公开(公告)号：US20170058985A1

公开(公告)日：2017-03-02

申请号：US15247013

申请日：2016-08-25

Applicant: Airbus Operations S.L.

Inventor： Esteban MARTINO GONZALEZ ,  Andrea Iván MARASCO ,  Diego FOLCH CORTÉS ,  Javier TORAL VÁZQUEZ ,  Vasilis VOTSIOS ,  Raúl FERNANDEZ BALLESTEROS ,  Fernando PEREIRA MOSQUEIRA

IPC: F16F7/12 ,  G10K11/16 ,  F16F7/00

CPC classification number: F16F7/12 ,  B29C44/357 ,  B29K2995/0002 ,  B29K2995/0091 ,  B29L2009/00 ,  B29L2031/30 ,  B29L2031/60 ,  B32B1/08 ,  B32B3/12 ,  B32B3/18 ,  B32B25/00 ,  B32B2250/03 ,  B32B2307/102 ,  B32B2307/51 ,  B32B2307/56 ,  B32B2307/734 ,  B32B2605/18 ,  F16F3/00 ,  F16F7/00 ,  F16F7/121 ,  G10K11/16

Abstract: A deformable structure, such as a panel or a shock absorber, for absorbing energy from a mechanical and/or acoustic impact. The structure comprises an inner core and one or more external layers covering the inner core. The inner core comprises a set of first segments having a positive Poison's ratio and second segments having a negative Poisson's ratio. The first and second segments are arranged alternately and joined to one another so that the deformation received by one first segment is transmitted to an adjacent second segment and vice versa.

Abstract translation: 用于从机械和/或声学冲击中吸收能量的可变形结构，例如面板或减震器。 该结构包括内芯和覆盖内芯的一个或多个外层。 内芯包括具有正毒力比的一组第一段和具有负泊松比的第二段。 第一和第二段交替地布置并且彼此连接，使得由一个第一段接收的变形被传递到相邻的第二段，反之亦然。

公开(公告)号：US20170158304A1

公开(公告)日：2017-06-08

申请号：US15366126

申请日：2016-12-01

Applicant: AIRBUS OPERATIONS S.L.

Inventor： Jesús Javier VÁZQUEZ CASTRO ,  Fernando PEREIRA MOSQUEIRA

IPC: B64C1/10 ,  B64C1/34

CPC classification number: B64C1/10 ,  B64C1/34 ,  B64C2001/0072

Abstract: A pressure bulkhead for an aircraft comprising a fuselage. The pressure bulkhead comprises an inflatable element, suitable for being filled with air, which in turn comprises a cover which delimits an inner zone. The pressure bulkhead further comprises a seal suitable for providing an airtight seal between the cover and the fuselage of the aircraft.

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。

公开(公告)号：US20150183508A1

公开(公告)日：2015-07-02

申请号：US14584480

申请日：2014-12-29

Applicant: AIRBUS OPERATIONS S.L.

Inventor： Andrea Ivan MARASCO ,  Fernando PEREIRA MOSQUEIRA ,  Enrique GUINALDO FERNÁNDEZ ,  Carlos GARCÍA NIETO ,  Francisco Javier HONORATO RUIZ ,  Francisco José CRUZ DOMÍNGUEZ

IPC: B64C5/02 ,  B64C3/18

CPC classification number: B64C5/02 ,  B64C3/18

Abstract: Horizontal tail plane of an aircraft which comprises a single torsion box which also comprises a front spar (1), a rear spar (2), an upper cover and a lower cover, ribs and two closing ribs (3), the front spar (1), the rear spar (2) and the upper and lower covers extending between said two closing ribs (3) and along the whole span of the horizontal tail plane in a symmetric layout with respect to the symmetry axis of the aircraft.

Abstract translation: 飞机的水平尾翼平面包括一个单一的扭转箱，它还包括前翼梁（1），后翼梁（2），上盖和下盖，肋和两个关闭肋（3），前翼梁 后翼梁（2）和上盖和下盖在所述两个关闭肋（3）之间延伸并且沿着相对于飞行器的对称轴线的对称布局沿着水平尾翼平面的整个跨度延伸。