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1. 发明申请

US20180162559A1 LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF 审中-公开
公开(公告)号：US20180162559A1
公开(公告)日：2018-06-14
申请号：US15852815
申请日：2017-12-22
申请人： 8 RIVERS CAPITAL, LLC
发明人： Miles R. Palmer
IPC分类号： B64G1/40 , F41B6/00 , F42C11/00 , B64G1/00 , F02K9/95 , F41A1/04 , F41F1/00 , F42B6/00 , F42B15/10 , F42B15/12
CPC分类号： B64G1/409 , B64G1/002 , B64G1/402 , B64G1/406 , F02K9/95 , F41A1/04 , F41B6/00 , F41B6/006 , F41F1/00 , F41F3/04 , F41F3/0406 , F42B6/006 , F42B15/10 , F42B15/12 , F42C11/00 , F42C11/04
摘要： The present disclosure relates to a launch system, a launch vehicle for use with the launch system, and methods of launching a payload utilizing the launch vehicle and/or the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch vehicle can comprise a payload, a propellant tank, an electrical heater wherein propellant, such as a light gas (e.g., hydrogen) is electrically heated to significantly high temperatures, an exhaust nozzle from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec, and sliding electrical contacts in electrical connection with the electrical heater. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube formed of concentric electrically conductive tubes, as well as an electrical energy source, such as a battery bank and associated inductor.

2. 发明授权

US09862506B2 Launch vehicle and system and method for economically efficient launch thereof 有权
公开(公告)号：US09862506B2
公开(公告)日：2018-01-09
申请号：US15251408
申请日：2016-08-30
申请人： 8 Rivers Capital, LLC
发明人： Miles R. Palmer
IPC分类号： B64G1/40 , B64G1/00 , F42B6/00 , F41A1/04 , F42B15/10 , F42B15/12 , F02K9/95 , F41F1/00 , F42C11/00 , F41B6/00
CPC分类号： B64G1/409 , B64G1/002 , B64G1/402 , B64G1/406 , F02K9/95 , F41A1/04 , F41B6/00 , F41B6/006 , F41F1/00 , F41F3/04 , F41F3/0406 , F42B6/006 , F42B15/10 , F42B15/12 , F42C11/00 , F42C11/04
摘要： The present disclosure relates to a launch system, a launch vehicle for use with the launch system, and methods of launching a payload utilizing the launch vehicle and/or the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch vehicle can comprise a payload, a propellant tank, an electrical heater wherein propellant, such as a light gas (e.g., hydrogen) is electrically heated to significantly high temperatures, an exhaust nozzle from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec, and sliding electrical contacts in electrical connection with the electrical heater. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube formed of concentric electrically conductive tubes, as well as an electrical energy source, such as a battery bank and associated inductor.

3. 发明授权

US09425617B2 Modular electronically reconfigurable battery system 有权
标题翻译：模块化电子可重新配置的电池系统
公开(公告)号：US09425617B2
公开(公告)日：2016-08-23
申请号：US13842828
申请日：2013-03-15
申请人： L-3 Applied Technologies, Inc.
发明人： Douglas M Weidenheimer , Kevin J Donegan
IPC分类号： H02J1/00 , F41B6/00 , H02J7/00
CPC分类号： H02J1/00 , F41B6/00 , H02J7/0024 , Y02T10/7055 , Y10T307/297 , Y10T307/305 , Y10T307/653
摘要： An electronically reconfigurable battery includes a number of battery modules selectively interconnected by a number of electronic switches, wherein a selectable number of battery modules may be connected either in a series configuration or in a parallel configuration, as a result of placing selected switches of said plurality of switches in open states or closed states. In a parallel configuration, the battery provides power to a primary load, such as a propulsion load for a vehicle. In a series configuration, the battery is configured to provide a high voltage and high power output to a short-term and/or pulsed load, such as an additional load provided on the vehicle. Current from the battery is limited in one of three ways: a) by the batteries themselves; b) a current limiting device or system in series with the total erected battery; or c) a single level power converter or current limiter that is used to erect and charge the capacitor bank in a sequential one level at a time manner until the battery is fully erected and the capacitor is fully charged.
摘要翻译：一种电子可重新配置的电池包括通过多个电子开关选择性互连的多个电池模块，其中可选择数量的电池模块可以以串联配置或并联配置连接，作为将所述多个的开关状态或闭合状态。在并联配置中，电池为主负载提供电力，例如用于车辆的推进负载。在串联配置中，电池被配置为向诸如车辆上提供的附加负载的短期和/或脉冲负载提供高电压和高功率输出。电池的电流有三种限制：a）电池本身; b）与总直立电池串联的限流装置或系统; 或c）单级功率转换器或电流限制器，用于以时间方式对电容器组进行连续和充电，直到电池完全竖立并且电容器被完全充电。

4. 发明授权

US09290278B2 Systems and methods for launching space vehicles 有权
标题翻译：发射太空车的系统和方法
公开(公告)号：US09290278B2
公开(公告)日：2016-03-22
申请号：US14084006
申请日：2013-11-19
申请人： David G. Dillon
发明人： David G. Dillon
IPC分类号： B64G1/00 , B64G5/00 , F42B5/045 , F42B12/62 , F41B6/00 , B64G1/58
CPC分类号： B64G1/002 , B64G1/58 , B64G5/00 , F41B6/00 , F41B6/006 , F42B5/045 , F42B12/625
摘要： Systems and methods for launching space vehicles into orbit involve placing a space vehicle into a protective container. The protective container is placed on a sled in a maglev tunnel and then launched into the atmosphere. Once the protective container reaches a certain height the space vehicle is released from the protective container and the space vehicle then proceeds to the desired orbital position.
摘要翻译：将空间车辆发射进入轨道的系统和方法涉及将空间车辆放入保护容器中。将保护容器放置在磁悬浮隧道中的雪橇上，然后发射到大气中。一旦保护容器达到一定高度，空间车辆就从保护容器中释放出来，然后空间车辆进入所需的轨道位置。

5. 发明授权

US09074915B2 Photovoltaic system having module monitoring 有权
标题翻译：光伏系统具有模块监控功能
公开(公告)号：US09074915B2
公开(公告)日：2015-07-07
申请号：US13144356
申请日：2009-12-18
申请人： Johannes Kalhoff , Thorsten Temme , Roland Bent
发明人： Johannes Kalhoff , Thorsten Temme , Roland Bent
IPC分类号： H02J1/00 , H02J3/00 , G01D21/00 , G01D4/00 , H01L31/02 , F41B6/00 , G05F1/62 , H02J7/00 , H02J7/35 , G06F15/00 , H04W84/18 , H02S50/10
CPC分类号： G01D21/00 , F41B6/00 , G01D4/002 , G05F1/62 , G06F15/00 , H01L31/02021 , H02J7/0024 , H02J7/35 , H02S50/10 , H04W84/18 , Y02B70/346 , Y02B90/241 , Y02B90/246 , Y02E10/50 , Y02T10/7055 , Y04S20/32 , Y04S20/42 , Y04S20/525 , Y10T307/653
摘要： The invention concerns a PV system in which a multitude of PV modules are interconnected to PV generators. Each of the PV modules comprises a network interface for transmitting module-specific data to a control device and analyzing the same. The data network is designed as a self-organizing network, in particular as a self-organizing meshed radio network.
摘要翻译：本发明涉及一种PV系统，其中多个PV模块互连到光伏发电机。每个PV模块包括用于将特定于模块的数据发送到控制设备并对其进行分析的网络接口。数据网络被设计为自组织网络，特别是作为自组织网状无线电网络。

6. 发明申请

US20140026876A1 CONTROLLABLE LAUNCHER 有权
标题翻译：可控发射器
公开(公告)号：US20140026876A1
公开(公告)日：2014-01-30
申请号：US13668731
申请日：2012-11-05
申请人： DEKA Products Limited Partnership
发明人： Dean Kamen , Larry B. Gray , Richard J. Lanigan
IPC分类号： F41B11/00 , F41B15/00
CPC分类号： F41B11/00 , A63G31/08 , A63J3/00 , F41B6/00 , F41B7/00 , F41B15/00 , F41F7/00
摘要： A controllable launcher for propelling a payload through a predictable and repeatable trajectory to a desired height. The launcher has an energy source for propelling a carriage and a piston in substantially opposing directions and a controller for controlling the trajectory of the propelled payload to enable the payload to land gently at a safe impact distance from the edge of a destination structure.
摘要翻译：一种可控的发射器，用于通过可预测和可重复的轨迹将有效载荷推进到所需的高度。发射器具有用于在基本相反的方向上推动滑架和活塞的能量源，以及用于控制推进式有效载荷的轨迹的控制器，以使有效载荷能够在距离目的地结构的边缘的安全冲击距离处轻轻地着陆。

7. 发明申请

US20110140526A1 MODULAR ELECTRONICALLY RECONFIGURABLE BATTERY SYSTEM 有权
标题翻译：模块化电子可重新配置的电池系统
公开(公告)号：US20110140526A1
公开(公告)日：2011-06-16
申请号：US13031365
申请日：2011-02-21
申请人： Douglas M. WEIDENHEIMER , Kevin J. DONEGAN , David Wayne MORTON
发明人： Douglas M. WEIDENHEIMER , Kevin J. DONEGAN , David Wayne MORTON
IPC分类号： H02J1/10 , H01M10/38
CPC分类号： F41B6/00 , B60K6/00 , H02J7/0024 , Y02T10/7055 , Y10T307/653
摘要： An electronically reconfigurable battery includes a number of battery modules selectively interconnected by a number of electronic switches, wherein a selectable number of battery modules may be connected either in a series configuration or in a parallel configuration, as a result of placing selected switches of said plurality of switches in open states or closed states. In a parallel configuration, the battery provides power to a primary load, such as a propulsion load for a vehicle. In a series configuration, the battery is configured to provide a high voltage and high power output to a short-term and/or pulsed load, such as an additional load provided on the vehicle. Current from the battery is limited in one of three ways: a) by the batteries themselves; b) a current limiting device or system in series with the total erected battery; or c) a single level power converter or current limiter that is used to erect and charge the capacitor bank in a sequential one level at a time manner until the battery is fully erected and the capacitor is fully charged.
摘要翻译：一种电子可重新配置的电池包括通过多个电子开关选择性互连的多个电池模块，其中可选择数量的电池模块可以以串联配置或并联配置连接，作为将所述多个的开关状态或闭合状态。在并联配置中，电池为主负载提供电力，例如用于车辆的推进负载。在串联配置中，电池被配置为向诸如车辆上提供的附加负载的短期和/或脉冲负载提供高电压和高功率输出。电池的电流有三种限制：a）电池本身; b）与总直立电池串联的限流装置或系统; 或c）单级功率转换器或电流限制器，用于以时间方式对电容器组进行连续和充电，直到电池完全竖起并且电容器被充满电为止。

8. 发明授权

US07753040B2 Helical field accelerator 有权
标题翻译：螺旋场加速器
公开(公告)号：US07753040B2
公开(公告)日：2010-07-13
申请号：US10972661
申请日：2004-10-25
申请人： Michael Victor , Robert Victor
发明人： Michael Victor , Robert Victor
IPC分类号： F41F7/00
CPC分类号： F41B6/00 , F41F7/00
摘要： A helical field device that accelerates an object to high velocity by converting rotational kinetic energy in the device into linear kinetic energy in the object, and alternatively, that decelerates objects from high velocity by converting the linear kinetic energy in the object into rotational kinetic energy in the device. The device transfers kinetic energy between the device and an object through the use of a localized high pressure field in the form of a helix having a variable pitch along the length of the device, which couples the object to the device without the pressure field itself significantly contributing energy into the system. Instead, the energy that is used to accelerate the object comes from the kinetic energy imparted to the device by an outside source, such as an engine, or a potential energy storage device.
摘要翻译：通过将装置中的旋转动能转换成物体中的线性动能，将物体加速到高速度的螺旋现场装置，或者通过将物体中的线性动能转换成旋转动能，从而将物体从高速度减速装置。该装置通过使用沿着装置的长度具有可变间距的螺旋形式的局部高压场来传递装置和物体之间的动能，其将物体耦合到装置而没有压力场本身显着为系统贡献力量。相反，用于加速物体的能量来自外部源（例如发动机）或潜在的能量存储装置给予设备的动能。

9. 发明授权

US07406829B2 Cryogenic liquid oxidizer cooled high energy system 有权
标题翻译：低温液体氧化器冷却高能量系统
公开(公告)号：US07406829B2
公开(公告)日：2008-08-05
申请号：US11131690
申请日：2005-05-18
申请人： George Albert Coffinberry
发明人： George Albert Coffinberry
IPC分类号： F02C6/08 , F02C6/14
CPC分类号： F41H13/0043 , F02C1/00 , F41B6/00 , H02K7/1823 , H02K9/20 , H02K55/02 , Y02E40/622
摘要： A high energy system comprising a high energy electrical device powered by an electrical generator both of which are cooled by a cryogenic liquid oxidant stored in a storage tank. A power turbine powered by a combustor using fuel and the oxidant drives the electrical generator. A turbopump powered by a portion of exhaust flow from the power turbine pumps the cryogenic liquid oxidant from the storage tank to the generator and the device. In an exemplary embodiment of the system, the electrical device is a directed energy weapon, uses liquid air as the liquid oxidant, and uses a variable geometry turbine nozzle in the power turbine. A reheater may be used between a high pressure turbine and a lower pressure turbine of the power turbine. Compressor bleed from a gas turbine engine may provide air augmentation to the power turbine.
摘要翻译：一种高能量系统，其包括由发电机供电的高能电子装置，两者都由储存在储罐中的低温液体氧化剂冷却。由使用燃料的燃烧器供电的动力涡轮机，氧化剂驱动发电机。由来自动力涡轮机的一部分排气供给的涡轮泵将低温液体氧化剂从储罐泵送到发生器和装置。在系统的示例性实施例中，电气装置是定向能量武器，使用液体空气作为液体氧化剂，并且在动力涡轮机中使用可变几何涡轮喷嘴。可以在动力涡轮机的高压涡轮机和低压涡轮机之间使用再热器。来自燃气涡轮发动机的压缩机流出可以向动力涡轮机提供空气增加。

10. 发明授权

US07380504B2 Telescoped projectile 有权
公开(公告)号：US07380504B2
公开(公告)日：2008-06-03
申请号：US11204575
申请日：2005-08-16
申请人： Richard Dryer
发明人： Richard Dryer
IPC分类号： F42B14/00
CPC分类号： F41B6/00 , F42B6/006 , F42B10/00 , F42B10/02 , F42B10/663
摘要： A projectile reconfigures in flight from a launch configuration, in which the center of gravity is aft of the center of pressure, to a flight configuration, in which the center of gravity is forward of the center of pressure. The projectile includes a forward portion and an aft portion, and the reconfiguration involves movement of at least part of one of the portions relative to the other portion. The projectile may have an overall substantially conical shape when in the launch configuration. The forward portion may include a substantially conical nose, and a cylindrical central body attached to the nose. In the launch configuration, at least part of the central body may be located within a hollow in a base of the aft portion. The base may be slidable relative to the central body.

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