CPC F01D 25/18 (2013.01) [B64D 27/10 (2013.01); B64D 27/24 (2013.01); F01D 15/10 (2013.01); B64D 2027/026 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2260/609 (2013.01)] | 11 Claims |
1. A turbogenerator for an aircraft comprising:
a turboshaft engine;
an electric generator comprising a rotor driven mechanically by the turboshaft engine and a stator supported by a casing of the electric generator;
wherein the turbogenerator comprises a static decanter of an air/oil mixture coming from the turboshaft engine, the static decanter being positioned around the casing of the electric generator.
|