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    • 72. 发明申请
    • AIRCRAFT GALLEY CONFIGURATION
    • 飞机GALLEY配置
    • WO2015162575A3
    • 2016-01-21
    • PCT/IB2015052946
    • 2015-04-22
    • BOMBARDIER INCSHORT BROTHERS PLC
    • MIRON BRUNOTREMBLAY MICHELLADD GRADYNTREMBLAY BENJAMIN
    • B64D11/04
    • B64D11/04
    • An aircraft galley configuration (10) extending along a longitudinal axis of a fuselage of an aircraft and on one side of the aircraft includes a forward end (12) of the galley (10) closest to the front of the aircraft and a rear end (14) of the galley (10) on an opposite longitudinal end of the galley (10) and closest to a passenger section of the aircraft, and a plurality of galley modules (20, 22, 24, 26) disposed in the galley (10) between the forward (12) and rear ends (14) of the galley. The galley modules comprise a storage module (20), a heating module (22), a preparation module (24), and a service module (26). The storage module (20) is disposed at the forward end (12) of the galley (10) and the service module (26) is disposed at the rear end (14) of the galley (10), An efficient work flow in the direction of the passenger section is created by the galley configuration (10).
    • 沿着飞行器的机身的纵向轴线延伸并且在飞机的一侧上的飞机厨房结构(10)包括最靠近飞行器前部的厨房(10)的前端(12)和后端 并且最靠近飞行器的乘客部分的多个厨房模块(20,22,24,26)设置在所述厨房(10)的相对的纵向端部上并且最靠近所述飞机的乘客部分的多个厨房模块(20,22,24,26) )在厨房的前部(12)和后端(14)之间。 厨房模块包括存储模块(20),加热模块(22),准备模块(24)和服务模块(26)。 存储模块(20)设置在厨房(10)的前端(12)处,并且维修模块(26)设置在厨房(10)的后端(14)处。 乘客部分的方向由厨房配置(10)创建。
    • 76. 发明申请
    • AIRCRAFT ANGLED CONFERENCE TABLE CONFIGURATION
    • 飞机安装会议台配置
    • WO2015162574A1
    • 2015-10-29
    • PCT/IB2015/052944
    • 2015-04-22
    • BOMBARDIER INC.SHORT BROTHERS PLC
    • BANG, Seung JoonFAGAN, Tim MichaelMALEK, Bruce
    • B64D11/06
    • B64D11/0638A47B5/04A47B9/00A47B13/088A47B13/10A47B37/00A47B2200/0079
    • An aircraft table configuration includes a first table section and a second table section. The first and second table sections are hingedly connected along a first hinge line so that the second table section is configurable between a deployed, opened position and a folded, closed position. The first table section presents a first angled side and the second table section table presents a second angled side. The first angled side defines a first angle with respect to the first hinge line, and the second angled side defines a second angle with respect to the first hinge line. The first angled side and the second angled side are opposite to one another on either side of the first hinge line, wherein the first and second angled sides are adapted to define an aisle width in the aircraft. The aisle width does not change between the open position and the closed position.
    • 飞机台配置包括第一台部分和第二台部分。 第一和第二台部分沿着第一铰链线铰接连接,使得第二工作台部分可配置在展开的打开位置和折叠的关闭位置之间。 第一台部分呈现第一倾斜侧面,第二台部分台呈现第二倾斜侧面。 所述第一倾斜侧面相对于所述第一铰链线限定第一角度,并且所述第二倾斜侧面相对于所述第一铰链线限定第二角度。 第一成角度侧和第二倾斜侧在第一铰链线的任一侧彼此相对,其中第一和第二倾斜侧适于在飞行器中限定过道宽度。 过道宽度在打开位置和关闭位置之间不变。
    • 80. 发明申请
    • AIRCRAFT DIVAN CONVERTIBLE INTO A BED
    • 飞机司机可以转换成床
    • WO2015097630A1
    • 2015-07-02
    • PCT/IB2014/067168
    • 2014-12-19
    • BOMBARDIER INC.SHORT BROTHERS PLC
    • ERHEL, Philippe Andre Eugene
    • B64D11/06
    • B64D11/0641B64D2011/0069Y02T50/46
    • An aircraft divan includes a lateral bracket connecting between front and rear legs with lateral bracket front and rear ends, a first track defined by the lateral bracket between the lateral bracket front and rear ends, an upright, having upright top and bottom ends, a second track defined by the upright between the upright top and bottom ends, a seat pan having seat pan front and rear ends, the seat pan being slidingly connected to the first track adjacent to the seat pan rear end, and a backrest having backrest top and bottom ends, the backrest being slidingly connected to the second track adjacent to the backrest top end. The seat pan rear end is pivotably connected to the backrest adjacent to the backrest bottom end such that movement of the seat pan is transmitted to the backrest so as to move together between upright and berth positions.
    • 一个飞机上的舷窗包括一个横向支架,它连接在前后两侧之间,侧支架前后两端,由横向支架在侧支架前端和后端之间限定的第一轨道,一个具有直立的顶端和底端的立柱, 由直立的顶部和底部之间的竖立部分限定的轨道,具有座盘前端和后端的座盘,座盘滑动地连接到邻近座盘后端的第一轨道,以及靠背,其具有靠背顶部和底部 靠背靠近靠背顶端滑动地连接到第二轨道。 座椅底座后端可靠地靠靠靠背底端连接到靠背,使得座椅底盘的运动传递到靠背,以便在直立位置和泊位之间一起移动。