Results 1 to 10 of about 46,539 (155)

Numerical investigation on the influence of nonuniform tip clearance on rotor tip-clearance flow field structure [PDF]

open access: yesHeliyon
A numerical study was conducted on an axial compressor, the NASA Stage 35, with three nonuniform tip clearances to understand the effect of a different shape tip clearances rotor on the compressor's performance. The results demonstrated that by modifying
Guochen Zhang   +4 more
doaj   +4 more sources

Mixing Performance of the Modified Tesla Micromixer with Tip Clearance [PDF]

open access: yesMicromachines, 2022
A passive micromixer based on the modified Tesla mixing unit was designed by embedding tip clearance above the wedge-shape divider, and its mixing performance was simulated over a wider range of the Reynolds numbers from 0.1 to 80. The mixing performance
Makhsuda Juraeva, Dong-Jin Kang
doaj   +4 more sources

An Optical Fiber Bundle Sensor for Tip Clearance and Tip Timing Measurements in a Turbine Rig [PDF]

open access: yesSensors, 2013
When it comes to measuring blade-tip clearance or blade-tip timing in turbines, reflective intensity-modulated optical fiber sensors overcome several traditional limitations of capacitive, inductive or discharging probe sensors. This paper presents the signals and results corresponding to the third stage of a multistage turbine rig, obtained from a ...
Iker Garcia   +2 more
exaly   +6 more sources

Numerical investigation of tip clearance effects on the performance of ducted propeller

open access: yesInternational Journal of Naval Architecture and Ocean Engineering, 2015
Tip clearance loss is a limitation of the improvement of turbomachine performance. Previous studies show the Tip clearance loss is generated by the leakage flow through the tip clearance, and is roughly linearly proportional to the gap size.
Ding Yongle, Song Baowei, Wang Peng
doaj   +3 more sources

Review of research on tip-timing and tip clearance measurement technology

open access: yesJournal of Hebei University of Science and Technology, 2021
Turbine blades will fail due to fatigue fracture caused by vibration at high-speed rotation,resulting in damage of rotating machinery.Blade tip-timing measurement technology is the most promising non-contact blade vibration real-time monitoring method at
Liang ZHANG   +3 more
doaj   +2 more sources

Numerical investigations of tip clearance flow characteristics of a pumpjet propulsor

open access: yesInternational Journal of Naval Architecture and Ocean Engineering, 2018
In this study, numerical investigations of the tip clearance flow characteristics of a pumpjet propulsor based on Computational Fluid Dynamics (CFD) method have been presented.
Lin Lu, Yuefei Gao, Qiang Li, Lin Du
doaj   +3 more sources

Energy Performance and Flow Patterns of a Mixed-Flow Pump with Different Tip Clearance Sizes

open access: yesEnergies, 2017
Tip clearance between blade end and shroud is inevitable in pump operation and of great importance on pump energy performance and pressure fluctuation. As the tip clearance size increases, the head and efficiency of the mixed flow pump drop accordingly ...
Yabin Liu, Lei Tan, Yue Hao, Yun Xu
doaj   +3 more sources

Experimental Investigation of High Temperature-Resistant Inductive Sensor for Blade Tip Clearance Measurement [PDF]

open access: yesSensors, 2018
Turbine tip clearance of aero-engine is important to engine performance. Proper control of rotor tip clearance contributes to engine efficiency improvement and fuel consumption reduction. Therefore, accurate tip clearance measurement is essential.
Ziyu Zhao   +3 more
doaj   +2 more sources

Blade by Blade Tip Clearance Measurement [PDF]

open access: yesInternational Journal of Rotating Machinery, 2011
This paper describes a capacitance-based tip clearance measurement system which engineers have used in the most demanding turbine test applications.
A. G. Sheard
doaj   +2 more sources

Tip Clearance Flows in Turbine Cascades

open access: yesChinese Journal of Aeronautics, 2008
AbstractThis article describes the effects of some factors on the tip clearance flow in axial linear turbine cascades. The measurements of the total pressure loss coefficient are made at the cascade outlets by using a five-hole probe at exit Mach numbers of 0.10, 0.14 and 0.19.
Wei, Li, Weiyang, Qiao, Dawei, Sun
exaly   +2 more sources

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