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71.
赖英 《自动化技术与应用》2010,29(2):132-134
本文主要介绍了重钢集团股份有限公司的CCPP(燃气-蒸汽联合循环发电机组)特点和PLC控制系统在这个项目中应用。PLC控制系统完成了CCPP工程中的燃气轮机、煤压机、余热锅炉、汽轮机等主体系统的主要功能和控制逻辑,在整个项目中起到了举足轻重的作用。 相似文献
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《低温学》2016
This research paper focuses on the performance prediction and its validation via experimental investigation of a Stirling-type pulse tube refrigerator (PTR) equipped with a cold linear compressor. When the working gas is compressed at cryogenic temperature, the acoustic power (PV power) can be directly transmitted through the regenerator to the pulsating tube without experiencing unnecessary precooling process. The required PV power generated by the linear compressor, furthermore, can be significantly diminished due to the relatively small specific volume of the working gas at low temperature. The PTR can reach lower temperature efficiently with higher heat lift at the corresponding temperature than other typical single-stage Stirling-type PTRs. Utilizing a cryogenic reservoir as a warm end and regulating the entire operating temperature range of the PTR will enable a PTR to operate efficiently under space environment.In this research, the experimental validation as a proof of concept was carried out to demonstrate the capability of PTR operating between 80 K and 40 K. The linear compressor was submerged in a liquid nitrogen bath and the lowest temperature was measured as 38.5 K. The test results were analyzed to identify loss mechanisms with the simple numerical computation (linear model) which considers the dynamic characteristics of the cold linear compressor with thermo-hydraulic governing equations for each of sub components of the PTR. All the mass flows and pressure waves were assumed to be sinusoidal. 相似文献
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Aerodynamic instabilities that naturally occur in compression systems, such as surge and rotating stall, largely reduce the life duration and performance of system components. The prediction of the compressor operating range is thus a key parameter for the design of gas turbines. This paper investigates the ability of an unsteady flow solver to simulate the rotating stall phenomenon in the full annulus of an axial compressor stage. A comparison with experimental data indicates that the simulation correctly estimates the stability limit. However the rotating stall flow patterns are different. While measurements show only one full span rotating stall cell (40 Hz), the simulation shows first a part span stall with 10 cells (790 Hz) that evolves then towards a full span stall with three cells (170 Hz). A spectral analysis based on numerical results underlines the role of rotor-stator interactions in the development of rotating stall. The effects of downstream volumes and inlet distortions are also discussed, showing the necessity to consider the whole geometry to correctly predict the rotating stall frequency. 相似文献
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Mitsuru SatoAuthor Vitae Minako HosonoAuthor VitaeKazuhiko YamashitaAuthor Vitae Sawako NakajimaAuthor VitaeShuichi InoAuthor Vitae 《Sensors and actuators. B, Chemical》2011,156(1):108-113
A metal hydride (MH) actuator provides mechanical work by applying the hydrogen pressure transition that originates from the reversible reaction of the MH alloy as it absorbs and desorbs hydrogen gas. The MH actuators that have been reported employ a Peltier element or an electrical heating resistance wire as a heat source. This paper describes the design of an MH actuator that is driven by low-quality heat sources, such as solar heat or surplus heat. A certain composition of a LaNi5-based alloy that produces desorbing and absorbing reactions through a low-temperature difference is specified. This alloy composition can provide a large amount of hydrogen desorption using solar heat or surplus heated water and a large amount of hydrogen absorption by natural air cooling in an adequate reaction time. To improve the moving speed and to control the performance, a reciprocating air compressor that applies this solar or surplus heat-driven MH actuator is proposed. These findings support the efficacy of an MH actuator operating without electric or fossil fuel energy consumption. 相似文献
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针对某航天发射场整流罩空调机组经常出现前级蒸发器结霜和送风温湿度波动问题,进行问题机理分析,结合新风与表冷后目标露点的焓值差提出了一种基于冷量阈值的压缩机PID控制方法;该方法首先根据新风和目标露点的焓值差计算出处理空气所需的实际冷量,然后将该冷量作为基于露点PID控制压缩机输出的上限值;冷量阈值的使用一方面使PID控制一直保持欠调节状态,避免了压缩机投入比的上下跳变而导致送风温湿度波动的问题;另一方面有效解决了压缩机投入冷量过多而导致的蒸发器结霜问题;实践证明,优化后的空调机组运行稳定可靠,温湿度控制精度得到有效提升,分别达到了±0.5 ℃和±3%,满足航天器产品保障需求。 相似文献
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