Ignition and combustion characteristics of the gas turbine slinger combustor

被引：42

作者：

Choi, Seongman

Lee, Donghun ^{[1
]}

Park, Jeongbae ^{[2
]}

机构：

[1] Samsung Techwin Co Ltd, Power Syst R&D Ctr, Chang Won 641717, South Korea

[2] Agcy Def Dev, Taejon 300600, South Korea

来源：

JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY | 2008年 / 22卷 / 03期

关键词：

slinger combustor; rotating fuel injection system; ignition; combustion;

D O I：

10.1007/s12206-007-1106-6

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

This paper describes the ignition and combustion characteristics of a gas turbine slinger combustor with rotating fuel injection system. An ignition test was performed under various airflow, temperature and pressure conditions with fuel nozzle rotational speed. From the test, there are two major factors influencing the ignition limits: the rotational speed of the fuel nozzle, and the mass flow parameter. Better ignition capability could be attained through increasing the rotational speed and air mass flow. From the spray visualization and drop size measurement, it was verified that there is a strong correlation between ignition performance and drop size distribution. Also, we performed a combustion test to determine the effects of rotational speed by measuring gas temperature and emission. The combustion efficiency was smoothly enhanced from 99% to 99.6% with increasing rotational speed. The measured pattern factor was 15% and profile factor was 3%.

引用

页码：538 / 544

页数：7