Targeting the influencing factors such as starting speed
fuel temperature and ignition energy
an experimental research on the cold start performance of aviation kerosene engine was carried out on a single-cylinder testing machine with a displacement of 650 mL. The results showed that with the increase of the starting speed
the starting time became shorter but then longer
the starting time was the shortest when the starting speed was 1 200 r/min. The rise of the fuel temperature improved the cold starting performance and combustion characteristics. Under the given test conditions
the engine can be successfully started when the fuel temperature was 50 ℃. Increasing ignition energy had a positive effect on the formation of the fire core and the flame propagation
Effect of ignition on detonation combustion of kerosene engine based on time-frequency analysis
Effect of key parameters on knock of two⁃stroke kerosene engine
Calculation method of fuel temperature conforming to requirements of airworthiness certification
Effect of lean blowout performance of trapped vortex combustor of the afterburner
Research on mixture formation of two⁃stroke heavy fuel direct injection engine
Related Author
HU Chunming
ZHAO Yingbo
Xiaosheng HU
Minxiang WEI
Cheng CHANG
Zhao SHA
Yuzhang DING
Ruihua ZHANG
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Key Laboratory of Aircraft Environmental Control and Life Support of Ministry of Industry and Information Technology,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics
Jincheng Nanjing Engineering Institute of Aircraft System,Aviation Industry Corporation of China Limited
Sichuan Gas Turbine Establishment,Aero Engine Corporation of China
Energy and Power Technology Research Department,Aerospace Times FeiHong Technology Company Limited