A gas turbine engine flow mixer includes at least one chute having first and second spaced apart sidewalls joined together at a leading edge, with the sidewalls having first and second trailing edges defining therebetween a chute outlet. The first trailing edge is spaced longitudinally downstream from the second trailing edge for defining a septum in the first sidewall extending downstream from the second trailing edge. The septum includes a plurality of noise attenuating apertures.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Sound suppression mixer


    Contributors:

    Publication date :

    1994-03-08


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Mixer-ejector nozzle for jet noise suppression

    LORD, W. / JONES, C. / STERN, A. et al. | AIAA | 1990


    IN-SEAT SOUND SUPPRESSION

    SEFFERNICK DANIEL R / VANDE HEY PETER D | European Patent Office | 2019

    Free access

    In-seat sound suppression

    SEFFERNICK DANIEL R / VANDE HEY PETER D | European Patent Office | 2024

    Free access

    In-seat sound suppression

    SEFFERNICK DANIEL R / VANDE HEY PETER D | European Patent Office | 2025

    Free access

    IN-SEAT SOUND SUPPRESSION

    SEFFERNICK DANIEL R / VANDE HEY PETER D | European Patent Office | 2021

    Free access