An aircraft battery exhaust system (10) comprises a fluid discharge opening (12) formed in an aircraft outer skin (14) and a fluid discharge line (16) having a first end connected to the fluid discharge opening (12) and a second end. A first fluid discharge branch line (18) has a first end connected to the second end of the fluid discharge line (16) and a second end connected to a first battery (20) in such a manner that a fluid leaking from the first battery (20) is directed into the first fluid discharge branch line (18). A second fluid discharge branch line (22) has a first end connected to the second end of the fluid discharge line (16) and a second end connected to a second battery (24) in such a manner that a fluid leaking from the second battery (24) is directed into the second fluid discharge branch line (22).
Aircraft battery exhaust system
Flugzeugbatterieentleerungssystem
Système d'échappement des batteries d'aéronef
11.11.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY |
DESIGN ASPECTS of AIRCRAFT EXHAUST SYSTEM
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