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公开(公告)号:USD714699S1
公开(公告)日:2014-10-07
申请号:US29448807
申请日:2013-03-13
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公开(公告)号:USD710771S1
公开(公告)日:2014-08-12
申请号:US29449086
申请日:2013-03-14
申请人: Steven H. Hovind , Wallace A. Peltola , Kenny Yi
设计人: Steven H. Hovind , Wallace A. Peltola , Kenny Yi
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公开(公告)号:USD702609S1
公开(公告)日:2014-04-15
申请号:US29449484
申请日:2013-03-15
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公开(公告)号:USD549364S1
公开(公告)日:2007-08-21
申请号:US29276207
申请日:2007-01-18
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公开(公告)号:US5178345A
公开(公告)日:1993-01-12
申请号:US754654
申请日:1991-09-04
IPC分类号: B64D11/06
CPC分类号: B64D11/0693
摘要: An aircraft seat assembly (14) is convertible between three seats (LA, LM, LW) with a first seat width and two seats (LA, W) with a second wider seat width. The seat assembly includes a tube-in-tube support frame for the seats which allows the conversion to be accomplished by a simple sliding movement of the aisle and middle seat frames towards and away from the window seat frame which is fixed in position. Movement of the aisle and middle seat frames automatically changes the position of the two inside armrests (22, 24). The middle seat back frame (66) is vertically split into parts (66A, 66B). Movement of the seat frames from the three-seat configuration to the two-seat configuration disconnects seat back parts (66A, 66B) from each other and locks one part (66A) to the window seat back frame (64) and the other part (66B) to the aisle seat back frame (68). Movement of the seat frames in the opposite direction disconnects the parts (66A, 66B) from the window and aisle seat back frames ( 64, 68) and connects the two parts (66A, 66B) together to provide a unified seat back frame (66) for the middle seat (LM). A lock mechanism (124, 130) locks the seat frame parts together, both in the three-seat configuration and in the two-seat configuration. The lock mechanism is locked and unlocked by movement of a handle (H) located at the aisle end of the aisle seat (LA). A key lock (160) is provided to keep the lock mechanism (124, 130) locked in between authorized and intended movements of the seat frames to convert the seat assembly (14).
摘要翻译: 飞机座椅组件(14)可以在具有第一座椅宽度的三个座椅(LA,LM,LW)和两个座椅宽度的座椅(LA,W)之间转换。 座椅组件包括用于座椅的管内支撑框架,其允许通过通道和中间座椅框架朝向和远离固定就位的窗口座椅框架的简单滑动来实现转换。 通道和中间座椅框架的移动自动改变两个内部扶手(22,24)的位置。 中间座椅靠背框架(66)垂直分割成部分(66A,66B)。 座椅框架从三座椅构型向双座椅构型的移动将座椅靠背部分(66A,66B)彼此分离,并将一部分(66A)锁定到窗口座椅靠背框架(64),另一部分 66B)连接到过道座椅靠背框架(68)。 座椅框架沿相反方向的移动将部件(66A,66B)从窗口和通道座椅靠背框架(64,68)分离,并将两个部件(66A,66B)连接在一起,以提供统一的座椅靠背框架(66 )用于中座(LM)。 锁定机构(124,130)将座椅框架部件锁定在三座椅构型和双座椅构型中。 锁定机构通过位于通道座(LA)的通道端的手柄(H)的移动而被锁定和解锁。 提供钥匙锁(160)以使锁定机构(124,130)锁定在座椅框架的授权和预期的运动之间以转换座椅组件(14)。
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