This document establishes standard gland design criteria and dimensions for static axial O-ring seal applications without anti-extrusion devices specifically for engines and engine control systems operating at a maximum pressure of 1500 psi (10345 kPa). NOTE: The criteria herein are similar, but not identical, to those in AS4716 and the legacy standard MIL-G-5514. This standard has been reformatted for ease of use, with no technical changes. NOTE: This standard was transferred from E-25 General Standards for Aerospace and Propulsion Systems Committee to the A-6C Seals Committee.


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    Titel :

    Static Axial O-Ring Seal Applications Without Anti-Extrusion Devices for Engine and Engine Control Systems


    Erscheinungsdatum :

    2020-11-09



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch