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    • 5. 发明专利
    • High-speed missile destructing device
    • 高速故障破坏设备
    • JP2010117059A
    • 2010-05-27
    • JP2008289403
    • 2008-11-12
    • Toshihisa Shirakawa白川 利久
    • SHIRAKAWA TOSHIHISA
    • F41H13/00F42B3/00F42B10/30F42B12/02F42B15/00F42B19/00G21J3/00
    • PROBLEM TO BE SOLVED: To provide a device for destructing a high-altitude high-speed missile such as a huge meteorite by generating small nuclear explosion by small fissile substance amount. SOLUTION: By opening/closing through the remote control of a valve 268 attached in the middle of a propulsion gas pipe 69, propulsion gas 65 is emitted from a nozzle 71 fixed to the outer face of each of a storage container 3 and an auxiliary tank 60 to the external world to wait a high-speed missile in its advancing direction. By injecting an excessive moderator nuclear fuel solution 61 into the air gap of excessively small solid moderator-mixed gadolinium addition nuclear fuel rod lattice 50 with a pump 63, a moderator ratio is optimized and kinf is maximized. When the kinf becomes maximum, neutron is generated to cause nuclear explosion. COPYRIGHT: (C)2010,JPO&INPIT
    • 要解决的问题:提供一种用于通过以小的易裂变物质量产生小型核爆炸来破坏诸如巨大陨石的高空高速导弹的装置。 解决方案:通过安装在推进气管69中间的阀门268的遥控器打开/关闭,推进气体65从固定在每个储存容器3的外表面上的喷嘴71发出, 向外部世界等待高速导弹前进方向的辅助水箱60。 通过将过量的缓和剂核燃料溶液61注入到具有泵63的过小的固体慢化剂混合的钆添加核燃料棒格50的气隙中,调节剂比率被优化并且kinf最大化。 当kinf变得最大时,产生中子以引起核爆炸。 版权所有(C)2010,JPO&INPIT
    • 9. 发明专利
    • Energy generation
    • GB2546276B
    • 2021-04-28
    • GB201600585
    • 2016-01-12
    • FRANK WOODBINE
    • FRANK WOODBINE
    • F22B3/06F22B3/00F42B1/02F42B1/032G21J3/00
    • The present invention provides an apparatus for generating energy suitable for use in an electrical power station. The apparatus comprises a quench chamber, the chamber quench chamber containing a quench fluid, the quench chamber having a fuel inlet and an outlet in fluid communication with at least one turbine of the power station, a target located within the quench chamber, and a propulsion means operable to propel a projectile towards the target. The projectile comprises a shaped charge comprising a charge liner having a front portion and a rear portion, an explosive material located adjacent to at least the rear portion of the charge liner and a detonator operable to detonate the explosive material. In use, the propulsion means propels the projectile through the fuel inlet towards the target and, before the projectile reaches the target, the detonator detonates the explosive material generating a jet of particles which impacts the target, thereby releasing energy, which heats the quench fluid causing a gas to be released through the outlet, which gas then drives the at least one turbine.
    • 10. 发明专利
    • СПОСОБ СИРОТЫ ОСУЩЕСТВЛЕНИЯ ВЗРЫВНОЙ РЕАКЦИИ, В ТОМ ЧИСЛЕ ЯДЕРНОЙ ИЛИ ТЕРМОЯДЕРНОЙ
    • RU2014123449A
    • 2015-12-20
    • RU2014123449
    • 2014-06-10
    • G21J3/00
    • 1. Способосуществлениявзрывнойреакции, втомчислеядернойилитермоядерной, путемпериодическогоподрывавзрывногоустройствав массиверасплаваметаллаилимассивенагретогопараводы, размещенноговнутрипрочногокорпуса, черезкоторыйосуществляютотбортеплоты, аккумулированнойв указанныхмассивахрасплаваметаллаилинагретогопараводы, приэтомвзрывноеустройствоподаютв указанныемассивычерезканалс затворнымустройством, открываемымприпроходевзрывногоустройствавнутрьмассиваи закрываемымпослеэтогопрохода, нодонаступлениямоментавзрывавзрывногоустройства, отличающийсятем, чтов массиврасплававыстреливаютвзрывноеустройствов видеснаряда.2. Способпоп. 1, отличающийсятем, чтомассиврасплававыполняютизстеклаилистеклоподобногоматериала.