Air-Conditioning System For An Aircraft
Air-Conditioning System For An Aircraft
- Neue Suche nach: HEUER THOMAS
- Neue Suche nach: BÄUMLE PATRICK
- Neue Suche nach: SCHERER THOMAS
- Neue Suche nach: HEUER THOMAS
- Neue Suche nach: BÄUMLE PATRICK
- Neue Suche nach: SCHERER THOMAS
An air-conditioning system for an aircraft has a fresh air line, a recirculation device, an air-mixing device, an air distribution system with multiple cabin air outlets, and a control unit. The control unit is designed to determine or to receive flight-specific parameters characterizing the flight state of the aircraft, and to determine or to receive environment-specific parameters which characterize an air quality in the environment of the aircraft. A first operating state of the air-conditioning system is brought about in the case of a predefined limit value of at least one environment-specific parameter being exceeded, and a second operating state of said system is brought about during a second flight state, which is outside the first flight state. In the second operating state, the fresh air line is fluidically connected to the air-mixing device, and in the first operating state, the fresh air line is separated from the air-mixing device.
Dokumentinformationen
Air-Conditioning System For An Aircraft
2019-05-30
Patent
Elektronische Ressource
Englisch
| IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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