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燃气轮机冷却技术综述 总被引:2,自引:0,他引:2
详细地阐述了对气膜冷却、内部强化换热以及热管冷却等的影响因素,目前的应用状况以及发展前景.重点集中在内部强化换热和热管冷却.本文可以使刚开始接触燃气轮机冷却技术的人员对冷却技术有个整体的了解,还可以对研究设计人员提供必要的参考依据. 相似文献
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燃气轮机压气机喘振及其控制算法 总被引:1,自引:0,他引:1
压气机是燃气轮机的三大部件之一,它运行的安全、高效对燃气轮机性能至关重要。本文扼要地介绍了压气机喘振的影响因素,分析了压气机的性能曲线和喘振线;在此基础上针对压气机某一种喘振控制策略,分析其各种控制设定曲线和控制算法。通过以上两方面的介绍,希望对燃气轮机压气机的喘振防治有所帮助。 相似文献
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The present investigation analyzes the effects of major geometrical modifications to the interior of a convection cooled gas
turbine rotor blade. The main focus lies on the flow of the leading edge channels and the impact on the heat transfer. An
experimental approach is performed with flow visualization via paint injection into water. Also numerical calculations are
carried out in two sets, on the one hand water calculations accompanying the experiments and on the other hand conjugate heat
transfer calculations under realistic engine conditions. The latter calculations are still ongoing delivering preliminary
results.
Five geometry configurations are investigated, three of them with differing turbulator arrangements in the leading edge channels.
The operating point of the base configuration is set to Re = 50,000 at the inlet while for the modified geometries the pressure
ratio is held constant compared to the base. 相似文献
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The performances of two natural gas small‐scale trigeneration plants are dealt with in the paper. The two plants are part of a new cogeneration and trigeneration system laboratory at the Politecnico di Torino (Turin, Italy), which will be set up and exploited for scientific and technical purposes. The first plant has 126/220/210 kW electrical, heating and cooling capacities, respectively, and it is characterized by an innovative internal combustion engine (ICE) that has been coupled to a liquid LiCl–water desiccant cooling system. The other plant has 100/145/98 kW electrical, heating and cooling capacities and is composed of a micro gas turbine, coupled to a LiBr–Water absorption chiller. The aim of the paper was comparing the performances of the two plants from an energetic and economic point of view; the Primary Energy Savings are calculated for both installations through a commonly accepted methodology proposed by the European Union, and through another methodology, reported in literature, which seems more suitable to describe the energetic performances of trigeneration plants. The savings calculated with this second procedure result to be lower than those of the European Union methodology; moreover, the ICE installation always denotes higher performances with respect to the microturbine. From the economic point of view, it is evident that a fuel tax reduction for high‐efficiency cogeneration plants is an essential contribution for the support and development of these systems. Copyright © 2011 John Wiley & Sons, Ltd. 相似文献
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受可靠性和成本制约,微型燃气轮机冷却技术的发展和应用一直较为缓慢,已成为其进一步提升热效率的主要瓶颈。针对此问题,提出了一种简单可靠的径流涡轮新型冷却技术-背盘冲击冷却,使用气热耦合的方法对该冷却技术的冷却特性进行了仿真研究。结果表明:背盘冲击冷却可以大幅降低径流涡轮背盘的温度。当冷却气体流量为主流的2%时,冷却流体温度从473.0降到323.0 K,背盘平均温度降低了143.0~202.0 K;当冷却温度为323.0 K时,冷却气体消耗量从主流质量流量的1%增加到4%时,背盘平均温度降低150.0~252.0 K。冷却流体流入主流后会对其产生一定的影响,每增加1%的冷却流量,涡轮机效率下降约1%。 相似文献
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In this paper, a new approach to enhance the performance of gas turbines operating in hot climates is investigated. Cooling the intake air at the compressor bell mouth is achieved by an air Brayton refrigerator (reverse Joule Brayton cycle) driven by the gas turbine and uses air as the working fluid. Fraction of the air is extracted from the compressor at an intermediate pressure, cooled and then expands to obtain a cold air stream, which mixes with the ambient intake. Mass and energy balance analysis of the gas turbine and the coupled Brayton refrigerator are performed. Relationships are derived for a simple open gas turbine coupled to Brayton refrigeration cycle, the heat rejected from the cooling cycle can be utilized by an industrial process such as a desalination plant. The performance improvement in terms of power gain ratio (PGR) and thermal efficiency change (TEC) factor is calculated. The results show that for fixed pressure ratio and ambient conditions, power and efficiency improvements are functions of the extraction pressure ratio and the fraction of mass extracted from the air compressor. The performance improvement is calculated for ambient temperature of 45°C and 43.4% relative humidity. The results indicated that the intake temperature could be lowered below the ISO standard with power increase up to 19.58% and appreciable decrease in the thermal efficiency (5.76% of the site value). Additionally, the present approach improved both power gain and thermal efficiency factors if air is extracted at 2 bar which is unlike all other mechanical chilling methods. Copyright © 2007 John Wiley & Sons, Ltd. 相似文献
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Mist film cooling simulation at gas turbine operating conditions 总被引:1,自引:0,他引:1
Air film cooling has been successfully used to cool gas turbine hot sections for the last half century. A promising technology is proposed to enhance air film cooling with water mist injection. Numerical simulations have shown that injecting a small amount of water droplets into the cooling air improves film-cooling performance significantly. However, previous studies were conducted at conditions of low Reynolds number, temperature, and pressure to allow comparisons with experimental data. As a continuous effort to develop a realistic mist film cooling scheme, this paper focuses on simulating mist film cooling under typical gas turbine operating conditions of high temperature and pressure. The mainstream flow is at 15 atm with a temperature of 1561 K. Both 2D and 3D cases are considered with different hole geometries on a flat surface, including a 2D slot, a simple round hole, a compound-angle hole, and fan-shaped holes. The results show that 10–20% mist (based on the coolant mass flow rate) achieves 5–10% cooling enhancement and provides an additional 30–68 K adiabatic wall temperature reduction. Uniform droplets of 5–20 μm are used. The droplet trajectories indicate the droplets tend to move away from the wall, which results in a lower cooling enhancement than under low pressure and temperature conditions. The commercial software Fluent is adopted in this study, and the standard k–ε model with enhanced wall treatment is adopted as the turbulence model. 相似文献
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本文介绍了M701F型燃气轮机冷却系统的组成、日本三菱公司在F系列或G系列燃气轮机上所采用的冷却技术及其应用情况,阐明了三菱公司研发的大型燃气轮机之所以能够安全稳定运行并具有很高的可靠性和热效率,采用先进的冷却技术是其成功的重要因素之一。 相似文献
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《International Communications in Heat and Mass Transfer》1994,21(5):695-706
An overview of the experimental techniques employed or developed for the measurement of local and mean heat transfer coefficients and adiabatic wall effectiveness from film cooled surfaces is presented. The scope of this work is confined to heat transfer techniques applied to film cooling of gas turbine blades, steady state and transient. The latter technique have significant advantages over the former in that it yields results at parameters duplicating those at the full-scale operating engine conditions, although the former technique offers simplicity. 相似文献
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《International Communications in Heat and Mass Transfer》1994,21(5):707-718
This paper presents an overview of the analogous mass transfer experimental techniques that are used or developed for the measurement of local and mean heat-mass transfer coefficients and adiabatic wall effectiveness, chiefly for the film-cooled blades of gas turbines. The mass transfer techniques yield comprehensive results that are more difficult to obtain using the conventional heat transfer methods. They also provide results such that the errors associated with direct heat transfer methods are eliminated. 相似文献
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无气体产生燃料在AIP装置上的应用具有优势,如不会释放燃烧反应气体,不存在燃烧产物排放问题,不会形成排气尾迹。针对闭式循环气轮机装置使用的无气体产生燃料,提出了无气体产生燃料及其氧化剂选择和需满足的技术要求,给出了一些无气体产生燃料及其相应氧化剂的种类和性质,介绍了无气体产生燃料的燃烧方式和燃烧设备,描述了使用无气体产生燃料的闭式循环蒸汽轮机装置和燃气轮机装置的系统组成及工作原理,并对一些应用上问题进行了分析。 相似文献
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通过对燃机内环水所携带热量的研究,设计换热器,论证了用内环水加热燃机天然气进气的可行性,从而达到回收内环水余热,节约能源的目的。 相似文献
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Turbine air inlet cooling is one of many available commercial methods to improve the efficiency of an existing gas turbine. The method has various configurations which could be utilized for almost all installed gas turbines. This paper presents a comparison between two commons and one novel inlet air cooling method using turbo-expanders to improve performance of a gas turbine located at the Khangiran refinery in Iran. These methods have been applied to one of the refinery gas turbines located at the Khangiran refinery in Iran. Two common air cooling methods use evaporative media or a mechanical chiller. The idea behind the novel method is to utilize the potential cooling and power capacity of the refinery natural gas pressure drop station by replacing throttling valves with a turbo-expander. The study is part of a comprehensive program with the goal of enhancing gas turbine performance at the Khangiran gas refinery. Based on the results, it is found that using turbo-expanders is the most economically feasible option and so is recommended to be utilized for improving gas turbine performance at the Khangiran refinery. 相似文献
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