TY - GEN
T1 - Discussion on the Reliability Work of Future Combat Aircraft under Aircraft/Engine Integrated Design
AU - Ding, Yu
AU - Li, Tianhao
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - Traditional independent methods of aircraft and engine design can no longer meet the mission requirements of future aircraft, including high maneuverability, high energy, large airspace, and wide speed range. To achieve optimal matching between aircraft and engine and promote full play to the maximum performance potential of aircraft and engines, aircraft-engine integration designs are essential. Therefore, considering the highly coupled structure, complex control logic, and dramatic increase in energy and heat dissipation requirements under the integration design to ensure a high mission success rate, corresponding reliability analysis work and reliability level improvement of the whole aircraft are necessary. In this paper, the characteristics of work, structure, environment, and other aspects of aircraft-engine integrated design are initially considered, and the steps to conduct reliability work are discussed.
AB - Traditional independent methods of aircraft and engine design can no longer meet the mission requirements of future aircraft, including high maneuverability, high energy, large airspace, and wide speed range. To achieve optimal matching between aircraft and engine and promote full play to the maximum performance potential of aircraft and engines, aircraft-engine integration designs are essential. Therefore, considering the highly coupled structure, complex control logic, and dramatic increase in energy and heat dissipation requirements under the integration design to ensure a high mission success rate, corresponding reliability analysis work and reliability level improvement of the whole aircraft are necessary. In this paper, the characteristics of work, structure, environment, and other aspects of aircraft-engine integrated design are initially considered, and the steps to conduct reliability work are discussed.
KW - aircraft-engine integrated design
KW - complex control logic
KW - highly coupled
KW - hypersonic flight
KW - reliability analysis
UR - https://www.scopus.com/pages/publications/85212249386
U2 - 10.1109/ICRMS59672.2023.00190
DO - 10.1109/ICRMS59672.2023.00190
M3 - 会议稿件
AN - SCOPUS:85212249386
T3 - Proceedings - 2023 14th International Conference on Reliability, Maintainability and Safety, ICRMS 2023
SP - 1098
EP - 1103
BT - Proceedings - 2023 14th International Conference on Reliability, Maintainability and Safety, ICRMS 2023
A2 - Ren, Liming
A2 - Wong, W. Eric
A2 - Cheng, Hailong
A2 - Li, Xiaopeng
A2 - Wang, Shu
A2 - Liu, Kanglun
A2 - Li, Ruifeng
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 14th International Conference on Reliability, Maintainability and Safety, ICRMS 2023
Y2 - 26 August 2023 through 29 August 2023
ER -