عنوان

Computational Investigation of Cavitation Performance and Heat Transfer in Cryogenic Centrifugal Pumps with Helical Inducers

Number

TLpq2275500485

.Language of Text, Soundtrack etc

انگلیسی

Title Proper

Computational Investigation of Cavitation Performance and Heat Transfer in Cryogenic Centrifugal Pumps with Helical Inducers

General Material Designation

[Thesis]

First Statement of Responsibility

Karakas, Enver Sinan

Subsequent Statement of Responsibility

Evrensel, Cahit A.

Name of Publisher, Distributor, etc.

University of Nevada, Reno

Date of Publication, Distribution, etc.

2019

Specific Material Designation and Extent of Item

161

Dissertation or thesis details and type of degree

Ph.D.

Body granting the degree

University of Nevada, Reno

Text preceding or following the note

2019

Text of Note

In this dissertation, heat transfer and cooling mechanism of a cryogenic submerged pump motor, and cavitation behavior of a cryogenic pump are investigated. Cryogenic pumps for Liquefied Natural Gas (LNG) applications are unique in design with respect other industrial pump applications. The two distinct features of the cryogenic pumps are: (1) pump motor is submerged to process liquid for improved cooling, and (2) a helical style inducer is utilized at the suction side of the pump to enhance the cavitation performance. The first part of this dissertation investigates the cooling of the submerged induction motor considering normal operating conditions of a typical cryogenic pump to understand the effect of the motor rotor geometry. In this effort, the flow structure across the motor annulus, which is commonly known as "motor air gap", is investigated in the presence of realistic rotor geometries commonly found in practical applications. The purpose of this study is to observe and understand the fluid dynamics of Taylor-Couette-Poiseuille (TCP) flow and its significance to the cooling performance of the submerged motor, considering various configurations of the rotor surface. Computational Fluid Dynamics (CFD) simulations are conducted to determine the flow characteristic across the "motor air gap" and temperature distribution at the stator section of the motor. CFD simulations results are compared to temperature and flow calculations according to previously published TCP flow equations and dimensionless correlations. The entrance region is explored for each rotor geometry and its impact to overall cooling performance is discussed. It is concluded that while the rotor surface has modest effect to heat transfer, TCP flow characteristics differ for each geometric configuration. In addition, TCP flow and heat transfer correlations can predict the temperature profile, if the similarity between dimensionless parameters are obtained. In the second part of this dissertation, the cavitation performance of the cryogenic pump in terms of Net Positive Suction Head (NPSH) is investigated considering two different style helical inducers. The inducers utilized in cryogenic industrial pumps have open shroud design with a constant tip diameter. Due to the open shroud design, inducers tip clearance has an important role in cavitation performance due to possible back leakage through the gap. The effect of the tip clearance is investigated to understand the flow structure at the inducer tip location and its impact to cavitation performance. A constant pitch inducer and a variable pitch inducer are considered in the study of the tip clearance effect. CFD simulations are performed for various tip clearances. CFD simulation results are compared to actual test data to validate the simulation predictions. The objective of this research is not only to determine the tip clearance effect to the cavitation performance, but also to understand how the tip clearance can change the cavitation performance of different style inducers. A transport-equation based cavitation model based on Rayleigh-Plesset's bubble dynamics is implemented in the CFD code to explore the bubble dynamics and cavitation at the inducer and impeller eye sections. It is concluded that tip clearance plays an important role in cavitation performance and sensitivity to tip clearance in terms of cavitation performance is different for each style inducer. The third and last part of this dissertation is concerned with the review of four commonly used transport-equation based cavitation models. Comparison of these models and assessment of their applicability to predict cavitation performance of a cryogenic industrial pump with a variable pitch helical inducer are discussed in detail. To this aim, experimental results are compared to simulation findings to validate accuracy and assumptions of each model. Lastly, modifications to original empirical constants are proposed to obtain agreement with the actual cavitation and bubble dynamics observed during experimental testing. Two new sets of empirical constants are proposed to improve the prediction of cavitation in cryogenic pumps. Results show that with the new empirical constants, cavitation performance of a cryogenic pump with a helical inducer can be determined. It is shown that including the concentration of undissolved non-condensable gases and the turbulent pressure fluctuations in the models had no impact to the cavitation performance for this particular case.

Aerospace engineering

Fluid mechanics

Thermodynamics

Evrensel, Cahit A.

Karakas, Enver Sinan

Electronic name

p

[Thesis]

276903

a

Y