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公开(公告)号:US5505053A
公开(公告)日:1996-04-09
申请号:US351834
申请日:1994-12-08
申请人: Peter Luger , Franz Grafwallner , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Alexsander S. Shengardt
发明人: Peter Luger , Franz Grafwallner , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Alexsander S. Shengardt
CPC分类号: F17C13/123 , B60K15/013 , F17C2201/0109 , F17C2201/035 , F17C2205/0341 , F17C2221/011 , F17C2221/012 , F17C2221/014 , F17C2221/033 , F17C2223/0161 , F17C2227/0135 , F17C2227/0178 , F17C2265/012 , F17C2270/0189 , Y02E60/321 , Y10S220/901
摘要: Cryosystem for cryogenic liquids which contain small amounts of foreign fluids with higher melting and boiling points, wherein the cryosystem comprises at least one tank, pipelines and assembly units and is used under defined gravitation conditions. The pipelines slope, at least in some areas, toward the tank, and areas of the pipelines and assembly units, from which the cryogenic liquid and the foreign fluids cannot flow back into the tank under the action of gravity, are provided with drain openings and drain lines, which open into the tank or into at least one additional collection tank.
摘要翻译: 含有少量具有较高熔点和沸点的外来流体的低温液体的冷冻系统,其中该冷冻系统包括至少一个罐,管道和组装单元,并且在确定的重力条件下使用。 管道至少在某些区域朝向油罐,以及管道和组装单元的区域,其中低温液体和外来流体在重力作用下不能从该液体和外来流体返回到罐中,排放开口和 排放管线,其通向罐中或至少一个附加的收集罐。
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公开(公告)号:US5833172A
公开(公告)日:1998-11-10
申请号:US749736
申请日:1996-11-15
申请人: Franz Grafwallner , Peter Luger , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Sergei B. Galperin , Andrew E. Kovalev , Alexsander S. Shengardt
发明人: Franz Grafwallner , Peter Luger , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Sergei B. Galperin , Andrew E. Kovalev , Alexsander S. Shengardt
摘要: An arrangement of outlet devices for releasing into the atmosphere cryogenic, combustible exhaust vapors in the near-surface, flow-swept, outer area of aircraft, land vehicles and watercraft. The arrangement provides at least one outlet device on the top side of a component at the top end of a pylon, which is favorable in terms of flow, in the free, undisturbed air flow. Each outlet device is arranged, designed and oriented such that the exhaust vapor is released in at least one directed jet oriented to the rear or to the rear and upward, with or without a lateral component, and is kept away from air inlets, hot exhaust gas jets and other sources of ignition, as well as from surfaces of components.
摘要翻译: 用于释放到大气中的出口装置的布置用于飞机,陆地车辆和船只的近表面,流动扫掠的外部区域中的低温,可燃排气蒸气。 该装置在塔的顶端部分的顶部的顶侧提供至少一个出口装置,其在流动方面是有利的,在自由的,未受干扰的空气流中。 每个出口装置被布置,设计和定向,使得排气蒸气以至少一个定向到后部或后部和向上的定向喷射器被释放,具有或不具有侧向部件,并且远离空气入口,热排气 气体喷射和其他火源,以及部件表面。
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公开(公告)号:US5660358A
公开(公告)日:1997-08-26
申请号:US395677
申请日:1995-02-28
申请人: Franz Grafwallner , Peter Luger , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Sergei B. Galperin , Igor V. Golov
发明人: Franz Grafwallner , Peter Luger , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Sergei B. Galperin , Igor V. Golov
CPC分类号: B64D37/14 , Y02T90/44 , Y10T137/86035 , Y10T137/86131 , Y10T137/86196
摘要: Fuel supply system for multijet airplanes using cryogenic fuel with one tank or one tank group for each engine or for all engines on one side of the longitudinal central plane of the airplane, and, if desired, with an additional, common tank or an additional, common tank group for all engines. A transfer line with shut-off valve leads from each tank/tank group associated with a defined engine or with the engines of one side of the airplane to at least one other tank/tank group and/or, if desired, to the tank/tank group common to all engines. If desired, at least one transfer line leads from the common tank/tank group to at least one other tank/tank group.
摘要翻译: 用于使用低温燃料的多喷气机的燃料供应系统,每个发动机具有一个罐或一个罐组,或者用于在飞机的纵向中心平面的一侧上的所有发动机,并且如果需要,使用附加的公共罐或附加的, 所有发动机的普通坦克组。 具有截止阀的传输线从与定义的发动机相关联的每个罐/罐组引导,或与飞机的一侧的发动机连接至至少另一个罐/罐组,和/或如果需要, 坦克组通用于所有发动机。 如果需要,至少一条输送管线从公共罐/罐组引导到至少另一个罐/罐组。
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公开(公告)号:US5548962A
公开(公告)日:1996-08-27
申请号:US396686
申请日:1995-03-01
申请人: Peter Luger , Franz Grafwalliner , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Viacheslav P. Logviniouk , Vladmimir S. Ozeretskovsky , Alexander S. Shengardt
发明人: Peter Luger , Franz Grafwalliner , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Viacheslav P. Logviniouk , Vladmimir S. Ozeretskovsky , Alexander S. Shengardt
CPC分类号: F17C9/00 , F17C6/00 , F17C2205/0157 , F17C2205/0341 , F17C2221/012 , F17C2221/033 , F17C2223/0161 , F17C2225/0161 , F17C2227/0337 , F17C2260/031 , F17C2265/065 , F17C2270/0189 , Y02E60/321 , Y10S62/908
摘要: A refueling process for cryogenic liquids, in which the cryogenic liquid in question is transferred from a storage tank into a receiving tank via a detachable line connection. Before or during the refueling process, the cryogenic liquid is cooled in the storage tank to a temperature that is below the lowest operating temperature intended in the tank and above the freezing point of the liquid. The cryogenic liquid is transferred into the tank through a filter with a fineness of 5 to 40 .mu.m, and its temperature is increased during the transfer to a value that at least approximately corresponds to the intended operating temperature in the receiving tank.
摘要翻译: 低温液体的加油工艺,其中所讨论的低温液体通过可拆卸的线路连接从储罐转移到接收罐中。 在加油过程之前或过程中,低温液体在储罐中被冷却至低于罐中最低工作温度并高于液体凝固点的温度。 低温液体通过细度为5至40微米的过滤器转移到罐中,并且在转移期间其温度升高至至少大约对应于接收罐中的预期操作温度的值。
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公开(公告)号:US5548961A
公开(公告)日:1996-08-27
申请号:US351835
申请日:1994-12-08
申请人: Peter Luger , Franz Grafwallner , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Sergey B. Galperin , Viacheslav P. Logviniouk
发明人: Peter Luger , Franz Grafwallner , Helmuth Peller , Martin Muller , Valentin V. Malyshev , Sergey B. Galperin , Viacheslav P. Logviniouk
IPC分类号: F17C13/00 , B60K15/03 , B60K15/077 , B64D37/02 , B64D37/20 , F17C13/02 , F17C13/12 , F17C5/02
CPC分类号: B60K15/077 , B60K15/03006 , B64D37/02 , F17C13/025 , F17C13/123 , F17C2205/0332 , F17C2205/0391 , F17C2221/012 , F17C2221/033 , F17C2223/0161 , F17C2223/033 , F17C2223/041 , F17C2227/0135 , F17C2227/0178 , F17C2227/0386 , F17C2260/027 , F17C2265/02 , F17C2270/0189 , Y02E60/321 , Y02T90/44
摘要: Process for the temperature stratification-free storage of a cryogenic liquid in a thermally insulated tank under gravitation conditions or under gravitation and movement conditions, which generate a liquid volume with a clearly limited, unmoving or only moderately moving liquid level as well as with a gas space located above it in the storage volume of the tank. Liquid is pumped off from the area near the bottom of the tank continuously or at time intervals, it is fed into the area of the gas space, and it is directed vertically or at an acute angle toward the liquid level there in the form of at least one high-energy jet.
摘要翻译: 用于在重力条件下或在重力和运动条件下在绝热罐中温度分层地存储低温液体的方法,其产生具有明显有限的,不流动的或仅适度移动的液面以及气体的液体体积 位于其上方的空间在储罐的存储容积中。 液体从罐底部附近的区域被连续地或间隔地从泵送到气体空间的区域中,并且以垂直方向或以锐角方向朝向液面的方向以 至少一台高能喷气机。
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公开(公告)号:US4708065A
公开(公告)日:1987-11-24
申请号:US709507
申请日:1985-03-08
CPC分类号: F42B8/12
摘要: A spin-stabilized training projectile provides a reliable reduction of a firing range by means of the special construction of a recess in the body of the projectile. The flight path of the training projectile is adaptable to the corresponding flight path of a corresponding live reference projectile over a distance in a predetermined region of the first portion of the flight path of the training projectile.
摘要翻译: 旋转稳定的训练射弹通过在射弹身体中的凹陷的特殊构造可靠地减少射击范围。 训练射弹的飞行路径适应于在训练射弹的飞行路径的第一部分的预定区域中相应的实时参考射弹的相应飞行路径。
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