Experimental Study on the Friction Contact Between a Labyrinth Seal Fin and a Honeycomb StatorSource: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 006::page 62501DOI: 10.1115/1.4031791Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents results from an extensive experimental study on the rubbing behavior of labyrinth seal fins (SFs) and a honeycomb liner. The objective of the present work is to improve the understanding of the rub behavior of labyrinth seals by quantifying the effects and interactions of sliding speed, incursion rate, seal geometry, and SF rub position on the honeycomb liner. In order to reduce the complexity of the friction system studied, this work focuses on the contact between a single SF and a single metal foil. The metal foil is positioned in parallel to the SF to represent contact between the SF and the honeycomb double foil section. A special test rig was set up enabling the radial incursion of a metal foil into a rotating labyrinth SF at a defined incursion rate of up to 0.65 mm/s and friction velocities up to 165 m/s. Contact forces, friction temperatures, and wear were measured during or after the rub event. In total, 88 rub tests including several repetitions of each rub scenario have been conducted to obtain a solid data base. The results show that rub forces are mainly a function of the rub parameters incursion rate and friction velocity. Overall, the results demonstrate a strong interaction between contact forces, friction temperature, and wear behavior of the rub system. The presented tests confirm basic qualitative observations regarding blade rubbing provided in literature.
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| contributor author | Pychynski, Tim | |
| contributor author | Hأ¶fler, Corina | |
| contributor author | Bauer, Hans | |
| date accessioned | 2017-05-09T01:28:32Z | |
| date available | 2017-05-09T01:28:32Z | |
| date issued | 2016 | |
| identifier issn | 1528-8919 | |
| identifier other | gtp_138_06_062501.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/161105 | |
| description abstract | This paper presents results from an extensive experimental study on the rubbing behavior of labyrinth seal fins (SFs) and a honeycomb liner. The objective of the present work is to improve the understanding of the rub behavior of labyrinth seals by quantifying the effects and interactions of sliding speed, incursion rate, seal geometry, and SF rub position on the honeycomb liner. In order to reduce the complexity of the friction system studied, this work focuses on the contact between a single SF and a single metal foil. The metal foil is positioned in parallel to the SF to represent contact between the SF and the honeycomb double foil section. A special test rig was set up enabling the radial incursion of a metal foil into a rotating labyrinth SF at a defined incursion rate of up to 0.65 mm/s and friction velocities up to 165 m/s. Contact forces, friction temperatures, and wear were measured during or after the rub event. In total, 88 rub tests including several repetitions of each rub scenario have been conducted to obtain a solid data base. The results show that rub forces are mainly a function of the rub parameters incursion rate and friction velocity. Overall, the results demonstrate a strong interaction between contact forces, friction temperature, and wear behavior of the rub system. The presented tests confirm basic qualitative observations regarding blade rubbing provided in literature. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Experimental Study on the Friction Contact Between a Labyrinth Seal Fin and a Honeycomb Stator | |
| type | Journal Paper | |
| journal volume | 138 | |
| journal issue | 6 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4031791 | |
| journal fristpage | 62501 | |
| journal lastpage | 62501 | |
| identifier eissn | 0742-4795 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 006 | |
| contenttype | Fulltext |