Aircraft turbojet engine mount

Details Aircraft turbojet engine mount Aircraft turbojet engine mount

B - Operations, Transporting

64

D

B64D 27/18 (2006.01)

Patent

CA 2624457

The invention concerns a turbojet engine mounting structure for aircraft comprising a central structure box (22) formed by the assembly of two panels joined via transverse ribs (23), the mounting structure further comprising two lateral structure boxes (24a) secured to a front part of the structure box (22) and arranged on either side thereof, each lateral structure box being provided with a rear closure frame (46a). The invention is characterized in that one of the ribs (23) forming the structure box (22) is equipped with two lateral extensions (52a) formed integrally with said rib (23) and respectively projecting from the two side panels outwards of the structure box (22), the two extensions (52a) being fixedly mounted on the frame (46a) of both the lateral structure boxes respectively.

L'invention se rapporte à un mât d'accrochage de turboréacteur pour aéronef comportant un caisson central (22) formé par l'assemblage de deux panneaux latéraux raccordés par l'intermédiaire de nervures transversales (23), le mât comportant également deux caissons latéraux (24a) solidaires d'une partie avant du caisson (22) et disposés de part et d'autre de celui-ci, chaque caisson latéral disposant d'un cadre de fermeture arrière (46a). Selon l'invention, l'une des nervures (23) formant le caisson (22) est équipée de deux extensions latérales (52a) réalisées d'un seul tenant avec cette nervure (23) et faisant respectivement saillie des deux panneaux latéraux vers l'extérieur du caisson (22), les deux extensions (52a) étant montées fixement sur le cadre (46a) de l'un et l'autre des deux caissons latéraux, respectivement.

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