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81. 发明申请

WO2015087216A1 APPARATUS AND METHODS FOR PROVIDING NETWORK SECURITY ON A MOBILE PLATFORM 审中-公开
标题翻译：在移动平台上提供网络安全的装置和方法
公开(公告)号：WO2015087216A1
公开(公告)日：2015-06-18
申请号：PCT/IB2014/066605
申请日：2014-12-04
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： COTE, Jean - Richard , AGAGNIER, Jayson
IPC分类号： H04L29/06 , H04L29/08
CPC分类号： H04L67/1095 , G06F3/0619 , G06F3/065 , G06F3/067 , H04L63/02 , H04L67/12
摘要： The disclosure describes components, apparatus and methods for providing network security between computing devices and/or networks on mobile platforms such as aircraft. One such apparatus may comprise: a first memory configured for data communication with a first computing device of the mobile platform; a second memory configured for data communication with a second computing device of the mobile platform; and a controller. The controller may be configured to detect a change in data stored In the first memory and cause the change in data stored in the first memory to be reflected in the second memory by causing data transfer from the first memory to the second memory. Data transfer between the first memory and the second memory may be conducted using a non-internet protocol.
摘要翻译：本公开描述了用于在诸如飞机的移动平台上的计算设备和/或网络之间提供网络安全性的组件，设备和方法。一种这样的设备可以包括：配置用于与移动平台的第一计算设备的数据通信的第一存储器; 配置用于与所述移动平台的第二计算设备的数据通信的第二存储器; 和控制器。控制器可以被配置为检测存储在第一存储器中的数据的变化，并且通过使从第一存储器到第二存储器的数据传送，使存储在第一存储器中的数据的变化反映在第二存储器中。第一存储器和第二存储器之间的数据传输可以使用非互联网协议进行。

82. 发明申请

WO2015044895A3 ADJUSTMENT DEVICE 审中-公开
公开(公告)号：WO2015044895A3
公开(公告)日：2015-04-02
申请号：PCT/IB2014/064835
申请日：2014-09-25
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： MAHAITS, Martin , TREMBLAY, Michel
IPC分类号： E05D7/00 , E05D7/04 , B64D11/06
摘要： Devices and assemblies for adjusting a position of a movable body (24) are disclosed. An exemplary device for adjusting a position of a body rotatable about a hinge axis comprises: a first portion (36a) configured to be secured to a structure (32a); and a second portion (38a) adjustably coupled to the first portion and configured to be rotatably coupled to the body. The second portion comprises an adjustment mechanism for adjusting the body along the hinge axis relative to the second portion.

83. 发明申请

WO2015044895A2 ADJUSTMENT DEVICE 审中-公开
标题翻译：调整装置
公开(公告)号：WO2015044895A2
公开(公告)日：2015-04-02
申请号：PCT/IB2014064835
申请日：2014-09-25
申请人： BOMBARDIER INC , SHORT BROTHERS PLC
发明人： MAHAITS MARTIN , TREMBLAY MICHEL
IPC分类号： E05D7/00 , B64D11/06 , E05D7/04
CPC分类号： E05D7/0415 , B64D11/0636 , E06B3/385
摘要： Devices and assemblies for adjusting a position of a movable body are disclosed. An exemplary device for adjusting a position of a body rotatable about a hinge axis comprises: a first portion configured to be secured to a structure; and a second portion adjustably coupled to the first portion and configured to be rotatably coupled to the body. The second portion comprises an adjustment mechanism for adjusting the body along the hinge axis relative to the second portion.
摘要翻译：公开了用于调节可移动体的位置的装置和组件。用于调节围绕铰链轴线旋转的主体的位置的示例性装置包括：构造成固定到结构的第一部分; 以及第二部分，其可调节地联接到所述第一部分并且被配置为可旋转地联接到所述主体。第二部分包括用于相对于第二部分沿着铰链轴线调节主体的调节机构。

84. 发明申请

WO2015019147A1 AIR DATA PROBE CONTAMINATION MONITOR 审中-公开
标题翻译：空气数据探测器污染监测
公开(公告)号：WO2015019147A1
公开(公告)日：2015-02-12
申请号：PCT/IB2014/001429
申请日：2014-07-31
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： CADOTTE, Patrick , LAHEY, Sean
IPC分类号： G01P5/16 , G01P13/02 , G01P21/02
CPC分类号： G07C5/0808 , B64C13/503 , G01D5/02 , G01L19/0092 , G01L19/086 , G01N19/08 , G01N25/72 , G01P5/16 , G01P13/025 , G01P21/025 , G07C5/0816
摘要： An aircraft air data probe contamination monitor includes at least two air data sensor probes, a first probe located on one side of the aircraft, a second probe located on an opposite side of the aircraft, each probe being operable to generate a parameter value from an airflow passing the in-flight aircraft. The monitor also includes a processor operable to compare the generated parameter value from the first probe to the generated parameter value from the second probe to determine if one of the first probe and the second probe is contaminated.
摘要翻译：飞机空气数据探测器污染物监测器包括至少两个空气数据传感器探针，位于飞行器一侧的第一探针，位于飞机相对侧的第二探针，每个探头可操作以从气流通过飞行中的飞机。监视器还包括处理器，其可操作以将来自第一探针的生成的参数值与来自第二探针的生成的参数值进行比较，以确定第一探针和第二探针中的一个是否被污染。

85. 发明申请

WO2014135945A1 HIGH LIFT CONTROL METHOD AND SYSTEM FOR AIRCRAFT 审中-公开
标题翻译：用于飞机的高起升控制方法和系统
公开(公告)号：WO2014135945A1
公开(公告)日：2014-09-12
申请号：PCT/IB2014/000213
申请日：2014-02-26
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： YOUNG, Robert , GRENIER, Yves , SADEK, Hany
IPC分类号： B64C9/28 , B64C13/04 , 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。

86. 发明申请

WO2014135942A1 APPARATUS FOR PROTECTING AIRCRAFT COMPONENTS AGAINST FOREIGN OBJECT DAMAGE 审中-公开
标题翻译：保护飞机组件对付外来物体损坏的装置
公开(公告)号：WO2014135942A1
公开(公告)日：2014-09-12
申请号：PCT/IB2014/000204
申请日：2014-02-25
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： AFRIANTO, Sigit , BROUSSEAU, Jean
IPC分类号： F02C6/08 , F02C7/055 , F02C7/18 , F02C9/18
CPC分类号： F02C7/055 , F02C6/08 , F02C7/18 , F02C9/18 , F05D2220/32 , Y02T50/675
摘要： A device for protecting aircraft equipment against contact by a foreign object including an interference arrangement disposed in an air inlet upstream from the aircraft equipment where the interference arrangement is configured to physically obstruct passage of the foreign object within the air inlet.
摘要翻译：一种用于保护飞机设备免受外来物体接触的装置，包括设置在飞机设备上游的空气入口中的干涉布置，其中干涉布置构造成物理地阻挡异物进入空气入口内的通道。

87. 发明申请

WO2014084809A1 FAILURE DETECTION MECHANISM FOR SELECTOR LEVER 审中-公开
标题翻译：用于选择杆的故障检测机构
公开(公告)号：WO2014084809A1
公开(公告)日：2014-06-05
申请号：PCT/US2012/066620
申请日：2012-11-27
申请人： BOMBARDIER INC. , LEARJET INC. , ILIESCU, Vlad , SALIB, Menas
发明人： ILIESCU, Vlad , SALIB, Menas
IPC分类号： B64C13/10 , B64D31/04
CPC分类号： B64C13/10 , B64D31/04 , G05G5/03 , Y10T74/20612
摘要： A selector lever includes a housing (16) with front and rear ends and a lever (12) with a shaft (22) pivotally disposed on a cross-shaft (20). The shaft defines a shaft axis. The lever has a top that is disposed outside of the housing. A movable shaft (24) moves substantially axially along the shaft axis. A pin (40), having first and second protrusions (50,52), is disposed adjacent to a bottom end (38) of the movable shaft. A first detent plate (44) is disposed on a first side of the movable shaft and includes at least a first slot (42) that receives the first protrusion. A second detent plate (44) 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 (74) is associated with the first slot, permitting movement of the first protrusion (50) therein in the absence of the second protrusion (52).
摘要翻译：选档杆包括具有前端和后端的壳体（16）和具有枢转地设置在横轴（20）上的轴（22）的杆（12）。轴定义轴轴。杠杆具有设置在壳体外部的顶部。可移动轴（24）沿着轴的轴线基本轴向移动。具有第一和第二突起（50,52）的销（40）邻近可动轴的底端（38）设置。第一制动板（44）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（42）。第二制动板（44）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（74）与第一槽相关联，允许在没有第二突起（52）的情况下第一突起（50）在其中的移动。

88. 发明申请

WO2014051638A1 AIRCRAFT SIDEBOARD 审中-公开
标题翻译：飞机侧栏
公开(公告)号：WO2014051638A1
公开(公告)日：2014-04-03
申请号：PCT/US2012/059188
申请日：2012-10-08
申请人： BOMBARDIER INC. , LEARJET INC. , GAGNON, Pierre , DEKA, Tom , FAHMY, Patrick , MONARDO, Michele
发明人： GAGNON, Pierre , DEKA, Tom , FAHMY, Patrick , MONARDO, Michele
IPC分类号： B64D11/00 , B64D11/06
CPC分类号： B64D11/0638 , B64D11/0007 , B64D11/0015 , B64D11/0604 , B64D11/0624 , B64D11/0636
摘要： An aircraft sideboard (10) includes a first portion (26) with a first top surface (32) and a first panel (62). The first top surface (32) is disposed substantially horizontally at a first height and the first panel (62) is disposed substantially vertically adjacent to the first top surface (32). A second portion (28) is disposed adjacent to the first portion (26) at a first end of the first portion. The second portion (28) includes a second top surface (34) and a second panel (64). The second top surface (34) is disposed substantially horizontally at a second height and the second panel (64) is disposed substantially vertically adjacent to the second top surface (43). A table (76) is stowed interiorly to the first portion (26). The table (76) extends from the first portion when deployed. The first top surface (32) is immovable. The table (76) deploys by tilting the first panel (62) along a pivot axis defined adjacent to a bottom end thereof. The first height is greater than the second height.
摘要翻译：飞机侧板（10）包括具有第一顶表面（32）和第一面板（62）的第一部分（26）。第一顶表面（32）基本上水平地设置在第一高度处，并且第一面板（62）基本上垂直地布置成与第一顶表面（32）相邻。第二部分（28）在第一部分的第一端处邻近第一部分（26）设置。第二部分（28）包括第二顶表面（34）和第二面板（64）。第二顶表面（34）基本上水平地设置在第二高度处，并且第二面板（64）基本上垂直地布置成与第二顶表面（43）相邻。桌子（76）内部收纳在第一部分（26）上。当展开时，桌子（76）从第一部分延伸。第一顶面（32）是不可移动的。桌子（76）通过沿着与其底端相邻限定的枢转轴线倾斜第一面板（62）来部署。第一个高度大于第二个高度。

89. 发明申请

WO2012120321A1 STANDOFF DEVICE AND METHOD OF INSTALLATION OF HARNESS 审中-公开
标题翻译： STANDOFF设备及其安装方法
公开(公告)号：WO2012120321A1
公开(公告)日：2012-09-13
申请号：PCT/IB2011/000512
申请日：2011-03-10
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC , PAUZÉ, Martin , WOOD, Keith, Antony , DESHAIES, Martin , LANDRY, Pierre
发明人： PAUZÉ, Martin , WOOD, Keith, Antony , DESHAIES, Martin , LANDRY, Pierre
IPC分类号： H02G3/30 , B60R16/02
CPC分类号： H01B17/16 , F16L3/221 , F16L3/237 , H01B17/14 , H02G3/30 , H02G3/32
摘要： A device connects a wire harness to a structure. A fixation portion of the device is secured to the structure. A spacing portion is connected to the fixation portion and to a connector portion. A retaining clip on the connector portion deforms when a wire harness connector component moves axially toward the fixation portion. The clip opposes an abutment edge against the component into engagement position when the component is past the clip to prevent it from moving back onto the clip. An abutment surface contacts another portion of the component in engagement position to prevent further axial movement of the component toward the fixation portion. The component is held captive between the edge and the abutment surface. Also provided are a cable support for connecting the wire harness to the device, a method for connecting and disconnecting the wire harness to a structure with the device, and an aircraft.
摘要翻译：设备将线束连接到结构。该装置的固定部分固定在该结构上。间隔部分连接到固定部分和连接器部分。当线束连接器部件沿固定部分轴向移动时，连接器部分上的固定夹变形。当组件经过夹子以防止其回到夹子上时，夹子将抵靠部件的抵接边缘与接合位置相对。邻接表面接合部件的接合位置的另一部分以防止部件朝着固定部分进一步轴向移动。该部件保持在边缘和邻接表面之间。还提供了用于将线束连接到装置的电缆支撑件，用于将线束连接和断开到具有该装置的结构的方法以及飞行器。

90. 发明申请

WO2012050587A1 AIRCRAFT INTERIOR CONFIGURATION 审中-公开
标题翻译：飞机内部配置
公开(公告)号：WO2012050587A1
公开(公告)日：2012-04-19
申请号：PCT/US2010/052846
申请日：2010-10-15
申请人： BOMBARDIER INC. , LEARJET INC. , MALEK, Bruce , GAGNON-SEGUIN, Louis, Joseph , MIRON, Bruno , ERHEL, Philippe, André Eugène , FAGAN, Tim, Michael
发明人： MALEK, Bruce , GAGNON-SEGUIN, Louis, Joseph , MIRON, Bruno , ERHEL, Philippe, André Eugène , FAGAN, Tim, Michael
IPC分类号： B64D11/00
CPC分类号： B64D11/06 , B64D11/00 , B64D11/0601 , B64D11/0638
摘要： An aircraft interior configuration includes a first passageway (32) extending along a longitudinal axis (33) of a fuselage (10) of the aircraft and a second passageway extending along the longitudinal axis. A transitional region (102) is disposed between the first passageway and the second passageway. The transitional region extends perpendicularly to the longitudinal axis, between starboard and port sides of the aircraft. The transitional region is configurable from at least a first configuration to at least a second configuration.
摘要翻译：飞行器内部构造包括沿着飞行器的机身（10）的纵向轴线（33）延伸的第一通道（32）和沿着纵向轴线延伸的第二通道。过渡区域（102）设置在第一通道和第二通道之间。过渡区域垂直于纵向轴线，在飞机的右舷和端口侧之间延伸。过渡区域可以从至少第一配置至至少第二配置来配置。

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