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SYNTHESIS OF DIARYL ETHERS THROUGH PHASE TRANSFER CATALYSIS WITH POTASSIUN FLUORIDE COATED ALUMINA AS A STRONG BASE
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作者 Ru Hong KANG Ji Sheng ZHU Wen Zi LI Shu Rong LIU Department of Chemistry,Hebei Normal University,Shijiazhuang 《Chinese Chemical Letters》 SCIE CAS CSCD 1990年第1期55-56,共2页
Seven diaryl ethers were synthesized with potassium fluoride coated alumina as a strong base and the addition of catalytic amount of PTC. The yield of diaryl ethers with addition of PTC was much higher than that witho... Seven diaryl ethers were synthesized with potassium fluoride coated alumina as a strong base and the addition of catalytic amount of PTC. The yield of diaryl ethers with addition of PTC was much higher than that without PTC.A discussion of the catalysis mechanism was given in this paper. 展开更多
关键词 TEBA SYNTHESIS OF DIARYL ETHERS THROUGH PHASE transfer CATALYSIS WITH POTASSIUN FLUORIDE COATED ALUMINA AS A STRONG BASE PTC AS
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Conjugate Heat Transfer Investigation on the Cooling Performance of Air Cooled Turbine Blade with Thermal Barrier Coating 被引量:5
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作者 JI Yongbin MA Chao +1 位作者 GE Bing ZANG Shusheng 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第4期325-335,共11页
A hot wind tunnel of annular cascade test rig is established for measuring temperature distribution on a real gas turbine blade surface with infrared camera.Besides,conjugate heat transfer numerical simulation is perf... A hot wind tunnel of annular cascade test rig is established for measuring temperature distribution on a real gas turbine blade surface with infrared camera.Besides,conjugate heat transfer numerical simulation is performed to obtain cooling efficiency distribution on both blade substrate surface and coating surface for comparison.The effect of thermal barrier coating on the overall cooling performance for blades is compared under varied mass flow rate of coolant,and spatial difference is also discussed.Results indicate that the cooling efficiency in the leading edge and trailing edge areas of the blade is the lowest.The cooling performance is not only influenced by the internal cooling structures layout inside the blade but also by the flow condition of the mainstream in the external cascade path.Thermal barrier effects of the coating vary at different regions of the blade surface,where higher internal cooling performance exists,more effective the thermal barrier will be,which means the thermal protection effect of coatings is remarkable in these regions.At the designed mass flow ratio condition,the cooling efficiency on the pressure side varies by 0.13 for the coating surface and substrate surface,while this value is 0.09 on the suction side. 展开更多
关键词 gas turbine blade thermal barrier coating cooling efficiency conjugate heat transfer
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