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    PRESSURE FUSELAGE OF AN AIRCRAFT WITH A FUSELAGE SHELL AND A PRESSURE BULKHEAD DISPOSED THEREIN
    1.
    发明申请
    PRESSURE FUSELAGE OF AN AIRCRAFT WITH A FUSELAGE SHELL AND A PRESSURE BULKHEAD DISPOSED THEREIN 有权
    具有熔断壳的飞机的压力熔断器和其中的压力容器

    公开(公告)号：US20150008285A1

    公开(公告)日：2015-01-08

    申请号：US14491251

    申请日：2014-09-19

    Applicant: AIRBUS OPERATIONS GMBH

    Inventor： M. Ichwan Zuardy ,  Karim Grase ,  Carsten Rowedder ,  Claas DeJong ,  Markus Mueller ,  Mathias Jessrang

    IPC: B64C1/10

    CPC classification number: B64C1/10

    Abstract: A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.

    Abstract translation: 具有机身壳体和压力舱壁的飞机的压力舱壁优选地设置在后部区域中，用于形成机身内部压力区域，该压力舱壁附接在机身壳体内部的边缘上，其中压力舱壁 具有透镜状横截面和夹层结构，其包括夹在两个相对的外壳之间的泡沫芯。

    Method for producing a rail-shaped hybrid component, and such a hybrid component
    2.
    发明授权
    Method for producing a rail-shaped hybrid component, and such a hybrid component 有权

    公开(公告)号：US10472070B2

    公开(公告)日：2019-11-12

    申请号：US15598462

    申请日：2017-05-18

    Applicant: Airbus Operations GmbH

    Inventor： Johannes Born ,  Alexander Gillessen ,  Carsten Rowedder

    IPC: B64D11/06 ,  B64G1/60

    Abstract: In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component made of a titanium material is positioned on a first bar of a first profile rail that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction, in a fixed position relative to the first profile rail, such that a bar portion of the first bar is arranged between a first connecting portion of the second rail component and a second connecting portion of the second rail component, and the second rail component is cohesively connected to the first profile rail. Furthermore, the hybrid component has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.

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