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    APPARATUS FOR COMBUSTING A FUEL AT HIGH PRESSURE AND HIGH TEMPERATURE, AND ASSOCIATED SYSTEM
    4.
    发明申请
    APPARATUS FOR COMBUSTING A FUEL AT HIGH PRESSURE AND HIGH TEMPERATURE, AND ASSOCIATED SYSTEM 审中-公开
    用于燃烧高压和高温燃料的装置及相关系统

    公开(公告)号：US20150198331A1

    公开(公告)日：2015-07-16

    申请号：US14638656

    申请日：2015-03-04

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

    发明人： Miles R. Palmer ,  Rodney John Allam ,  Glenn William Brown, JR. ,  Jeremy Eron Fetvedt

    IPC分类号： F23L7/00 ,  F02C3/26 ,  F23L9/00 ,  F23D1/00 ,  F23C5/32 ,  F23C7/08

    CPC分类号： F23L7/007 ,  F02C3/26 ,  F23C5/32 ,  F23C7/08 ,  F23C2900/03004 ,  F23D1/005 ,  F23J15/027 ,  F23L7/00 ,  F23L9/00 ,  F23L2900/07002 ,  F23M5/085 ,  F23M2900/05004 ,  Y02E20/322 ,  Y02E20/344

    摘要： A combustor apparatus is provided, comprising a mixing arrangement for mixing a carbonaceous fuel with enriched oxygen and a working fluid to form a fuel mixture. A combustion chamber is at least partially defined by a porous perimetric transpiration member, at least partially surrounded by a pressure containment member. The combustion chamber has longitudinally spaced apart inlet and outlet portions. The fuel mixture is received by the inlet portion for combustion within the combustion chamber at a combustion temperature to form a combustion product. The combustion chamber directs the combustion product longitudinally toward the outlet portion. The transpiration member is configured to substantially uniformly direct a transpiration substance therethrough toward the combustion chamber, such that the transpiration substance is directed to flow helically about the perimeter and longitudinally between the inlet and outlet portions, for buffering interaction between the combustion product and the transpiration member. Associated systems are also provided.

    摘要翻译： 提供了一种燃烧器装置，其包括用于混合含碳燃料和富氧的混合装置和工作流体以形成燃料混合物。 燃烧室至少部分地由多孔周边蒸腾构件限定，至少部分地被压力容纳构件包围。 燃烧室具有纵向间隔开的入口和出口部分。 燃料混合物被入口部分接收以在燃烧室内在燃烧温度下燃烧以形成燃烧产物。 燃烧室将燃烧产物纵向引导到出口部分。 蒸腾构件构造成基本均匀地将蒸腾物质引导通过其朝向燃烧室，使得蒸腾物质被引导以围绕周边螺旋地流动并且在入口部分和出口部分之间纵向流动，以缓冲燃烧产物和蒸腾作用之间的相互作用 会员。 还提供了相关系统。

    LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF
    5.
    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。