Safran Aircraft Engines

Romain Harold Patrice Pou

Frédéric Dautreppe

Bertrand Romain Adrien Dufour

Frédéric Jacques Eugène Goupil

Plate of pieces of hydraulic equipment of an aeronautical turbomachine comprising channels for circulation of fluids entering and leaving each of the pieces of hydraulic equipment, on the one hand further comprising a support part of a housing body of each of the pieces of hydraulic equipment intended to receive fastening means to these pieces of hydraulic equipment and on the other hand a housing body part of at least one of these pieces of hydraulic equipment.

Hydraulic equipment plate for aeronautical turbomachine

The invention relates to a firewall () for a turbomachine () auxiliary arm (). This firewall (), which has one or more through openings () in a thickness direction (Z) of the firewall (), comprises a fixed portion () and a first removable portion () extending, in a width direction (Y), orthogonal to said thickness direction (Z), from at least one adjacent opening among the through openings (), to a first outer edge () of the firewall (). To open this firewall () in order to allow access to one or more ducts and/or electrical cables () received in the through openings (), the first removable portion () can be dismantled.

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Moissy-Cramayel, France

Romain Harold Patrice Pou