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1. 发明授权

US3985058A Self-sealing fluidic explosive initiator 失效
标题翻译：自密封流体爆炸物引发剂
公开(公告)号：US3985058A
公开(公告)日：1976-10-12
申请号：US603210
申请日：1975-08-08
申请人： Anthony P. Corrado , Frank Timte , Edward L. Rakowsky , Vincent P. Marchese , Charles W. Bing
发明人： Anthony P. Corrado , Frank Timte , Edward L. Rakowsky , Vincent P. Marchese , Charles W. Bing
IPC分类号： F42C15/29 , F42C5/00
CPC分类号： F42C15/29
摘要： A self-sealing fluidic explosive initiator utilizes a tapered sliding innerleeve, having a nozzle element, resonance tube and an explosive charge proximately disposed adjacent the resonance tube, to mate with a fitting sleeve for terminating a gas supply flow to the nozzle, and for containing the products of explosion of the initiator upon activation of the explosive charge. The initiation of the explosive charge is used to move a piston cutter valve.
摘要翻译：自密封流体爆炸引发器利用锥形滑动内套筒，其具有喷嘴元件，共振管和邻近谐振管附近的爆炸装置，与装配套管配合以终止到喷嘴的气体供应流，并且在爆炸炸药活化后，含有引发剂爆炸的产物。爆炸装药的启动用于移动活塞切割阀。

2. 发明授权

US3994232A Pneumatic match through use of a conical nozzle flare 失效
标题翻译：通过使用锥形喷嘴的气流匹配耀斑
公开(公告)号：US3994232A
公开(公告)日：1976-11-30
申请号：US606816
申请日：1975-08-22
申请人： Edward L. Rakowsky , Vincent P. Marchese , Robert H. Page , Anthony P. Corrado
发明人： Edward L. Rakowsky , Vincent P. Marchese , Robert H. Page , Anthony P. Corrado
IPC分类号： F42C15/29 , F42C5/00
CPC分类号： F42C15/29 , F05D2260/99
摘要： An improved pneumatic match utilizes a vented conically shaped nozzle flareositioned in a downstream region of a convergent nozzle to permit the match to be used in applications where fast functioning time is a necessity and where the fluid activating medium comprises a low helium pressure source or only high pressure air.
摘要翻译：改进的气动匹配利用位于会聚喷嘴的下游区域中的通风锥形喷嘴火炬，以允许该匹配用于需要快速运行时间的应用中，并且其中流体激活介质包括低氦压力源高压空气

3. 发明授权

US3994226A Flueric explosive initiation device for a fuel-air explosive bomb 失效
标题翻译：用于燃油炸弹的易燃爆炸装置
公开(公告)号：US3994226A
公开(公告)日：1976-11-30
申请号：US642086
申请日：1975-12-18
申请人： Edward L. Rakowsky , Vincent P. Marchese , Anthony P. Corrado
发明人： Edward L. Rakowsky , Vincent P. Marchese , Anthony P. Corrado
IPC分类号： F42C15/29 , F42B25/16 , F42C5/00
CPC分类号： F42C15/29 , F05D2260/99
摘要： A flueric initiator for a fuel-air explosive bomb possesses a sealed hous containing a pressurized gas, a plurality of igniter devices and a means for rupturing the housing and ejecting the igniter devices into the atmosphere. Each igniter device consists of a small gas container, a resonance tube, and explosive charge adjacent to the closed end of the resonance tube, and a nozzle connected to the gas container and communicating with the housing plenum through one or more vents. The housing is initially charged to a pressure considerably higher than the functioning pressure of the nozzle-resonance tube combination.When the sealed housing is ruptured and the igniter devices are ejected after bomb impact and fuel dispersal, the pressure outside the igniter devices is reduced to ambient pressure, causing the pressurized gas in the gas container to flow out through said nozzle and impinge upon the open end of the resonance tube, thereby reducing the gas pressure until it reaches the level at which resonance tube heating occurs. This rapid heating takes place only after a well-defined, predetermined, settable time delay, detonating the explosive charge and consequently the fuel-air cloud.
摘要翻译：用于燃料 - 空气爆炸炸弹的轻油起动器具有包含加压气体的密封壳体，多个点火装置和用于破裂壳体并将点火装置喷射到大气中的装置。每个点火器装置包括一个小的气体容器，一个共振管和与该共振管的封闭端相邻的爆炸装置，一个连接到气体容器并通过一个或多个通风口与壳体通风室连通的喷嘴。初始将壳体充电至显着高于喷嘴共振管组合的功能压力的压力。

4. 发明授权

US3982488A Flueric through bulkhead rocket motor ignitor 失效
标题翻译：通过舱壁火箭发动机点火器
公开(公告)号：US3982488A
公开(公告)日：1976-09-28
申请号：US551434
申请日：1975-02-19
申请人： Edward L. Rakowsky , Vincent P. Marchese
发明人： Edward L. Rakowsky , Vincent P. Marchese
IPC分类号： F02K9/95 , F42C15/29 , F42C5/00
CPC分类号： F02K9/95 , F42C15/29 , F05D2260/99
摘要： A flueric through bulkhead rocket motor ignitor in which a flueric thermalnergy generator is used to set off a pyrotechnic/explosive pickup charge that in turn sets off a donor pyrotechnic/explosive charge that transmits its energy through a thick metallic bulkhead that is utilized to maintain pressure integrity of a rocket motor, and the donor charge transmits its energy to a pyrotechnic/explosive pickup charge that in turn sets off a receptor charge that is utilized to ignite a solid propellant composition.
摘要翻译：一个通过舱壁火箭发动机的轻型火箭发动机，其中使用微波热能发电机来摧毁烟火/爆炸物拾取装置，从而引爆一个供体烟火/炸药，其能量通过用于维持的厚的金属隔板传递火箭发动机的压力完整性，并且供体电荷将其能量传递到烟火/爆炸性拾取装置，其依次降低用于点燃固体推进剂组合物的受体电荷。

5. 发明授权

US4240257A Heat pipe turbo generator 失效
标题翻译：热管涡轮发电机
公开(公告)号：US4240257A
公开(公告)日：1980-12-23
申请号：US334901
申请日：1973-02-22
申请人： Edward L. Rakowsky , Lawrence S. Galowin
发明人： Edward L. Rakowsky , Lawrence S. Galowin
IPC分类号： F01K9/02 , F01K11/02 , F28D15/04
CPC分类号： F01K9/026 , F01K11/02 , F28D15/04 , F28F2200/005
摘要： The adaptation of a heat pipe as a turbo-generator or other power output device for a reliable, quiet, light-weight high-endurance power source is shown. The device requires input thermal energy from a burner radioisotope (or solar heat) and also forced or natural heat rejection from condenser surfaces. Thermal energy conversion to a suitable power output is accomplished by encapsulating a turbine wheel within a heat pipe shell, located in an appropriately geometrical contoured section. Flow work extracted from the kinetic energy of the vapor flow provides rotary shaft power output. The shaft power can drive an electrical generator, pump, compressor, or similar device, also mounted within the heat pipe shell structure. A completely self-contained enclosed unit is provided which requires only external power connection at attachment terminals.
摘要翻译：示出了作为涡轮发电机或其他功率输出装置的热管的适应性，用于可靠，安静，重量轻的高耐久性电源。该设备需要来自燃烧器放射性同位素（或太阳能热）的输入热能，并且还需要来自冷凝器表面的强制或自然的排热。将热能转换成合适的功率输出是通过将涡轮机叶片封装在位于适当几何轮廓部分的热管壳体内来实现的。从蒸汽流的动能中提取的流动提供旋转轴功率输出。轴功率可以驱动也安装在热管壳结构内的发电机，泵，压缩机或类似装置。提供完全独立封闭的单元，仅在连接端子处需要外部电源连接。

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