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    AIRCRAFT WING WITH TRAILING EDGE PANEL
    21.
    发明申请
    AIRCRAFT WING WITH TRAILING EDGE PANEL 有权

    公开(公告)号：US20220306274A1

    公开(公告)日：2022-09-29

    申请号：US17703733

    申请日：2022-03-24

    Applicant: Airbus Operations Ltd.

    Inventor： William Tulloch

    IPC: B64C3/18 ,  B64C3/14 ,  B64C3/28

    Abstract: An aircraft wing including a wingbox with an upper cover, a lower cover, and a rear spar. A lower trailing edge panel is provided with a leading edge attached to the wingbox. The wing includes a flap, a flap deployment mechanism which is configured to deploy the flap, and a fairing which covers the flap deployment mechanism. A first end of a link is pivotally attached to the lower trailing edge panel at a first pivot joint, and a second end of the link is pivotally attached to the fairing at a second pivot joint. The second pivot joint is lower than the first pivot joint.

    Wing arrangement for an aircraft
    22.
    发明授权
    Wing arrangement for an aircraft 有权

    公开(公告)号：US10994827B2

    公开(公告)日：2021-05-04

    申请号：US15979806

    申请日：2018-05-15

    Applicant: Airbus Operations GmbH ,  Airbus Operations Ltd

    Inventor： Christoph Winkelmann ,  Wilfried Ellmers ,  Stephen Briancourt ,  David Brakes

    IPC: B64C3/54 ,  B64C3/56 ,  F16B45/02

    Abstract: A wing arrangement for an aircraft, comprising a wing having a base section and a tip section pivotably connected to base section such that the tip section is pivotable about a pivot axis between a deployed position and a stowed position. The wing arrangement also comprises a latching arrangement which includes an engagement portion, a latching actuator selectively movable between a first actuator position and a second actuator position, an elastically deformable structure, and a latching element. When the tip section is pivoted from the stowed or deployed position into an engagement position, the elastically deformable structure is initially deformed, and as the tip section pivots further into the deployed or stowed position, the elastic deformation of the elastically deformable structure decreases.

    Latching device for a foldable wing arrangement
    23.
    发明授权
    Latching device for a foldable wing arrangement 有权

    公开(公告)号：US10597139B2

    公开(公告)日：2020-03-24

    申请号：US15619126

    申请日：2017-06-09

    Applicant: Airbus Operations GmbH ,  Airbus Operations Ltd.

    Inventor： Christoph Winkelmann ,  Johannes Rupp ,  Benjamin Bishop

    IPC: B64C3/56

    Abstract: A latching device for a wing including a support structure (29), a latching bolt (35) having a longitudinal axis (36) and being slidably supported by the support structure (29) such that the latching bolt (35) is movable between a retracted position and an extended position. The latching device (27) includes a first hydraulic actuator (47a) and a first connector assembly (38a) adapted to be connected to a first hydraulic system of an aircraft (1), and at least one second hydraulic actuator (47b) and a second connector assembly (38b) connected to a second hydraulic system. The first hydraulic actuator (47a) and the second hydraulic actuator (47b) are adapted to effect movement of the latching bolt (35) from the extended position into the retracted position independent of the other one of the at least one first hydraulic actuator (47a) and the at least one second hydraulic actuator (47b).

    Guiding device which is intended to be interposed between a device for fixing components of an assembly, and a device for protecting the fixing device
    26.
    发明授权
    Guiding device which is intended to be interposed between a device for fixing components of an assembly, and a device for protecting the fixing device 有权
    旨在夹在用于固定组件的部件的装置之间的引导装置和用于保护定影装置的装置

    公开(公告)号：US09011062B2

    公开(公告)日：2015-04-21

    申请号：US14265994

    申请日：2014-04-30

    Applicant: Airbus Operations (SAS) ,  Airbus Operations Ltd

    Inventor： Clement Chirol ,  Philip Cresswell ,  Florian Dapot

    IPC: F16B37/14 ,  F16B33/00 ,  B64D45/02 ,  F16B5/02 ,  F16B19/05 ,  F16B39/02

    CPC classification number: F16B33/004 ,  B64D45/02 ,  F16B5/025 ,  F16B19/05 ,  F16B33/02 ,  F16B37/14 ,  F16B39/025 ,  Y10T29/49925

    Abstract: An assembly comprising at least two non-metal components which are fixed to each other using at least one fixing system. The fixing system includes a fixing device with a fixing element which is provided with a head and a rod, and a crimping ring which is in contact with one of the components. A protection device is a part of the fixing system which delimits a cavity for confining gas around a portion of the device comprising the crimping ring. In order to improve the repeatability of the operation for positioning the protection device, a guiding device is provided which includes an assembly element on the portion of the fixing device, and an element for guiding the protection device.

    Abstract translation: 一种组件，其包括使用至少一个固定系统彼此固定的至少两个非金属部件。 固定系统包括具有固定元件的固定装置，该固定元件设置有头部和杆，以及与其中一个部件接触的压接环。 保护装置是定影系统的一部分，其限定用于围绕包括压接环的装置的一部分围绕气体的空腔。 为了提高用于定位保护装置的操作的重复性，提供了一种引导装置，其包括在固定装置的部分上的组件元件和用于引导保护装置的元件。

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