Numerical and Experimental Investigations on Windage Heating Effect of Labyrinth SealsSource: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005DOI: 10.1061/(ASCE)AS.1943-5525.0001175Publisher: ASCE
Abstract: The heat load caused by windage heating effect of labyrinth seals seriously influences the sealing of shaft air flow. To reveal the windage heating effect of labyrinth seals to reasonably design an aeroengine rotor, this paper studies the windage heating characteristics of labyrinth seals from theoretical, numerical, and experimental perspectives. First, the theoretical analysis of the windage heating effect of labyrinth is conducted, and the experimental platform of heating labyrinth was established to test the heating labyrinth effect. Then, an RNG k-ε turbulence model was adopted to investigate the characteristics of flow field, leakage characteristics, and windage heating characteristics of labyrinth seals. Last, the influences of pressure ratio, rotational speed and other factors on the windage heating characteristics of labyrinth seals were investigated by theoretical calculation, numerical simulation, and experiment. Through the comprehensive study, we find that: (1) windage heating is indeed induced when leakage flow absorbs the frictional heat caused by the rub of leakage flow with the rotor; (2) when the speed is lower than 1,000 rpm, the windage heating effect is small and enhances with the rise of rotation speed from 1,000−6,000 rpm, and the maximum increase of temperature reaches to 12.87 K; and (3) the pressure ratio increases from 1∶1 to 1∶3, and the temperature rise decreases by ∼7 K. The results of this paper offer a useful insight for the design of labyrinth seals with the emphasis on windage beating effect, to improve the performance of rotor seals.
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contributor author | Dan Sun | |
contributor author | Min Zhou | |
contributor author | Huan Zhao | |
contributor author | Jiang Lu | |
contributor author | Cheng-Wei Fei | |
contributor author | Huan Li | |
date accessioned | 2022-01-30T21:40:03Z | |
date available | 2022-01-30T21:40:03Z | |
date issued | 9/1/2020 12:00:00 AM | |
identifier other | %28ASCE%29AS.1943-5525.0001175.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4268631 | |
description abstract | The heat load caused by windage heating effect of labyrinth seals seriously influences the sealing of shaft air flow. To reveal the windage heating effect of labyrinth seals to reasonably design an aeroengine rotor, this paper studies the windage heating characteristics of labyrinth seals from theoretical, numerical, and experimental perspectives. First, the theoretical analysis of the windage heating effect of labyrinth is conducted, and the experimental platform of heating labyrinth was established to test the heating labyrinth effect. Then, an RNG k-ε turbulence model was adopted to investigate the characteristics of flow field, leakage characteristics, and windage heating characteristics of labyrinth seals. Last, the influences of pressure ratio, rotational speed and other factors on the windage heating characteristics of labyrinth seals were investigated by theoretical calculation, numerical simulation, and experiment. Through the comprehensive study, we find that: (1) windage heating is indeed induced when leakage flow absorbs the frictional heat caused by the rub of leakage flow with the rotor; (2) when the speed is lower than 1,000 rpm, the windage heating effect is small and enhances with the rise of rotation speed from 1,000−6,000 rpm, and the maximum increase of temperature reaches to 12.87 K; and (3) the pressure ratio increases from 1∶1 to 1∶3, and the temperature rise decreases by ∼7 K. The results of this paper offer a useful insight for the design of labyrinth seals with the emphasis on windage beating effect, to improve the performance of rotor seals. | |
publisher | ASCE | |
title | Numerical and Experimental Investigations on Windage Heating Effect of Labyrinth Seals | |
type | Journal Paper | |
journal volume | 33 | |
journal issue | 5 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)AS.1943-5525.0001175 | |
page | 9 | |
tree | Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005 | |
contenttype | Fulltext |