公开(公告)号：US20170001703A1

公开(公告)日：2017-01-05

申请号：US15201762

申请日：2016-07-05

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

Inventor： Jesús Javier VAZQUEZ CASTRO ,  Fernando PEREIRA MOSQUEIRA ,  Juan José GUTIERREZ SANTIAGO ,  Anthony LANGLEY ,  Guy TOTHILL ,  Davood SARCHAMY ,  Miguel MARÍN MUÑOS

IPC: B64C1/12 ,  B64C7/00 ,  B64C1/06

CPC classification number: B64C1/12 ,  B64C1/061 ,  B64C1/064 ,  B64C1/34 ,  B64C3/26 ,  B64C7/00 ,  B64C7/02

Abstract: An external part of an aircraft (such as a fairing) comprising a skin made with flexible materials attached to rigid supporting elements (such as longerons and frames) arranged in, at least, two directions. The skin comprises inner inflatable panels in all bays delimited by the rigid supporting elements and/or an external inflatable panel. The skin is joined to the supporting elements so that its external surface complies with aerodynamic requirements.

Abstract translation: 飞机（例如整流罩）的外部部件包括以柔性材料制成的皮肤，所述柔性材料连接到至少两个方向上布置的刚性支撑元件（例如龙骨和框架）。 皮肤包括由刚性支撑元件和/或外部可充气面板界定的所有托架中的内部充气面板。 皮肤被接合到支撑元件，使得其外表面符合空气动力学要求。