2.
    发明专利
    未知

    公开(公告)号:NO873227D0

    公开(公告)日:1987-08-03

    申请号:NO873227

    申请日:1987-08-03

    Abstract: A composite article includes a compressively stressed plating which provides increased static strength and fatigue life. In particular, a fan exit guide vane (1), made of a graphite fiber reinforced composite material and including a conductive plating (7), achieves a 380% increase in static load capability over an unplated composite vane and a low cycle fatigue life of over 1 million cycles through the application of a compressively stressed nickel plating (8) which produces a residual compressive stress state of between -5,000 and -15,000 psi.

    4.
    发明专利
    未知

    公开(公告)号:NO873227L

    公开(公告)日:1988-02-05

    申请号:NO873227

    申请日:1987-08-03

    Abstract: A composite article includes a compressively stressed plating which provides increased static strength and fatigue life. In particular, a fan exit guide vane (1), made of a graphite fiber reinforced composite material and including a conductive plating (7), achieves a 380% increase in static load capability over an unplated composite vane and a low cycle fatigue life of over 1 million cycles through the application of a compressively stressed nickel plating (8) which produces a residual compressive stress state of between -5,000 and -15,000 psi.

    GAS TURBINE ENGINE AIRFOILS
    8.
    发明专利

    公开(公告)号:GB2194553B

    公开(公告)日:1991-03-06

    申请号:GB8718302

    申请日:1987-08-03

    Abstract: A composite article includes a compressively stressed plating which provides increased static strength and fatigue life. In particular, a fan exit guide vane (1), made of a graphite fiber reinforced composite material and including a conductive plating (7), achieves a 380% increase in static load capability over an unplated composite vane and a low cycle fatigue life of over 1 million cycles through the application of a compressively stressed nickel plating (8) which produces a residual compressive stress state of between -5,000 and -15,000 psi.

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