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公开(公告)号：US20180077765A1
公开(公告)日：2018-03-15
申请号：US15701915
申请日：2017-09-12
发明人： Brian Gray
CPC分类号： H05B33/0842 , B64D45/08 , B64D2203/00 , B64F1/20 , H01Q1/06 , H05B37/0218 , Y02B20/46
摘要： The system is for use with an AM transmission tower and comprises: a LED light mounted in use on the tower; a photocell; a LED beacon mounted in use on the tower; a controller; an RF choke interposed between and operatively coupling the beacon and the controller; and an RF choke interposed between and operatively coupling the photocell and the controller.
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公开(公告)号：US09802716B2
公开(公告)日：2017-10-31
申请号：US15173966
申请日：2016-06-06
发明人： Jan Vana , Joseph J. Cox , Isaiah W. Cox , Jonathan S. Edelson
CPC分类号： B64F1/002 , B64C25/405 , B64D47/06 , B64D2203/00 , Y02T50/823
摘要： An identification system and method are provided for aircraft equipped with electric taxi systems for autonomous ground movement that enables airport ground personnel and others outside the aircraft to safely and easily identify the aircraft moving on ground surfaces at an airport as equipped with a pilot-controlled electric taxi system and to distinguish these aircraft from aircraft not moved by electric taxi systems. The identification system may be mounted with nose or main landing gear drive wheels supporting the electric taxi system. The identification system includes an identifying lighting system with lighting elements of a selected number, shape, color, or arrangement positioned on at least a visible face of one or more landing gear wheels. Automatic or manual controls may actuate the identification system to identify electric taxi system-equipped aircraft when the aircraft are moved with the electric taxi system or are stopped.
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63.发明申请公开(公告)号：US20170287224A1
公开(公告)日：2017-10-05
申请号：US15469555
申请日：2017-03-26
申请人： THALES
发明人： Thierry GANILLE , Bruno AYMERIC , Johanna LUX
CPC分类号： G06T19/006 , B64D45/08 , G01C23/005 , G01S7/24 , G01S13/89 , G01S13/913 , G01S13/94 , G01S17/89 , G02B27/01 , G02B27/0101 , G02B2027/0134 , G02B2027/0138 , G02B2027/014 , G06K9/0063 , G06T15/205 , G06T2215/16 , G08G5/0021 , G08G5/0086 , G08G5/025 , H04N5/33 , H04N7/183
摘要： A method of synthetic representation of elements of interest in a viewing system for aircraft, the viewing system comprises location sensors, a cartographic database and a database of elements of interest, an image sensor, a unit for processing images and a unit for generating three-dimensional digital images representative of the terrain overflown and a viewing device, wherein, when the terrain overflown comprises an element of interest, the method of synthetic representation comprises: a first step of searching for and detecting the element of interest in each image of a sequence of images, and; a second step of generating three-dimensional digital images representative of the terrain overflown, the element of interest represented according to a first representation if it has not been detected in any of the images of the sequence of images and according to a second representation if it is detected.
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公开(公告)号：US09776734B2
公开(公告)日：2017-10-03
申请号：US14750688
申请日：2015-06-25
发明人： Matthias Eberle
CPC分类号： B64D45/08 , G01C9/005 , G01C21/20 , G01C23/00 , G05D1/0676 , G08G5/0021 , G08G5/025
摘要： A landing aid method and device for an aircraft including a unit for calculating automatically in a repetitive manner, during a final approach of the aircraft with a view to landing on a landing runway, using at least a ground speed of the aircraft, a height of the aircraft in relation to the ground, and a target vertical speed representing a vertical speed required on contact with the landing runway, a slope angle of a flight path allowing the aircraft to perform a flare, checking at least the target vertical speed on contact with the landing runway, and a unit for displaying automatically, on at least one screen of the flight deck of the aircraft, a first symbol illustrating the current slope angle of the aircraft and a second symbol illustrating the calculated slope angle.
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公开(公告)号：US20170158349A1
公开(公告)日：2017-06-08
申请号：US15357249
申请日：2016-11-21
CPC分类号： B64D45/08 , B64D43/00 , G05D1/0676 , G08G5/0021 , G08G5/0047 , G08G5/025
摘要： A method for aiding the landing of an aircraft on a landing runway comprising the following steps implemented in an automatic manner by a processing unit: a) acquiring information relating to the landing runway; b) acquiring information relating to a current situation of the aircraft; f) determining a maximum roll angle, in absolute value, necessary to allow a flight of the aircraft along a trajectory between a current position and a target landing position on the landing runway; g) comparing this maximum roll angle with a predetermined limit; and h) as a function of the result of the comparison carried out in step g), commanding, if appropriate, the signaling of an alert by means of a signaling system of the aircraft.
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公开(公告)号：US20170152059A1
公开(公告)日：2017-06-01
申请号：US15431079
申请日：2017-02-13
发明人： Bin PENG , Yousheng CHEN
CPC分类号： B64D45/08 , B64C27/08 , B64C27/12 , B64C39/024 , B64C2201/024 , B64C2201/18 , B64D31/00 , B64D47/08
摘要： A rotorcraft and an automatic landing system and method thereof are provided in the present disclosure. The automatic landing system of the rotorcraft includes a controller, a laser emitter, a camera, an electronic governor and a motor configured to drive a propeller of the rotorcraft to rotate. The laser emitter and the camera are both locate in a bottom portion of an airframe of the rotorcraft. The laser emitter has two emission heads, laser beams emitted from the two emission heads respectively are symmetrical about a central axis, the central axis is perpendicular to a horizontal plane of a ground, and an angle between each laser beam and the central axis is an acute angle. Simply with an operation of the laser emitter, the camera and the controller, the flight speed and displacement of the rotorcraft can be controlled to realize automatic landing in the present disclosure.
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公开(公告)号：US20170132767A1
公开(公告)日：2017-05-11
申请号：US15410538
申请日：2017-01-19
CPC分类号： G06T5/009 , B60R1/00 , B60R2300/103 , B60R2300/80 , B60R2300/8053 , B60R2300/8073 , B60Y2200/52 , B60Y2400/92 , B64D45/08 , G06K9/6289 , G06K2009/6295 , G06T5/002 , G06T5/10 , G06T7/90 , G06T2207/10048 , G06T2207/20064 , H04N5/33
摘要： One aspect of the present invention includes artificial vision system. The system includes an image system comprising a video source that is configured to capture sequential frames of image data of non-visible light and at least one processor configured as an image processing system. The image processing system includes a wavelet enhancement component configured to normalize each pixel of each of the sequential frames of image data and to decompose the normalized image data into a plurality of wavelet frequency bands. The image processing system also includes a video processor configured to convert the plurality of wavelet frequency bands in the sequential frames into respective visible color images. The system also includes a video display system configured to display the visible color images.
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公开(公告)号：US09598180B1
公开(公告)日：2017-03-21
申请号：US14948622
申请日：2015-11-23
申请人： Stephen Browder
发明人： Stephen Browder
摘要： The aircraft landing clearance indication system is constructed of a faceplate that is adapted to be secured against a surface in a cockpit. The faceplate includes a front surface that includes instructions as to operation of the system. A push button is mounted on the front surface of the faceplate. Depression of the push button illuminates the push button providing an instantaneous feedback as to the authorization of the respective airplane to land on a runway. Once the airplane has landed, the push button is depressed a second time in order to reset itself for future use. The aircraft landing clearance indication system is used during the landing checklist.
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69.发明授权Method and apparatus for generating a virtual inner marker for an aircraft landing approach 有权用于生成用于飞机着陆方法的虚拟内标记的方法和装置公开(公告)号：US09527601B2
公开(公告)日：2016-12-27
申请号：US13759408
申请日：2013-02-05
发明人： Ivan Sandy Wyatt , Gang He , Thea L. Feyereisen
CPC分类号： B64D45/08 , G08G5/0021 , G08G5/02 , G08G5/025
摘要： A system and method is provided for anticipating a missed approach point (MAP) during an instrument landing of an aircraft. Symbology is generated and displayed that graphically represents a lateral distance between a runway threshold and a virtual inner marker. The MAP is identified as the location of the aircraft when the symbology reaches a displayed runway threshold.
摘要翻译： 提供了一种系统和方法，用于在飞行器的仪表着陆期间预测错过的接近点（MAP）。 生成和显示符号学，其以图形方式表示跑道阈值和虚拟内标记之间的横向距离。 当符号系统达到显示的跑道阈值时，MAP被标识为飞机的位置。
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公开(公告)号：US09522742B2
公开(公告)日：2016-12-20
申请号：US14218672
申请日：2014-03-18
申请人： The Boeing Company
发明人： Mark Hall Henderson
CPC分类号： B64D45/04 , B64D45/08 , G05D1/0607 , G05D1/0653 , G05D1/0676 , G08G5/0047 , G08G5/04 , G08G5/045
摘要： A method can include determining that an aircraft is on approach to a runway. The method can include determining a flight path vector (FPV) location of the aircraft based at least in part on a projected landing location with respect to the runway and determining a current airspeed of the aircraft. The method can also include performing at least one of the following: issuing a landing short alert to a pilot of the aircraft if the FPV location is at or before the runway threshold, issuing an airspeed caution alert if the FPV location is between the runway threshold and the target runway location and if the current airspeed is below a landing short envelope, and determining not to issue an alert if the FPV location is between the runway threshold and the target runway location and if the current airspeed is at or above the landing short envelope.
摘要翻译： 一种方法可以包括确定飞机正在接近跑道。 该方法可以包括至少部分地基于相对于跑道的预计着陆位置来确定飞行器的飞行路线向量（FPV）位置，并确定飞机的当前空速。 该方法还可以包括执行以下中的至少一个：如果FPV位置在跑道阈值之前或之前，向飞机的飞行员发出着陆短警报，如果FPV位置在跑道阈值之间，则发出空速警告警报 目标跑道位置以及当前空速是否低于着陆短信号，并且如果FPV位置在跑道阈值和目标跑道位置之间以及当前空速是否在着陆短路之上或之上时，确定不发出警报 信封。
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