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    High Efficiency Power Production Methods, Assemblies, and Systems
    11.
    发明申请
    High Efficiency Power Production Methods, Assemblies, and Systems 审中-公开
    高效率电力生产方法，组件和系统

    公开(公告)号：US20140331687A1

    公开(公告)日：2014-11-13

    申请号：US14341327

    申请日：2014-07-25

    申请人： Palmer Labs, LLC ,  8 Rivers Capital, LLC

    发明人： Miles R. Palmer ,  Jeremy Eron Fetvedt ,  Rodney John Allam

    IPC分类号： F01D5/18 ,  F01D5/28

    CPC分类号： F01D5/183 ,  F01D5/085 ,  F01D5/282 ,  F01D25/14 ,  F02C3/34 ,  F05D2220/32 ,  F05D2230/22 ,  F05D2260/203 ,  F05D2260/95 ,  F05D2300/702

    摘要： The present disclosure provides methods, assemblies, and systems for power production that can allow for increased efficiency and lower cost components arising from the control, reduction, or elimination of turbine blade mechanical erosion by particulates or chemical erosion by gases in a combustion product flow. The methods, assemblies, and systems can include the use of turbine blades that operate with a blade velocity that is significantly reduced in relation to conventional turbines used in typical power production systems. The methods and systems also can make use of a recycled circulating fluid for transpiration protection of the turbine and/or other components. Further, recycled circulating fluid may be employed to provide cleaning materials to the turbine.

    摘要翻译： 本公开提供了用于功率生产的方法，组件和系统，其可以允许由燃烧产物流中的气体的微粒或化学侵蚀来控制，减少或消除涡轮机叶片机械侵蚀而产生的效率提高和成本较低的部件。 方法，组件和系统可以包括利用相对于在典型电力生产系统中使用的传统涡轮机显着降低的叶片速度来操作的涡轮机叶片。 所述方法和系统还可以利用循环的循环液体来进行涡轮机和/或其他部件的蒸腾保护。 此外，再循环的循环流体可用于向涡轮机提供清洁材料。

    LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF
    13.
    发明申请
    LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF 有权
    发射车辆及其经济有效发射的系统及方法

    公开(公告)号：US20140306064A1

    公开(公告)日：2014-10-16

    申请号：US14211698

    申请日：2014-03-14

    申请人： Palmer Labs, LLC

    发明人： Miles R. Palmer

    IPC分类号： B64G1/40

    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.

    摘要翻译： 本公开涉及一种发射系统，与发射系统一起使用的运载火箭，以及使用该运载火箭和/或发射系统发射有效载荷的方法。 本公开可以提供在地面位置，地球轨道位置或眶外位置处的有效载荷的传送。 运载火箭可以包括有效载荷，推进剂罐，电加热器，其中诸如轻质气体（例如氢气）的推进剂被电加热到显着高的温度，加热的推进剂从该喷嘴膨胀以提供排气速度 例如为7-16km / sec，以及与电加热器电连接的滑动电触头。 运载火箭可以与发射系统一起使用，其可以进一步包括由同心导电管形成的发射管，以及电能源，例如电池组和相关联的电感器。

    DIVERGED-BEAM COMMUNICATIONS SYSTEM
    17.
    发明申请
    DIVERGED-BEAM COMMUNICATIONS SYSTEM 审中-公开

    公开(公告)号：US20180048390A1

    公开(公告)日：2018-02-15

    申请号：US15790961

    申请日：2017-10-23

    申请人： PALMER LABS, LLC ,  8 RIVERS CAPITAL, LLC

    发明人： Miles R. Palmer ,  Aleksander Edward Osadzinski ,  William J. Brown

    IPC分类号： H04B10/112 ,  H04B7/06 ,  H04B10/50 ,  H04B10/116

    CPC分类号： H04B10/1123 ,  H04B7/0617 ,  H04B10/116 ,  H04B10/503

    摘要： An apparatus is provided that includes a modulator and an optical transmitter coupled to the modulator and configured to emit an optical beam that the modulator is configured to modulate with data. The optical transmitter may thereby be configured to emit the optical beam carrying the data and without artificial confinement for receipt by an optical receiver configured to detect and recover the data from the optical beam. The optical transmitter may be configured to emit the optical beam with a divergence angle greater than 0.1 degrees, and with a photonic efficiency of less than 0.05%. The photonic efficiency may relate a number of photons of the optical beam detectable by the optical receiver, to a number of photons of the optical beam emitted by the optical transmitter.

    LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF
    18.
    发明申请
    LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF 有权
    发射车辆及其经济有效发射的系统及方法

    公开(公告)号：US20140306065A1

    公开(公告)日：2014-10-16

    申请号：US14211779

    申请日：2014-03-14

    申请人： 8 Rivers Capital, LLC ,  Palmer Labs, LLC

    发明人： Miles R. Palmer ,  Glenn William Brown, JR.

    IPC分类号： B64G1/40

    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, and an exhaust nozzle from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube formed of at least one tube, which can be electrically conductive and which can be combined with at least one insulator tube. An electrical energy source, such as a battery bank and associated inductor, can be provided.

    摘要翻译： 本公开涉及一种发射系统，与发射系统一起使用的运载火箭，以及使用该运载火箭和/或发射系统发射有效载荷的方法。 本公开可以提供在地面位置，地球轨道位置或眶外位置处的有效载荷的传送。 运载火箭可以包括有效载荷，推进剂罐，电加热器，其中推进剂，例如轻质气体（例如氢气）被电加热至显着高的温度，以及排气喷嘴，加热的推进剂从该喷嘴膨胀以提供排气 例如7-16公里/秒的速度。 运载火箭可以与发射系统一起使用，其可以进一步包括由至少一个管形成的发射管，其可以是导电的并且可以与至少一个绝缘管组合。 可以提供诸如电池组和相关电感器的电能源。