TY - GEN
T1 - Assessment the safety of alternative aviation fuels in aeroengine
AU - Liu, Ziyu
AU - Yang, Xiaoyi
AU - Ding, Shuiting
N1 - Publisher Copyright:
© Copyright 2016 by ASME.
PY - 2016
Y1 - 2016
N2 - There are three challenges existing in the current certification process, which results in three challenges including high cost in fuel refinement, fuel-cost in certification testing, lack available testing condition and the acceptance criteria. If alternative fuel is considered as one of the engine replacement parts, and then the certification of alternative fuels can be achieved through compliance verification. This compliance verification method contain two logical relationships: the mapping from fuel to engine, the gap from petroleum-based aviation turbine fuel to drop-in fuel. For similar analogy to carry out parameterization, the system safety assessment reaches a series of critical parameters related to the engine safety and engine performance which provide the boundaries on the variation of critical parameters. This method is achieved by extracting safety criteria from the "history experience" of petroleum-based aviation turbine fuel in aero-engine and to predict the safety of alternative aviation fuels in aero-engine by "similar analogy".
AB - There are three challenges existing in the current certification process, which results in three challenges including high cost in fuel refinement, fuel-cost in certification testing, lack available testing condition and the acceptance criteria. If alternative fuel is considered as one of the engine replacement parts, and then the certification of alternative fuels can be achieved through compliance verification. This compliance verification method contain two logical relationships: the mapping from fuel to engine, the gap from petroleum-based aviation turbine fuel to drop-in fuel. For similar analogy to carry out parameterization, the system safety assessment reaches a series of critical parameters related to the engine safety and engine performance which provide the boundaries on the variation of critical parameters. This method is achieved by extracting safety criteria from the "history experience" of petroleum-based aviation turbine fuel in aero-engine and to predict the safety of alternative aviation fuels in aero-engine by "similar analogy".
KW - Aero-engine model
KW - Alternative aviation fuel
KW - Fuel-independent safety criteria
KW - Similar analogy
UR - https://www.scopus.com/pages/publications/84997427317
U2 - 10.1115/POWER2016-59520
DO - 10.1115/POWER2016-59520
M3 - 会议稿件
AN - SCOPUS:84997427317
T3 - American Society of Mechanical Engineers, Power Division (Publication) POWER
BT - ASME 2016 Power Conference, POWER 2016, collocated with the ASME 2016 10th International Conference on Energy Sustainability and the ASME 2016 14th International Conference on Fuel Cell Science, Engineering and Technology
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 2016 Power Conference, POWER 2016, collocated with the ASME 2016 10th International Conference on Energy Sustainability and the ASME 2016 14th International Conference on Fuel Cell Science, Engineering and Technology
Y2 - 26 June 2016 through 30 June 2016
ER -