To eliminate the hazards associated with hydraulic fluid fires resulting from aircraft accidents and component failures, the Air Force established a program to develop a nonflammable aircraft hydraulic system using a nonflammable fluid over the -45\mDC to 135\mDC (-65\mDF to 275\mDF) temperature range. The Air Force is developing a chlorotrifluoroethylene oligomeric based fluid, compatible elastomeric seals, and necessary hydraulic component/system redesign. The status of this program is discussed which includes a summary of the flammability tests, fluid and seal development and performance testing of candidate materials in hydraulic components/systems.


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    Titel :

    Nonflammable Aircraft Hydraulic Systems Development


    Weitere Titelangaben:

    Sae Technical Papers



    Kongress:

    SAE International Congress and Exposition ; 1982



    Erscheinungsdatum :

    01.10.1982




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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