公开(公告)号：US10124876B2

公开(公告)日：2018-11-13

申请号：US14952376

申请日：2015-11-25

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

Inventor： Esteban Martino Gonzalez ,  Diego Folch Cortes ,  Pablo Goya Abaurrea ,  Angel Pascual Fuertes ,  Sandra Linares Mendoza ,  Julien Guillemaut ,  Eric Bouchet ,  Jerome Colmagro ,  Jonathan Blanc

IPC: B64C1/06 ,  B64C1/12 ,  B64C1/16 ,  B64C1/26 ,  B64C3/32

Abstract: An aircraft fuselage frame including a central element adapted to be located within the perimeter of the fuselage, and two lateral extensions projecting outside the perimeter of the fuselage from both sides of the central element that are a portion of a longitudinal structure of a lifting surface. The central element and the two lateral extensions are configured as an integrated piece.

公开(公告)号：US20140131511A1

公开(公告)日：2014-05-15

申请号：US13942880

申请日：2013-07-16

Applicant: Airbus Operations S.L.

Inventor： Angel Pascual Fuertes ,  Sergio Rodriguez Sanchez

IPC: B64C3/40 ,  B64C39/12

CPC classification number: B64C3/40 ,  B64C3/10 ,  B64C5/02 ,  B64C5/04 ,  B64C39/12

Abstract: An aircraft lifting surface attached to the rear or frontal end of the aircraft fuselage with a variable sweep angle α in an inboard part and with a constant sweep angle α1 in an outboard part. The aircraft lifting surface can be for example a horizontal tail plane or a vertical tail plane attached to the rear end fuselage or a canard attached to the frontal end fuselage.

Abstract translation: 在机内部分附近具有可变的扫掠角α并且在外侧部分具有恒定的扫掠角α1的飞行器提升表面附接到飞行器机身的后部或前端。 飞机提升表面可以是例如附接到后端机身的水平尾翼平面或垂直尾翼平面，或者附着在前端机身上的卡车。