Safran Aircraft Engines

Franck Serge Jacques Liotte

Josselin Xavier Coupard

Alméric Pierre Louis Garnier

Tony Alain Roger Joël Lhommeau

François Maurice Marcel Demaison

Tony Alain Roger Joel Lhommeau

Yves Roland Crochemore

Almeric Pierre Louis Garnier

The invention relates to a device for connecting parts of an aircraft engine. The connection device comprises connectors suitable for connecting a first and a second part so as to establish a physical transfer link between these parts and means which enable it to monitor the state of the connection in particular by means of an impedance measurement carried out in a circuit formed by components integrated into said connectors.

Device for connecting parts of an aircraft engine and method for using same

Analysis device for detecting solid particles in suspension in a lubricant, the analysis device comprising one or more ferromagnetic solid particle sensors, one or more other sensors able to detect non-ferromagnetic solid particles, and one or more magnets. The ferromagnetic solid particle sensors are offset in a direction perpendicular to a main direction of flow of the lubricant in relation to the other sensors, and the magnets are arranged so as to attract ferromagnetic solid particles towards the sensors of ferromagnetic solid particles by drawing them away from the other sensors.

Analysis device for detecting solid particles in a lubricant

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MOISSY-CRAMAYEL, France

Franck Serge Jacques Liotte