B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 13/40 (2006.01)
Patent
CA 2663628
The present invention provides a device and a method for regulating a temperature (T) of hydraulic fluid in at least one hydraulic circuit (2) of an aircraft (1). In this case the temperature (T) of the hydraulic fluid is regulated so that it is above an adjustable minimum temperature limit value {Tmin) of approximately 20°C, for example, at all times.
La présente invention concerne un dispositif et un procédé pour réguler une température (T) d'un fluide hydraulique dans au moins un circuit hydraulique (2) d'un avion (1). Dans ce cas, la température (T) du fluide hydraulique est régulée de telle sorte qu'elle se situe au-dessus d'une valeur limite de température minimale ajustable (Tmin) d'approximativement 20°C, par exemple, à tout instant.
Behr Robert
Goessing Rolf
Lauckner Sebastian
Laude Juergen
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
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