LIU Zuo-hong, HE Zhi-qiang, LIU Guo-yin, LIU Jia-xin, KANG Chen, CHENG Lu.Aeroengine Ground-level Test with Inlet Air Heating[J].航空发动机,2024,50(3):148-153
Aeroengine Ground-level Test with Inlet Air Heating
DOI:
Key Words:inlet air heating  ground-level test  temperature field  temperature distortion  aeroengine
Author NameAffiliation
LIU Zuo-hong, HE Zhi-qiang, LIU Guo-yin, LIU Jia-xin, KANG Chen, CHENG Lu AECC Shenyang Engine Research InstituteShenyang 110015China 
Hits: 14
Download times: 9
Abstract:In order to conduct engine inlet heating simulation tests, an inlet heating test was carried out on a ground-level test bed, a set of suitable inlet heating equipment was designed, and the inlet heating testing scheme and test method were proposed. The results show that at the inlet temperature of 108.88℃, the circumferential extent of the high-temperature region was 180°, the high-temperature regions were mainly distributed at 0° and 180°, the low-temperature regions were distributed at 90° and 270°, separating the high-temperature regions. The difference between the average temperature in the high-temperature regions and the area-weighted face-average temperature was small, and the circumferential temperature distortion intensity was 0.43%, indicating a uniform temperature distribution and no strong temperature distortion; it took 80 seconds for the inlet temperature rose from 94.82℃ to 108.88℃, and the temperature rise rate of high- temperature region was 0.18 ℃/s, the time-variant temperature distortion was small, the stability margin loss was small, the temperature field was irrotational, and the distribution of high-temperature regions and the circumferential temperature distortion intensity did not show significant changes obviously with time. When the inlet temperature rose from 65.34℃ to 108.88℃ , the circumferential distribution remained uniform, and the linear relationship between the area-weighted face-average temperature and the area-weighted average temperature of the high-temperature regions was established. The relationship between the area-weighted face-average temperature and the inlet air temperature acquired by the engine control system was obtained.
View Full Text  View/Add Comment  Download reader