Safran Power Units

Gilles Aime Yann Guyader

Victor Georges Maurice Lhomme

Franck Jean-Louis Galibert

Claire Madeleine Martin

A lubrication reservoir for a turbine engine for an aircraft or self-propelled flying machine, comprising a suction strainer in a lower part of the chamber, and at least one degassing device and at least one vent in an upper part. The reservoir is wherein, in order to make it possible to supply the strainer and prohibit lubricant from intruding into the at least one vent, it includes at least one first partition that separates the lower part from the upper part and is pierced with calibrated holes, two vents arranged on either side of a vertical median plane of the chamber and two vent ducts which extend into the upper part below the degassing device, each duct comprising a bend and having the bend located on the other side of the median plane with respect to the inlet thereof.

Growing community of inventors

Moissy-Cramayel, France

Gilles Aime Yann Guyader