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    IMAGE OPTIMIZATION BY AIRCRAFT EXTERIOR CAMERA SYSTEM
    11.
    发明申请
    IMAGE OPTIMIZATION BY AIRCRAFT EXTERIOR CAMERA SYSTEM 审中-公开

    公开(公告)号：US20190068880A1

    公开(公告)日：2019-02-28

    申请号：US15687320

    申请日：2017-08-25

    Applicant: Rosemount Aerospace Inc.

    Inventor： Jonathan Boer

    IPC: H04N5/232 ,  H04N5/225 ,  G06T7/13 ,  G06T7/174 ,  H04N5/247 ,  H05B1/02 ,  H05B3/84

    Abstract: Exterior camera systems of an aircraft include an image sensor configured to capture image data and one or more processors. The one or more processors are configured to determine a contrast of at least a portion of the captured image data; evaluate whether the contrast is less than a threshold contrast level; and output, in response to the contrast being less than the threshold contrast level, an initiate heating command configured to initiate heating of a camera window positioned between the image sensor and an exterior of the aircraft.

    TOOL-LESS LOW PROFILE ROTATION MOUNT
    12.
    发明申请
    TOOL-LESS LOW PROFILE ROTATION MOUNT 有权
    工具低型轮廓安装

    公开(公告)号：US20160368431A1

    公开(公告)日：2016-12-22

    申请号：US14744317

    申请日：2015-06-19

    Applicant: Rosemount Aerospace Inc.

    Inventor： Jonathan Boer ,  Kenneth Freeman ,  Eric Lovaasen

    IPC: B60R11/02 ,  B64D43/00 ,  F16M13/02

    CPC classification number: B60R11/0235 ,  B60R2011/0003 ,  B60R2011/0078 ,  B60R2011/0085 ,  B64D43/00 ,  B64D2045/0075 ,  F16B21/04 ,  F16M11/041 ,  F16M13/00 ,  F16M13/02 ,  F16M2200/02

    Abstract: A mount includes a keyed insert and a key receiver. The keyed insert includes a key base and a keyed plate mounted to the key base and having one or more key features extending from a periphery of the keyed plate. The key receiver accepts the keyed insert and includes a receiver base, a retaining ring, a key set ring, a key entrance ring, and a spring plate. The retaining ring is connected to the receiver base. The key set ring is disposed between the retaining ring and the receiver base and includes one or more receiving notches and one or more locking notches. The one or more receiving notches is configured to receive the one or more key features the one or more locking notch is spaced away from the one or more receiving notch and is configured to lockingly engage the one or more key features.

    Abstract translation: 安装座包括一个带键的插入件和一个钥匙接收器。 钥匙插入件包括安装在钥匙基座上的键座和键盘，并具有从键盘周边延伸的一个或多个键特征。 密钥接收器接受带键的插入件，包括接收器底座，保持环，钥匙圈，钥匙入口环和弹簧板。 保持环连接到接收器底座。 钥匙圈设置在保持环和接收器底座之间，并且包括一个或多个接收槽口和一个或多个锁定槽口。 一个或多个接收槽口被配置成接收一个或多个锁定槽口与一个或多个接收槽口间隔开的一个或多个关键特征，并被配置成锁定地接合一个或多个关键特征。

    AIRCRAFT DOOR CAMERA SYSTEM FOR JET BRIDGE ALIGNMENT MONITORING
    17.
    发明申请
    AIRCRAFT DOOR CAMERA SYSTEM FOR JET BRIDGE ALIGNMENT MONITORING 有权

    公开(公告)号：US20230048101A1

    公开(公告)日：2023-02-16

    申请号：US17886193

    申请日：2022-08-11

    Applicant: Rosemount Aerospace Inc.

    Inventor： Joseph T. Pesik ,  Jonathan Boer

    IPC: G08G5/06 ,  B64D47/08 ,  G06V20/56

    Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that a jet bridge cabin is within the field of view of the camera when the aircraft is within a docking distance of the jet bridge cabin. 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 by identifying physical characteristics of the jet bridge cabin, extracting, using the identified physical characteristics of the jet bridge cabin, alignment features corresponding to the physical characteristics of the jet bridge cabin that are indicative of alignment between the jet bridge cabin and the aircraft door, determining, based on the alignment features, whether the physical characteristics of the jet bridge cabin within the captured image data satisfy threshold alignment criteria to produce an alignment state, and outputting an indication of the alignment state.

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