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    Engine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft

    Source: Journal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001::page 11
    Author:
    R. W. Cue
    ,
    D. E. Muir
    DOI: 10.1115/1.2906519
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The F404-GE-400 engines of the CF-18 aircraft are the first engines of the Canadian Forces to be maintained under a formal on-condition maintenance program. In support of this program, the Canadian Forces are developing advanced troubleshooting and performance monitoring procedures based on information recorded by the aircraft In-flight Engine Condition Monitoring System (IECMS). A suite of computer programs has been developed that enables maintenance personnel to access, display, and analyze in-flight event data recorded by the IECMS and to track the performance of individual engines based on “health indices” derived from the IECMS take-off ground roll recordings. The new techniques have been under evaluation at each of the CF-18 main operating bases for a period of approximately 14 months. Results to date indicate that the IECMS recordings provide a considerable amount of information of benefit to engine technicians and maintenance planners.
    keyword(s): Engines , Carbon fibers , Aircraft , Maintenance , Force , Flight , Computer software AND Condition monitoring ,
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      Engine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/108562
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. W. Cue
    contributor authorD. E. Muir
    date accessioned2017-05-08T23:35:33Z
    date available2017-05-08T23:35:33Z
    date copyrightJanuary, 1991
    date issued1991
    identifier issn1528-8919
    identifier otherJETPEZ-26683#11_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108562
    description abstractThe F404-GE-400 engines of the CF-18 aircraft are the first engines of the Canadian Forces to be maintained under a formal on-condition maintenance program. In support of this program, the Canadian Forces are developing advanced troubleshooting and performance monitoring procedures based on information recorded by the aircraft In-flight Engine Condition Monitoring System (IECMS). A suite of computer programs has been developed that enables maintenance personnel to access, display, and analyze in-flight event data recorded by the IECMS and to track the performance of individual engines based on “health indices” derived from the IECMS take-off ground roll recordings. The new techniques have been under evaluation at each of the CF-18 main operating bases for a period of approximately 14 months. Results to date indicate that the IECMS recordings provide a considerable amount of information of benefit to engine technicians and maintenance planners.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEngine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft
    typeJournal Paper
    journal volume113
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906519
    journal fristpage11
    journal lastpage19
    identifier eissn0742-4795
    keywordsEngines
    keywordsCarbon fibers
    keywordsAircraft
    keywordsMaintenance
    keywordsForce
    keywordsFlight
    keywordsComputer software AND Condition monitoring
    treeJournal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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