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
2015-11-11
Patent
Electronic Resource
English
IPC: | B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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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