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    PIVOT BIN ASSEMBLY
    72.
    发明公开
    PIVOT BIN ASSEMBLY 有权
    飞机的回转行李架安排

    公开(公告)号：EP2560874A1

    公开(公告)日：2013-02-27

    申请号：EP11772659.6

    申请日：2011-04-20

    Applicant: C&D Zodiac, Inc.

    Inventor： LEE, Nick ,  SAVIAN, Scott

    IPC: B64D11/00

    CPC classification number: B64D11/003 ,  Y02T50/46 ,  Y10T29/49826

    Abstract: A bin assembly that includes a bin housing and a bin that is pivotal between an open and a closed position within the bin housing. The bin housing includes a forward bulkhead panel, aft bulkhead panel and an aft housing panel that includes a rigid valence panel having one of a latch striker or a latch assembly secured thereto. The rigid valence panel has opposite ends that are secured to the forward and aft bulkhead panels. The bin includes an aft wall, a forward wall, a bin bottom and the other of a latch striker or a latch assembly secured to the bin bottom, thereby defining a latching location. A downward load in the bin is distributed from the latching location, along the rigid valence panel and to the aft and forward bulkhead panels.

    SEAT TRACK FITTINGS
    73.
    发明公开
    SEAT TRACK FITTINGS 审中-公开
    SEAT轨支座

    公开(公告)号：EP2252509A1

    公开(公告)日：2010-11-24

    申请号：EP09710634.8

    申请日：2009-02-13

    Applicant: Weber Aircraft LLC ,  C&D Zodiac, Inc.

    Inventor： YAMASAKI, Scott

    IPC: B64D11/06

    CPC classification number: B64D11/0696 ,  Y10T29/49826

    Abstract: Fittings (10) configured primarily, although not necessarily exclusively, for connection, to- aircraft seat tracks (T) are detailed. The fittings may engage multiple openings (38) of a seat track concurrently. No rotation of a fitting need occur when connecting it to a track. Instead, if desired the fitting need move only linearly.

    PIVOT BIN ASSEMBLY
    79.
    发明公开
    PIVOT BIN ASSEMBLY 审中-公开

    公开(公告)号：EP3412570A1

    公开(公告)日：2018-12-12

    申请号：EP18185344.1

    申请日：2015-07-10

    Applicant: C&D Zodiac, Inc.

    Inventor： SAVIAN, Scott

    IPC: B64D11/00

    CPC classification number: B64D11/003 ,  Y02T50/46

    Abstract: A dual pivot bin assembly comprising first and second aircraft storage bins, wherein the first and second aircraft storage bins are positioned adjacent one another; and an upper housing common to the first and second aircraft storage bins. Each of the first and second aircraft storage bins comprise a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior, wherein the bucket includes a bottom, a front edge and first and second opposing side walls extending upwardly from the bottom, wherein the bucket pivots about a pivot axis with respect to the upper housing between an open position and a closed position. When the storage bin is installed in an aircraft, a first horizontal distance is defined between a first vertical line that extends through the pivot axis and the front edge of the bucket when the bucket is in the closed position, and a second horizontal distance is defined between the first vertical line and the front edge of the bucket when the bucket is in the open position. The first horizontal distance is greater than the second horizontal distance. A center side panel having first and second opposite sides is positioned between the first and second aircraft storage bins, and wherein a first clevis assembly of the first aircraft storage bin is secured to the first side of the center side panel, and wherein a second clevis assembly of the second aircraft storage bin is secured to the second side of the center side panel.

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