TY - GEN
T1 - A cleaner design of nuclear-powerd hybrid aero engine
AU - Xu, Xinze
AU - Hong, Guanxin
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/7
Y1 - 2019/7
N2 - This artical is an analysis as well as a comparison of technical traits of the nuclear reactor, coolant, Intermediate Heat Exchanging System, Intermediate Fluid Medium and heat transfer devices. It proposed a possible formation of nuclear propulsion system, which also works as the basis of the nuclear reactor, the Intermedia Heat Transfer system and the engine. In this artical the author also respectively analysed the whole heat transfer process of the transfer system and engine, as well as estimated the propulsive force that is generated by the hybrid nuclear-engine. With the help of the capability model of the engine, the author proposed a method to anticipate the total contamination emissions based on the flying parameters and engine capability model. Through utilizing the ICAO(International Civil Aviation Organization) emission data fitting, the author gained the referential emission index of the engine in ground status and through utilizing the relative process, the author gained the emission index in air status. By comparing the estimated contamination emisson of the hybrid nuclear engine and the ordinary air engine, the author discovered that the hybrid nuclear engine produces less emission than the ordinary air engine by 75%.
AB - This artical is an analysis as well as a comparison of technical traits of the nuclear reactor, coolant, Intermediate Heat Exchanging System, Intermediate Fluid Medium and heat transfer devices. It proposed a possible formation of nuclear propulsion system, which also works as the basis of the nuclear reactor, the Intermedia Heat Transfer system and the engine. In this artical the author also respectively analysed the whole heat transfer process of the transfer system and engine, as well as estimated the propulsive force that is generated by the hybrid nuclear-engine. With the help of the capability model of the engine, the author proposed a method to anticipate the total contamination emissions based on the flying parameters and engine capability model. Through utilizing the ICAO(International Civil Aviation Organization) emission data fitting, the author gained the referential emission index of the engine in ground status and through utilizing the relative process, the author gained the emission index in air status. By comparing the estimated contamination emisson of the hybrid nuclear engine and the ordinary air engine, the author discovered that the hybrid nuclear engine produces less emission than the ordinary air engine by 75%.
KW - Aeroengine
KW - Aeroengine design
KW - Nuclear powered large aircraft
KW - Pollution emission
KW - Thrust estimation
UR - https://www.scopus.com/pages/publications/85074829697
U2 - 10.1109/ICMAE.2019.8880976
DO - 10.1109/ICMAE.2019.8880976
M3 - 会议稿件
AN - SCOPUS:85074829697
T3 - 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
SP - 37
EP - 41
BT - 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
Y2 - 22 July 2019 through 25 July 2019
ER -