This paper describes environmental effects which impact the design of interfaces to fiber-optic sensors and data buses in aircraft engine controls. Emphasis is placed on selection of components and designs which maintain their performance and reliability in the harsh environment of an electronics enclosure mounted on a modern aircraft turbine engine. Particular attention is given to the effects of temperature on electro-optical component and system performance. The main conclusion is that electro-optical interfaces to a variety of fiber-optic systems can be installed in an engine-mounted control if the designs and components are selected after careful analysis of the effects of the engine environment.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Fiber-Optic Circuits For Aircraft Engine Controls


    Beteiligte:

    Kongress:

    Fiber Optic Systems for Mobile Platforms ; 1986 ; San Diego,CA,United States


    Erschienen in:

    Erscheinungsdatum :

    03.12.1987





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Fiber optic sensing for engine and flight controls

    Emo, S.M. / Gustus, J. | IEEE | 1993


    Fiber optic controls for aircraft engines: issues and implications

    Dasgupta, Samhita / Poppel, Gary L. / Anderson, William P. | SPIE | 1991