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Optimization Study on a Single-cylinder Compressed Air Engine 被引量:2
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作者 YU Qihui CAI Maolin +1 位作者 SHI Yan XU Qiyue 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2015年第6期1285-1292,共8页
The current research of compressed air engine(CAE) mainly focused on simulations and system integrations. However, energy efficiency and output torque of the CAE is limited, which restricts its application and popul... The current research of compressed air engine(CAE) mainly focused on simulations and system integrations. However, energy efficiency and output torque of the CAE is limited, which restricts its application and popularization. In this paper, the working principles of CAE are briefly introduced. To set a foundation for the study on the optimization of the CAE, the basic mathematical model of working processes is set up. A pressure-compensated valve which can reduce the inertia force of the valve is proposed. To verify the mathematical model, the prototype with the newly designed pressure-compensated intake valve is built and the experiment is carried out, simulation and experimental results of the CAE are conducted, and pressures inside the cylinder and output torque of the CAE are obtained. Orthogonal design and grey relation analysis are utilized to optimize structural parameters. The experimental and optimized results show that, first of all, pressure inside the cylinder has the same changing tendency in both simulation curve and experimental curve. Secondly, the highest average output torque is obtained at the highest intake pressure and the lowest rotate speed. Thirdly, the optimization of the single-cylinder CAE can improve the working efficiency from an original 21.95% to 50.1%, an overall increase of 28.15%, and the average output torque increases also increases from 22.047 5 N · m to 22.439 N · m. This research designs a single-cylinder CAE with pressure-compensated intake valve, and proposes a structural parameters design method which improves the single-cylinder CAE performance. 展开更多
关键词 single-cylinder compressed air engine experimental study mathematical model orthogonal design grey relation analysis
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面向飞行员飞行全生命周期的作风胜任能力画像 被引量:1
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作者 陈农田 宁威峰 齐少桓 《人类工效学》 2023年第3期30-36,共7页
目的建立面向飞行技能全生命周期的飞行员作风胜任能力客观量化评价画像方法。方法采用问卷调查、量表分析法建立飞行员作风胜任能力画像指标体系,运用层次分析熵权法确定各指标权重,通过实证分析得到飞行技能全生命周期的作风胜任能力... 目的建立面向飞行技能全生命周期的飞行员作风胜任能力客观量化评价画像方法。方法采用问卷调查、量表分析法建立飞行员作风胜任能力画像指标体系,运用层次分析熵权法确定各指标权重,通过实证分析得到飞行技能全生命周期的作风胜任能力雷达图。结果(1)通过对现有胜任力指标加以归纳总结形成飞行员作风胜任力画像的初始指标,并通过调查问卷的形式对指标加以验证和分析,保证其适用性,最终形成3个维度,16项具体胜任力能力指标(2)基于各项指标内部的结构关系,利用层次分析法和熵权法的组合赋权为各项指标和维度设计权重,最终形成量化表格。(3)以被试者群体为例,展开作风胜任力的评估,设计作风胜任力画像的雷达图。结论该方法适用于飞行员飞行技能作风胜任力的量化评估,适用于飞行员飞行技能选拔以及为同行业的研究人员提供一定的参考。 展开更多
关键词 航空交通工程 人因工程 交通安全 技能全生命周期 飞行员 作风胜任能力 胜任特征理论模型 画像方法
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Aerosol Filtration Application Using Fibrous Media—An Industrial Perspective 被引量:4
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作者 YANG Chuanfang 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2012年第1期1-9,共9页
Filtration of aerosol particles using non-woven fibrous media is a common practice for air cleaning. It has found wide applications in industries and our daily lives. This paper overviews some of these applications an... Filtration of aerosol particles using non-woven fibrous media is a common practice for air cleaning. It has found wide applications in industries and our daily lives. This paper overviews some of these applications and provides an industrial perspective. It starts from discussing aerosol filtration theory, followed by a brief review on the advancement of filtration media. After that, filtration applications in respiratory protection, dust collection, and engine in-take air cleaning are elaborated. These are the areas that the author sees as the typical needed ones in China's fast pace economical development endeavor, where air filtration enables the protection of human health, environment and equipment for sustainability. 展开更多
关键词 aerosol filtration filter media fiber technology RESPIRATOR dust collection engine in-take air cleaning SUSTAINABILITY
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Overspeeding characteristics of turbomachinery for gas generator cycle air turbo ramjet engine
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作者 Ryojiro Minato Daisuke Nakata +2 位作者 Masaharu Uchiumi Ryoji Imai Kazuyuki Higashino 《Propulsion and Power Research》 SCIE 2022年第4期444-456,共13页
The main interest in the current study focuses on the possibility of overspeeding for the gas-generator cycle air turbo ramjet(GG-ATR)engine.The authors developed the air turbo ramjet engine and investigated its compr... The main interest in the current study focuses on the possibility of overspeeding for the gas-generator cycle air turbo ramjet(GG-ATR)engine.The authors developed the air turbo ramjet engine and investigated its compressor performance.Based on those data,the authors developed the analytical code for the air turbo ramjet engine,which calculates the performances of turbomachinery,gas-generator,and ram combustor.The previous study described that the rotor overspeeding would not occur in the air turbo rocket engine.However,the current results show that degraded ram combustion can decrease the compressor pressure ratio and the compressor power.This reduced compressor power can cause overspeeding for the air turbo ramjet engine.The experimental results of compressor power and turbine inlet pressure support those analytical results. 展开更多
关键词 air turbo ramjet engine Compressor map Overspeeding Combustion efficiency
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Solution of Modern Thermo Physical Problems of Applied External and Internal Aerodynamics with Dark Matter-Energy Simulation
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作者 Mikhail Ja. Ivanov 《Journal of Energy and Power Engineering》 2014年第5期812-825,共14页
The paper is devoted to new, experimentally registered thermo physical problems of high temperature applied external and internal aerodynamics which is defined first of all by intensive interaction of the gaseous medi... The paper is devoted to new, experimentally registered thermo physical problems of high temperature applied external and internal aerodynamics which is defined first of all by intensive interaction of the gaseous media and thermal radiation. The first report section analyses basic complexities of designing high temperature air breathing engines related to origin of so-called "unexpected" heat of working process. The next parts of the report consider physical, chemical and plasma features of aerodynamics of reentry space blunt bodies and meteors with specified account of thermal radiation influence. Our solutions are based on the classical Dark Matter-Energy simulation. We present special experimental data for Dark Matter pressure registration on the earth conditions. 展开更多
关键词 AERODYNAMICS thermal radiation air breathing engine blunt bodies dark matter pressure.
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