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    Brush Seals Used in Steam Environments—Chronological Wear Development and the Impact of Different Seal Designs

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 005::page 51901
    Author:
    Raben, Markus
    ,
    Friedrichs, Jens
    ,
    Helmis, Thomas
    ,
    Flegler, Johan
    DOI: 10.1115/1.4031531
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: During the last decades, turbo machine efficiency was considerably increased by using more efficient seals. Brush seals, as a compliant contacting filament seal, have become an attractive alternative to conventional labyrinth seals in the field of aircraft engines as well as in stationary gas and steam turbines. The aim of today's research related to brush seals is to understand the characteristics and their connections, in order to be able to make performance predictions, and to ensure the reliability over a defined operating period. The wear behavior is essentially influenced by frictional contacts at the sealtorotor interface during operation. For realistic investigations with representative circumferential velocities, the TU Braunschweig, Germany, operates a specially developed steam test rig which enables endurance investigations under varying operating steam conditions up to 50 bar and 450 آ°C. Wear measurements and the determination of seal performance characteristics, such as blow down and bristle stiffness, are enabled by an additional test facility, using pressurized cold air up to 8 bar as a working fluid. This work presents the chronological wear development on both rotor and seal sides in a steam test lasting 25 days or 11 days, respectively. Interruptions after stationary and transient intervals were made in order to investigate the degree of wear. Two different seal arrangements, a single tandem seal, and a twostage single seal arrangement, using different seal elements were considered. Besides a continuous wear development, the results clearly show that the abrasive wear of the brush seal and rotor is mainly caused by transient test operations, particularly by enforced contacts during shaft excursions. Despite the increasing wear to the brushes, all seals have shown a functioning radialadaptive behavior over the whole test duration with a sustained seal performance. Thereby, it could be shown that the twostage arrangement displays a load shift during transients, leading to a balanced loading and unloading status for the two single brush seals. From load sharing, and in comparison with the wear data of the tandem seal arrangement, it can be derived that the twostage seal is less prone to wear. However, the tandem seal arrangement, bearing the higher pressure difference within one configuration, shows a superior sealing performance under constant load, i.e., under stationary conditions.
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      Brush Seals Used in Steam Environments—Chronological Wear Development and the Impact of Different Seal Designs

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    http://yetl.yabesh.ir/yetl1/handle/yetl/161064
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    contributor authorRaben, Markus
    contributor authorFriedrichs, Jens
    contributor authorHelmis, Thomas
    contributor authorFlegler, Johan
    date accessioned2017-05-09T01:28:22Z
    date available2017-05-09T01:28:22Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_05_051901.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161064
    description abstractDuring the last decades, turbo machine efficiency was considerably increased by using more efficient seals. Brush seals, as a compliant contacting filament seal, have become an attractive alternative to conventional labyrinth seals in the field of aircraft engines as well as in stationary gas and steam turbines. The aim of today's research related to brush seals is to understand the characteristics and their connections, in order to be able to make performance predictions, and to ensure the reliability over a defined operating period. The wear behavior is essentially influenced by frictional contacts at the sealtorotor interface during operation. For realistic investigations with representative circumferential velocities, the TU Braunschweig, Germany, operates a specially developed steam test rig which enables endurance investigations under varying operating steam conditions up to 50 bar and 450 آ°C. Wear measurements and the determination of seal performance characteristics, such as blow down and bristle stiffness, are enabled by an additional test facility, using pressurized cold air up to 8 bar as a working fluid. This work presents the chronological wear development on both rotor and seal sides in a steam test lasting 25 days or 11 days, respectively. Interruptions after stationary and transient intervals were made in order to investigate the degree of wear. Two different seal arrangements, a single tandem seal, and a twostage single seal arrangement, using different seal elements were considered. Besides a continuous wear development, the results clearly show that the abrasive wear of the brush seal and rotor is mainly caused by transient test operations, particularly by enforced contacts during shaft excursions. Despite the increasing wear to the brushes, all seals have shown a functioning radialadaptive behavior over the whole test duration with a sustained seal performance. Thereby, it could be shown that the twostage arrangement displays a load shift during transients, leading to a balanced loading and unloading status for the two single brush seals. From load sharing, and in comparison with the wear data of the tandem seal arrangement, it can be derived that the twostage seal is less prone to wear. However, the tandem seal arrangement, bearing the higher pressure difference within one configuration, shows a superior sealing performance under constant load, i.e., under stationary conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBrush Seals Used in Steam Environments—Chronological Wear Development and the Impact of Different Seal Designs
    typeJournal Paper
    journal volume138
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4031531
    journal fristpage51901
    journal lastpage51901
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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