In order to improve the energy conversion efficiency of the gas at the outlet of the pulse detonation combustor
a numerical calculation method was used to study the energy distribution characteristics of the gas at the outlet of the pulse detonation combustor with a pneumatic valve and detonation reinforcement structure. Results showed that the expansion process of pulse detonation gas had three stages: primary expansion
secondary expansion and over expansion. The proportion of secondary expansion time and energy was largest in a single cycle; the distribution of gas pressure potential energy
kinetic energy
internal energy and energy flow density at the outlet of the combustion chamber was mainly affected by the gas pressure
and the change law was consistent with the gas pressure; the pressure potential energy
kinetic energy and internal energy of gas increased during the primary expansion stage accounted for 479%
259% and 251%
respectively
in a single cycle; the pressure potential energy
kinetic energy and internal energy of gas increased during the secondary expansion stage accounted for 502%
Pulse detonation gas expansion process and evaluation method of energy conversion difficulty degree
Analysis on interaction between centrifugal compressor and ,pulse detonation combustor
Correlation analysis of energy and stress distributions on variable thickness turbine disk
Principle experiments on two phase pulse detonation turbine engine
基于自适应MOMEDA滚动轴承故障特征提取方法
Related Author
Xiaofeng LI
Junfeng XIAO
Mengqi HU
Wei WANG
Feng WANG
WANG Lingyi
ZHENG Longxi
JIA Shengxi
Related Institution
Gas Turbine Technology Department, Xi'an Thermal Power Research Institute Company Limited
Airworthiness Technologies Research Center, National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University