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公开(公告)号：US20160144944A1
公开(公告)日：2016-05-26
申请号：US14900973
申请日：2014-07-11
Applicant: William A. GOINGS , Eric LONG , LEARJET INC. , C&D ZODIAC INC.
Inventor： William A. GOINGS , Eric LONG
CPC classification number: B64C1/14 , B64D11/0023 , B64D11/02 , E05F11/54 , E05Y2900/502
Abstract: A door for an aircraft includes a first panel divisible into at least two first slats that are releasably connected to one another, a first tensioning cable attached between the at least two first slats, and a first tensioner connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.
Abstract translation: 一种用于飞行器的门包括可分成至少两个彼此可释放地连接的第一板条的第一板，连接在所述至少两个第一板条之间的第一张紧绳索，以及连接到所述第一张紧绳索并且被操作的第一张紧器 以向其施加第一张力，从而允许第一张紧缆索将至少两个第一板条保持在一起以形成第一板，并且在出现释放动作时释放第一张紧缆索中的第一张力，从而允许至少 两个第一个板条彼此离解，使第一个面板碎片。
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公开(公告)号：US20150307208A1
公开(公告)日：2015-10-29
申请号：US14441413
申请日：2013-11-14
Applicant: LEARJET INC.
Inventor： Harris K. BUTLER, III , Kris RUSTMAN
CPC classification number: B64D47/08 , B64C1/1407 , B64D45/00 , G02B6/06 , G02B23/08 , H04N7/183 , H04N7/186
Abstract: A viewing device for an aircraft includes an image receiver adapted to receive an image of a predetermined spatial area of an exterior of an aircraft, an image projector adapted to display the image of the predetermined spatial area, and an image conduit connecting the image receiver to the image projector. The image receiver is adapted to be positioned on an exterior side of the aircraft below a lateral width of a fuselage of the aircraft while the image projector is adapted to be positioned on an interior side of the aircraft above the lateral width of the fuselage of the aircraft. The image projector is adapted to be positioned at a first predetermined height above a floor on the interior side of the aircraft, consistent with a person's eye level. The image projector is separated from the image receiver by a first predetermined distance.
Abstract translation: 一种用于飞行器的观察装置，包括适于接收飞机外部预定空间区域的图像的图像接收器，适于显示预定空间区域的图像的图像投影仪，以及将图像接收器连接到 图像投影机。 图像接收器适于被定位在飞行器的外侧，在飞机的机身的横向宽度之下，同时图像投影仪适于被定位在飞行器的内侧，高于机身的机身的横向宽度 飞机。 图像投影仪适于被定位在飞行器内侧上的地板上方的第一预定高度，与人的眼睛水平一致。 图像投影仪与图像接收器分离第一预定距离。
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公开(公告)号：US10252818B2
公开(公告)日：2019-04-09
申请号：US14441413
申请日：2013-11-14
Applicant: LEARJET INC. , Harris K. Butler, III , Kris Rustman
Inventor： Harris K. Butler, III , Kris Rustman
Abstract: A viewing device for an aircraft includes an image receiver adapted to receive an image of a predetermined spatial area of an exterior of an aircraft, an image projector adapted to display the image of the predetermined spatial area, and an image conduit connecting the image receiver to the image projector. The image receiver is adapted to be positioned on an exterior side of the aircraft below a lateral width of a fuselage of the aircraft while the image projector is adapted to be positioned on an interior side of the aircraft above the lateral width of the fuselage of the aircraft. The image projector is adapted to be positioned at a first predetermined height above a floor on the interior side of the aircraft, consistent with a person's eye level. The image projector is separated from the image receiver by a first predetermined distance.
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公开(公告)号：US20170287239A1
公开(公告)日：2017-10-05
申请号：US15510359
申请日：2015-09-09
Applicant: LEARJET INC.
Inventor： Peter Fleming LEVY
Abstract: Methods and apparatus disclosed herein may facilitate the evaluation of time-correlated operational data associated with a mobile platform more effectively by presenting the relevant data in ways that are relatively straightforward to interpret and more favorable to the identification of potential root causes. In some aspects, the methods and apparatus disclosed herein may facilitate the evaluation of multiple systems simultaneously at different points in time to study the initiation and evolution of one or more faults across one or more systems. In various embodiments, the methods and apparatus disclosed herein make use of graphic user interfaces containing synchronized elements such as two-dimensional plots, fault timelines, alert timelines and status information to facilitate diagnostics of mobile platforms.
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公开(公告)号：US20160167332A1
公开(公告)日：2016-06-16
申请号：US14907317
申请日：2014-07-01
Applicant: Khassan MOURTAZOV , Pierre DROLET , Pierre HARTER , David WILSON , LEARJET INC.
Inventor： Khassan MOURTAZOV , Pierre DROLET , Pierre HARTER , David WILSON
CPC classification number: B32B3/12 , B29D99/0021 , B32B5/022 , B32B5/024 , B32B5/26 , B32B7/10 , B32B7/12 , B32B37/12 , B32B37/146 , B32B2038/0076 , B32B2262/0269 , B32B2262/106 , B32B2307/54 , B32B2307/542 , B32B2307/714 , B32B2605/00 , B32B2605/08 , B32B2605/12 , B32B2605/18
Abstract: A composite material includes a honeycomb layer with top and bottom sides. The honeycomb layer includes a plurality of walls defining a plurality of cells therein. A first adhesive layer is disposed adjacent to the top side of the honeycomb layer. A second adhesive layer is disposed adjacent to the bottom side of the honeycomb layer. A third adhesive layer is disposed adjacent to the first adhesive layer on the top side of the honeycomb layer. A first composite layer is disposed adjacent to the third adhesive layer on the top side of the honeycomb layer. A second composite layer is disposed adjacent to the second adhesive layer on the bottom side of the honey comb layer. At least the third adhesive layer comprises viscous properties that discourage the creation of channels within the first composite layer when co-cured.
Abstract translation: 复合材料包括具有顶侧和底侧的蜂窝层。 蜂窝层包括在其中限定多个电池的多个壁。 第一粘合剂层邻近蜂窝层的顶侧设置。 第二粘合剂层邻近蜂窝层的底侧设置。 第三粘合剂层邻近第一粘合剂层布置在蜂窝层的顶侧上。 第一复合层与蜂窝层的顶侧上的第三粘合剂层相邻设置。 第二复合层邻近蜂巢层底部的第二粘合剂层设置。 至少第三粘合剂层包含粘合性质，其在共固化时阻止第一复合层内的通道的产生。
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Patent Agency Ranking
公开(公告)号：US10220593B2
公开(公告)日：2019-03-05
申请号：US14907317
申请日：2014-07-01
Applicant: LEARJET INC.
Inventor： Khassan Mourtazov , Pierre Drolet , Pierre Harter , David Wilson
IPC: B32B3/12 , B29D99/00 , B32B37/14 , B32B37/12 , B32B5/02 , B32B5/26 , B32B7/10 , B32B7/12 , B32B38/00
Abstract: A composite material includes a honeycomb layer with top and bottom sides. The honeycomb layer includes a plurality of walls defining a plurality of cells therein. A first adhesive layer is disposed adjacent to the top side of the honeycomb layer. A second adhesive layer is disposed adjacent to the bottom side of the honeycomb layer. A third adhesive layer is disposed adjacent to the first adhesive layer on the top side of the honeycomb layer. A first composite layer is disposed adjacent to the third adhesive layer on the top side of the honeycomb layer. A second composite layer is disposed adjacent to the second adhesive layer on the bottom side of the honey comb layer. At least the third adhesive layer comprises viscous properties that discourage the creation of channels within the first composite layer when co-cured.
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公开(公告)号：US20180093752A1
公开(公告)日：2018-04-05
申请号：US15833317
申请日：2017-12-06
Applicant: LEARJET INC.
Inventor： Alain LANDRY , Germain BELANGER
IPC: B64C1/06 , B29C65/00 , B29C31/08 , B29C33/26 , B29C65/50 , B29C70/54 , B29C70/46 , B29C70/30 , B29C70/08 , B29C65/48 , B29C35/02 , B29L31/30 , B64C1/00
CPC classification number: B64C1/068 , B29C31/08 , B29C31/085 , B29C33/26 , B29C35/02 , B29C65/483 , B29C65/505 , B29C65/5071 , B29C65/5078 , B29C66/1162 , B29C66/12822 , B29C66/12842 , B29C66/543 , B29C66/721 , B29C66/72525 , B29C66/73752 , B29C70/088 , B29C70/30 , B29C70/462 , B29C70/54 , B29L2031/3079 , B29L2031/3082 , B64C2001/0072 , B64F5/10 , Y02T50/43 , Y10T428/13
Abstract: A method for fabricating a composite material assembly includes: a) providing an assembly system, b) laying down a first module on a first mold, the first module comprising a first laminate covering a first laminate support structure, c) laying down a second module on a second mold, the second module comprising a second laminate covering a second laminate support structure and extending over the at least one removable insert, d) removing the at least one removable insert from the second mold, and e) assembling the first mold with the second mold while overlapping a section of the second laminate extending over the at least one removable insert over the first laminate.
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公开(公告)号：US20160129996A1
公开(公告)日：2016-05-12
申请号：US14897101
申请日：2014-06-12
Applicant: BOMBARDIER INC. , LEARJET INC.
Inventor： Frederic BOUCHER , Clovis S. RIBAS
Abstract: A landing gear system includes landing gear, an uplock that is releasably engageable with the landing gear, an uplock hydraulic actuator operably connected to the uplock, a landing gear hydraulic actuator operatively connected to the landing gear, and a controller operatively connected to the uplock hydraulic actuator and the landing gear hydraulic actuator. In response to receipt of a command to deploy the landing gear, the controller actuates the uplock hydraulic actuator and the landing gear hydraulic actuator to the UP condition and then actuates the uplock hydraulic actuator and the landing gear actuator to the DOWN condition. An alternative embodiment incorporates a piloted check valve upstream of the landing gear hydraulic actuator. The piloted check valve delays operation of the landing gear hydraulic actuator until release of the landing gear by the uplock.
Abstract translation: 起落架系统包括起落架，可拆卸地与起落架接合的上锁，可操作地连接到起重装置的上锁液压致动器，可操作地连接到起落架的起落架液压致动器，以及可操作地连接到起重机液压的控制器 执行器和起落架液压执行器。 响应于接收到部署起落架的命令，控制器将升压液压致动器和起落架液压致动器致动到UP状态，然后将升压液压致动器和起落架致动器致动到DOWN状态。 替代实施例包括起落架液压致动器上游的先导止回阀。 引导式止回阀延长起落架液压执行机构的操作，直到起落架松开。
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公开(公告)号：US10515491B2
公开(公告)日：2019-12-24
申请号：US15510359
申请日：2015-09-09
Applicant: LEARJET INC.
Inventor： Peter Fleming Levy
IPC: G07C5/12 , G07C5/08 , G06Q10/00 , G06Q10/06 , B64D45/00 , G07C5/00 , G05B19/042 , G06F11/32 , G06F11/30
Abstract: Methods and apparatus disclosed herein may facilitate the evaluation of time-correlated operational data associated with a mobile platform more effectively by presenting the relevant data in ways that are relatively straightforward to interpret and more favorable to the identification of potential root causes. In some aspects, the methods and apparatus disclosed herein may facilitate the evaluation of multiple systems simultaneously at different points in time to study the initiation and evolution of one or more faults across one or more systems. In various embodiments, the methods and apparatus disclosed herein make use of graphic user interfaces containing synchronized elements such as two-dimensional plots, fault timelines, alert timelines and status information to facilitate diagnostics of mobile platforms.
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公开(公告)号：US10106248B2
公开(公告)日：2018-10-23
申请号：US14897101
申请日：2014-06-12
Applicant: BOMBARDIER INC. , LEARJET INC.
Inventor： Frederic Boucher , Clovis S. Ribas
Abstract: A landing gear system includes landing gear, an uplock that is releasably engageable with the landing gear, an uplock hydraulic actuator operably connected to the uplock, a landing gear hydraulic actuator operatively connected to the landing gear, and a controller operatively connected to the uplock hydraulic actuator and the landing gear hydraulic actuator. In response to receipt of a command to deploy the landing gear, the controller actuates the uplock hydraulic actuator and the landing gear hydraulic actuator to the UP condition and then actuates the uplock hydraulic actuator and the landing gear actuator to the DOWN condition. An alternative embodiment incorporates a piloted check valve upstream of the landing gear hydraulic actuator. The piloted check valve delays operation of the landing gear hydraulic actuator until release of the landing gear by the uplock.
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