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    • 2. 发明公开
    • SHARED ENTRANCE SEATING ARRANGEMENT
    • EP3126241A4
    • 2017-11-29
    • EP15773979
    • 2015-04-02
    • C&D ZODIAC INC
    • SAVIAN SCOTT
    • B64D11/06B64D11/00
    • B64D11/0605B64D11/0015B64D11/003B64D11/0604B64D11/0606B64D11/0624B64D11/0627
    • There is an aircraft lounge assembly (85) comprising an enclosure that includes a rear wall (46), first and second side walls (48) and a forward wall (44) that cooperate to define a seating area. First and second seats (18) are positioned in the seating area. A first dividing wall (124) is positioned between the first and second seats. The first dividing wall divides the seating area into a first seat section (126) and a second seat section (128). The front wall includes a shared entrance space (84) defined therein. A first seat path (P1) is defined between the shared entrance space and the first seat section. A second seat path (P2) is defined between the shared entrance space and the second seat section. The aircraft lounge assembly further comprises third and fourth seats (18) positioned in the seating area. A second dividing wall (130) is positioned between the second and third seats and a third dividing wall (132) is positioned between the third and fourth seats. The third dividing wall divides the seating area into a third seat section (134) and a fourth seat section (136). The front wall includes a second shared entrance space (84) defined therein, wherein a third seat path (P3) is defined between the second shared entrance space and the third seat section and a fourth seat path (P4) is defined between the second shared entrance space and the fourth seat section. The second dividing wall extends between the rear wall and the front wall.
    • 6. 发明公开
    • COMPACT CABIN ATTENDANT SEAT STOWAGE
    • KOMPAKTE FLUGBEGLEITERSITZVERSTAUUNG
    • EP2991899A4
    • 2017-05-10
    • EP14791218
    • 2014-04-29
    • C&D ZODIAC INC
    • NABIH NAJDREAMS EDWARDSAVIAN SCOTTZARROUATI OLIVIER
    • B64D11/06
    • B64D11/02B60N2/3018B60N2/3029B60N2/3031B60N2/3047B60N2/4855B64D11/0691
    • An aircraft monument that includes an enclosure with an enclosure interior, a compartment with a compartment interior positioned in the enclosure interior, and a stowable seat assembly disposed in the compartment. The compartment includes at least a first vertically oriented wall. The seat assembly includes a chair assembly with a back portion and a seat portion pivotably connected to the back portion along a seat pivot axis such that the seat is pivotable between closed and open positions. The chair assembly is movable between a stowed position where the seat pivot axis extends generally parallel to the first wall and the chair assembly is positioned in the compartment interior, and a deployed position where the seat pivot axis extends generally perpendicular to the first wall and the chair assembly is positioned outside of the compartment interior.
    • 一种飞机纪念碑,其包括具有外壳内部的外壳,具有定位在外壳内部中的隔室内部的隔室以及设置在隔室中的可收起座椅组件。 隔室至少包括第一竖直取向的壁。 座椅组件包括具有后部和座椅部分的座椅组件,座椅部分沿着座椅枢转轴线可枢转地连接到后部,使得座椅能够在关闭位置和打开位置之间枢转。 椅子组件可在座椅枢转轴线基本上平行于第一壁并且椅子组件被定位在舱室内部的收起位置和座椅枢转轴线大体上垂直于第一壁和第二壁的展开位置之间移动, 椅子组件定位在隔间内部的外部。
    • 9. 发明申请
    • AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS
    • 具有声学材料的飞机内部面板
    • WO2014008507A2
    • 2014-01-09
    • PCT/US2013049597
    • 2013-07-08
    • C & D ZODIAC INC
    • SAVIAN SCOTTLONG ERICDE BOTTON JORDAN
    • B64C1/40
    • B64C1/40B64C1/066
    • A panel assembly that includes a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface. The second panel includes a plurality of rib members formed, therein that extend inwardly. The rib members include an inner surface and an outer surface. A plurality of panel portions are defined between the plurality of rib members. The panel portions include an inner surface and an outer surface. The inner surface of the rib members are secured to the inner surface of the first panel, and the inner surface of the panel portions is spaced apart from the inner surface of the first panel to define at least first and second cavities.
    • 一种面板组件,其包括具有内表面和外表面的第一面板,以及具有内表面和外表面的第二面板。 第二面板包括在其中形成的多个肋构件,其向内延伸。 肋构件包括内表面和外表面。 在多个肋构件之间限定多个面板部。 面板部分包括内表面和外表面。 肋构件的内表面固定到第一面板的内表面,并且面板部分的内表面与第一面板的内表面间隔开以限定至少第一和第二空腔。