Study and test validation of turboshaft engine on-line performance monitoring technology
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Study and test validation of turboshaft engine on-line performance monitoring technology
Vol. 28, Issue 4, (2013)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 中国航空工业集团公司 中国航空动力机械研究所,湖南,株洲,412002
作者简介:
基金信息:
DOI:
CLC:
Published:2013
稿件说明:
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SHAN Xiao-ming, HUANG Jin-quan, ZHOU Wen-xiang, et al. Study and test validation of turboshaft engine on-line performance monitoring technology[J]. 2013, 28(4).
DOI:
SHAN Xiao-ming, HUANG Jin-quan, ZHOU Wen-xiang, et al. Study and test validation of turboshaft engine on-line performance monitoring technology[J]. 2013, 28(4).DOI:
Study and test validation of turboshaft engine on-line performance monitoring technology
A model based on-line turboshaft engine(TSE) performance monitoring technology was studied
while an on-line TSE performance monitoring software was developed and subsequently applied to an actual TSE land rig test. Test results show that the software could automatically distinguish the working state of TSE on rig test. With use of the atmosphere pressure and temperature
gas turbine rotor speed and power turbine rotor speed
the software could calculate the TSE performance parameters such as compressor pressure ratio
power turbine inlet gas total temperature
output shaft power and specific fuel consumption et al. The calculation error of compressor pressure ratio between TSE model and the specific engine in rig test is less than 2.3%
which shows the significant performance difference between testing engine and baseline engine
and the effectiveness of the on-line TSE performance monitoring technology is confirmed.