Improvements to the load introduction zone in the rear end of an aircraft comprising receiving elements of the loads of the horizontal and vertical tail stabilizers connected to structural elements wherein: a) said structural elements are the cladding, two contiguous load-bearing frames with a .PI. or omega cross-section and, at least, a third frame; b) the receiving element of the horizontal tail stabilizer load is a first fitting structured as a torque box, transversely arranged between said load-bearing frames and connected to them, and the receiving elements of the vertical tail stabilizer loads are some second fittings coupled to these frames; c) said frames and said first and second fittings are entirely made of composite material.
STRUCTURE OF THE LOAD INTRODUCTION ZONE IN THE REAR END OF AN AIRCRAFT
STRUCTURE DE LA ZONE D'INTRODUCTION DE CHARGES DANS LE FUSELAGE ARRIERE D'UN AERONEF
2017-02-21
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |