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公开(公告)号：US20150201529A1
公开(公告)日：2015-07-16
申请号：US14152677
申请日：2014-01-10
Applicant: Rosemount Aerospace Inc.
Inventor： Curtis Wicks , Eric Lovaasen , Kaleb Anderson , Jonathan Boer
CPC classification number: H05K7/20418 , B23P15/26 , B23P2700/10 , F28D15/0275 , F28D2021/0028 , F28F2275/08 , F28F2275/20 , H01L23/4006 , H01L23/427 , H01L2924/0002 , Y10T29/4935 , H01L2924/00
Abstract: A heat exchanger system may have a base, a mounting apparatus for attaching the base to a device, a gasket shelf for placing a gasket, a dissipation member for dissipating heat, and heat generator attachment sites for absorbing heat. A mounting apparatus may have finger-like extensions which flex and draw the base into contact with an underlying electronic device from which the system conducts heat. A base may also have an integrated heat pipe clamp attachment forming an aperture in the base into which a heat pipe may extend and may be clamped in thermal communication. The dissipation device may be a series of fins and troughs and a fan may direct air over the dissipation device to cool the apparatus.
Abstract translation: 热交换器系统可以具有基座，用于将基座附接到装置的安装装置，用于放置垫圈的垫圈架，用于散热的散热构件和用于吸收热量的发热器附接位置。 安装设备可以具有指状的延伸部，其弯曲并拉动底座与系统传导热量的下面的电子设备接触。 基座也可以具有集成的热管夹紧附件，其在基座中形成孔，热管可以延伸到其中，并且可以热连接夹紧。 散热装置可以是一系列翅片和槽，并且风扇可以将空气引导到耗散装置上以冷却装置。
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公开(公告)号：US12170029B2
公开(公告)日：2024-12-17
申请号：US17886147
申请日：2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor： Joseph T. Pesik , Jonathan Boer
IPC: G08G5/06 , B64D45/00 , B64D47/08 , G06T7/13 , G06T7/246 , G06T7/70 , G06T7/73 , G06V10/22 , G06V10/75 , G06V10/82 , G06V20/10 , G06V20/17 , G06V20/52 , G06V20/56 , G06V20/64 , G06V40/10 , H04N7/18 , B64C1/14 , B64C25/36 , B64D25/14
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an evacuation slide deployment path is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to identify a region within the captured image data that corresponds to the evacuation slide deployment path, determine whether the evacuation slide deployment path will generate a failed deployment outcome, and produce a warning associated with the evacuation slide deployment path in response to determining that the evacuation slide deployment path will generate the failed deployment outcome.
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公开(公告)号：US20230050216A1
公开(公告)日：2023-02-16
申请号：US17886185
申请日：2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor： Joseph T. Pesik , Jonathan Boer
IPC: G06V20/52 , H04N7/18 , G06V10/22 , G06V40/10 , G06V10/82 , G06T7/246 , G06T7/70 , G06V10/75 , B64D47/08 , B64D45/00
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an engine inlet of an engine of the aircraft is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to determine whether persons or foreign objects are present near the engine inlet, or detect damage or deformation of the engine inlet.
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公开(公告)号：US09854707B2
公开(公告)日：2017-12-26
申请号：US14152677
申请日：2014-01-10
Applicant: Rosemount Aerospace, Inc.
Inventor： Curtis Wicks , Eric Lovaasen , Kaleb Anderson , Jonathan Boer
CPC classification number: H05K7/20418 , B23P15/26 , B23P2700/10 , F28D15/0275 , F28D2021/0028 , F28F2275/08 , F28F2275/20 , H01L23/4006 , H01L23/427 , H01L2924/0002 , Y10T29/4935 , H01L2924/00
Abstract: A heat exchanger system may have a base, a mounting apparatus for attaching the base to a device, a gasket shelf for placing a gasket, a dissipation member for dissipating heat, and heat generator attachment sites for absorbing heat. A mounting apparatus may have finger-like extensions which flex and draw the base into contact with an underlying electronic device from which the system conducts heat. A base may also have an integrated heat pipe clamp attachment forming an aperture in the base into which a heat pipe may extend and may be clamped in thermal communication. The dissipation device may be a series of fins and troughs and a fan may direct air over the dissipation device to cool the apparatus.
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公开(公告)号：US12170030B2
公开(公告)日：2024-12-17
申请号：US17886185
申请日：2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor： Joseph T. Pesik , Jonathan Boer
IPC: G06T7/13 , B64D45/00 , B64D47/08 , G06T7/181 , G06T7/246 , G06T7/70 , G06T7/73 , G06V10/22 , G06V10/75 , G06V10/82 , G06V20/10 , G06V20/17 , G06V20/52 , G06V20/56 , G06V20/64 , G06V40/10 , G08G5/06 , H04N7/18 , B64C1/14 , B64C25/36 , B64D25/14
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an engine inlet of an engine of the aircraft is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to determine whether persons or foreign objects are present near the engine inlet, or detect damage or deformation of the engine inlet.
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Patent Agency Ranking
公开(公告)号：US20230052176A1
公开(公告)日：2023-02-16
申请号：US17886196
申请日：2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor： Joseph T. Pesik , Jonathan Boer
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that a ground surface is within the field of view of the camera during taxiing of the aircraft. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera for docking guidance by identifying, within the captured image data, a region on the ground surface corresponding to an alignment fiducial indicating a parking location for the aircraft, determining, based on the region of the captured image data corresponding to the alignment fiducial indicating the parking location, a relative location of the aircraft with respect to the alignment fiducial, and outputting an indication of the relative location of the aircraft to the alignment fiducial.
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公开(公告)号：US20230049312A1
公开(公告)日：2023-02-16
申请号：US17886181
申请日：2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor： Joseph T. Pesik , Jonathan Boer
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that a leading edge of a wing of the aircraft is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to predict a likelihood of foreign object collision with the leading edge of the wing, or detect damage or deformation to the leading edge.
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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：US20240212365A1
公开(公告)日：2024-06-27
申请号：US18087271
申请日：2022-12-22
Applicant: Rosemount Aerospace Inc.
Inventor： Douglas Eucken , Joseph T. Pesik , Isaac A. Jensen , Jonathan Boer , Dat Nguyen
IPC: G06V20/59 , A61B5/00 , A61B5/0205 , A61B5/024 , A61B5/08 , A61B5/18 , G06V10/141 , G06V40/19 , G08B7/06 , H04N23/23
CPC classification number: G06V20/59 , A61B5/02055 , A61B5/02433 , A61B5/0816 , A61B5/18 , A61B5/6802 , G06V10/141 , G06V40/19 , G08B7/06 , H04N23/23
Abstract: A biometric sensing system for an aircraft cockpit includes an infrared camera, infrared illuminators, and a CPU. The infrared camera is mounted in a flight deck display surface of the cockpit and has a field of view including an upper body region of a flight crew member when the flight crew member is seated in the cockpit. The infrared illuminators are mounted in the flight deck display surface and directed to illuminate the upper body region of the flight crew member when the flight crew member is seated in the cockpit. The CPU can communicate instructions to the infrared camera and infrared illuminators, receive image data captured by the infrared camera, and process the image data captured by the infrared camera in order to determine an alertness level of the flight crew member based on at least one biometric characteristic within the captured image data.
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公开(公告)号：US20230048021A1
公开(公告)日：2023-02-16
申请号：US17886147
申请日：2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor： Joseph T. Pesik , Jonathan Boer
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an evacuation slide deployment path is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to identify a region within the captured image data that corresponds to the evacuation slide deployment path, determine whether the evacuation slide deployment path will generate a failed deployment outcome, and produce a warning associated with the evacuation slide deployment path in response to determining that the evacuation slide deployment path will generate the failed deployment outcome.
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