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The MARK V 32 MW Self Excited Rocket Driven MHD Generator

机译:Mark V 32 MW自兴奋火箭驱动MHD发电机

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The Mark V self excited rocket engine driven MHD generator (RMHD) program was initiated at the Avco Everett Research Laboratory (AERL) in 1962 to demonstrate a solution for the then perceived need for a simple, low cost source of extremely high power for limited duty cycle applications. At the time the Mark V program was initiated, the maximum power which had been achieved by an MHD generator was several hundred kilowatts for a few seconds. The Mark V was the first MHD generator to achieve more than 1.5 W output, the first to be self excited, the first to deal with engineering a high power water cooled MHD channel with literally thousands of electrically isolated elements, and the first to experience the potentially catastrophic consequences of improper management of the electric fields and interelectrode potentials in a high power MHD generator. The program objectives and specifications and design of the overall experiment, fluid mechanics of the MHD interaction, the heat sink self excited magnet, combustion chamber, water cooled MHD channels, load bank and initial checkout are outlined. Two channels were employed. The first channel included an upstream continuous electrode Faraday (CEF) section for magnet excitation followed by a segmented electrode Faraday (SEF) section for net power output. The second channel was CEF design with the load switched in series with the magnet following excitation. Both channels were water cooled. Fifty six power generation runs were carried out with the first channel, and twelve with the second CEF channel. The Paper focuses on the first channel. Initial effort with the first channel focused on self excitation which was readily achieved, but not without some breakdown issues. Effort then concentrated on ramping up the net power output and was confronted immediately with the issue of controlling the voltage potential between adjacent channel electrodes in such a way as to avoid catastrophic breakdown between elements. The tedious attention which was required to control these interelement potentials is described . An important factor uncovered during testing of the first channel was the performance improvement and reduction in magnet excitation power when the generator was operated in the supersonic mixed impulse-reaction mode at lower magnetic field rather than with the design reaction mode. A straight pipe supersonic diffuser was added to facilitate operation in this mode. The need to adjust channel loading to avoid damaging interelectrode breakdown prevented a systemic mapping of generator performance over a wide range of operating conditions, including those which would clearly have led to improved performance. Optimum results were a net power output of 23.6 MW with magnet dissipation of 8 MW. The maximum net output for the second CEF channel was 14 MW. The lessons learned from the Mark V program were: 1: The need in a high power MHD generator to limit interelement potentials to avoid catastrophic electrical breakdown between the elements, 2: The engineering difficulties in the design of a high power water cooled MHD channel with literally thousands of electrically isolated elements, 3: The practical necessity for reducing the number of individual power outputs in order to enable a tractable power conditioning solution. These lessons were invaluable for the design of later high power MHD generators.
机译:驱动磁流体发电机(RMHD)计划的Mark V型自励火箭发动机是在富高埃弗雷特研究实验室(AERL)于1962年发起的证明为当时认为需要一种简单,有限责任极高功率的低成本源的溶液循环应用。在已启动的标志V节目的时候,它已经被MHD发电机达到的最大功率为几秒钟几百千瓦。所述标记v是第MHD发电机达到超过1.5 W的输出,首先被自激,第一处理工程高功率水冷MHD通道与成千上万电隔离元件,并且所述第一体验电场和极间电位高功率磁流体发电机的管理不当可能带来的灾难性后果。计划目标和规格和整体实验的设计中,MHD相互作用的流体力学,散热器自励磁铁,燃烧室,水冷MHD通道,负载组和初始化检查进行了概述。两个信道进行了使用。第一通道包括一个上游连续电极法拉第(CEF)为磁铁励磁后跟一个分段电极法拉第(SEF),用于净功率输出部部分。所述第二信道是CEF设计与负载串联的开关与以下励磁磁铁。两个通道均用水冷却。五个十六发电运行中与第一信道,和12与第二CEF信道进行。本文侧重第一通道上。与第一通道最初的努力集中在这是很容易实现,但并非没有击穿的问题自激。努力然后浓缩上斜升的净功率输出,并与控制以这样的方式,以避免元件之间的灾难性故障的相邻信道电极之间的电压电势的问题立即面对。描述这是需要控制这些元件间的电势的繁琐的关注。所述第一信道的测试期间发现的一个重要因素是改进性能和减少磁铁激励功率时,发电机在超音速混合冲动反应模式在较低的磁场,而不是与设计反应模式下操作。的溶液中加入甲直管超音速扩压器,以促进在该模式下操作。需要调整信道负载,以避免损坏防止性能发电机全身映射在宽范围的操作条件下,包括那些显然导致改进的性能极间击穿。最佳结果是23.6兆瓦的8 MW磁体耗散的净功率输出。用于第二CEF信道的最大净输出为14兆瓦。从标记V节目学到的经验是:1:在高功率MHD发电机的必要限制元件间的电势,以避免2元件之间灾难性电击穿,:所述工程难度高功率水的设计冷却MHD信道与数以千计电隔离元件,3:用于减少为了使易处理的功率调节溶液的各个功率输出的数目的实际必要性。这些教训是无价供以后大功率发电机MHD的设计。

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