With the development of functional integration and compactness design for next generation aeroengine,the ineffective dissipation and utilization of excess heat is one of the key research topics.This paper develops a n...With the development of functional integration and compactness design for next generation aeroengine,the ineffective dissipation and utilization of excess heat is one of the key research topics.This paper develops a novel air-fuel wing-shaped fin radiator(WFR)to further improve aerodynamic performance,load-bearing capacity and lightweight.The performance of WFR is validated by fluid-thermal-solid coupling method.From this study,it is revealed that the WFR structure respectively reduces the aerodynamic loss by 44.58%and 28.45%and the mass by 16.48%and 13.64%while ensuring the thermal efficiency,compared with structures of the frequently-used rectangular fin radiator and wing-rectangle fin radiator.The WFR is demonstrated to have excellent aerodynamic performance,high heat dissipation and light weight.The efforts of this study develop a promising WFR structure and provide an insight to support the high-performance and lightweight design of advanced aeroengines.展开更多
基金co-supported by National Natural Science Foundation of China(Grant No.52375237)China and National Science and Technology Major Project(Grant No.J2022-IV-0012),China.
文摘With the development of functional integration and compactness design for next generation aeroengine,the ineffective dissipation and utilization of excess heat is one of the key research topics.This paper develops a novel air-fuel wing-shaped fin radiator(WFR)to further improve aerodynamic performance,load-bearing capacity and lightweight.The performance of WFR is validated by fluid-thermal-solid coupling method.From this study,it is revealed that the WFR structure respectively reduces the aerodynamic loss by 44.58%and 28.45%and the mass by 16.48%and 13.64%while ensuring the thermal efficiency,compared with structures of the frequently-used rectangular fin radiator and wing-rectangle fin radiator.The WFR is demonstrated to have excellent aerodynamic performance,high heat dissipation and light weight.The efforts of this study develop a promising WFR structure and provide an insight to support the high-performance and lightweight design of advanced aeroengines.
