Flüssigkeitsbehälter für Flugzeuge.

摘要

The invention relates to a tank (1) for aircraft, such as for example a helicopter, of the type containing a fluid and provided with orifices (5) which are situated in its lateral band (1B) in the vicinity of its bottom (1C) and to which supply and return ducts of the fluid (6, 7, 8) are capable of being connected. …According to the invention, the tank (1) is noteworthy in that, in order to permit the said aircraft to carry out temporary flight phases under a negative charge factor, the said tank (1) comprises means (10) for slowing the displacement of the fluid (3) contained in the tank, in such a way that the fluid (3) moving from the bottom (1C) towards the top (1A) of the said tank during the said temporary flight phases by passing through the said means of slowing (10), remains in communication with the said orifices (5) during the duration of the said flight phases, avoiding air getting into the said ducts (6, 7, 8). ……