公开(公告)号：US09481443B2

公开(公告)日：2016-11-01

申请号：US14445537

申请日：2014-07-29

Applicant: Airbus Operations S.L.

Inventor： Alfonso Gonzalez Gozalbo ,  Raul Carlos Llamas Sandin

IPC: B64C1/06 ,  B64C1/10 ,  B64C1/26 ,  B64C7/00 ,  B64C9/00 ,  B64C25/00 ,  B64C5/02 ,  B64C5/16

CPC classification number: B64C1/068 ,  B64C1/10 ,  B64C1/26 ,  B64C5/02 ,  B64C5/16 ,  B64C7/00 ,  B64C9/00 ,  B64C25/00 ,  B64C2025/005

Abstract: A rear fuselage section of an aircraft comprises at least one closed frame constructed as a unitary body, and a horizontal tail plane comprising a box-type central element and two lateral torsion boxes, said horizontal tail plane trimmable with respect to a pivot axis. The horizontal tail plane is mounted at the closed frame and the pivot axis is contained in a horizontal plane below the lowest end of said closed frame.

Abstract translation: 飞行器的后部机身部分包括构造为整体的至少一个封闭框架，以及包括箱型中心元件和两个横向扭转箱的水平尾翼平面，所述水平尾翼平面相对于枢转轴线可修剪。 水平尾翼平面安装在闭合的框架上，枢转轴线包含在所述闭合框架的最下端下方的水平平面内。

公开(公告)号：US20150034765A1

公开(公告)日：2015-02-05

申请号：US14445537

申请日：2014-07-29

Applicant: Airbus Operations S.L.

Inventor： Alfonso Gonzalez Gozalbo ,  Raul Carlos Llamas Sandin

IPC: B64C1/06 ,  B64C25/00 ,  B64C7/00 ,  B64C1/10 ,  B64C1/26 ,  B64C9/00

CPC classification number: B64C1/068 ,  B64C1/10 ,  B64C1/26 ,  B64C5/02 ,  B64C5/16 ,  B64C7/00 ,  B64C9/00 ,  B64C25/00 ,  B64C2025/005

Abstract: A rear fuselage section of an aircraft comprises at least one closed frame constructed as a unitary body, and a horizontal tail plane comprising a box-type central element and two lateral torsion boxes, said horizontal tail plane trimmable with respect to a pivot axis. The horizontal tail plane is mounted at the closed frame and the pivot axis is contained in a horizontal plane below the lowest end of said closed frame.

Abstract translation: 飞行器的后部机身部分包括构造为整体的至少一个封闭框架，以及包括箱型中心元件和两个横向扭转箱的水平尾翼平面，所述水平尾翼平面相对于枢转轴线可修剪。 水平尾翼平面安装在闭合的框架上，枢转轴线包含在所述闭合框架的最下端下方的水平平面内。