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51. 发明申请

US20190092474A1 IN-VEHICLE POSITION DETECTION AND CONFIGURATION OF VEHICLE COMPONENTS 审中-公开
公开(公告)号：US20190092474A1
公开(公告)日：2019-03-28
申请号：US16199626
申请日：2018-11-26
申请人： BOMBARDIER INC.
发明人： Alexis MORIN , Marc Kirmoyan , Brad Nolen
IPC分类号： B64D11/00 , H04W4/02 , H04L29/08 , H04W4/33 , H04W4/021 , H04W4/40 , H04W4/80
摘要： There is described herein a method and system for the configuration of vehicle management components using in-vehicle position detection. The in-vehicle position detection may also be used for providing a floor plan of the vehicle. In some embodiments, in-vehicle position detection may be used concurrently for configuring vehicle management components and for providing floor plans.

52. 发明授权

US10222766B2 System and method of operation of the system incorporating a graphical user interface on a mobile computing device for a member of a flight crew in a vehicle cabin 有权
公开(公告)号：US10222766B2
公开(公告)日：2019-03-05
申请号：US14165068
申请日：2014-01-27
申请人： BOMBARDIER INC.
发明人： Tim Michael Fagan , Erin Murphy , Linsey Nancarrow , Jeff Bartenbach
IPC分类号： G05B15/02 , B64D11/00
摘要： A method of operation for a system incorporating a graphical user interface in a mobile computing device for a crew member 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 include a plurality of controllable parameters selected from a group encompassing light intensity, light color, temperature, and the degree of openness of at least one window shade. A system and executable computer program product also are provided.

53. 发明授权

US10167082B2 In-vehicle position detection and configuration of vehicle components 有权
公开(公告)号：US10167082B2
公开(公告)日：2019-01-01
申请号：US15526658
申请日：2015-11-09
申请人： BOMBARDIER INC.
发明人： Alexis Morin , Marc Kirmoyan , Brad Nolen
IPC分类号： G08G1/02 , B64D11/00 , H04W4/02 , H04W4/04 , H04L29/08 , H04W4/80 , H04W4/021
摘要： There is described herein a method and system for the configuration of vehicle management components using in-vehicle position detection. The in-vehicle position detection may also be used for providing a floor plan of the vehicle. In some embodiments, in-vehicle position detection may be used concurrently for configuring vehicle management components and for providing floor plans.

54. 发明申请

US20180297299A1 METHOD AND APPARATUS FOR FORMING A COMPOSITE SKIN-STIFFENER ASSEMBLY 审中-公开
公开(公告)号：US20180297299A1
公开(公告)日：2018-10-18
申请号：US15768361
申请日：2016-10-18
申请人： BOMBARDIER INC.
发明人： Richard CARON , Mouhcine RIFAY , Hasan SALEK , Didier HOSTE , Richard LANGLOIS
IPC分类号： B29C70/44 , B29C33/76 , B64C3/18 , B29D99/00 , B64C1/06
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.

55. 外观设计

USD830085S1 Aircraft credenza 有权
公开(公告)号：USD830085S1
公开(公告)日：2018-10-09
申请号：US29593184
申请日：2017-02-07
申请人： BOMBARDIER INC.
设计人： Alexandre Curthelet , Adrian Goring , Louis-Xavier Lavallee , Louis Gagnon-Seguin , Timothy Michael Fagan

56. 发明申请

US20180286531A1 CONFIGURABLE HARNESS 审中-公开
公开(公告)号：US20180286531A1
公开(公告)日：2018-10-04
申请号：US15736571
申请日：2016-06-17
申请人： BOMBARDIER INC.
发明人： Anthony EL HADDAD , Philippe DESY , Jean-Guy GAUDREAU
IPC分类号： H01B7/00 , B64D47/00 , H01R24/28
CPC分类号： H01B7/009 , B60R16/0207 , B64D47/00 , B64D2221/00 , F16D66/00 , H01B7/0045 , H01R24/28
摘要： There is described herein a harness (106) that remains neutral until configured by a configuration device (110). Wires that connect to specific pins responsible for the configuration of a system are taken out and connected to a configuration port (108) on the harness (106). The configuration port (108), when mated with the configuration device (110), sets a configuration setting of the system. The configuration device (110) may be used to set the power and/or signal parameters of the harness (106) for a system or to configure various options within the system itself or another system.

57. 发明申请

US20180281990A1 SYSTEM AND METHOD FOR REPRESENTING A LOCATION OF A FAULT IN AN AIRCRAFT CABIN 审中-公开
公开(公告)号：US20180281990A1
公开(公告)日：2018-10-04
申请号：US15778164
申请日：2015-11-23
申请人： BOMBARDIER INC.
发明人： Tim FAGAN , Erin MURPHY , Linsey NANCARROW , Jeff BARTENBACH
IPC分类号： B64F5/60 , B64D45/00 , H04L29/08
摘要： A method and a distributed architecture for representing a location of a fault in an aircraft cabin, comprising: a controller operatively connected to a processor; a crew IO node operatively connected to the controller; the processor being configured to perform: detecting, by the controller, that an event of a system of the aircraft cabin corresponding to a fault has occurred; determining, by the processor, which aircraft cabin section amongst a plurality of aircraft cabin sections is associated with the system for which the event corresponding to the fault has occurred; and displaying, on the crew IO node, (i) a graphical user interface (GUI) component representing at least a portion of the aircraft cabin comprising at least some of the plurality of aircraft cabin sections and (ii) a visual indication identifying the aircraft cabin section associated with the system for which the event corresponding to the fault has occurred.

58. 发明申请

US20180180446A1 SYSTEM FOR DETECTING MECHANICAL DISCONNECT OF A SENSOR FROM A CONTROLLED ELEMENT 有权
公开(公告)号：US20180180446A1
公开(公告)日：2018-06-28
申请号：US15128739
申请日：2015-03-23
申请人： BOMBARDIER INC.
发明人： Timothy SMITH
IPC分类号： G01D3/08 , G01D5/22 , B64C13/42
摘要： A system for detecting mechanical failure of a connection between a variable differential transformer and a controlled element. The sensor system includes a variable differential transformer with a housing encapsulating a first coil, a bore in the housing, wherein the bore is adjacent to the first coil, a core disposed in the bore, a shaft connectible between the core, at a first end, and the controlled element, at a second end, and a biasing element connected to the shaft. Responsive to a break in the shaft, the biasing element moves the core to an out-of-range position detectable by at least the first coil.

59. 发明申请

US20180162540A1 METHOD AND SYSTEM FOR ALIGNING PROPULSION SYSTEM AND VEHICLE HAVING SUCH PROPULSION ALIGNMENT 审中-公开
公开(公告)号：US20180162540A1
公开(公告)日：2018-06-14
申请号：US15576996
申请日：2016-05-27
申请人： BOMBARDIER INC.
发明人： Alexandros ILIOPOULOS , Laurent REGNAULT , Marcin KULCZYK , Alain RICHER
IPC分类号： B64D27/18 , B64F5/10 , G01M1/12
CPC分类号： B64D27/18 , B64C15/02 , B64F5/10 , G01M1/125
摘要： An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thrust vector axis, where the turbofan engine (18) is disposed on the aircraft with the thrust vector feature (43) oriented with respect to the reference axis of the aircraft.

60. 发明申请

US20180072433A1 SIMULATION OF LOADS ON AEROSTRUCTURES DURING AIRCRAFT ASSEMBLY 审中-公开
公开(公告)号：US20180072433A1
公开(公告)日：2018-03-15
申请号：US15558779
申请日：2016-03-07
申请人： BOMBARDIER INC.
发明人： Jean-Marc LECLERC
IPC分类号： B64F5/60 , B64F5/10 , B64D43/02 , G01C21/16
CPC分类号： B64F5/60 , B64D13/02 , B64D43/02 , B64F5/10 , G01C21/165
摘要： Methods and systems useful during assembly of aircraft are disclosed. One such method comprises loading a fuselage of the aircraft that is unassembled with a wing of the aircraft to obtain a configuration of the fuselage corresponding to when the fuselage is assembled with the wing. The method also comprises calibrating a device of a navigation system of the aircraft when the fuselage is unassembled with the wing and is being loaded to obtain the loaded configuration and, after calibrating the device of the navigation system, assembling the fuselage with the wing.

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