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.


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    Titel :

    Sound suppression mixer


    Beteiligte:

    Erscheinungsdatum :

    08.03.1994


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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