Study Over Thermal State of Gas Turbine Engine Metal-ceramic Rotor Blades and Nozzle Guide Vanes Under Thermal Shock and Thermal-cyclic Loading Conditions
A.V. SOUDAREV; A.A. SOURYANINOV; V.Ya. PODGORETS; V.V. GRISHAEV; V.Yu. TIKHOPLAV; A.S. MOLCHANOV; B.V. SOUDAREV
刊名JOURNAL OF THERMAL SCIENCE
2004
卷号13期号:2页码:163,166
关键词Metal-ceramic Blades High Temperature Thermal-cyclic Loading
英文摘要To ensure a reliable operation of the 2.5 MW gas turbine engine (GTE- 2.5)[1] with the inlet gas temperature TIT=1623 K, studies were performed over the thermal state of the nozzle guide vanes and rotor blades with the temperatures, rates and flows of the working media and cooling air simulating all the potential turbine stage operating duties. The steady state and thermal-cyclic tests having been accomplished, there was no visible defect on the rotor blades and the nozzle vanes. Afterwards, they survived the endurance tests at the rated cooling. Therefore, the functionality of the shell thin-wall hybrid nozzle vanes and rotor blades under the variable operating duties of the gas turbine at the “shock” and “cyclic” loads of the working media temperature variations has been demonstrated.
公开日期2013-03-11
内容类型期刊论文
源URL[http://ir.etp.ac.cn/handle/311046/53324]  
专题工程热物理研究所_Journal of Thermal Science
推荐引用方式
GB/T 7714
A.V. SOUDAREV,A.A. SOURYANINOV,V.Ya. PODGORETS,et al. Study Over Thermal State of Gas Turbine Engine Metal-ceramic Rotor Blades and Nozzle Guide Vanes Under Thermal Shock and Thermal-cyclic Loading Conditions[J]. JOURNAL OF THERMAL SCIENCE,2004,13(2):163,166.
APA A.V. SOUDAREV.,A.A. SOURYANINOV.,V.Ya. PODGORETS.,V.V. GRISHAEV.,V.Yu. TIKHOPLAV.,...&B.V. SOUDAREV.(2004).Study Over Thermal State of Gas Turbine Engine Metal-ceramic Rotor Blades and Nozzle Guide Vanes Under Thermal Shock and Thermal-cyclic Loading Conditions.JOURNAL OF THERMAL SCIENCE,13(2),163,166.
MLA A.V. SOUDAREV,et al."Study Over Thermal State of Gas Turbine Engine Metal-ceramic Rotor Blades and Nozzle Guide Vanes Under Thermal Shock and Thermal-cyclic Loading Conditions".JOURNAL OF THERMAL SCIENCE 13.2(2004):163,166.
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