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    An Experimental Determination of Losses in a Three-Port Wave Rotor

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 004::page 833
    Author:
    J. Wilson
    DOI: 10.1115/1.2818476
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Wave rotors, used in a gas turbine topping cycle, offer a potential route to higher specific power and lower specific fuel consumption. In order to calculate this potential realistically, a knowledge of the loss mechanisms is required. The experiment reported here was designed as a statistical experiment to identify the losses due to finite passage opening time, friction, and leakage, using a three-port, flow divider, wave rotor cycle. Incidence loss was also found to be important. Rotors of 12 in. diameter were used, with two different lengths, 9 in. and 18 in., and two different passage widths, 0.25 in. and 0.54 in., in order to vary friction and opening time. To vary leakage, moveable end walls were provided so that the rotor to end wall gap could be adjusted. The experiment is described, and the results are presented, together with a parametric fit to the data.
    keyword(s): Waves , Rotors , Cycles , Leakage , Friction , Flow (Dynamics) , Gas turbines , Fuel consumption AND Mechanisms ,
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      An Experimental Determination of Losses in a Three-Port Wave Rotor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/120377
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. Wilson
    date accessioned2017-05-08T23:56:29Z
    date available2017-05-08T23:56:29Z
    date copyrightOctober, 1998
    date issued1998
    identifier issn1528-8919
    identifier otherJETPEZ-26785#833_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120377
    description abstractWave rotors, used in a gas turbine topping cycle, offer a potential route to higher specific power and lower specific fuel consumption. In order to calculate this potential realistically, a knowledge of the loss mechanisms is required. The experiment reported here was designed as a statistical experiment to identify the losses due to finite passage opening time, friction, and leakage, using a three-port, flow divider, wave rotor cycle. Incidence loss was also found to be important. Rotors of 12 in. diameter were used, with two different lengths, 9 in. and 18 in., and two different passage widths, 0.25 in. and 0.54 in., in order to vary friction and opening time. To vary leakage, moveable end walls were provided so that the rotor to end wall gap could be adjusted. The experiment is described, and the results are presented, together with a parametric fit to the data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Experimental Determination of Losses in a Three-Port Wave Rotor
    typeJournal Paper
    journal volume120
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818476
    journal fristpage833
    journal lastpage842
    identifier eissn0742-4795
    keywordsWaves
    keywordsRotors
    keywordsCycles
    keywordsLeakage
    keywordsFriction
    keywordsFlow (Dynamics)
    keywordsGas turbines
    keywordsFuel consumption AND Mechanisms
    treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 004
    contenttypeFulltext
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