A Fuel Spiking Test for the Surge Margin Measurements in Gas Turbine Engines
가스 터빈 엔진의 서지마진 측정을 위한 연료 돌출 시험
- Lee, Jin-Kun ;
-
Kim, Chun-Taek
;
-
Lee, Kyung-Jae
;
- Ha, Man-Ho ;
- An, Dong-Chan ;
-
Yang, Soo-Seok
;
-
Lee, Dae-Sung
- 이진근 (한국항공우주연구원 항공추진그룹) ;
-
김춘택
(한국항공우주연구원 항공추진그룹)
;
-
이경재
(한국항공우주연구원 항공추진그룹)
;
- 하만호 (한국항공우주연구원 항공추진그룹) ;
- 안동찬 (한국항공우주연구원 항공추진그룹) ;
-
양수석
(한국항공우주연구원 항공추진그룹)
;
-
이대성
(한국항공우주연구원 항공기술실)
- Published : 2003.12.05
Abstract
A fuel spiking test was performed to measure the surge margin of gas turbine engines. The surge marin was mainly determined by the compressors and fuel spiking was used to change the operating point in the compressor characteristic map while speed remained constant. To access the surge margin region different spiking signals were applied by modulations of time(frequency) and fuel flow rate(amplitude). The test results showed good agreements with expected fuel spiking patterns and possibility of further studies.