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Final design and commissioning test results for the hypervelocity launcher research complex battery power supply

机译:超级型启动器研究复杂电池供电的最终设计和调试测试结果

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The preliminary design of the battery power supply (BPS) was reported to the 6th IEEE Pulsed Power Conference [1]. In 1987, the final design was completed, assembled, and sequentially verified during approximately 1750 operational verification tests. These experiments consisted of single-string verifications at 1000 amperes to a system discharge of 21,500,000 amperes. Final system design is very similar to the preliminary design previously presented. System fabrication is complete and at the present time consists of 858, 16-battery series strings resulting in 13,728 operational batteries. The final switching design has evolved into several levels of redundancy at varying current levels. These include 36 pneumatic, 100,000 ampere switches that control 24, 16-battery strings in parallel. These switches are used for the primary make and break of system current to charge the inductor. There are also 18 pneumatic crowbar switches at the 24-string level that are used to short the inductor from the BPS prior to system opening. At the string level there are 2000 ampere DC conductors that are used as a secondary current break and to pre-set the BPS in the appropriate parallel/series configuration prior to a discharge sequence. Explosively driven opening and closing switches are also employed at the interface junction to any hypervelocity launcher test article. These switches allow the inductor to charge prior to hypervelocity firings, are then opened for the event, and then explosively closed again to allow the inductively stored energy remaining to be dissipated in the busswork and pneumatic crowbar circuits. Detailed descriptions and operations of these switching sequences are discussed further in the switching section along with descriptions and operational data of the final hardware tested. Control system philosophy, capability, and operation during the commissioning tests are also discussed in detail. A BPS system artist's conception drawing is shown as the facility has been built, in Figure 1.
机译:将电池电源(BPS)的初步设计报告给第六IEEE脉冲功率会议[1]。 1987年,在大约1750个操作验证测试期间完成了最终设计,组装和顺序验证。这些实验包括单弦验证,在1000台上,系统排放为21,500,000安培。最终的系统设计与先前呈现的初步设计非常相似。系统制造完整,目前由858,16电池系列串组成,导致13,728个操作电池。最终的开关设计在不同电流水平下演变成几个冗余。这些包括36个气动,100,000安培的开关,该开关并联控制24,16电池串。这些开关用于系统电流的主要制作和断裂,以对电感充电。在24弦级别,还有18个气动撬棍开关,用于在系统打开之前从BPS短路。在字符串级别,有2000个安培的直流导线用作次级电流中断,并在放电序列之前将BPS预先设置为适当的并行/串联配置。爆炸性的打开和关闭开关也用于接口连接到任何超高速发射器测试制品。这些开关允许电感器在超细燃烧之前充电,然后为事件打开,然后再次爆炸地关闭以允许电感存储的能量留在总线上和气动撬棍电路中散发。这些交换序列的详细描述和操作在切换部分中进一步讨论以及所测试的最终硬件的描述和操作数据。还详细讨论了控制系统哲学,能力和调试测试期间的操作。 BPS系统艺术家的概念绘图如图1所构建的设施所示。

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