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    • 1. 发明授权
    • Externally accessible thermal ground plane for tactical missiles
    • 用于战术导弹的外部热地面
    • US06578491B2
    • 2003-06-17
    • US09950893
    • 2001-09-10
    • Bruce R. Babin
    • Bruce R. Babin
    • F42B1200
    • F42B15/34F28D15/02
    • A tactical missile includes a heat pipe connecting heat sources with heat sinks within the missile. The system includes a removable external heat dissipation device that connects to the heat pipe while the missile is being tested or reprogrammed. The external heat dissipation device draws heat out of the heat pipe and so maintains the electronic components acceptably cool during extended testing or reprogramming. During the relatively short tactical flight, the heat pipe transfers heat from the electronic components to the heat sinks within the missile. The high heat transfer rate of the heat pipe enables elements such as structural members and propellant to be used as heat sinks, elements not heretofore incorporated into thermal management of the heat generating electronic components.
    • 战术导弹包括将热源与导弹内的散热片连接的热管。 该系统包括可拆卸的外部散热装置,其在导弹被测试或重新编程时连接到热管。 外部散热装置将热量从热管中吸出,从而在延长的测试或重新编程期间保持电子部件可接受的冷却。 在相对较短的战术飞行中,热管将热量从电子部件传递到导弹内的散热片。 热管的高传热速率使得诸如结构构件和推进剂的元件可以用作散热器,这些元件迄今未被并入发热电子部件的热管理中。
    • 3. 发明授权
    • Smooth bore barrel system with self spinning ammunition
    • 具有自旋弹药的平滑钻孔系统
    • US06679178B2
    • 2004-01-20
    • US10023260
    • 2001-12-15
    • Gueorgui M. MihaylovEvdokia K. Mihaylova
    • Gueorgui M. MihaylovEvdokia K. Mihaylova
    • F42B1200
    • F42B14/04F42B10/24
    • A smooth bore barrel system utilizes an ammunition round capable to provide the projectile, covered with predetermined usually spiral grooves (44) and lands (42) congruently engaged in the rifled by the same manner inner surface (30A) of the cartridge case (30). When fired the rifled cartridge case serves as a short disposable rifled barrel spinning the projectile. A front short non-rifled part (40B) of the cylindrical portion of the projectile is extended into the smooth bore barrel (20) having sliding fit within. Alternatively, spinning momentum is provided by having the grooves tapering to narrow channels extended through the short cylindrical portion of the projectile forming jets (48), which rotate the projectile by jet propulsion forces. Spinning momentum is gained by two independent approaches which effect could be combined or used separately.
    • 光滑的钻孔系统利用能够提供射弹的弹药圆,覆盖有预定的通常为螺旋槽(44)和平滑地接合在与盒壳体(30)的内​​表面(30A)相同的方向上的平台(42) 。 当发射时,步枪弹药筒作为一个短的一次性膛枪旋转射弹。 抛射体的圆柱形部分的前部短的非膛部分(40B)延伸到具有滑动配合的平滑孔筒(20)内。 或者,通过使凹槽逐渐缩小以延伸穿过射弹形成喷嘴(48)的短圆柱形部分的狭槽,从而通过射流推进力旋转射弹来提供旋转​​动量。 通过两种独立方法获得旋转动量,这些方法的效果可以单独组合或使用。
    • 9. 发明授权
    • Radiative countermeasures method
    • 辐射对策方法
    • US06352031B1
    • 2002-03-05
    • US05281815
    • 1972-08-18
    • Philip L. Barbaccia
    • Philip L. Barbaccia
    • F42B1200
    • H01Q15/145F41H11/02H01Q17/00
    • A method for creating coherent masses of burning matter for countermeasures purposes such as for protecting an aircraft and other vehicles from infrared “heat seeking” hostile missiles and also from high power Laser beams and Laser radar. One or more spurious sources of radiation are created controllably in the general vicinity of the aircraft being protected; in missile countermeasures, each of these spurious sources is capable of emitting infrared energy comparable in wave length and at a higher intensity than that emitted by the target aircraft itself such that the hostile missile will be decoyed away from its intended target by the spurious radiation sources. In this method, the spurious source of radiation is created by igniting a small amount of aircraft fuel that is gelled and controllably ejected from the aircraft. Protection against Laser weapons and radar is provided by interposing the burning mass of matter in the Laser beam so that combusion products in the burning mass serve to degrade beam power. Apparatus for practicing the method is disclosed comprising means for withdrawing a small quantity of fuel from the aircraft fuel tank, means for adding a gelling agent to the quantity of fuel, and means for simultaneously igniting and ejecting the quantity of gelled fuel such that a persistent source of radiant energy that can be used for decoy purposes and attenuating Laser beams is produced.
    • 一种用于制造相关质量的燃烧物质的方法,用于对策,例如用于保护飞机和其他车辆免受红外“寻热”敌对导弹以及大功率激光束和激光雷达的影响。 在被保护的飞机的一般附近可控制地产生一个或多个虚假的辐射源; 在导弹对策中,这些杂散源中的每一个都能够发射波长长度相当的红外能量,并且具有比目标飞机本身发射的强度更高的强度,使得敌对导弹将被杂散辐射源从其预期目标中解脱出来 。 在这种方法中,通过点燃从飞机凝胶化并可控地弹出的少量飞行器燃料来产生辐射源。 激光武器和雷达的保护是通过将激光质量物质置于激光束中来提供的,从而使燃烧物质中的混合物质能够降低光束功率。 公开了一种用于实施该方法的装置,包括用于从飞机燃料箱中取出少量燃料的装置,用于向燃料量添加胶凝剂的装置,以及用于同时点燃和喷射凝胶燃料量的装置, 产生可用于诱饵目的和衰减激光束的辐射能源。