Results 61 to 70 of about 44,613 (142)
The operation of gas turbine engines inevitably increases the blade roughness and tip clearance in multistage axial compressors. The result is an increase in its thermogasodynamic parameters. The reason for the increase in the roughness of the blades and
Vadym Datsenko
doaj +1 more source
The clearance existing between the impeller rim and the adjacent shroud within the pump configuration establishes conducive circumstances for the initiation of cavitation. The bubbles generated by cavitation will flow forward with the water, blocking the
Lei Yu +3 more
doaj +1 more source
The complex tip flow instability and its induced non-synchronous vibration have become significant challenges, especially as aerodynamic loading continues to increase.
Songbai Wang, Yong Chen, Yadong Wu
doaj +1 more source
Creep-Based Reliability Evaluation of Turbine Blade-Tip Clearance with Novel Neural Network Regression. [PDF]
Zhang CY +5 more
europepmc +1 more source
Design, Fabrication and Testing of a High-Sensitive Fibre Sensor for Tip Clearance Measurements. [PDF]
Durana G +6 more
europepmc +1 more source
The axial tip clearance leakage analysis of the squealer blade tip for the liquid-ring pump. [PDF]
Wei X, Guo X, Zhou C, Zhang T, Wang W.
europepmc +1 more source
Eddy Current Sensor System for Blade Tip Clearance Measurement Based on a Speed Adjustment Model. [PDF]
Wu J +6 more
europepmc +1 more source
High-temperature resistant resonant cavity microwave sensor for precision blade tip clearance monitoring in aeroengines. [PDF]
Sun H.
europepmc +1 more source
A Blade Defect Diagnosis Method by Fusing Blade Tip Timing and Tip Clearance Information. [PDF]
Zhang JW, Zhang LB, Duan LX.
europepmc +1 more source

