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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Design of a Wide-Range Centrifugal Compressor Stage for Supercritical CO_2 Power Cycles
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Design of a Wide-Range Centrifugal Compressor Stage for Supercritical CO_2 Power Cycles

机译:超临界CO_2功率循环大范围离心压缩机级的设计

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摘要

Supercritical carbon dioxide (sCO _( 2 ) ) power cycles require high compressor efficiency at both the design point and over a wide operating range. Increasing the compressor efficiency and range helps maximize the power output of the cycle and allows operation over a broader range of transient and part-load operating conditions. For sCO _( 2 ) cycles operating with compressor inlets near the critical point, large variations in fluid properties are possible with small changes in temperature or pressure. This leads to particular challenges for air-cooled cycles where compressor inlet temperature and associated fluid density are subject to daily and seasonal variations as well as transient events. Design and off-design operating requirements for a wide-range compressor impeller are presented where the impeller is implemented on an integrally geared compressor–expander concept for a high temperature sCO _( 2 ) recompression cycle. In order to satisfy the range and efficiency requirements of the cycle, a novel compressor stage design incorporating a semi-open impeller concept with a passive recirculating casing treatment is presented that mitigates inducer stall and extends the low flow operating range. The stage design also incorporates splitter blades and a vaneless diffuser to maximize efficiency and operating range. These advanced impeller design features are enabled through the use of direct metal laser sintering (DMLS) manufacturing. The resulting design increases the range from 45% to 73% relative to a conventional closed impeller design while maintaining high design point efficiency.
机译:超临界二氧化碳(sCO _(2))功率循环在设计点和较宽的工作范围内都要求高压缩机效率。增加压缩机效率和范围有助于最大程度地提高循环的功率输出,并允许在更大范围的瞬态和部分负载运行条件下运行。对于在临界点附近的压缩机入口运行的sCO _(2)循环,流体性质的大变化可能随温度或压力的小变化而变化。这给空冷循环带来了特别的挑战,在空冷循环中,压缩机进口温度和相关的流体密度会受到每日和季节性变化以及瞬态事件的影响。提出了大范围压缩机叶轮的设计和非设计运行要求,其中叶轮在高温sCO _(2)再压缩循环的整体齿轮式压缩机-膨胀机概念上实施。为了满足循环的范围和效率要求,提出了一种新型压缩机级设计,该设计结合了半开式叶轮概念和被动循环壳体处理,可减轻诱导器失速并扩展低流量工作范围。舞台设计还结合了分流叶片和无叶扩散器,以最大程度地提高效率和工作范围。这些先进的叶轮设计功能可通过使用直接金属激光烧结(DMLS)制造来实现。相对于传统的封闭式叶轮设计,最终的设计将范围从45%增加到73%,同时保持了较高的设计效率。

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