AIRCRAFT REFUELING BOOM SOFT LIMITS SYSTEM
    1.
    发明申请
    AIRCRAFT REFUELING BOOM SOFT LIMITS SYSTEM 审中-公开
    飞机补救汽车软限制系统

    公开(公告)号:US20170008637A1

    公开(公告)日:2017-01-12

    申请号:US14793331

    申请日:2015-07-07

    IPC分类号: B64D39/00

    CPC分类号: B64D39/00

    摘要: A control system for an aircraft refueling boom controls the movements of the boom in certain areas in a total field of movement volume of possible boom movements based on the location of the boom in the total field of movement volume and based on the current rate of movement of the boom in the total field of movement volume.

    摘要翻译: 用于飞机加油吊杆的控制系统基于在整个移动体积的体积中的起重臂的位置并且基于当前的移动速度来控制在可能的起重臂运动的总运动体积中的某些区域中的起重臂的运动 的总体运动量的繁荣。

    Boom elevation estimation using hoist cable system

    公开(公告)号:US10436583B1

    公开(公告)日:2019-10-08

    申请号:US16189384

    申请日:2018-11-13

    摘要: A system for detecting a sensor fault of an aerial refueling boom. The system comprises a data collector configured to receive sensor data from a plurality of sensors and determine an aerial refueling boom elevation angle of the aerial refueling boom based on the sensor data, wherein the sensor data comprises at least one of cable length data, a dynamic pressure data or aerial refueling boom position data. The system further comprises a processing unit configured access a database table in a storage unit to determine an estimated aerial refueling boom elevation angle, a comparator configured to compare the estimated aerial refueling boom elevation angle to the determined aerial refueling boom elevation angle, and a fault detector configured to generate a sensor fault signal based on the comparison.