公开(公告)号：US20160046392A1

公开(公告)日：2016-02-18

申请号：US14820792

申请日：2015-08-07

Applicant: Airbus Operations GmbH

Inventor： Eugen Gorr ,  Andreas Jespersen

IPC: B64F5/00 ,  B64C1/40 ,  B64C1/12 ,  B64D11/00 ,  B64C1/20

CPC classification number: B64C1/12 ,  B64C1/20 ,  B64C1/40 ,  B64C2211/00 ,  B64D11/003 ,  B64D2011/0046 ,  B64F5/10

Abstract: A method for assembling an aircraft fuselage includes different steps. In a first step the secondary structural components and interior components are assembled to form a core structure. The core structure comprises a cabin floor, side wall panels and ceiling panels. In another step of the method a primary structure is arranged around the core structure to form a part of a fuselage.

Abstract translation: 一种组装飞机机身的方法包括不同的步骤。 在第一步骤中，二次结构部件和内部部件被组装以形成芯部结构。 核心结构包括一个机舱地板，侧壁板和天花板。 在该方法的另一步骤中，主结构布置在芯结构周围以形成机身的一部分。

公开(公告)号：US20140152159A1

公开(公告)日：2014-06-05

申请号：US14160966

申请日：2014-01-22

Applicant: Airbus Operations GmbH

Inventor： Uwe SCHNEIDER ,  Andreas Jespersen

IPC: B64D11/00 ,  A47B46/00

CPC classification number: B64D11/003 ,  A47B46/00 ,  Y02T50/46

Abstract: A storage compartment for a passenger cabin of an aircraft is provided. The storage compartment comprises a storage compartment body, a mounting, a fixing brace and a pull rod. The fixing brace is connected to a frame of the primary structure of an aircraft and to the mounting and takes up forces transversely to the direction of flight. The pull rod is connected to a stringer of the aircraft primary structure and also to the mounting and takes up forces in the direction of flight in such a way that even in the event of an impact event, only low torques are to be taken up by the supporting primary structure of the aircraft.

Abstract translation: 提供了一种用于飞机客舱的储藏室。 储藏室包括储藏室主体，安装件，固定支架和拉杆。 固定支架连接到飞行器的主要结构的框架并且安装并横向于飞行方向承受力。 拉杆连接到飞机初级结构的纵梁，并且还以安装方式并且沿着飞行方向占据力，使得即使在碰撞事件的情况下，只有低扭矩将被 飞机的辅助主体结构。

公开(公告)号：US09511863B2

公开(公告)日：2016-12-06

申请号：US14160966

申请日：2014-01-22

Applicant: Airbus Operations GmbH

Inventor： Uwe Schneider ,  Andreas Jespersen

IPC: B64C1/20 ,  B64D11/00 ,  A47B46/00

CPC classification number: B64D11/003 ,  A47B46/00 ,  Y02T50/46

Abstract: A storage compartment for a passenger cabin of an aircraft is provided. The storage compartment comprises a storage compartment body, a mounting, a fixing brace and a pull rod. The fixing brace is connected to a frame of the primary structure of an aircraft and to the mounting and takes up forces transversely to the direction of flight. The pull rod is connected to a stringer of the aircraft primary structure and also to the mounting and takes up forces in the direction of flight in such a way that even in the event of an impact event, only low torques are to be taken up by the supporting primary structure of the aircraft.

Abstract translation: 提供了一种用于飞机客舱的储藏室。 储藏室包括储藏室主体，安装件，固定支架和拉杆。 固定支架连接到飞行器的主要结构的框架并且安装并横向于飞行方向承受力。 拉杆连接到飞机初级结构的纵梁，并且还以安装方式并且沿着飞行方向占据力，使得即使在碰撞事件的情况下，只有低扭矩将被 飞机的辅助主体结构。

公开(公告)号：US20150090840A1

公开(公告)日：2015-04-02

申请号：US14494995

申请日：2014-09-24

Applicant: Airbus Operations GmbH

Inventor： Andreas Jespersen ,  Felix Harden ,  Juergen Klare

IPC: B64C1/14

CPC classification number: B64C1/1415

Abstract: A cargo door arrangement for an aircraft includes a fuselage portion, a cargo door and a locking mechanism. The fuselage portion includes a skin portion, at least one fuselage former and an opening. The cargo door includes at least one door former. The locking mechanism includes a first engagement element, a second engagement element and a connecting means. The first engagement element has a tapered portion and is rigidly connected to the door former. The second engagement element includes a tapered cavity having a shape matching the shape of the tapered portion and is rigidly connected the fuselage former. In the closed position the tapered portion is engageable with the cavity. The connecting means is adapted to rigidly connect in the closed position the door former to the first or second engagement element.

Abstract translation: 飞机的货物门装置包括机身部分，货物门和锁定机构。 机身部分包括皮肤部分，至少一个机身形成器和开口。 货门包括至少一个门形成器。 锁定机构包括第一接合元件，第二接合元件和连接装置。 第一接合元件具有锥形部分并且刚性地连接到门形成器。 第二接合元件包括具有与锥形部分的形状匹配的形状的锥形空腔，并且刚性地连接到机身形成器。 在关闭位置，锥形部分可与空腔接合。 连接装置适于在关闭位置中将门形成器刚性地连接到第一或第二接合元件。

公开(公告)号：US20230026741A1

公开(公告)日：2023-01-26

申请号：US17868162

申请日：2022-07-19

Applicant: Airbus Operations GmbH

Inventor： Scott Clair ,  Andreas Jespersen ,  Paul Jörn ,  Norbert Heltsch

IPC: B64C1/12 ,  B29C70/22 ,  B29C70/30

Abstract: A method for manufacturing a structural element for a fuselage of an aircraft. To improve the manufacture of structural elements, a method includes laying up textile material members on a mandrel to form a plurality of structural element preforms that are space apart along an extended direction of the mandrel. The structural element preforms form closed loops and are subsequently cured to obtain annular structural elements. The annular structural elements are used as basic building blocks for stiffening panel members or are directly used as structural frame elements reinforcing cut-outs in a fuselage for windows and/or doors.