公开(公告)号：US20170066518A1

公开(公告)日：2017-03-09

申请号：US15259585

申请日：2016-09-08

Applicant: Airbus Operations SAS ,  Airbus Operations S.L.

Inventor： Guillaume Gallant ,  Jose Luis Martinez Munoz

IPC: B64C1/06 ,  B64D29/06 ,  B64D41/00 ,  B64C5/02

CPC classification number: B64C1/068 ,  B64C1/069 ,  B64C1/26 ,  B64C5/02 ,  B64C5/06 ,  B64D29/06 ,  B64D41/00 ,  B64D2041/002

Abstract: To optimize the structure of an aircraft tail section, an aircraft rear section comprises a fuselage section, a tail section, and a vertical stabilizer comprising a box-section structure which comprises a box-section upper part extending on the outside of the tail section, and a box-section lower part housed inside the tail section, such that the tail section is wholly supported by the box-section structure.

Abstract translation: 为了优化飞机尾部的结构，飞机后部包括机身部分，尾部和垂直稳定器，其包括箱部结构，该箱部结构包括在尾部的外侧延伸的箱部上部， 以及容纳在尾部内的箱部下部，使得尾部完全由箱部结构支撑。

公开(公告)号：US10967979B2

公开(公告)日：2021-04-06

申请号：US16067655

申请日：2016-12-22

Applicant: Airbus Operations S.L.

Inventor： Jose Luis Martinez Munoz

IPC: B64D27/02 ,  B64C5/02 ,  B64D27/10 ,  B64C5/16 ,  B64C5/18 ,  B64D27/00

Abstract: An aircraft with rear mounted engines, comprising a vertical tail plane and a horizontal tail plane, in which the engines are mounted on top of the horizontal tail plane, such that the horizontal tail plane comprises an inner fixed part attached to the fuselage of the aircraft, the inner fixed part comprising an elevator, and two outer movable parts, each one of the outer movable parts being located at each side end of the horizontal tail plane which is furthest away from the fuselage of the aircraft, such that both the inner fixed part and the outer movable parts are at least partially subjected to a flow coming from the engines when the engines are in use.