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61. 发明申请

WO2017089926A1 GROMMET 审中-公开
公开(公告)号：WO2017089926A1
公开(公告)日：2017-06-01
申请号：PCT/IB2016/056873
申请日：2016-11-15
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： BRAIS, Sylvain , DESJARDINS, Mathieu
IPC分类号： F16L5/00 , F16L3/20 , F16B9/02 , B64C1/40
CPC分类号： F16L3/137 , B64C1/406 , F16B9/023 , F16L5/00 , F16L5/027
摘要： A grommet for surrounding a conduit received through a hole in a part, including a grommet body configured for engagement with a perimeter of the hole in the part and defining a closed or substantially closed perimeter, and a plurality fingers, the fingers extending axially from the grommet body and being circumferentially spaced from one another, each of the fingers being elongated and having a free end axially spaced from the grommet body. An assembly includes the part, the grommet, the conduit, and an adjustable length fastener spaced from the part, the adjustable length fastener forming a loop having an adjustable perimeter, the conduit and the fingers extending within the loop, the adjustable length fastener retaining the fingers against the outer surface of the conduit. A method of supporting a conduit within a hole through a part is also discussed.
摘要翻译：用于围绕通过部件中的孔接收的导管的护环，所述护环包括配置用于与部件中的孔的周边接合并限定闭合或基本闭合的周边的索环本体，以及多个所述指状物从所述索环主体轴向延伸并且沿周向彼此间隔开，每个所述指状物都是细长的并且具有与所述索环主体轴向隔开的自由端。组件包括该部件，护环，导管以及与该部件间隔开的可调节长度的紧固件，可调节长度的紧固件形成具有可调节周边的环，导管和指状件在环内延伸，可调节长度紧固件保持手指抵靠导管的外表面。还讨论了通过零件在孔内支撑导管的方法。

62. 发明申请

WO2017068497A1 METHOD AND APPARATUS FOR FORMING A COMPOSITE SKIN-STIFFENER ASSEMBLY 审中-公开
标题翻译：形成复合皮肤 - 增强器组件的方法和设备
公开(公告)号：WO2017068497A1
公开(公告)日：2017-04-27
申请号：PCT/IB2016/056257
申请日：2016-10-18
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： CARON, Richard , RIFAY, Mouhcine , SALEK, Hasan , HOSTE, Didier , LANGLOIS, Richard
IPC分类号： B29C70/44 , B29C33/50 , B29C33/76 , B29D99/00 , B64C1/06 , B64C3/18 , B64C1/00
CPC分类号： B29C70/446 , B29C33/505 , B29C33/76 , B29D99/0014 , B29D99/0025 , B64C1/064 , B64C3/182 , B64C2001/0072 , Y02T50/43
摘要： A method of forming a composite part (10) having a skin (12) and at least one elongated stiffener (14) extending from the skin (12), the method comprising: providing a mold (20) having a mold surface (22, 26) and a respective elongated compaction cavity for each stiffener (14), each compaction cavity (24) opening into the mold surface (22, 26); for each stiffener (14): placing a bagged insert (30) including an insert (40) received in a tubular bag (42) in the respective compaction cavity (24), supporting the stiffener (14) with the bagged insert (30), the stiffener (14) having a first part extending in the compaction cavity (24) snuggly between a side surface of the bagged insert (30) and an adjacent side surface of the mold (20) bordering the compaction cavity (24), the stiffener (14) having a second part connected to the first part and extending over at least one of the mold surface (22, 26) and a top surface of the bagged insert (30); placing a skin (12) over and in contact with the mold surface (22, 26), and over and in contact with the second part of each stiffener (14); forming a sealed enclosure containing the skin (12) and each stiffener (14), the sealed enclosure being formed in part by each tubular bag (42), each insert being located outside of the sealed enclosure; reducing a pressure within the sealed enclosure; removing each insert from the tubular bag (42); and curing the skin (12) and each stiffener (14). An insert assembly and an assembly for forming a composite part (10) are also discussed.
摘要翻译：一种形成具有蒙皮（12）和从所述蒙皮（12）延伸的至少一个细长加强件（14）的复合部件（10）的方法，所述方法包括：提供模具（20 ）具有用于每个加强件（14）的模具表面（22,26）和相应的细长压实腔，每个压实腔（24）通向模具表面（22,26）; 对于每个加强件（14）：将包括容纳在管状袋（42）中的插入件（40）的袋装插入件（30）放置在相应的压实腔（24）中，用袋装插入件（30）支撑加强件（14），所述加强件（14）具有第一部分和第二部分，所述第一部分紧密地在所述袋装插入件（30）的侧表面和邻接所述压实腔（24）的所述模具（20）的相邻侧表面之间在所述压实腔（24）中延伸，所述（14），其具有连接到所述第一部分并且在所述模具表面（22,26）和所述袋装嵌入件（30）的顶部表面中的至少一个上方延伸的第二部分; 将表皮（12）放置在模具表面（22,26）上并与模具表面（22,26）接触，并且在每个加强件（14）的第二部分上方并与之接触; 形成包含蒙皮（12）和每个加强件（14）的密封外壳，密封外壳部分地由每个管状袋（42）形成，每个插入件位于密封外壳的外部; 减小密封外壳内的压力; 从管状袋（42）中取出每个插入物; 并固化蒙皮（12）和每个加强件（14）。还讨论了插入组件和用于形成复合部件（10）的组件。

63. 发明申请

WO2017055975A1 METHOD OF AND SYSTEM FOR PRESENTING AN OPERATING STATUS OF AN AIRCRAFT ENGINE 审中-公开
标题翻译：提供飞机发动机的运行状态的方法和系统
公开(公告)号：WO2017055975A1
公开(公告)日：2017-04-06
申请号：PCT/IB2016/055673
申请日：2016-09-22
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： DANIELSON, Michael Dwight , GALLEA, Mathieu
IPC分类号： B64D31/00 , G01D7/08 , B64D43/00 , B64D45/00
CPC分类号： B64D43/00 , B64D31/00 , B64D45/00 , G01C23/00 , G01D7/08
摘要： A method of and a system for presenting an operating status of an aircraft engine. The method comprises accessing a first indication indicative of a position of an aircraft engine start switch and accessing a second indication indicative of an aircraft engine start operating mode, the second indication having been generated based on an analysis of a parameter associated with an operating condition of the aircraft engine. The method, upon determining that the position of the aircraft engine start switch is an "on" position and the aircraft engine start operating mode is a healthy start causes the display of a visual indication indicative of the healthy start. The method upon determining that the position of the aircraft engine start switch is an "on" position and the aircraft engine start operating mode is an abnormal start causes the display of a visual indication indicative of the abnormal start.
摘要翻译：一种用于呈现飞机发动机的操作状态的方法和系统。该方法包括访问指示飞机发动机启动开关的位置的第一指示并且访问指示飞机发动机起动操作模式的第二指示，所述第二指示是基于与与运行条件的操作条件相关联的参数的分析而生成的飞机发动机。该方法在确定飞行器发动机起动开关的位置是“开”位置并且飞行器发动机起动操作模式是健康的起动时，显示表示健康的起动的视觉指示。在确定飞机发动机起动开关的位置是“开”位置并且飞机发动机起动操作模式是异常起动的方法导致显示表示异常起动的视觉指示。

64. 发明申请

WO2017042712A1 APPARATUS AND METHODS FOR DISTRIBUTING ELECTRIC POWER ON AN AIRCRAFT DURING A LIMITED POWER AVAILABILITY CONDITION 审中-公开
标题翻译：用于在有限的动力可用性条件下分配飞机上的电力的装置和方法
公开(公告)号：WO2017042712A1
公开(公告)日：2017-03-16
申请号：PCT/IB2016/055362
申请日：2016-09-08
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： NFONGUEM, Gustave , ILIESCU, Vlad
IPC分类号： B64D41/00
CPC分类号： B64D41/00 , B64D41/007 , B64D2221/00 , Y02T50/44
摘要： Methods and apparatus for distributing electric power from a power source of an aircraft to a plurality of electrical loads of the aircraft during a limited power availability condition are disclosed. An exemplary method comprises: distributing electric power from the power source of the aircraft to the plurality of electrical loads; receiving one or more signals indicative of a demand for electric power by one or more of the plurality of electrical loads; and adjusting the power distribution to the plurality of electrical loads based on the demand for electric power by the one or more plurality of electrical loads. The power distribution is also adjusted to maintain an overall power consumption of the plurality of electrical loads at or below a threshold.
摘要翻译：公开了在有限的功率可用性条件期间将电力从飞行器的电源分配到飞行器的多个电负载的方法和装置。一种示例性方法包括：将电力从飞机的电源分配到多个电负载; 通过所述多个电负载中的一个或多个接收指示电力需求的一个或多个信号; 以及基于所述一个或多个多个电负载对电力的需求来调整对所述多个电负载的功率分配。还调整功率分布以维持等于或低于阈值的多个电负载的总功耗。

65. 发明申请

WO2016189421A1 AIRFLOW MANAGEMENT IN CABIN OF AIRCRAFT 审中-公开
标题翻译：飞机仓库空气管理
公开(公告)号：WO2016189421A1
公开(公告)日：2016-12-01
申请号：PCT/IB2016/052832
申请日：2016-05-16
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： FAGUNDES, Sandro, A.S. , MEISLITZER, Boris , AYRE, Keith
IPC分类号： B64D13/00 , B64D13/06
CPC分类号： B64D13/08 , B64D13/00 , B64D13/04 , B64D13/06 , B64D2013/0688 , Y02T50/54 , Y02T50/56
摘要： Cabin air is managed in the aircraft as a function of the minimum requirements for defined air quality needs, temperature control needs, and cabin pressurization needs. Airflow may be varied dynamically as a function of aircraft or cabin altitude, and the minimum requirements for airflow may be determined in real time so as to dynamically set an airflow schedule.
摘要翻译：客舱空气在飞机上进行管理，作为对空气质量需求，温度控制需求和客舱加压需求的最低要求的函数。气流可以作为飞机或机舱高度的函数而动态变化，并且可以实时确定气流的最小要求，以便动态地设定气流调度。

66. 发明申请

WO2015162542A9 BUFFER ZONE FOR INTERIOR AIRCRAFT FEATURES 审中-公开
标题翻译：缓冲区的内部飞机功能
公开(公告)号：WO2015162542A9
公开(公告)日：2016-11-24
申请号：PCT/IB2015052876
申请日：2015-04-20
申请人： BOMBARDIER INC , SHORT BROTHERS PLC
发明人： MALEK BRUCE , HOLOWKA STEFAN , BEAUDIN NIKOLAS
IPC分类号： B64C1/06
CPC分类号： B64C1/066 , B64C1/10 , B64D11/0023 , B64D2011/0046 , B64F5/10
摘要： Several embodiments of buffer zones are provided that are contemplated to be disposed with respect to two or more adjacent elements on an aircraft. The buffer zones adjust for dynamic spacing between the elements to help control different gapping requirements between the elements installed in the aircraft. Embodiments include an aircraft interior panel configuration, an aircraft interior wall panel configuration, an adjustable width aircraft bulkhead, and an aircraft personal service unit.
摘要翻译：提供缓冲区的几个实施例，其被设想为相对于飞机上的两个或更多个相邻元件进行布置。缓冲区调整元件之间的动态间距，以帮助控制安装在飞机上的元件之间的不同间隙要求。实施例包括飞机内部面板配置，飞机内部墙板配置，可调节宽度的飞机舱壁以及飞机个人服务单元。

67. 发明申请

WO2016092440A1 HEADREST WITH ADJUSTABLE SIDE ELEMENTS 审中-公开
标题翻译：具有可调节的元素的头部
公开(公告)号：WO2016092440A1
公开(公告)日：2016-06-16
申请号：PCT/IB2015/059372
申请日：2015-12-04
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： LESSARD, David
IPC分类号： B60N2/48
CPC分类号： B60N2/885 , B60N2/888
摘要： A headrest for a seat of a vehicle includes a body securable to the seat, a side portion adjacent the body, a receiver pivotally attached to the body, a slide attached to the side portion so as to be movable along the receiver between a first position in which the side portion is in a retracted position and a second position in which the side portion is in an extended position, and a friction member on one of the receiver and the slide. A securing mechanism causes the friction member to hold the slide in a selected position relative to the receiver.
摘要翻译：用于车辆座椅的头枕包括可安装到座椅的主体，与身体相邻的侧部，可枢转地附接到主体的接收器，附接到侧部的滑块，以便能够沿着接收器在第一位置其中所述侧部处于缩回位置，并且所述侧部处于伸出位置的第二位置以及所述接收器和所述滑块中的一个上的摩擦构件。固定机构使得摩擦构件相对于接收器将滑块保持在选定位置。

68. 发明申请

WO2016092438A1 METHOD OF MAKING PAD-UPS FOR COMPOSITE STRUCTURES AND COMPOSITE STRUCTURES INCLUDING PAD-UPS 审中-公开
标题翻译：用于复合结构的PAD-UPS的制造方法和包括PAD-UPS的复合结构
公开(公告)号：WO2016092438A1
公开(公告)日：2016-06-16
申请号：PCT/IB2015/059367
申请日：2015-12-04
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： DE GROSBOIS, Marc - Arthur , LACHANCE, Jean - Philippe
IPC分类号： B29C70/34 , B29C70/38 , B29D99/00
CPC分类号： B64C3/185 , B29C70/08 , B29C70/24 , B29C70/34 , B29C70/382 , B29C70/50 , B29C70/887 , B29D24/008 , B29D99/0003 , B29D99/0014 , B29L2031/3085 , B64C1/068 , Y02T50/43
摘要： A composite component (16) for a vehicle (10) includes a laminate (18) made from a composite material, a first pad-up area (22) applied to the laminate (18), where the first pad-up area (22) includes a plurality of first tows laid next to one another in a side-by-side arrangement and where the first pad-up area (22) defines a first fiber orientation, and a second pad-up area (24), where the second pad-up area (24) includes a plurality of second tows laid next to one another in a side-by-side arrangement and where the second pad-up area (24) defines a second fiber orientation that differs by a predetermined angle from the first fiber orientation. The first pad-up area (22) and the second pad-up area (22) intersect at an intersecting area and together form a first pad-up ply on the laminate (18).
摘要翻译：用于车辆（10）的复合部件（16）包括由复合材料制成的层压体（18），施加到层叠体（18）的第一平铺区域（22），其中第一平铺区域（22））包括以并排布置彼此相邻放置的多个第一丝束，并且其中所述第一垫片区域（22）限定第一纤维取向，以及第二垫片区域（24），其中第二垫片区域（24）包括并列布置的彼此相邻的多个第二丝束，并且其中第二垫片区域（24）限定与第一纤维取向不同的第二纤维取向第一个纤维取向。第一平铺区域（22）和第二平铺区域（22）在交叉区域相交并且一起形成层叠体（18）上的第一平铺层。

69. 发明申请

WO2016049346A8 AIRCRAFT SEAT 审中-公开
标题翻译：飞机座位
公开(公告)号：WO2016049346A8
公开(公告)日：2016-03-31
申请号：PCT/US2015/052002
申请日：2015-09-24
申请人： BOMBARDIER INC. , LEARJET INC. , ERHEL, Philippe
发明人： ERHEL, Philippe
IPC分类号： B60N2/06 , B60N2/14
摘要： A vehicle seat includes a seat, a swivel connected to and rotatably supporting the seat, a swivel frame connected to the swivel, a first lateral rail supporting the swivel frame, the first lateral rail permitting the swivel frame to move in a first direction, and a first longitudinal rail supporting the first lateral rail such that the first lateral rail is movable along the first longitudinal rail, thereby permitting the swivel frame to move in a second direction that is perpendicular to the first direction.
摘要翻译：车辆座椅包括座椅，连接到座椅并可旋转地支撑座椅的旋转架，连接到旋转架的旋转架，支撑旋转架的第一侧轨，第一侧轨允许旋转架以沿第一方向移动;以及第一纵向导轨，其支撑所述第一侧向导轨，使得所述第一侧向导轨可沿着所述第一纵向导轨移动，由此允许所述旋转框架沿垂直于所述第一方向的第二方向移动。

70. 发明申请

WO2016046788A1 LASER VISION INSPECTION SYSTEM AND METHOD 审中-公开
标题翻译：激光视觉检测系统和方法
公开(公告)号：WO2016046788A1
公开(公告)日：2016-03-31
申请号：PCT/IB2015/057365
申请日：2015-09-24
申请人： BOMBARDIER INC. , SHORT BROTHERS PLC
发明人： SHADMEHRI, Farjad
IPC分类号： G01B21/04 , G01B11/00 , G01B11/25
CPC分类号： G01B11/002 , G01B11/16 , G01B11/25 , G01B21/045 , G01N21/1717 , G01N29/2418 , Y02B10/30
摘要： There is described herein a method and system for inspecting various fabrication features of composite components, such as tow/ply location, angle deviation, and gap size, using a laser-vision assembly. In some embodiments, a tolerance for that fabrication feature is provided as an inspection feature and a laser projecting device projects the inspection feature onto the material. Alternatively or in combination thereof, a calibration feature is projected onto the material, the calibration feature comprising known dimensional information. An image acquisition device acquires an image of the material with the inspection/calibration feature(s) projected thereon. The images can be analysed automatically or manually to detect whether the fabrication features are compliant and/or to obtain measurement data of the fabrication features.
摘要翻译：这里描述了使用激光视觉组件来检查复合部件的各种制造特征的方法和系统，例如丝束/层位置，角度偏差和间隙尺寸。在一些实施例中，提供了该制造特征的公差作为检查特征，并且激光投射装置将检查特征投影到材料上。替代地或组合地，将校准特征投影到材料上，校准特征包括已知的尺寸信息。图像采集装置获取投射有检查/校准特征的材料的图像。可以自动或手动地分析图像，以检测制造特征是否符合和/或获得制造特征的测量数据。

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