An airplane is provided. The airplane includes an environmental control system (100) that provides a pressurized medium to a chamber of the airplane. The airplane also includes a bleed system (400). The bleed system (400) includes a plurality of ports (415,420,425), each of which can provide a bleed medium from an engine of the airplane to the environmental control system (100). The plurality of ports includes at least a first port (415), a second port (420), and a third port (425). The first port (415) is selected for an idle condition. The second port (420) is selected for a hot day cruise condition. The third port (425) is selected for a standard operating condition. The bleed system (400) can operate in a first mode, a second mode, or a third mode to provide the bleed medium to the environmental control system from the first port (415), the second port (420), or the third port (425) respectively.
ECS WITH MULTIPLE OPERATION MODES AND METHOD
ECS MIT MEHREREN OPERATIONSMODI UND VERFAHREN
ECS AVEC PLUSIEURS MODES D'OPERATION ET PROCÉDÉ
2019-08-07
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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