公开(公告)号：US20160152315A1

公开(公告)日：2016-06-02

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 ,  B64C3/32 ,  B64C1/12

CPC classification number: B64C1/061 ,  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.

Abstract translation: 一种包括适于位于机身周边内的中心元件的飞行器机身框架，以及从作为提升表面的纵向结构的一部分的中心元件的两侧突出到机身的周边外侧的两个侧向延伸部。 中心元件和两个横向延伸部被配置为一体的部件。