B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01)
Patent
CA 2576100
The invention relates to a turbojet pylon for an aircraft, comprising a rigid structure (10) which is equipped with a plurality of half-rings (30) that are arranged such as to define part of an essentially-cylindrical imaginary surface (32) with a circular cross-section. The aforementioned half-rings include two lateral thrust-bearing half-rings (28) which are disposed on either side of a central casing (20). Each of said two lateral half-rings (28) is solidly connected to (i) each half-ring taking the form of an annular segment (26) that is centred on the longitudinal axis of the imaginary surface and (ii) the central casing.
L'invention se rapporte à un mât d'accrochage de turboréacteur pour aéronef, le mât disposant d'une structure rigide (10) munie d'une pluralité d'arceaux (30) agencés de façon à délimiter conjointement une partie d'une surface fictive (32) sensiblement cylindrique de section circulaire. La pluralité d'arceaux comporte notamment deux arceaux latéraux de reprise des efforts de poussée (28) disposés respectivement de part et d'autre d'un caisson central (20), chacun des deux arceaux latéraux (28) étant solidarisé d'une part à chaque arceau en forme de portion annulaire (26) centré sur l'axe longitudinal de la surface fictive, et d'autre part au caisson central.
Diochon Lionel
Durand Jerome
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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