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71. 外观设计

USD773892S1 Oven 有权
公开(公告)号：USD773892S1
公开(公告)日：2016-12-13
申请号：US29489048
申请日：2014-04-25
申请人： BOMBARDIER INC.
设计人： Bruno Miron , Alexis Morin , Nevenka Prijic , Marie-Josée de la Cruz

72. 发明申请

US20160202701A1 ABNORMAL AIRCRAFT RESPONSE MONITOR 审中-公开
标题翻译：异常飞机反应监控
公开(公告)号：US20160202701A1
公开(公告)日：2016-07-14
申请号：US14912748
申请日：2014-08-18
申请人： Bombardier Inc.
发明人： Gregory BURTE
IPC分类号： G05D1/00 , B64C13/50
CPC分类号： G05D1/0077 , B64C13/503 , B64C13/505
摘要： An aircraft flight control system includes at least two flight control computers at least one of which is utilized at any one time to control aircraft flight, each of the at least two flight control computers having at least two processors, each processor being responsive to an aircraft input signal indicative of at least one of a plurality of aircraft flight parameters and being responsive to control laws to provide a control output command signal indicative of a desired control of an aircraft flight control surface. Also, at least one of the at least two processors for each of the at least two flight control computers comprises an abnormal response monitor that is responsive to at least one aircraft input signal indicative of at least one of a plurality of aircraft flight parameters to determine whether the control output command signal is within an acceptable value.
摘要翻译：飞行器飞行控制系统包括至少两个飞行控制计算机，其中至少一个飞行控制计算机在任何一个时间用于控制飞行器飞行，所述至少两个飞行控制计算机中的每一个具有至少两个处理器，每个处理器响应飞行器输入信号，其指示多个飞行器飞行参数中的至少一个，并响应于控制规律提供指示飞机飞行控制表面的期望控制的控制输出命令信号。此外，用于至少两个飞行控制计算机中的每一个的至少两个处理器中的至少一个包括响应于至少一个飞行器输入信号的异常响应监视器，其指示多个飞行器飞行参数中的至少一个以确定控制输出命令信号是否在可接受的值内。

73. 外观设计

USD752352S1 Seat 有权
公开(公告)号：USD752352S1
公开(公告)日：2016-03-29
申请号：US29489040
申请日：2014-04-25
申请人： BOMBARDIER INC.
设计人： Philippe Andre Eugene Erhel , Adrian Goring , Dorothée Redon , Chen Hua Yu

74. 发明申请

US20160059953A1 SYSTEM AND A METHOD OF OPERATION OF THE SYSTEM INCORPORATING A GRAPHICAL USER INTERFACE IN A BULKHEAD OF A VEHICLE CABIN 有权
标题翻译：系统和系统的操作方法，其中包括一个车厢的大型图形用户界面
公开(公告)号：US20160059953A1
公开(公告)日：2016-03-03
申请号：US14164932
申请日：2014-01-27
申请人： BOMBARDIER INC.
发明人： Tim Michael FAGAN , Brian CONNER , Jeff BARTENBACH , Linsey NANCARROW , Tom HOBBS , Erick WALDMAN , Sebastian PETRY
IPC分类号： B64C19/00
CPC分类号： B64D11/0015 , B60K2350/1024 , B64D2013/0655
摘要： A method of operation for a system incorporating a graphical user interface disposed in a bulkhead within a cabin of an aircraft. The method includes displaying a menu for at least one controllable parameter, receiving a selection of the controllable parameter, displaying at least one control for the selected controllable parameter, receiving a control input for the selected controllable parameter, and adjusting the selected controllable parameter consistent with the control input. The controllable parameter may be one from a plurality of controllable parameters selected from a group that includes cabin light intensity, cabin light color, temperature, and the degree of openness of at least one window shade. A system and an executable computer program product also are provided.
摘要翻译：一种用于系统的操作方法，该系统包括布置在飞行器舱室内的隔板中的图形用户界面。该方法包括显示用于至少一个可控参数的菜单，接收可控参数的选择，显示所选择的可控参数的至少一个控制，接收所选择的可控参数的控制输入，以及调整与控制输入。可控参数可以是从包括车厢光强度，车厢光色，温度和至少一个窗帘的开度的组中选择的多个可控参数中的一个。还提供了系统和可执行计算机程序产品。

75. 发明申请

US20160031553A1 ELECTRIC BRAKING SYSTEM WITH POWER CONSERVATION AND METHOD OF OPERATING THE SAME 审中-公开
标题翻译：具有功率保护的电动制动系统及其操作方法
公开(公告)号：US20160031553A1
公开(公告)日：2016-02-04
申请号：US14770183
申请日：2014-02-27
申请人： BOMBARDIER INC.
发明人： Marco DI ZAZZO , Bertrand PLANTE
IPC分类号： B64C25/44 , B64C25/34 , B60T8/17
CPC分类号： B64C25/44 , B60T8/1703 , B60T8/885 , B60T2270/414 , B64C25/34 , B64D2221/00
摘要： A method of operating electric brakes (30, 32, 34) on an aircraft (10) in a low power mode of operation includes determining if the aircraft is in a first configuration, if the aircraft is in the first configuration, disengaging power to the electric brakes (30, 32, 34) the from all power supplies (40, 42), determining if the aircraft (10) is in a second configuration, if the aircraft is in the second configuration, engaging power to the electric brakes (30, 32, 34) from one of the power supplies (40, 42), determining if the aircraft (10) is in a third configuration, and if the aircraft (10) is in the third configuration, engaging power to the electric brakes (30, 32, 34) from at least two of the power supplies (40, 42).
摘要翻译：在低功率操作模式下在飞机（10）上操作电制动器（30,32,34）的方法包括确定飞行器是否处于第一配置，如果飞行器处于第一配置，则将功率分离到电动制动器（30,32,34），从所有电源（40,42）中，确定飞行器（10）是否处于第二配置，如果飞行器处于第二配置，则将电力接合到电制动器（30,42），32,34），确定所述飞行器（10）是否处于第三构造，并且如果所述飞行器（10）处于所述第三构造，则将动力接合到所述电制动器（ 30,32,34）从至少两个电源（40,42）中取出。

76. 发明申请

US20160009375A1 HIGH LIFT CONTROL METHOD AND SYSTEM FOR AIRCRAFT 有权
标题翻译：用于飞机的高起升控制方法和系统
公开(公告)号：US20160009375A1
公开(公告)日：2016-01-14
申请号：US14771974
申请日：2014-02-26
申请人： BOMBARDIER INC.
发明人： Robert YOUNG , Yves GRENIER , Hany SADEK
IPC分类号： B64C13/04 , B64C9/28 , B64C13/16
CPC分类号： B64C13/04 , B64C9/28 , B64C13/16 , B64D2045/001
摘要： A high lift control system for an aircraft having at least one high lift surface includes a selector having a predetermined number of discrete positions, at least one of the predetermined positions corresponding to different positions of the at least one high lift surface.
摘要翻译：用于具有至少一个高升程表面的飞行器的高升程控制系统包括具有预定数量的离散位置的选择器，至少一个预定位置对应于至少一个高升程表面的不同位置。

77. 发明申请

US20150266564A1 FAILURE DETECTION MECHANISM FOR SELECTOR LEVER 有权
标题翻译：用于选择杆的故障检测机构
公开(公告)号：US20150266564A1
公开(公告)日：2015-09-24
申请号：US14441432
申请日：2012-11-27
申请人： Vlad ILIESCU , Menas SALIB , BOMBARDIER INC.
发明人： Vlad Iliescu , Menas Salib
IPC分类号： B64C13/10 , G05G5/03
CPC分类号： B64C13/10 , B64D31/04 , G05G5/03 , Y10T74/20612
摘要： A selector lever includes a housing with front and rear ends and a lever with a shaft pivotally disposed on a cross-shaft. The shaft defines a shaft axis. The lever has a top that is disposed outside of the housing. A movable shaft moves substantially axially along the shaft axis. A pin, having first and second protrusions, is disposed adjacent to a bottom end of the movable shaft. A first detent plate is disposed on a first side of the movable shaft and includes at least a first slot that receives the first protrusion. A second detent plate is disposed on a second side of the moveable shaft and includes at least a second slot therein receiving the second protrusion. A first failure detection slot is associated with the first slot, permitting movement of the first protrusion therein in the absence of the second protrusion.
摘要翻译：选档杆包括具有前端和后端的壳体和具有枢转地设置在横轴上的轴的杠杆。轴定义轴轴。杠杆具有设置在壳体外部的顶部。可动轴沿轴线基本轴向移动。具有第一和第二突起的销被布置成与可动轴的底端相邻。第一制动板设置在可动轴的第一侧上，并且至少包括容纳第一突起的第一槽。第二制动板设置在可动轴的第二侧上，并且在其中至少包括第二槽，其中容纳第二突起。第一故障检测槽与第一槽相关联，允许在没有第二突起的情况下第一突起在其中移动。

78. 发明申请

US20150146443A1 LIGHTING ARRAY FOR AN AIRCRAFT 有权
标题翻译：照明阵列飞机
公开(公告)号：US20150146443A1
公开(公告)日：2015-05-28
申请号：US14403906
申请日：2013-05-30
申请人： BOMBARDIER INC.
发明人： Pierre Gagnon , Nicolas Letendre
IPC分类号： B64D47/06
CPC分类号： B64D47/06 , B64D47/02 , B64D47/04 , B64D2203/00
摘要： A lighting arrangement for an aircraft includes a navigational lighting group disposed at a leading edge of a wing of the aircraft. The navigational lighting group includes at least one right of way light. The lighting arrangement also includes a light bar extending along at least a portion of the leading edge of the wing, adjacent to the navigational lighting group. The light bar is configured to emit light along a length thereof.
摘要翻译：用于飞机的照明装置包括设置在飞行器的翼的前缘的导航照明组。导航照明组至少包括一个光照权。照明装置还包括沿着翼的前缘的至少一部分延伸的灯条，与导航照明组相邻。光条被配置为沿其长度发光。

79. 外观设计

USD723313S1 Seat components 有权
标题翻译：座椅组件
公开(公告)号：USD723313S1
公开(公告)日：2015-03-03
申请号：US29482748
申请日：2014-02-21
申请人： Bombardier Inc.
设计人： Pierre Gagnon , Charles Beauchamp , Nicolas Letendre , Howard Guy , Patrick Fahmy , Michele Monardo

80. 外观设计

USD722259S1 Knob 有权
公开(公告)号：USD722259S1
公开(公告)日：2015-02-10
申请号：US29444588
申请日：2013-01-31
申请人： Bombardier Inc.
设计人： Brian Conner

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