Fluid machinery

Geometric Effects on Suction Recirculation, Cavitation, and Flow Instability of a Centrifugal Pump

A centrifugal pump may suffer severe degradation and failure when it operates at off-design conditions. In this device, three representative abnormal flow phenomena may appear: suction recirculation, cavitation, and flow instability. The suction recirculation is a phenomenon in which reverse flow and strong swirl flow develop upstream of the impeller in part-load conditions. Cavitation appears when the pressure of the liquid falls and vaporizes below the saturated pressure. Flow patterns become highly complex due to incidence or diffusion when the pump operates in part-load conditions. These finally lead to flow instability representing time-dependent unsteady characteristics. In this work, the parametric studies of the impeller and volute geometries were performed to control these flow phenomena. Also, surrogate-based optimization techniques were applied to establish the methodology of optimal pump design.

Related publications

Rotor-Stator (IGV-Rotor-Diffuser) Interaction of an Axial-Flow Pump

A submersible axial-flow pump consists of inlet guide vanes, rotor blades, and diffuser vanes to obtain hydrodynamic performance. Their relative motions may induce the rotor-stator interaction (RSI). RSI occurs when one rotor (or stator) blade passes through the wake of an upstream stator (or rotor) blade, it will clearly experience a fluctuation in the flow pattern and fluid forces. Indeed, the wakes from the upstream blades can cause a serious vibration problem for the downstream blades at blade passing frequency or some multiple thereof. This study numerically investigated the effects of the discharge angle of inlet guide vanes and the pitch angle of rotor blades on the hydrodynamic performance of a submersible axial-flow pump. Unsteady flow characteristics were also examined in off-design conditions considering the mutual effects of geometric parameters on RSI.

Related publications

Liquid Transport and Atomization of a Rotary Atomizer in a Gas Turbine Engine

A rotary atomizer transports the fluid from the internal reservoir toward the outside of the disk by centrifugal force. The liquid ejected by this device disperses in various forms like droplets, jets, ligaments, or thin film. The rotary atomizer can effectively supply atomized fuel into a slinger-typed combustor without a high-pressure source. On the other hand, this device has two major concerns: the atomization and transport of the fuel. Poor atomization may be achieved when the nozzle rotates at a low speed, deteriorating the ignition performance and combustion instability. Non-annular flow modes in the rotating pipe may cause uneven distributions of fuel along the circumference, resulting in the localized hot spot in the combustor. To overcome these problems, experimental studies were performed to investigate the liquid behaviors inside and outside the rotary slinger atomizer. 

Related publications