FASTENER SYSTEM
    41.
    发明公开
    FASTENER SYSTEM 审中-公开
    紧固件系统

    公开(公告)号:EP3122625A1

    公开(公告)日:2017-02-01

    申请号:EP15770358.8

    申请日:2015-03-25

    Inventor: MCCLURE, Richard

    Abstract: A fastener system that includes a female fastener assembly with a housing having a channel defined therein and a switch member movable within the channel between removing and fastening positions. The switch member includes a receiver portion having a post opening defined therein and a switch portion. The housing includes a lower opening. The post opening includes a removing portion that is aligned with the lower opening when the switch member is in the removing position and a fastening portion that is aligned with the post opening when the switch member is in the fastening position. The system also includes a male fastener assembly having a post with a slot therein. The post is received through the lower opening in the housing and the post opening so that the slot is aligned with the channel. The slot receives a portion of the receiver portion when the switch member is in the fastening position.

    Abstract translation: 一种紧固件系统,其包括阴型紧固件组件,该阴型紧固件组件具有壳体,该壳体具有限定在其中的通道和开关构件,开关构件可在通道内在移除和紧固位置之间移动。 开关构件包括具有限定于其中的柱开口的接收器部分和开关部分。 外壳包括一个下部开口。 柱开口包括当开关构件处于移除位置时与下开口对齐的移除部分和当开关构件处于紧固位置时与柱开口对齐的紧固部分。 该系统还包括具有其中具有狭槽的柱的雄紧固件组件。 通过外壳的下部开口和柱子开口接收柱子,使得槽子与通道对齐。 当开关构件处于紧固位置时,狭槽接收接收器部分的一部分。

    AIRCRAFT INTERIOR BRACKET
    44.
    发明公开
    AIRCRAFT INTERIOR BRACKET 审中-公开
    飞机内部CLAMP

    公开(公告)号:EP3068689A1

    公开(公告)日:2016-09-21

    申请号:EP14861422.5

    申请日:2014-11-13

    CPC classification number: F16B5/0614 F16B11/006 Y10T29/49895 Y10T29/49966

    Abstract: A bracket that includes a main body portion having a first portion and a second portion that form a first angle therebetween. The first portion includes opposing front and rear surfaces and the second portion includes opposing upper and lower surfaces. The first portion includes a fastener opening defined therethrough, the second portion includes an insert feature extending from the lower surface, and the second portion includes at least one adhesive opening defined therethrough.

    SEAT SHELL AND INTEGRATED OVERHEAD STORAGE BIN
    46.
    发明公开
    SEAT SHELL AND INTEGRATED OVERHEAD STORAGE BIN 有权
    座椅和集成存储TANK的头

    公开(公告)号:EP2694371A1

    公开(公告)日:2014-02-12

    申请号:EP12767726.8

    申请日:2012-04-04

    Inventor: SAVIAN, Scott

    Abstract: A lounge assembly configured to be positioned in the interior of an aircraft. The lounge assembly includes a first seat shell configured to at least partially surround a passenger seat, and an overhead storage bin assembly. The overhead storage bin assembly includes first and second posts configured to be secured to a floor of the aircraft, and an overhead bin housing supported by the first and second posts. The overhead bin housing includes at least a first overhead storage bin that is positioned generally above the first seat shell.

    AIRCRAFT LAVATORY DOOR LATCH
    47.
    发明公开

    公开(公告)号:EP3922789A1

    公开(公告)日:2021-12-15

    申请号:EP21181534.5

    申请日:2018-01-23

    Abstract: A door latch assembly (10) comprises a housing (12) that includes a housing interior, a switch member (14) operatively associated with the housing that is rotatable between a first position and a second position, a locking bolt (16) that is movable linearly between an unlocked position and a locked position, wherein rotation of the switch member from the first position to the second position moves the locking bolt from the unlocked position to the locked position, and an override assembly (50) that includes a main body portion and a finger lid (62) hingedly connected to the main body portion, wherein the finger lid is pivotable between a stowed position and a deployed position, wherein rotation of the finger lid from a first position to a second position moves the locking bolt from the unlocked position to the locked position.

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