Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Yang Yong, Fu Yaoming, Lin Binbin, Hou Kuanxin, Kong Ling Bing, X. Honghui, Gao Jie, Jiang Shiqi
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Abstract

Abstract In order to improve the effectiveness of compressor efficiency measurement results under the influence of complex factors, several research work have been carried out, such as inverse connection of thermocouple suitable for efficiency measurement under low pressure ratio and small temperature rise conditions, torque efficiency correction considering the mechanical loss of high speed gearbox under various working conditions, and identification of the impact of seal cavity leakage flow on efficiency measurement. Compared with the conventional connection method of thermocouple, the inverse connection method of thermocouple shows obvious advantages in efficiency measurement under low pressure ratio and small temperature rise conditions. At medium and low speeds, the conventional simplified correction method will lead to the high measurement results of torque efficiency after installing the high speed gearbox. The accuracy of torque efficiency measurement can be improved by adopting the improved correction method. Increasing the oil supply pressure of the high speed gearbox or reducing the oil supply temperature will increase the mechanical loss of the high speed gearbox. The air flow in the compressor bearing seal chamber will leak into the flow passage through the labyrinth clearance, resulting in discontinuous changes of the inlet/outlet flow of compressor.
多因素影响下轴流压缩机效率的精确测量与评价方法
摘要为了提高复杂因素影响下压缩机效率测量结果的有效性,开展了适用于低压比和小温升条件下效率测量的热电偶反连接、考虑高速齿轮箱各种工况下机械损耗的转矩效率校正、并识别了密封腔泄漏流量对效率测量的影响。与传统的热电偶连接方法相比,热电偶反连接方法在低压比和小温升条件下的效率测量中具有明显的优势。在中低速时,采用传统的简化校正方法,安装高速齿轮箱后的转矩效率测量结果较高。采用改进的修正方法,可以提高转矩效率测量的精度。提高高速变速箱的供油压力或降低供油温度都会增加高速变速箱的机械损耗。压缩机轴承密封腔内的气流将通过迷宫间隙泄漏到流道中,导致压缩机进出口流量的不连续变化。
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来源期刊
International Journal of Turbo & Jet-Engines
International Journal of Turbo & Jet-Engines 工程技术-工程:宇航
CiteScore
1.90
自引率
11.10%
发文量
36
审稿时长
6 months
期刊介绍: The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.
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