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221.
公开(公告)号:US20190114933A1
公开(公告)日:2019-04-18
申请号:US15783919
申请日:2017-10-13
Applicant: Rosemount Aerospace Inc.
Inventor: William A. Veronesi , David Ginsberg , Julian C. Ryde , Joseph T. Pesik , Michael James Haukom
CPC classification number: G08G5/065 , B64D45/00 , G08G5/0013 , G08G5/0021 , G08G5/0086 , G08G5/04
Abstract: Apparatus and associated methods relate to rendering an image of objects in a region of an airport taxiway. The image is rendered from data provided by multiple sources. Three-dimensional models of static airport structures located within the region of an airport taxiway are provided. Rendered image data of the region of the airport taxiway if formed based on the retrieved three-dimensional models of the static airport structures. Data indicative of locations of dynamic objects within the region of the airport taxiway is also provided. Symbols identifying the dynamic objects within the region of the airport taxiway are mapped into the rendered image data at the locations indicated by the provided data. The rendered image data is sent to a display device configured to display the rendered image data.
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公开(公告)号:US20190100327A1
公开(公告)日:2019-04-04
申请号:US15720701
申请日:2017-09-29
Applicant: Rosemount Aerospace Inc.
Inventor: William B. Krueger , Kenneth Freeman , Richard Alan Schwartz , Alexander N. Reid , Timothy DeAngelo
Abstract: An angle of attack sensor includes a housing, a heated chassis positioned at least partially within the housing and defining a pocket, a mounting plate positioned adjacent the heated chassis and having a circular opening, an external surface facing away from the housing, and an internal surface facing toward the housing, and a vane assembly extending through the circular opening of the mounting plate. The vane assembly includes a vane extending from a root to a tip and a vane base connected to the root of the vane and positioned within the pocket of the heated chassis such that the vane base is offset inwardly from the external surface toward the housing.
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公开(公告)号:US20190098207A1
公开(公告)日:2019-03-28
申请号:US15715701
申请日:2017-09-26
Applicant: Rosemount Aerospace Inc.
Inventor: Todd Anthony Ell
CPC classification number: H04N5/23232 , F41G7/226 , F41G7/2293 , G02B13/0085 , G02B27/1066 , G02B27/126 , G02B27/144 , G02B27/146 , G02B27/58 , G06T3/4053 , G06T3/4069 , H04N5/2254 , H04N5/3415
Abstract: A seeker imaging system and method includes at least one imager, a plurality of optical elements, and control electronics. The at least one imager is configured to output image frame data. The plurality of optical elements are configured to receive light and direct the light to the at least one imager. The control electronics are configured to receive the image frame data from the at least one imager. The control electronics is configured to obtain a plurality of initial images from each frame of the image frame data, and wherein the control electronics is configured to generate a single output image based upon the plurality of initial images.
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公开(公告)号:US20190068863A1
公开(公告)日:2019-02-28
申请号:US15687323
申请日:2017-08-25
Applicant: Rosemount Aerospace Inc.
Inventor: Jonathan Boer
Abstract: Camera systems of an aircraft include an image sensor configured to capture image data and one or more processors. The one or more processors configured to determine at least one image property of the captured image data; evaluate whether the at least one image property is within an acceptable range; and output, in response to the at least one image property being outside the acceptable range, a lighting command configured to adjust light provided by a lighting system of the aircraft.
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公开(公告)号:US10217371B1
公开(公告)日:2019-02-26
申请号:US15683215
申请日:2017-08-22
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Robert Rutkiewicz , Todd Anthony Ell
Abstract: Apparatus and associated methods relate to controlling, based on a mode selector, the field of view of an external object detector during aircraft taxi operations. For example, during high-speed taxi operations, the field of view can be controlled to have a relatively-small solid-angle of detection capability. The relatively-small solid-angle field of view can be aligned so as to detect more distant objects within a narrow corridor extending forward of the aircraft's wingtips. During low-speed taxi operations, for example, the field of view can be controlled to have a relatively-large solid-angle of detection capability. The relatively-large solid-angle field of view can be aligned so as to detect close objects in the vicinity of the aircraft wings and engine nacelle. The object detector projects structured light within the controlled field of view, thereby illuminating the object(s) external to the aircraft that are within the illumination field of view.
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226.
公开(公告)号:US20190027051A1
公开(公告)日:2019-01-24
申请号:US15653205
申请日:2017-07-18
Applicant: Rosemount Aerospace Inc.
Inventor: William A. Veronesi , David Ginsberg , Julian C. Ryde , Joseph T. Pesik
Abstract: Apparatus and associated methods relate to displaying an image of a taxiing aircraft in relation to objects in a surrounding environment. A first data set indicative of locations, relative to the taxiing aircraft, of objects external to the taxiing aircraft is collected. Then, image data of a map of an area external to and including the taxiing aircraft is formed. Symbols of the objects external to the aircraft at the locations, relative to the taxiing aircraft, indicated by the first data set are mapping into the image data. The image data is then sent to a display device for displaying the image data to a pilot of the taxiing aircraft. Displaying a map indicating the relative location of external objects with which the taxiing aircraft could potentially collide advantageously assists the pilot in taxi operation.
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公开(公告)号:US20190020234A1
公开(公告)日:2019-01-17
申请号:US15648717
申请日:2017-07-13
Applicant: Rosemount Aerospace Inc.
Inventor: Jagadeesh Kumar Tangudu , Andrew S. Babel
CPC classification number: H02K1/2733 , G01B7/30 , G01D5/145 , G01D5/24438 , H02K1/246 , H02K21/145 , H02K21/16 , H02P21/18
Abstract: A magnetic position sensing system includes at least one annular magnet mounted to a surface of a rotating body. The annular magnet includes a first end, a second end, an inner diameter surface, and an outer diameter surface. The inner diameter surface and outer diameter surface define a radial thickness therebetween, and the radial thickness varies from the first end to the second end.
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公开(公告)号:US20180356293A1
公开(公告)日:2018-12-13
申请号:US15617768
申请日:2017-06-08
Applicant: Rosemount Aerospace Inc.
Inventor: Scott D. Isebrand
CPC classification number: G01K1/08 , G01K13/028 , G01K2013/024
Abstract: A total air temperature probe includes a housing defining a total air temperature sensor flow passage and a sensor assembly positioned within the total air temperature sensor flow passage. The sensor assembly includes an element flow tube, and a sensing element within the element flow tube. An upper portion of the element flow tube is an entrance including a plurality of protrusions that extend in an upstream direction.
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公开(公告)号:US20180341014A1
公开(公告)日:2018-11-29
申请号:US15440796
申请日:2017-02-23
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Todd Anthony Ell
CPC classification number: G01S13/882 , B64C39/024 , B64C2201/024 , B64C2201/141 , G01S7/032 , G01S13/0209 , G01S13/10 , G01S13/881 , G01S13/9303 , G01S2007/027 , G08G5/0069 , H01Q1/28
Abstract: A system can include an unmanned aerial vehicle and an altimeter disposed on the unmanned aerial vehicle. The altimeter can include an ultra-wideband radar antenna disposed orthogonally to a plane of straight and level flight of the unmanned aerial vehicle and having an omnidirectional azimuthal beam pattern orthogonal to the plane of straight and level flight of the unmanned aerial vehicle. The altimeter can be configured to determine an altitude of the unmanned aerial vehicle above a target surface based on time of flight of radar pulses between the ultra-wideband radar antenna and the target surface.
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公开(公告)号:US20180337474A1
公开(公告)日:2018-11-22
申请号:US15601362
申请日:2017-05-22
Applicant: Rosemount Aerospace Inc.
Inventor: Tim DeAngelo
Abstract: A circuit card assembly includes a first printed wiring board with a first receiving feature and a trace attached to the first printed wiring board. The three dimensional trace is formed by layer-by-layer additive manufacturing. The three dimensional trace includes first and second ends. The first end of the three dimensional trace engages with the first receiving feature of the first printed wiring board. The second end of the three dimensional trace is configured to engage with a second printed wiring board.
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