ENVIRONMENTAL CONTROL SYSTEM FOR USE IN AN AIRCRAFT

ENVIRONMENTAL CONTROL SYSTEM FOR USE IN AN AIRCRAFT

An environmental control system (102) for use in an aircraft includes at least one component (122) positioned along a length of the aircraft and a decompression panel (120) assembly comprising an array of apertures. The array of apertures is based on a location of the decompression panel (120) assem...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MAHRE, Megan E, MABEN, Douglas Dean, VANDYKE, Bryce Avery
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:An environmental control system (102) for use in an aircraft includes at least one component (122) positioned along a length of the aircraft and a decompression panel (120) assembly comprising an array of apertures. The array of apertures is based on a location of the decompression panel (120) assembly along the length of the aircraft relative to the at least one component (122).