Computational Fluid Dynamics Investigation of Labyrinth Seal Leakage Performance Depending on Mushroom Shaped Tooth WearSource: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 003::page 32503Author:Dogu, Yahya
,
Sertأ§akan, Mustafa C.
,
Bahar, Ahmet S.
,
Piںkin, Altuؤں
,
Arؤ±can, Ercan
,
Kocagأ¼l, Mustafa
DOI: 10.1115/1.4031369Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Conventional labyrinth seal applications in turbomachinery encounter a permanent teeth tip damage and wear during transitional operations. This is the dominant issue that causes unpredictable seal leakage performance degradation. Since the gap between the rotor and the stator changes depending on engine transitional operations, labyrinth teeth located on the rotor/stator wear against the stator/rotor. This wear is observed mostly in the form of the labyrinth teeth becoming a mushroom shape. It is known that, as a result of this tooth tip wear, leakage performance permanently decreases, which negatively affects the engine's overall efficiency. However, very limited information about leakage performance degradation caused by mushroom wear is available in open literature. This paper presents a study that numerically quantifies leakage values for various radii of mushroomshaped labyrinth teeth by changing toothsurface clearance, pressure ratio, number of teeth, and rotor speed. Analyzed parameters and their ranges are mushroom radius (R = 0–0.508 mm), clearance (cr = 0.254–2.032 mm), pressure ratio (Rp = 1.5–3.5), number of teeth (nt = 1–12), and rotor speed (n = 0–80 krpm). Computational fluid dynamics (CFD) analyses were carried out by employing compressible turbulent flow in 2D axisymmetrical coordinate system. CFD leakage results were also compared with wellknown labyrinth seal semiempirical correlations. Given a constant clearance, leakage increases with the size of the mushroom radius that forms on the tooth. This behavior is caused by less flow separation and flow disturbance, and the vena contracta effect for flow over the smoothly shaped mushroom tooth tip compared to the sharpedged tooth tip. This leakage increase is higher when the tooth tip wear is considered as an addition to the unworn physical clearance, since the clearance dominates the leakage. The leakage affected by the number of teeth was also quantified with respect to the mushroom radius. The rotational effect was also studied as a secondary parameter.
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| contributor author | Dogu, Yahya | |
| contributor author | Sertأ§akan, Mustafa C. | |
| contributor author | Bahar, Ahmet S. | |
| contributor author | Piںkin, Altuؤں | |
| contributor author | Arؤ±can, Ercan | |
| contributor author | Kocagأ¼l, Mustafa | |
| date accessioned | 2017-05-09T01:28:11Z | |
| date available | 2017-05-09T01:28:11Z | |
| date issued | 2016 | |
| identifier issn | 1528-8919 | |
| identifier other | GTP_138_03_032503.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/161027 | |
| description abstract | Conventional labyrinth seal applications in turbomachinery encounter a permanent teeth tip damage and wear during transitional operations. This is the dominant issue that causes unpredictable seal leakage performance degradation. Since the gap between the rotor and the stator changes depending on engine transitional operations, labyrinth teeth located on the rotor/stator wear against the stator/rotor. This wear is observed mostly in the form of the labyrinth teeth becoming a mushroom shape. It is known that, as a result of this tooth tip wear, leakage performance permanently decreases, which negatively affects the engine's overall efficiency. However, very limited information about leakage performance degradation caused by mushroom wear is available in open literature. This paper presents a study that numerically quantifies leakage values for various radii of mushroomshaped labyrinth teeth by changing toothsurface clearance, pressure ratio, number of teeth, and rotor speed. Analyzed parameters and their ranges are mushroom radius (R = 0–0.508 mm), clearance (cr = 0.254–2.032 mm), pressure ratio (Rp = 1.5–3.5), number of teeth (nt = 1–12), and rotor speed (n = 0–80 krpm). Computational fluid dynamics (CFD) analyses were carried out by employing compressible turbulent flow in 2D axisymmetrical coordinate system. CFD leakage results were also compared with wellknown labyrinth seal semiempirical correlations. Given a constant clearance, leakage increases with the size of the mushroom radius that forms on the tooth. This behavior is caused by less flow separation and flow disturbance, and the vena contracta effect for flow over the smoothly shaped mushroom tooth tip compared to the sharpedged tooth tip. This leakage increase is higher when the tooth tip wear is considered as an addition to the unworn physical clearance, since the clearance dominates the leakage. The leakage affected by the number of teeth was also quantified with respect to the mushroom radius. The rotational effect was also studied as a secondary parameter. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Computational Fluid Dynamics Investigation of Labyrinth Seal Leakage Performance Depending on Mushroom Shaped Tooth Wear | |
| type | Journal Paper | |
| journal volume | 138 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4031369 | |
| journal fristpage | 32503 | |
| journal lastpage | 32503 | |
| identifier eissn | 0742-4795 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 003 | |
| contenttype | Fulltext |