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不可食用生物柴油在船用柴油发动机中作为一种环保和可持续的替代燃料在印度发展的潜力 被引量:1
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作者 Christopher Selvam Damian Yuvarajan Devarajan Ravikumar Jayabal 《哈尔滨工程大学学报(英文版)》 CSCD 2023年第4期870-881,共12页
This article explores the possibilities of inedible biodiesel as a viable and environmentally friendly substitute fuel for marine diesel engines in India.This article encompasses on various crucial elements,including ... This article explores the possibilities of inedible biodiesel as a viable and environmentally friendly substitute fuel for marine diesel engines in India.This article encompasses on various crucial elements,including engine compatibility,biodiesel blends,fuel quality,emissions reduction,regulatory compliance,cost analysis,environmental advantages,and research and development.Implementing biodiesel in maritime operations within India presents favourable opportunities for mitigating carbon emissions,improving air quality,bolstering energy security,promoting sustainable agriculture,and harmonizing with international environmental objectives.Nevertheless,the effective incorporation of biodiesel necessitates a meticulous examination of multiple variables and an all-encompassing methodology that involves formulating policies,investment in infrastructure,research and development,and collaboration among relevant parties.Adopting biodiesel in India’s maritime sector offers a promising prospect for substantially contributing to sustainability and environmental stewardship. 展开更多
关键词 BIODIESEL Marine diesel engines engine compatibility Emissions reduction Regulatory compliance Energy security SUSTAINABILITY Environmental stewardship
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Coupling Effect between Inlet Distortion Vortex and Fan
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作者 LIU Zepeng HUANG Guoping +1 位作者 CHEN Jie YU Zonghan 《Journal of Thermal Science》 SCIE EI CAS CSCD 2023年第3期1089-1104,共16页
In the process of inlet/engine matching,large-scale distortion vortexes would be generated due to lip separation,curved duct,shock-wave boundary layer interaction and other factors of inlet,resulting in complex combin... In the process of inlet/engine matching,large-scale distortion vortexes would be generated due to lip separation,curved duct,shock-wave boundary layer interaction and other factors of inlet,resulting in complex combination distortion of total pressure and swirl,which would affect the stable and efficient operation of fans/compressors of aero-engine.On the basis of main distortion vortex characteristics of a typical S-shape inlet and its theoretical model of velocity and pressure distribution,this paper establishes an inlet boundary condition definition method to generate three-dimensional distortion vortex,and presents a study of coupling effect between steady distortion vortex and NASA Rotor 67.The results show that the fan’s performance curve would move to smaller mass flow direction under the influence of the co-rotating distortion vortex,while fan’s operation curve would change to the opposite direction if the inlet distortion vortex direction is opposite to the fan’s rotating direction.Compared with co-rotating distortion vortex,the efficiency loss caused by counter-rotating distortion vortex would be larger and total pressure ratio loss would be smaller.The vortex core size has significant influence on the stability margin of the fan,but has little influence on the efficiency and total pressure ratio characteristic.As the vortex core size increases,the range of fan’s tip region with high attack angle would become larger and cause the fan to stall in advance.Due to the non-uniform suction of the downstream fan,the inlet distortion vortex accelerates to mix with the surrounding main flow.The total pressure distortion decreases and swirl distortion increases along sections from inlet boundary to the fan leading edge. 展开更多
关键词 inlet/engine compatibility distortion flow fan stall margin flow separation
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