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    • 15. 发明授权
    • Floating fitting cable attachment
    • 浮动接头电缆附件
    • US4890536A
    • 1990-01-02
    • US202656
    • 1988-05-27
    • Brian A. Floyd
    • Brian A. Floyd
    • F41F3/073
    • F41F3/073
    • Missile support cables are passed through cable fitter support blocks, which are ridgidly affixed to the silo, and are swaged to heavy blocks resting upon the support blocks via a canister having ductile mesh therein. Upon a downblast, the cables are maintained in tension due to the low downward acceleration of the heavy blocks, while the support blocks are rapidly downwardly accelerated and upon rebound, smash into the energy absorbing canister which prevents the failure of the cables by controlling excess tension therein.
    • 导弹支撑电缆通过电缆钳工支撑块,它们被固定在筒仓上,并通过其中具有延性网的罐而被模锻到搁置在支撑块上的重块。 在下降时,由于重块的低向下加速度,电缆被保持在张力中,同时支撑块快速向下加速并且在回弹时,通过控制过大的张力而粉碎到能量吸收罐中,从而防止电缆的故障 其中。
    • 16. 发明授权
    • Gas strut separation for staged rocket
    • 气体支柱分离用于分段火箭
    • US08091481B1
    • 2012-01-10
    • US12434388
    • 2009-05-01
    • Brian A. Floyd
    • Brian A. Floyd
    • F42B15/10
    • F42B15/36
    • A staged rocket apparatus includes first and second stages connected by a releasable connector. A plurality of pressurized gas struts are connected between the first and second stages and provide a separating force urging the first and second stages apart. The gas struts are held in a telescopingly collapsed first position by the releasable connector. The separating force is maintained at a minimum value so long as the releasable connector holds the struts in their first position. When the releasable connector is disconnected the separating force increases due to gas flow through a metering passage having a progressively increasing flow area from a high pressure chamber to a low pressure chamber.
    • 分段火箭装置包括通过可释放连接器连接的第一和第二阶段。 多个加压气体支柱连接在第一和第二平台之间,并提供分开力,以使第一和第二平台分开。 气体支柱通过可释放的连接器保持在可伸缩的第一位置。 分离力保持在最小值,只要可释放连接器将支柱固定在其第一位置即可。 当可释放连接器断开时,分离力由于气流通过具有从高压室到低压室逐渐增加的流动面积的计量通道而增加。
    • 19. 发明授权
    • Case burning rocket
    • 案例燃火箭
    • US07210282B1
    • 2007-05-01
    • US10916352
    • 2004-08-11
    • Brian A. Floyd
    • Brian A. Floyd
    • F02K9/32
    • F02K9/72F02K9/28F02K9/34F02K9/343
    • A case-burning rocket booster includes a combustible case containing a solid rocket fuel, a combustion chamber adjustably coupled to the case for burning the case and the solid rocket fuel, a nozzle connected to the combustion chamber for expelling the burned case and fuel to generate thrust, and a drive system for pulling the combustion chamber and nozzle up the case as the case and fuel burn. A hybrid version of the case-burning rocket also includes an oxidizer supply system for supplying varying amounts of oxidizer to the combustion chamber to vary the thrust generated by burning the case and the fuel.
    • 一种燃烧式火箭助推器包括一个包含固体火箭燃料的可燃壳体,一个可调节地联接到壳体上用于燃烧壳体和固体火箭燃料的燃烧室,连接到燃烧室的喷嘴,用于排出燃烧的壳体和燃料以产生 推力和驱动系统,用于拉动燃烧室并在壳体和燃料燃烧时将喷嘴向上喷出。 壳体燃烧火箭的混合版本还包括用于向燃烧室供应不同量的氧化剂的氧化剂供应系统,以改变由燃烧壳体和燃料产生的推力。