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公开(公告)号：US20180297299A1
公开(公告)日：2018-10-18
申请号：US15768361
申请日：2016-10-18
Applicant: BOMBARDIER INC.
Inventor： Richard CARON , Mouhcine RIFAY , Hasan SALEK , Didier HOSTE , Richard LANGLOIS
Abstract: 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.
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公开(公告)号：US20180286531A1
公开(公告)日：2018-10-04
申请号：US15736571
申请日：2016-06-17
Applicant: BOMBARDIER INC.
Inventor： Anthony EL HADDAD , Philippe DESY , Jean-Guy GAUDREAU
CPC classification number: H01B7/009 , B60R16/0207 , B64D47/00 , B64D2221/00 , F16D66/00 , H01B7/0045 , H01R24/28
Abstract: 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.
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公开(公告)号：US20180281990A1
公开(公告)日：2018-10-04
申请号：US15778164
申请日：2015-11-23
Applicant: BOMBARDIER INC.
Inventor： Tim FAGAN , Erin MURPHY , Linsey NANCARROW , Jeff BARTENBACH
Abstract: 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.
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公开(公告)号：US20180180446A1
公开(公告)日：2018-06-28
申请号：US15128739
申请日：2015-03-23
Applicant: BOMBARDIER INC.
Inventor： Timothy SMITH
Abstract: 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.
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Patent Agency Ranking
66.发明申请公开(公告)号：US20180162540A1
公开(公告)日：2018-06-14
申请号：US15576996
申请日：2016-05-27
Applicant: BOMBARDIER INC.
Inventor： Alexandros ILIOPOULOS , Laurent REGNAULT , Marcin KULCZYK , Alain RICHER
Abstract: 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.
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公开(公告)号：US20180072433A1
公开(公告)日：2018-03-15
申请号：US15558779
申请日：2016-03-07
Applicant: BOMBARDIER INC.
Inventor： Jean-Marc LECLERC
CPC classification number: B64F5/60 , B64D13/02 , B64D43/02 , B64F5/10 , G01C21/165
Abstract: 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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公开(公告)号：US20180050809A1
公开(公告)日：2018-02-22
申请号：US15557871
申请日：2016-03-07
Applicant: BOMBARDIER INC.
Inventor： Stephen COLAVINCENZO , Andre BRODEUR , Alexis CARON L'ECUYER , Mirel BOGDAN , Dragan JOVICIC
CPC classification number: B64D31/12 , F02C9/18 , F02C9/28 , F02C9/42 , F05D2220/323
Abstract: Methods and related apparatus for improving synchronization of two or more engines on an aircraft are disclosed. Such method may be used where each engine comprises a first spool and a second spool, and, where a rotational speed of a first spool of a first engine has been substantially synchronized with a rotational speed of a first spool of a second engine. An exemplary method comprises receiving a value of a sensed parameter useful in controlling the first engine; adding a bias to the value; and using the biased value for controlling the first engine to cause a change in rotational speed of the second spool of the first engine in relation to the rotational speed of the first spool of the first engine.
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公开(公告)号：US20170365049A1
公开(公告)日：2017-12-21
申请号：US15532799
申请日：2015-11-30
Applicant: BOMBARDIER INC.
Inventor： Octavian IOACHIM
CPC classification number: G06T7/0004 , B28B1/523 , B28B17/0072 , B29C70/384 , B29C70/388 , B29C70/54 , B29K2105/06 , G01N21/8806 , G01N2021/8472 , G01N2021/8825 , G06T2207/30164 , H04N5/2256
Abstract: There is described an online inspection method and system having an illumination system that provides bright-field and dark-field illumination concurrently or sequentially, at varying intensities, in order to acquire images that may be read by an image processing device. The image processing device may obtain measurements of features in the images and evaluate acceptability of the features.
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公开(公告)号：US09821902B2
公开(公告)日：2017-11-21
申请号：US14771974
申请日：2014-02-26
Applicant: Bombardier Inc.
Inventor： Robert Young , Yves Grenier , Hany Sadek
CPC classification number: B64C13/04 , B64C9/28 , B64C13/16 , B64D2045/001
Abstract: 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.
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