Optimization of the Straight-Through Labyrinth Seal With a Smooth Land
Author:
Szymański Artur1, Wróblewski Włodzimierz2, Frączek Daniel2, Bochon Krzysztof2, Dykas Sławomir2, Marugi Krzysztof3
Affiliation:
1. Silesian University of Technology, Gliwice 44-100, Poland e-mails: ; 2. Silesian University of Technology, Gliwice 44-100, Poland e-mail: 3. Avio Poland, Bielsko-Biala 43-300, Poland e-mail:
Abstract
This paper presents the methodology and results of the optimization of a straight-through labyrinth seal with two inclined fins against smooth-land. The optimization was performed using commercial tools implemented in the ANSYS environment, such as goal-driven optimization. The response surfaces were created based on Latin hypercube samples found from computational fluid dynamics (CFD) calculations. The CFD solver, using a steady-state scheme with the k–ω shear stress transport (SST) turbulence model, was applied. A screening algorithm was used to find the best candidates on the response surfaces. The objective function adopted in the labyrinth seal optimization was the minimization of the discharge coefficient value. A wide range of parameters of the fins position and shape were taken into account, with physically justified degrees-of-freedom. The optimization results were supported by the results of an in-house experiment performed on a stationary, linear test rig. The test rig was fed by a high-capacity vacuum air blower with high-precision hot-wire anemometry mass flow evaluation. The reductions in the leakage significantly exceed the uncertainties of the CFD model and the test rig accuracy. The factors that had the most substantial impact on the leakage reduction were the location, inclination, and thickness of the fins. The experimental results were compared with the calculations and the optimization effects, highlighting some tendencies in the labyrinth seal flow behavior. Good agreement was obtained between the optimization results and the experimental data, proving that the presented methodology is sufficient for the labyrinth seal optimization.
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Reference26 articles.
1. Development of a Two Dimensional Computational Fluid Dynamics Approach for Computing Three-Dimensional Honeycomb Labyrinth Leakage;ASME J. Eng. Gas Turbines Power,2004 2. Paolillo, R., Wang, C. Z., Vashist, T. K., Cloud, D., Bingen, F. M. G., and Kool, G. A., 2006, “Rotating Seal Rig Experiments: Test Results and Analysis Modeling,” ASME Paper No. GT2006-90957.10.1115/GT2006-90957 3. Kang, Y., Kim, T. S., Kang, S. Y., and Moon, H. K., 2010, “Aerodynamic Performance of Stepped Labyrinth Seals for Gas Turbine Applications,” ASME Paper No. GT 2010-23256.10.1115/GT2010-23256 4. Micio, M., Facchini, B., Innocenti, L., and Simonetti, F., 2011, “Experimental Investigation on Leakage Loss and Heat Transfer in a Straight Through Labyrinth Seal,” ASME Paper No. GT2011-46402.10.1115/GT2011-46402 5. Szymański, A., Dykas, S., Wróblewski, W., Frączek, D., and Marugi, K., 2017, “Experimental and Numerical Validation Study of the Labyrinth Seal Configurations,” 12th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Stockholm, Sweden, Apr. 3–7, Paper No. ETC2017-340.https://www.researchgate.net/publication/317170032_Experimental_and_Numerical_Validation_Study_of_the_Labyrinth_Seal_Configurations
Cited by
14 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
|
|