燃气涡轮试验与研究
燃氣渦輪試驗與研究
연기와륜시험여연구
GAS TURBINE EXPERIMENT AND RESEARCH
2014年
3期
44-48
,共5页
熊庆荣%石小江%徐芳%钟明
熊慶榮%石小江%徐芳%鐘明
웅경영%석소강%서방%종명
航空发动机%涡轮导向器%表面温度测试%温度场分布%示温漆%等温线
航空髮動機%渦輪導嚮器%錶麵溫度測試%溫度場分佈%示溫漆%等溫線
항공발동궤%와륜도향기%표면온도측시%온도장분포%시온칠%등온선
aero-engine%turbine nozzle%surface temperature measurement%temperature field distribution%temperature-sensitive paint%isotherm
掌握涡轮导向器温度场测试方法及准确的温度场分布,对于涡轮导向器的设计、改进具有重要的理论价值和实用价值。利用不可逆示温漆,测量了高压涡轮导向器在最大工况下的表面温度。结果表明:喷涂在高压涡轮导向器表面的不可逆示温漆,在高温、高压下附着牢靠,等温线清晰;成功录取了整个高压涡轮导向器的表面温度及温度场分布,可为该型发动机高压涡轮导向器的热应力与寿命分析提供数据支撑。
掌握渦輪導嚮器溫度場測試方法及準確的溫度場分佈,對于渦輪導嚮器的設計、改進具有重要的理論價值和實用價值。利用不可逆示溫漆,測量瞭高壓渦輪導嚮器在最大工況下的錶麵溫度。結果錶明:噴塗在高壓渦輪導嚮器錶麵的不可逆示溫漆,在高溫、高壓下附著牢靠,等溫線清晰;成功錄取瞭整箇高壓渦輪導嚮器的錶麵溫度及溫度場分佈,可為該型髮動機高壓渦輪導嚮器的熱應力與壽命分析提供數據支撐。
장악와륜도향기온도장측시방법급준학적온도장분포,대우와륜도향기적설계、개진구유중요적이론개치화실용개치。이용불가역시온칠,측량료고압와륜도향기재최대공황하적표면온도。결과표명:분도재고압와륜도향기표면적불가역시온칠,재고온、고압하부착뢰고,등온선청석;성공록취료정개고압와륜도향기적표면온도급온도장분포,가위해형발동궤고압와륜도향기적열응력여수명분석제공수거지탱。
The testing methods and precise distribution of temperature fields of turbine nozzle are of practi-cal and theoretical significance for the design and improvement of turbine nozzle. Temperature-sensitive paint was adopted to measure the surface temperature of HPT nozzle under maximum operating conditions. The test results proved that the temperature-sensitive paint can adhere to turbine nozzle firmly in the course of experiment with clear isotherm;the temperature field distribution of turbine nozzle was measured successfully, which could be helpful to analyze the thermal stress and life of the turbine nozzle.