公开(公告)号：US10538308B2

公开(公告)日：2020-01-21

申请号：US15588332

申请日：2017-05-05

Applicant: AIRBUS OPERATIONS SL

Inventor： Carlos Garcia Nieto ,  Fernando Pereira Mosqueira ,  Iker Velez De Mendizabal Alonso ,  Enrique Guinaldo Fernandez ,  Francisco Javier Honorato Ruiz

IPC: B64C9/00 ,  B64C5/02 ,  B64C9/02

Abstract: An aircraft aerodynamic surface (1) including a torsion box (2) having a front spar (21) and rear spar (22), a first control surface (3) including a front spar (31) and a trailing edge (32) and a second control surface (4) having a front spar (41), a trailing edge (42), and a pivot device (5, 6, 7, 8) for pivotally attaching the first control surface (3) and the second control surface (4) to the rear spar (22) of the torsion box (2), the first control surface is an inboard control surface (4) including two lateral ribs (9, 9′), six inner ribs (11, 12, 13, 14, 15, 10) and an inner spar (16), and the second control surface (3) is an outboard control surface which includes two lateral ribs (20, 20′), three internal ribs (17, 18, 19), two internal spars (24, 24′) and one internal spar (23).