Patent ID: 8672268
Filing Date: 2014-03-18
Classification: B64C

Abstract:
1. Aircraft structure that comprises a wing spar ( 10 ), with orbital frames ( 24 , 24 ′, 24 ″) arranged in transverse planes, right and left horizontal spars ( 26 ) connected to the wing spar ( 10 ) at the upper panel ( 14 ) of said spar respectively to the right and to the left of said spar, and for each right or left horizontal spar ( 26 ), a triangular panel ( 50 ) that comprises a wall ( 60 ), a first edge arranged at the horizontal spar ( 26 ), a second side arranged at the wing spar ( 10 ), and a third side at which a first rectilinear oblique reinforcement ( 62 ) connecting the horizontal spar ( 26 ) and the wing spar ( 10 ) is provided, wherein the triangular panel ( wherein junction points between the first and second rectilinear oblique reinforcement (