4836470A
公开(公告)日：1989-06-06
申请号：US744491
申请日：1985-06-13
申请人： David R. Criswell
发明人： David R. Criswell
摘要： An aerospace vehicle having multiple propulsion systems on a relatively rotatable flying wing capable of takeoff and subsequent landing with intermediate space flight in the manner of a conventional aircraft and rocket, respectively, comprising an elongated wing member having internal passenger and crew, cargo and fuel storage compartments. A plurality of propulsion systems are distributed about the wing member for providing thrust and aerodynamic control. The vehicle also includes rotating means for controlling the direction of the thrust of the propulsion systems relative to the longitudinal axis of the wing whereby to rotate the wing member relative to the direction of flight. The vehicle takes off and lands with the longitudinal wing axis being transverse to the direction of thrust and therefore to the flight direction in a manner similar to that of conventional aircraft. In flight as the vehicle approaches space, the rotating means rotates the longitudinal wing axis into alignment with the direction of thrust of the plurality of propulsion systems and therefore to the direction of flight for suborbital, orbital and space flight in the manner similar to that of conventional rockets.
摘要翻译： 一种在相对可旋转的飞翼上具有多个推进系统的航空航天车辆，其能够分别以常规飞行器和火箭的方式起飞和随后着陆，具有中间空间飞行，包括具有内部乘客和船员，货物和燃料储存器的细长翼构件 隔间 多个推进系统围绕翼构件分布以提供推力和空气动力学控制。 车辆还包括用于控制推进系统相对于翼的纵向轴线的推力方向的旋转装置，从而相对于飞行方向旋转机翼构件。 车辆起飞并着陆，其中纵向翼轴线以与常规飞行器类似的方式横向于推力方向并因此横向于飞行方向。 在飞行中，当车辆接近空间时，旋转装置使纵向翼轴旋转成与多个推进系统的推力方向一致，并因此使其以与眶下，轨道和太空飞行相似的方式飞行， 常规火箭。
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