1. School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics,Beijing,China,100191
2. Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China,Shenyang,China,110015
纸质出版:2014
移动端阅览
YANG Zhi-min. Influence of measure-density on combustor characteristics[J]. 航空动力学报, 2014,(5).
YANG Zhi-min. Influence of measure-density on combustor characteristics[J]. 2014, (5).
The apparatus of scan measurement was used to gather the temperature pattern at the combustor outlet
where the average working temperature of gas was about 1700K and the maximum temperature was about 1950K. Consequently
the measurement part was cooled by water or air. Usually
for intermittent measurement devices
the interval of circle angel could be changed to get a high-density temperature distribution. A continuous measurement manner was adopted to get point in circle. The angle between two measure-points was 1.286°.The annular combustor outlet was about 40 to 50mm in height
where 5 or 6 measure points were usually arranged. In this device
10 measure points were arranged in a range of 45.5mm. Four thermocouples were arranged in circle to obtain 2800 measure-points of the temperature field in a single experiment. Data were drawn from the whole datasheet at intervals. Each group of data whose number decreased in turn
included temperature points of 2800
1400
700
and 350
respectively. Several groups of temperature distributions with different densities were established. Subsequently
data processing was conducted to calculate the main combustor characteristics
including arithmetic or integral average temperature
OTDF (overall temperature distribution factor) and RTDF(radial temperature distribution factor). It is found that the data from different groups with different measuring densities result in significant difference on the combustor characteristics. The veracity of temperature characteristics increases with the growing measure-density.
The apparatus of scan measurement was used to gather the temperature pattern at the combustor outlet
where the average working temperature of gas was about 1700K and the maximum temperature was about 1950K. Consequently
the measurement part was cooled by water or air. Usually
for intermittent measurement devices
the interval of circle angel could be changed to get a high-density temperature distribution. A continuous measurement manner was adopted to get point in circle. The angle between two measure-points was 1.286°.The annular combustor outlet was about 40 to 50mm in height
where 5 or 6 measure points were usually arranged. In this device
10 measure points were arranged in a range of 45.5mm. Four thermocouples were arranged in circle to obtain 2800 measure-points of the temperature field in a single experiment. Data were drawn from the whole datasheet at intervals. Each group of data whose number decreased in turn
included temperature points of 2800
1400
700
and 350
respectively. Several groups of temperature distributions with different densities were established. Subsequently
data processing was conducted to calculate the main combustor characteristics
including arithmetic or integral average temperature
OTDF (overall temperature distribution factor) and RTDF(radial temperature distribution factor). It is found that the data from different groups with different measuring densities result in significant difference on the combustor characteristics. The veracity of temperature characteristics increases with the growing measure-density.
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