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    Conceptual Design of an Optic-Based Engine Control System

    Source: Journal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 001::page 28
    Author:
    W. J. Davies
    ,
    R. A. Baumbick
    ,
    R. W. Vizzini
    DOI: 10.1115/1.3240082
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Advanced integrated flight and propulsion control systems may require the use of optic technology to provide enhanced electromagnetic immunity and reduced weight. Immunity to electromagnetic interference and pulses is required for integrated systems where flight and propulsion control systems communicate with each other and diverse systems located throughout a composite aircraft. Weight reduction is crucial to the complex engine control systems required for advanced engines incorporating diagnostics, variable geometry and vectoring/reversing exhaust nozzles. A team of Pratt & Whitney, McDonnell Aircraft, Hamilton Standard, and United Technologies Research Center have developed the conceptual design of an optic engine control system, under a contract from NASA Lewis, entitled Fiber Optic Control System Integration (FOCSI). FOCSI is a triservice/NASA joint program designed to provide the optic technology requirements for advanced fighter/attack aircraft.
    keyword(s): Control systems , Engines , Conceptual design , Aircraft , Weight (Mass) , Propulsion , Flight , Nozzles , Integrated systems , Composite materials , Fibers , Electromagnetic interference , Exhaust systems , Geometry AND Teams ,
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      Conceptual Design of an Optic-Based Engine Control System

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/103911
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorW. J. Davies
    contributor authorR. A. Baumbick
    contributor authorR. W. Vizzini
    date accessioned2017-05-08T23:27:10Z
    date available2017-05-08T23:27:10Z
    date copyrightJanuary, 1988
    date issued1988
    identifier issn1528-8919
    identifier otherJETPEZ-26651#28_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103911
    description abstractAdvanced integrated flight and propulsion control systems may require the use of optic technology to provide enhanced electromagnetic immunity and reduced weight. Immunity to electromagnetic interference and pulses is required for integrated systems where flight and propulsion control systems communicate with each other and diverse systems located throughout a composite aircraft. Weight reduction is crucial to the complex engine control systems required for advanced engines incorporating diagnostics, variable geometry and vectoring/reversing exhaust nozzles. A team of Pratt & Whitney, McDonnell Aircraft, Hamilton Standard, and United Technologies Research Center have developed the conceptual design of an optic engine control system, under a contract from NASA Lewis, entitled Fiber Optic Control System Integration (FOCSI). FOCSI is a triservice/NASA joint program designed to provide the optic technology requirements for advanced fighter/attack aircraft.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleConceptual Design of an Optic-Based Engine Control System
    typeJournal Paper
    journal volume110
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3240082
    journal fristpage28
    journal lastpage32
    identifier eissn0742-4795
    keywordsControl systems
    keywordsEngines
    keywordsConceptual design
    keywordsAircraft
    keywordsWeight (Mass)
    keywordsPropulsion
    keywordsFlight
    keywordsNozzles
    keywordsIntegrated systems
    keywordsComposite materials
    keywordsFibers
    keywordsElectromagnetic interference
    keywordsExhaust systems
    keywordsGeometry AND Teams
    treeJournal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 001
    contenttypeFulltext
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