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A fan rotor blade (1) includes a blade body (10) made from a composite material of a resin and fibers, and having a pressure surface (10a) facing one side in a rotation direction and a suction surface (10b) facing the other side in the rotation direction. The blade body is provided ...
1、航空发动机叶片热障涂层技术Aircraft_Enginer_TBC_benchmark课件航空发动机叶片热障涂层技术Aircraft_Enginer_Operating Condition of Turbine BladesJourney through a jet engine Fan LPC HPC HPT LPTOperating Condition of TurbineData for Turbine BladesHigh Temperature: 1400oCHigh Pressure: 40atmHigh Rotating ...
Fan rotor blade of the present invention provides (1) includes a blade body (10), which is formed by a fiber reinforced resin composite material, having a side facing the direction of rotation of the pressure surface (10a) and facing the rotational direction of the other negative pressure ...
FanLPCHPCHPTLPT Journeythroughajetengine 1/Confidential/ 17.04.2020 DataforTurbineBlades •HighTemperature:~1400oC •HighPressure:~40atm •HighRotatingSpeed:~11,000rpm •Centrifugalforce,airflowimpactandvibration •Oxidationanderosion •ThermalMechanicalCycling HPTbladelifetime:•Currently:16,000...
航空发动机叶片热障涂层技术Aircraft_Enginer_TBC_benchmark 系统标签: benchmark热障tbcenginer航空发动机ebpvd 1/Confidential/3/2/2015TechBenchmarkTurbineBladesCoatingHighTempProtectiveCoatingtechforSXTurbineBlades2/Confidential/3/2/2015OperatingConditionofTurbineBladesJourneythroughajetengineFanLPCHPCHPTLPT3/Confident...
Effective fan blade inspection demands advanced metrology solutions to comprehensively test the complex geometries, functionality, and material integrity. Discover more Compressor blade Achieving efficiency in engine design Comprehensive compressor blade inspection necessitates precise measurements to thorough...
Inst Univ of Virginia* Novel TBC material, microstructure Spallation model, lifetime prediction Failure analysis, bondcoat modification Morphology, porosity Process para, material EBDVD, systematical exp&simulation Industrial USA UK USA USA USA Germany GE Aircraft Engine Rolls-Royce (England) Prat&...
FAN ROTOR BLADE OF AIRCRAFT JET ENGINE 专利名称：FAN ROTOR BLADE OF AIRCRAFT JET ENGINE 发明人：YAGI, Hiroyuki,KUROKI, Hiroshi,OBUCHI, Kenro 申请号：EP13742850.4 申请日：20130130 公开号：EP2811143B1 公开日：20190828 专利内容由知识产权出版社提供 摘要：A fan rotor blade (1) includes a blade ...
3.The electric fan module according to claim 2, each wherein the radially outer end of each vane constitutes an extension which follows a chord at a tip of a blade of said vane. 4.The electric fan module according to claim 3, wherein the annular wall of the removable annulus is an as...