Disclosed is an egress pack for egressing a craft. The egress pack includes an egress aid defining a cavity and an inflation port. The egress pack includes an inflation duct connected with the inflation port for supplying gas to the cavity. The inflation duct defines a flow direction oriented to supply the cavity. The inflation duct defines a first ingress port defined by a first boundary and defining a primary flow path in the flow direction. The inflation duct defines a second ingress port defining a secondary flow path in fluid communication with the primary flow path. The inflation duct defines a divider disposed between the first ingress port and the second ingress port that coincides with the first boundary.


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    Title :

    AIRCRAFT EGRESS SYSTEM



    Publication date :

    2021-07-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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