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51. 发明申请

WO2018104868A1 CUSHIONING ELEMENT WITH TUNED ABSORBER 审中-公开
公开(公告)号：WO2018104868A1
公开(公告)日：2018-06-14
申请号：PCT/IB2017/057665
申请日：2017-12-05
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC.
发明人： CARON-L'ECUYER, Alexis , BRODEUR, Andre , KATHIRCHELVAN, Thineshan , LEE MAN WONG, Raymond
IPC分类号： G10K11/172 , G10K11/168
摘要： A cushioning element for use in a vehicle, for example in an aircraft, includes at least one tuned absorber embedded within the cushioning element. The tuned absorber is tuned to absorb noise at a predetermined frequency of at least 20 Hz. A method of providing noise absorption within a cabin of a vehicle includes determining a predetermined frequency of at least 20 Hz of an undesirable noise within the cabin, and configuring an internal structure of a cushioning element to define a tuned absorber tuned to absorb noise at the predetermined frequency, the cushioning element in use being located in the cabin.

52. 发明申请

WO2018067370A1 NOISE REDUCING AIR DUCT 审中-公开
标题翻译：降低噪音的空气管道
公开(公告)号：WO2018067370A1
公开(公告)日：2018-04-12
申请号：PCT/US2017/053947
申请日：2017-09-28
申请人： BOMBARDIER INC. , LEARJET INC.
发明人： CARON-L'ECUYER, Alexis , BRODEUR, Andre
IPC分类号： B64D13/06 , F24F13/24 , F24F13/068
摘要： An air duct includes a first chamber and a second chamber, the first chamber being defined between an air handling device and the second chamber, and the second chamber being defined between the first chamber and an environment exterior to the air duct, a plurality of first openings between the first chamber and the second chamber, a plurality of second openings between the second chamber and the environment exterior to the air duct, and a sound absorbing material defining at least a portion of an interior surface of at least one of the first chamber and the second chamber.
摘要翻译：空气管道包括第一腔室和第二腔室，第一腔室限定在空气处理装置与第二腔室之间，并且第二腔室限定在第一腔室与第一腔室外部的环境之间所述空气管道，所述第一腔室与所述第二腔室之间的多个第一开口，所述第二腔室与所述空气管道外部的环境之间的多个第二开口以及限定至少一部分内表面的第一腔室和第二腔室中的至少一个。

53. 发明申请

WO2018005529A1 TEMPERATURE MONITORING UNIT FOR AIRCRAFT WING STRUCTURE AND ASSOCIATED INSTALLATION METHOD 审中-公开
标题翻译：飞机翼结构温度监测装置及相关安装方法
公开(公告)号：WO2018005529A1
公开(公告)日：2018-01-04
申请号：PCT/US2017/039548
申请日：2017-06-27
申请人： BOMBARDIER INC. , LEARJET INC.
发明人： POLONI, Matthew , BRACKIN, JR., Robert Lewis , THOMAS, Dave James
IPC分类号： B64C3/00 , B64C9/22 , B64D15/04 , B64D45/00 , G01K7/16 , G01K11/06
摘要： A temperature monitoring unit may be removably installed inside an aircraft wing structure for monitoring temperature conditions along the span of the wing. The wing structure has a temperature-sensitive device (162) for monitoring a temperature condition, which is attached to a support frame (173). The support frame and attached temperature-sensitive device may be installed as a unit within the wing structure. The support frame may be configured for sliding engagement inside the wing structure, for example, with a set of tracks.
摘要翻译：温度监测单元可以可拆卸地安装在飞行器机翼结构内，用于监测沿机翼跨度的温度状况。机翼结构具有用于监测温度状况的温度敏感装置（162），该温度状态连接到支撑框架（173）。支撑框架和附属的温度敏感装置可作为一个单元安装在机翼结构内。支撑框架可以被配置用于在机翼结构内滑动接合，例如用一组轨道。

54. 发明申请

WO2017221123A1 GUST LOADING MANAGEMENT 审中-公开
标题翻译：必须加载管理
公开(公告)号：WO2017221123A1
公开(公告)日：2017-12-28
申请号：PCT/IB2017/053603
申请日：2017-06-16
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： MCCLEMENTS, Arthur , KROESE, Paul
IPC分类号： B64C9/12 , B64C13/16 , B64C13/50
摘要： The present disclosure provides methods and system for managing gust loading in an aircraft. A deflection angle of one or more spoilers of the aircraft is monitored. When the spoiler deflection angle is above a first threshold value, one or more aileron control signals are sent to the ailerons. The aileron control signals cause the ailerons to deflect based on the spoiler deflection angle.
摘要翻译：本公开提供了用于管理飞行器中的阵风负载的方法和系统。监测飞机的一个或多个扰流板的偏转角。当扰流偏转角高于第一阈值时，一个或多个副翼控制信号被发送到副翼。副翼控制信号会根据扰流板的偏转角度导致副翼偏转。

55. 发明申请

WO2017221122A1 CONTROL LAWS FOR PEDAL-TO-ROLL COUPLING 审中-公开
标题翻译：控制法兰间的耦合
公开(公告)号：WO2017221122A1
公开(公告)日：2017-12-28
申请号：PCT/IB2017/053602
申请日：2017-06-16
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： OLSTHOORN, Matthew , THERIEN, Sylvain , KRON, Aymeric , YAN, Zhe , STIHARU-ALEXE, Ilie
IPC分类号： G05D1/08 , B64C13/50
摘要： The present disclosure provides methods and system for controlling the operation of a fly- by-wire aircraft. One or more yaw commands are received from an operator control, and one or more actual induced rolls rates are determined based on the yaw commands. A yaw signal and a roll-countering command are sent to flight control components of the aircraft, the yaw signal to cause a yaw motion in the aircraft, and the roll-countering command to counter the actual induced rolls. A standardized roll rate command is determined based on the yaw command, and the standardized roll rate command is sent to the flight control components to cause a roll motion in the aircraft.
摘要翻译：本公开提供了用于控制电传飞机的操作的方法和系统。从操作员控制器接收一个或多个偏航命令，并且基于偏航命令确定一个或多个实际感应的滚动速率。向航空器的飞行控制部件发送偏航信号和滚转反向命令，偏航信号在飞机中引起偏航运动，并且滚转反向命令反击实际引起的滚动。基于偏航指令确定标准化的侧倾率命令，并将标准化的侧倾率命令发送给飞行控制部件以在飞机中引起侧倾运动。

56. 发明申请

WO2017208117A1 AIRCRAFT ENGINE ASSEMBLY 审中-公开
标题翻译：飞机发动机总成
公开(公告)号：WO2017208117A1
公开(公告)日：2017-12-07
申请号：PCT/IB2017/053072
申请日：2017-05-24
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： GOUDARD, Olivier , COLUNI, Angelo
IPC分类号： F02K1/76 , F02K1/72
摘要： An aircraft has a fuselage, left and right wings, and left and right engine assemblies connected to the wings. Each engine assembly has a nacelle, an engine housed in the nacelle, the engine having a plurality of rotors defining an uncontained rotor impact area, a pylon connecting the nacelle to its wing, at least one hydraulic actuator connected to at least one of the engine and the nacelle, at least one directional control valve hydraulically connected to the at least one hydraulic actuator, and at least one isolation valve hydraulically connected to the at least one directional control valve for selectively cutting off a supply of hydraulic fluid to the at least one directional control valve, the at least one isolation valve being disposed rearward of the uncontained rotor impact area and forward of a trailing edge of its corresponding wing.
摘要翻译：一架飞机有一个机身，左右翼，以及与机翼相连的左右发动机组件。每个发动机组件具有机舱，容纳在机舱中的发动机，发动机具有限定未被包围的转子冲击区域的多个转子，将机舱连接到其机翼的吊架，连接到发动机中的至少一个的至少一个液压致动器以及机舱，至少一个方向控制阀液压地连接到至少一个液压致动器，以及至少一个隔离阀，液压地连接到至少一个方向控制阀，用于选择性地切断至少一个液压流体的供应所述至少一个隔离阀布置在所述非包含转子冲击区域的后方并且位于其相应机翼的后缘的前方。

57. 发明申请

WO2017191543A1 CREW ALERTING SYSTEMS AND METHODS FOR MOBILE PLATFORMS 审中-公开
标题翻译：用于移动平台的船员警报系统和方法
公开(公告)号：WO2017191543A1
公开(公告)日：2017-11-09
申请号：PCT/IB2017/052518
申请日：2017-05-01
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： OUELLETTE, Benoit
IPC分类号： G06Q50/30 , B64D43/00
摘要： Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.
摘要翻译：公开了用于向飞机或其他移动平台的机组警告与飞机相关的相关状况的系统，设备和方法。一个示例性方法包括接收指示与飞机相关联的相关状况的存在的数据; 接收指示与相关条件相关联的动态参数的基本上实时值的数据; 以及在飞机的机组人员告警系统的显示区域中显示与相关状况相关的提高意识的指示。意识增强指示包括文本消息和指示与相关条件相关联的动态参数的基本上实时值的补充指示。在各种实施例中，补充指示可以是文本或图形的。补充指示也可以指示动态参数的目标值。

58. 发明申请

WO2017187300A1 AIRCRAFT PITCH CONTROL SYSTEM WITH ELECTRONICALLY GEARED ELEVATOR 审中-公开
标题翻译：具有电子齿轮电梯的飞机俯仰控制系统
公开(公告)号：WO2017187300A1
公开(公告)日：2017-11-02
申请号：PCT/IB2017/052257
申请日：2017-04-19
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： AHN, Thomas , TANNER, Clinton Eric , NELSON, Thomas , BLACK, Scott
IPC分类号： B64C5/16 , B64C9/04 , B64C13/50 , G05D1/06 , G05D1/08
摘要： Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system (28) comprises a movable horizontal stabilizer (24) and an elevator (26) movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.
摘要翻译：公开了飞机桨距控制系统和方法。飞机俯仰控制系统（28）包括可移动的水平稳定器（24）和可移动地联接到水平稳定器的升降器（26）。电梯的电子齿轮与水平稳定器相连。

59. 发明申请

WO2017141213A1 VEHICLE COLOR-LIGHTING CONTROL SYSTEM AND METHOD 审中-公开
标题翻译：车辆彩色照明控制系统和方法
公开(公告)号：WO2017141213A1
公开(公告)日：2017-08-24
申请号：PCT/IB2017/050926
申请日：2017-02-17
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： HACK, Jonathan Wayne
IPC分类号： B60Q3/43 , B60Q3/74 , B60Q3/80 , B60Q3/47 , B64D11/00
CPC分类号： B60Q3/43 , B60Q3/47 , B60Q3/74 , B60Q3/80 , B64D2011/0038
摘要： There is described a vehicle color-lighting control system. The system comprises at least one sidewall (101) having an electrically-controllable coloring mechanism (106) embedded therein and arranged for coloring at least a portion of the at least one sidewall with at least one first color; a lighting sub-system (110) comprising at least one light source (112) mounted within the vehicle to illuminate an interior of the vehicle with at least one second color in a first state and with at least one third color in a second state; and a controller coupled to the coloring mechanism and the lighting sub-system and configured for operating the coloring mechanism to color the at least one portion of the at least one sidewall with the at least one first color and concurrently illuminate the interior of the vehicle with the at least one second color.
摘要翻译：描述了一种车辆颜色照明控制系统。所述系统包括至少一个侧壁（101），所述侧壁具有嵌入其中的电可控着色机构（106）并且布置成用至少一种第一颜色给所述至少一个侧壁的至少一部分着色; 照明子系统（110），其包括安装在所述车辆内的至少一个光源（112），以用第一状态的至少一种第二颜色和处于第二状态的至少一种第三颜色照亮所述车辆的内部; 以及控制器，其耦合到所述着色机构和所述照明子系统，并且被配置成用于操作所述着色机构以利用所述至少一种第一颜色对所述至少一个侧壁的所述至少一部分着色，并同时用所述车辆的内部照明至少有一种第二种颜色。

60. 发明申请

WO2017093871A1 MOBILE PLATFORM CABIN CONFIGURED FOR PASSENGER AND CARGO TRANSPORT 审中-公开
标题翻译：移动平台客舱配置为客运和货物运输
公开(公告)号：WO2017093871A1
公开(公告)日：2017-06-08
申请号：PCT/IB2016/057140
申请日：2016-11-25
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： CORBETT, Kent , MABEE, Stephen
IPC分类号： B64D9/00 , B60P7/14
CPC分类号： B64D9/00 , B64C1/10 , B64D9/003 , B64D11/0023 , Y02T50/46
摘要： The mobile platform cabin (20) disclosed herein comprises a passenger portion (22), a first cargo portion (24) disposed aft of the passenger portion (22), a partition (36) separating the passenger portion (22) from the first cargo portion (24), a second cargo portion (26) disposed aft of the first cargo portion (24) and a barrier net (38) separating the first cargo portion (24) from the second cargo portion (26). The first cargo portion (24) comprises a cargo-receiving zone (40) and a stay-out zone (44) in which cargo is not permitted. The barrier net (38) is configured to distend into the first cargo portion (24) when restraining forward movement of cargo (48) in the second cargo portion due to the cargo (48) in the second cargo portion being subjected to an acceleration relative to the cabin. At least part of the distension of the barrier net (38) is accommodated by the stay-out zone (44) of the first cargo portion (24).
摘要翻译：本文公开的移动平台客舱（20）包括乘客部分（22），设置在乘客部分（22）后面的第一货物部分（24），将乘客部分（24）的第一部分（22），设置在第一货物部分（24）后面的第二货物部分（26）和将第一货物部分（24）与第二货物部分（26）。第一货物部分（24）包括不允许货物的货物接收区（40）和停留区（44）。当限制第二货物部分中的货物（48）由于第二货物部分中的货物（48）经受相对加速度而相对于第二货物部分向前移动时，阻挡网（38）被构造成扩展到第一货物部分到客舱。阻挡网（38）的至少一部分扩张部分由第一货物部分（24）的停留区（44）容纳。

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