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31. 发明申请

WO2015151014A1 SPECIFIC RISK TOOLKIT 审中-公开
标题翻译：特殊风险工具包
公开(公告)号：WO2015151014A1
公开(公告)日：2015-10-08
申请号：PCT/IB2015/052337
申请日：2015-03-30
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： GUAY, Sebastien
IPC分类号： G06F11/00
CPC分类号： G06F11/0706 , G06F11/008 , G06F11/0751 , G06F11/0766 , G06Q10/0635
摘要： A system includes a processor and a memory system in communication with the processor. The memory system stores instructions that when executed by the processor result in the system being operable to access an event list that defines a plurality of events and a scenario list that defines a plurality of scenarios as routes through a tree structure that includes one or more of the events for each of the scenarios. The system is also operable to build a specific risk matrix that calculates a plurality of combined probabilities based on each pairing of an occurrence of each of the events in combination with each of the scenarios. The system is further operable to output a residual probability for each of the events based on a summation of the combined probabilities for each of the events.
摘要翻译：系统包括与处理器通信的处理器和存储器系统。存储器系统存储当处理器执行时使得系统可操作以访问定义多个事件的事件列表的定义指令，以及将多个场景定义为通过包括以下各项中的一个或多个的树结构的路由的场景列表每个场景的事件。该系统还可操作地构建特定的风险矩阵，其基于每个事件的发生与每个场景的组合的每个配对来计算多个组合概率。该系统还可操作以基于每个事件的组合概率的总和来输出每个事件的剩余概率。

32. 发明申请

WO2015130571A1 METHOD, SYSTEM, AND EXECUTABLE PROGRAM PRODUCT FOR CONTROLLING PASSENGER SERVICES 审中-公开
标题翻译：用于控制乘客服务的方法，系统和可执行程序产品
公开(公告)号：WO2015130571A1
公开(公告)日：2015-09-03
申请号：PCT/US2015/016912
申请日：2015-02-20
申请人： BOMBARDIER INC. , GAGNON, Pierre , REZILE, Joseph , KIRMOYAN, Marc , NOLEN, Brad , LACHERÉ, Julien Fabrice , KARCESKI, Jeffrey David
发明人： GAGNON, Pierre , REZILE, Joseph , KIRMOYAN, Marc , NOLEN, Brad , LACHERÉ, Julien Fabrice , KARCESKI, Jeffrey David
IPC分类号： B60Q3/02 , H05B37/02
CPC分类号： B64D11/00 , B60Q3/44 , B60Q3/47 , B60Q3/76 , B60Q3/80 , B60Q3/82 , B63B29/02 , B64C1/1484 , B64D2011/0053 , B64D2013/003 , B64D2203/00 , H05B37/0227
摘要： A system for controlling passenger services includes a sensor that generates a signal representative of the at least one of the position of the seat, the presence of passenger in the seat, the position of the at least one hand of the passenger, the configuration of the at least one hand of the passenger and the direction of movement of the at least one hand of the passenger. A first light source, an air supply, and a window shade are disposed at a predetermined locations with respect to the seat. A controller, connected to the sensor, generates a control signal that controls at least one parameter associated with at least one of light generated by the first light source, air supplied by the air supply and a degree of openness of the window shade.
摘要翻译：用于控制乘客服务的系统包括：传感器，其产生代表座椅的位置，乘客在座椅中的存在，乘客的至少一只手的位置，乘客的至少一只手和乘客的至少一只手的运动方向。第一光源，空气源和窗帘布置在相对于座椅的预定位置处。连接到传感器的控制器产生控制信号，该控制信号控制与由第一光源产生的光，空气供应的空气和窗帘的开度的至少一个相关联的至少一个参数。

33. 发明申请

WO2015028963A1 ELECTRONIC THROTTLE SYSTEM FOR AN AIRCRAFT 审中-公开
标题翻译：电子油门系统
公开(公告)号：WO2015028963A1
公开(公告)日：2015-03-05
申请号：PCT/IB2014/064120
申请日：2014-08-28
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： NOUHAUD, Christophe
IPC分类号： B64D31/04
CPC分类号： B64D31/04
摘要： A throttle system for providing throttle control for an engine on an aircraft includes a throttle quadrant assembly (TQA) module (92, 94) in electrical communication with a throttle lever (86) for receiving a position signal (88, 90) indicative of a magnitude for a throttle of the engine, the TQA module (92, 94) being operative to convert the position signal (88, 90) into a throttle signal, an engine electronic control (EEC) module (100, 102) connected to the TQA module (92, 94) to translate the throttle signal (88, 90) into a throttle control signal for the engine, and at least one signal/power line connecting the TQA module (92, 94) to the EEC module (100, 102). The signal/ power line at least carries the throttle signal from the TQA module to the EEC module.
摘要翻译：用于为飞机上的发动机提供节气门控制的节气门系统包括与节气门杆（86）电连通的节气门象限组件（TURA）模块（92,94），用于接收指示位置信号（88,90）的位置信号 TQA模块（92,94）可操作以将位置信号（88,90）转换成油门信号，连接到TQA的发动机电子控制（EEC）模块（100,102）模块（92,94）将所述油门信号（88,90）转换成用于所述发动机的油门控制信号，以及将所述TQA模块（92,94）连接到所述EEC模块（100,102）的至少一个信号/电力线）。信号/电力线至少将TQA模块的节气门信号传送到EEC模块。

34. 发明申请

WO2014135948A3 AFT PYLON FAIRING FOR AIRCRAFT 审中-公开
标题翻译：飞行员AFT PYLON FAIRING
公开(公告)号：WO2014135948A3
公开(公告)日：2014-11-27
申请号：PCT/IB2014000223
申请日：2014-02-28
申请人： BOMBARDIER INC , SHORT BROTHERS PLC
发明人： SHEPHARD KEVIN , YOUNG JEFFREY E , BEEDY LYLE
IPC分类号： B64D29/02 , B64C7/02 , B64D33/04
CPC分类号： B64D29/06 , B64C7/02 , B64D29/02 , B64D33/04 , B64D45/00
摘要： Aft fairings (22) for aircraft pylons (14) are disclosed. In one example, a fairing (22) comprises: two opposite side panels (24) extending generally along a longitudinal direction of the fairing (22); a plurality of transverse ribs (28) interconnecting the two opposite side panels (24); and a heat shield (30) for exposure to a primary flow (16) of an aircraft engine (10). The heat shield (30) comprises transversely opposed side end portions (30A, 30C) and a mid portion (30B) disposed between the transversely opposed side end portions (30A, 30C). The heat shield (30) is secured to the ribs (28) via the mid portion (30B) of the heat shield (30). The transversely opposed side end portions (30A, 30C) are permitted to move outwardly from the mid portion (30B) due to thermal expansion of the heat shield (30).
摘要翻译：披露了飞机塔架（14）的后整流罩（22）。在一个示例中，整流罩（22）包括：大致沿着整流罩（22）的纵向方向延伸的两个相对的侧板（24）。互连两个相对的侧板（24）的多个横向肋（28）; 以及用于暴露于飞机发动机（10）的主流（16）的隔热罩（30）。隔热罩（30）包括横向相对的侧端部（30A，30C）和设置在横向相对的侧端部（30A，30C）之间的中间部分（30B）。隔热罩（30）通过隔热罩（30）的中部（30B）固定在肋条28上。横向相对的侧端部（30A，30C）由于隔热罩（30）的热膨胀而允许从中间部分（30B）向外移动。

35. 发明申请

WO2013166390A1 SEATING ARRANGEMENT CONVERTIBLE TO A BUNK BED 审中-公开
标题翻译：搭配布置的布置
公开(公告)号：WO2013166390A1
公开(公告)日：2013-11-07
申请号：PCT/US2013/039476
申请日：2013-05-03
申请人： BOMBARDIER INC. , SAVARD, David , BARDIER, Rene , OLESON, Michael , SUAREZ, Alfredo
发明人： SAVARD, David , BARDIER, Rene , OLESON, Michael , SUAREZ, Alfredo
IPC分类号： B64D11/00 , B64D11/06
CPC分类号： B64D11/0641 , B60N2/24 , B60N2/34 , B60N2/62 , B64D11/06 , B64D11/0642 , B64D11/0643 , B64D2011/0069 , B64D2011/0084 , B65D17/4012 , Y02T50/46
摘要： A seating arrangement includes a seat with a seating surface and a top bunk disposed adjacent to the seat. The seat and the top bunk are configurable between a first configuration and a second configuration. In the first configuration, the seat accommodates a user in a seated position and the top bunk is stowed. In the second configuration, the seat and the top bunk form a bunk bed configured to accommodate users in prone positions. In the first configuration, the seating surface is disposed at a first predetermined height. In addition, in the second configuration, the seating surface is disposed at a second predetermined height that is lower than the first predetermined height.
摘要翻译：座椅装置包括具有座位表面的座椅和邻近座椅设置的顶部卧铺。座椅和顶层可以在第一配置和第二配置之间进行配置。在第一配置中，座椅容纳使用者处于就座位置，并且存放顶层床。在第二种配置中，座椅和顶部的双层床形成双层床，其配置为容纳处于俯卧位的使用者。在第一构造中，座面设置在第一预定高度。此外，在第二构造中，座表面设置在低于第一预定高度的第二预定高度。

36. 发明申请

WO2013132282A1 MECHANISM AND METHOD FOR ARMING/DISARMING THE ACTUATION OF AN EMERGENCY SLIDE 审中-公开
标题翻译：用于对紧急事件的执行进行装卸的机制和方法
公开(公告)号：WO2013132282A1
公开(公告)日：2013-09-12
申请号：PCT/IB2012/000457
申请日：2012-03-09
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC , MINCHAU, Ken , SAVIDGE, John , MUNGER, Eric
发明人： MINCHAU, Ken , SAVIDGE, John , MUNGER, Eric
IPC分类号： B64D25/14
CPC分类号： B64D25/14 , B64C1/1423
摘要： A mechanism (20) for arming and disarming an actuation of an emergency slide retained on a door (10) of an aircraft and selectively configurable between an armed configuration and a disarmed configuration. The mechanism includes at least one transport hook (80) extending radially from a rotating shaft (52) and rotatable therewith about the longitudinal axis of the shaft. The transport hook (80) has interconnected top and bottom portions defining a carrying slot therebetween. In the disarmed configuration, the transport hook (80) receives the girt bar (22) in the carrying slot, such that the transport hook(80) carries the girt (22) bar upon opening of the door (10). In the armed configuration, the transport hook (80) is pivoted away from the girt bar (22) and oriented such as to move over the girt bar (22) without contact therewith upon opening of the door (10).
摘要翻译：一种用于布置和撤防保持在飞行器的门（10）上的应急滑块的致动并且可以在布防配置和撤防配置之间可选择地配置的机构（20）。该机构包括至少一个从旋转轴（52）径向延伸并随其围绕轴的纵向轴线可旋转的传送钩（80）。运输钩（80）具有互连的顶部和底部，在它们之间限定承载槽。在卸载的构造中，运输钩（80）在承载槽中容纳棉条（22），使得运输钩（80）在打开门（10）时携带棉条（22）。在布置构造中，运送钩（80）从开口杆（22）枢转并定向成在门（10）打开时不与其接触。

37. 发明申请

WO2013114147A1 CABLE RETAINER DEVICE AND METHOD FOR RETAINING CABLE IN AN AIRCRAFT 审中-公开
标题翻译：电缆保持器装置和用于在飞机上保持电缆的方法
公开(公告)号：WO2013114147A1
公开(公告)日：2013-08-08
申请号：PCT/IB2012/000184
申请日：2012-02-02
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC , LANDRY, Pierre , MIRON, Jean-Philippe , CAUDRON, Marc-André , JACQUES, Charles , PAUL, Alexandre
发明人： LANDRY, Pierre , MIRON, Jean-Philippe , CAUDRON, Marc-André , JACQUES, Charles , PAUL, Alexandre
IPC分类号： H02G3/32 , F16L3/10
CPC分类号： H02G3/32 , F16L3/1058 , Y10T29/49863
摘要： A retainer device (10) for cable used e.g. in an aircraft and other vehicles comprises a base (12). A moveable member (14) is movably connected to the base (12) and forming with the base (12) a channel adapted to receive a cable (A). A pad-deforming portion is defined in the moveable member (14), the moveable member (14) being dis- placeable between an open position in which a portion of the moveable member (14) is separated from the base (12) to provide access to the channel, and closed positions in which the moveable member (14) is releasably connected to the base (12). A resilient pad (16) is located in the pad-deforming portion of the moveable member (14) adapted to contact the cable (A) received in the channel. The resilient pad (16) is sized to deform from a rest state to a deformed state by the pad-deforming portion during insertion thereinto, the resilient pad (16) being held captive after insertion into the pad-deforming portion by reforming toward the rest state. A method for retaining a cable in an aircraft is also provided.
摘要翻译：一种用于电缆的保持装置（10），例如在飞行器和其他车辆中包括基座（12）。可移动构件（14）可移动地连接到基座（12）并且与底座（12）形成适于接纳电缆（A）的通道。在可移动构件（14）中限定了垫变形部分，可移动构件（14）可在可移动构件（14）的一部分与基部（12）分离的打开位置之间分离，以提供进入通道，以及关闭位置，其中可移动构件（14）可释放地连接到基座（12）。弹性垫（16）位于适于接纳在通道中的电缆（A）的可移动构件（14）的焊盘变形部分中。弹性垫（16）的尺寸设计成在插入其中时通过垫变形部分从静止状态变形到变形状态，弹性垫（16）在通过朝向其余部分进行重整而插入到垫变形部分之后被保持住州。还提供了一种用于将电缆保持在飞行器中的方法。

38. 发明申请

WO2013052784A1 AIRCRAFT DIVAN CONVERTIBLE TO A BUNK BED 审中-公开
标题翻译：飞机组可转换为炸弹台
公开(公告)号：WO2013052784A1
公开(公告)日：2013-04-11
申请号：PCT/US2012/058929
申请日：2012-10-05
申请人： BOMBARDIER INC. , LEARJET INC. , SAVARD, David , BARDIER, Rene , LAROSE, Martin , GILLES, Michael , TREMBLAY, Michel , OLESON, Michael , SUAREZ, Alfredo
发明人： SAVARD, David , BARDIER, Rene , LAROSE, Martin , GILLES, Michael , TREMBLAY, Michel , OLESON, Michael , SUAREZ, Alfredo
IPC分类号： B64D11/06
CPC分类号： B64D11/06 , B64D11/00 , B64D11/0641 , B64D2011/0069 , B64D2011/0076 , Y02T50/46
摘要： A divan (10) includes a seating surface (32) and a backrest (34). In a first configuration, the backrest (34) is positioned adjacent to the seating surface (32) to support a person's back while the person is seated on the seating surface (32). In the first configuration, the seating surface (32) is disposed at a first predetermined height above a horizontal plane. In a second configuration, the backrest (34) establishes an upper bunk (94) above the seating surface. In the second configuration, the seating surface (32) establishes a lower bunk (92) beneath the upper bunk (94). In the second configuration, the seating surface (32) is disposed at a second predetermined height that is lower than the first predetermined height.
摘要翻译：沙发（10）包括座位表面（32）和靠背（34）。在第一配置中，靠背（34）邻近座位表面（32）定位，以在人坐在就座表面（32）上时支撑人的背部。在第一构造中，座面（32）设置在水平面上方的第一预定高度。在第二配置中，靠背（34）在就座表面上方建立一个上层（94）。在第二构造中，就座表面（32）在上铺板（94）的下面建立一个下层铺（92）。在第二构造中，座表面（32）设置在低于第一预定高度的第二预定高度处。

39. 发明申请

WO2009130576A1 INTEGRITY MONITORING OF INTERNAL REFERENCE UNIT 审中-公开
标题翻译：内部参考单位的完整性监测
公开(公告)号：WO2009130576A1
公开(公告)日：2009-10-29
申请号：PCT/IB2009/005327
申请日：2009-04-21
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC , TESSIER, Claude
发明人： TESSIER, Claude
IPC分类号： G01C21/16 , G05D1/00
CPC分类号： G05D1/0077 , G01C21/16
摘要： Systems 100, methods, and machine-executable programming products adapted for the control of aircraft or other vehicles by receiving from at least one lnertial Reference System (IRS) 102 comprising a plurality of lnertial Reference Units (IRUs) 110 signals representing vehicle state data; receiving from at least one Augmented Direct Mode Sensor (ADMS) 106 signals representing independently-acquired vehicle state data corresponding to least a subset of the signals received from the IRS; performing signal selection and fault detection processes on the signals received from the at least one IRS and on the corresponding signals received from the ADMS; based at least partly on the signal and fault detection processes, determining whether at least one component of at least one of the IRS and ADMS is in a fault condition; and based on the determination whether the at least one component is in a fault condition, providing to at least one vehicle control system device one or more vehicle control command signals.
摘要翻译：系统100，方法和机器可执行编程产品，适于通过从包括多个分频参考单元（IRU）110的代表车辆状态数据的信号的至少一个分散参考系统（IRS）102接收来控制飞行器或其他车辆; 从至少一个增强直接模式传感器（ADMS）106接收表示独立获取的车辆状态数据的信号，所述信号对应于从IRS接收的信号的至少一个子集; 对从至少一个IRS接收的信号和从ADMS接收到的相应信号执行信号选择和故障检测处理; 至少部分地基于信号和故障检测过程，确定IRS和ADMS中的至少一个的至少一个组件是否处于故障状态; 并且基于确定所述至少一个部件是否处于故障状态，向至少一个车辆控制系统装置提供一个或多个车辆控制命令信号。

40. 发明申请

WO2008122820A2 MULTI-AXIS SERIALLY REDUNDANT, SINGLE CHANNEL, MULTI-PATH FLY-BY-WIRE FLIGHT CONTROL SYSTEM 审中-公开
标题翻译：多轴冗余，单通道，多路飞行飞行控制系统
公开(公告)号：WO2008122820A2
公开(公告)日：2008-10-16
申请号：PCT/GB2008/050216
申请日：2008-03-26
申请人： BOMBARDIER INC. , LIN, Shu , SMITH, Timothy , DE SERRES, Pierre
发明人： LIN, Shu , SMITH, Timothy , DE SERRES, Pierre
IPC分类号： G05D1/00
CPC分类号： B64C13/503 , B64C13/04 , B64C19/00 , G05D1/0077
摘要： A multi-axis serially redundant, single channel, multi-path fly-by-wire control system comprising: serially redundant flight control computers in a single channel where only one "primary" flight control computer is active and controlling at any given time; a matrix of parallel flight control surface controllers including stabilizer motor control units (SMCU) and actuator electronics control modules (AECM) define multiple control paths within the single channel, each implemented with dissimilar hardware and which each control the movement of a distributed set of flight control surfaces on the aircraft in response to flight control surface commands of the primary flight control computer; and a set of (pilot and co-pilot) controls and aircraft surface/reference/navigation sensors and systems which provide input to a primary flight control computer and are used to generate the flight control surface commands to control the aircraft in flight in accordance with the control law algorithms implemented in the flight control computers.
摘要翻译：多轴串行冗余，单通道，多路径逐线控制系统，其包括：在单个通道中的串行冗余飞行控制计算机，其中只有一个“主要”飞行控制计算机处于活动状态并在任何给定时间进行控制; 包括稳定器电机控制单元（SMCU）和执行机构电子控制模块（AECM）在内的并行飞行控制面控制器矩阵定义了单个通道内的多个控制路径，每个控制路径用不同的硬件实现，每个控制路径分别控制一组分布式飞行响应于主飞行控制计算机的飞行控制表面命令来控制飞机上的表面; 以及一组（飞行员和副驾驶员）控制和飞机表面/参考/导航传感器和系统，其向主飞行控制计算机提供输入并用于产生飞行控制表面命令以根据控制算法在飞行控制计算机中实现。

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