FUEL PROCESSING SYSTEM AND RELATED METHODS
    3.
    发明申请
    FUEL PROCESSING SYSTEM AND RELATED METHODS 有权
    燃料加工系统及相关方法

    公开(公告)号:US20120272567A1

    公开(公告)日:2012-11-01

    申请号:US13094709

    申请日:2011-04-26

    CPC classification number: C10K1/004 B01J2219/00006 C10K3/04

    Abstract: A fuel processing system for converting a logistical fuel and air into a liquid product comprising methanol. One such system comprises a fuel injection system configured to combine a logistical fuel and ambient air to produce a logistical fuel and air mixture, a synthesis gas production system configured to convert the logistical fuel and air mixture to synthesis gas, and a methanol synthesis system configured to convert the synthesis gas to a crude methanol liquid. Related methods are additionally disclosed.

    Abstract translation: 一种用于将物流燃料和空气转化成包含甲醇的液体产物的燃料处理系统。 一种这样的系统包括燃料喷射系统,该燃料喷射系统被配置为组合后勤燃料和环境空气以产生后勤燃料和空气混合物,构造成将后勤燃料和空气混合物转化为合成气的合成气生产系统,以及配置 将合成气转化为粗甲醇液体。 另外公开了相关方法。

    Projectile structure
    9.
    发明授权
    Projectile structure 有权
    射弹结构

    公开(公告)号:US07051659B2

    公开(公告)日:2006-05-30

    申请号:US10164718

    申请日:2002-06-10

    Abstract: A scramjet has a cowl, a center structure, and a plurality of wide pylons connecting the cowl to the center structure, with scramjet engines positioned between adjacent pylons. Leading surfaces of adjacent pylons converge to one another to provide side wall compression to air entering the engines. The center structure includes a fore body, a center body and an aft body that, with the pylons, define a basic structure either formed entirely from one piece or several securely connected pieces. A method of testing the scramjet projectile comprises using a gun to accelerate the scramjet projectile to the takeover velocity of the engines.

    Abstract translation: 冲击式喷气发动机具有整流罩,中心结构和连接整流罩到中心结构的多个宽塔架,其中冲击式发动机位于相邻的塔架之间。 相邻塔架的主导面相互收敛,为进入发动机的空气提供侧壁压缩。 中心结构包括前体,中心体和后体,其中塔架限定了完全由一个或多个牢固连接的部件形成的基本结构。 一种测试冲击射弹的方法包括使用枪将加速喷射射弹加速到发动机的收取速度。

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