A cabin air compressor (CAC) motor cooling flow enhancement cowl includes a cowl body (204) contoured to extend from a CAC motor cooling duct discharge (156) of a ram air outlet header (108). The cowl body includes a backward facing step (206) to form an air dam in a ram air flow path to divert ram system air away from the CAC motor cooling duct discharge. The CAC motor cooling flow enhancement cowl also includes a coupling interface (308) formed at an upstream end of the cowl body to engage with a transition edge (162) of the CAC motor cooling duct discharge.
CABIN AIR COMPRESSOR MOTOR COOLING FLOW ENHANCEMENT COWL
VERKLEIDUNG ZUR STRÖMUNGSVERBESSERUNG DER KÜHLUNGSLUFT DES KABINENLUFTKOMPRESSOR-MOTORS
CARÉNAGE POUR AMÉLIORATION DU FLUX D'AIR POUR REFROIDISSEMENT DU MOTEUR DU COMPRESSEUR D'AIR DE LA CABINE
2021-01-06
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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