METHODOLOGY FOR HEIGHT MEASUREMENT IN PNEUMATIC DEICER BOOTS

    公开(公告)号:EP4438482A1

    公开(公告)日:2024-10-02

    申请号:EP24165679.2

    申请日:2024-03-22

    IPC分类号: B64D15/16 B64D45/00

    摘要: The present disclosure provides for methodologies for height measurement in pneumatic deicer boots for aircraft, and related models, systems and methods of use. More particularly, the present disclosure provides for methods, models, systems and applications to detect the life or failure of pneumatic deicer boots for aircraft. A method for detecting the life or failure of pneumatic deicer boots for aircraft is provided.

    FLIGHT CONTROL DEVICE
    8.
    发明公开

    公开(公告)号:EP4428041A1

    公开(公告)日:2024-09-11

    申请号:EP22889785.6

    申请日:2022-10-20

    申请人: DENSO CORPORATION

    发明人: TAKEMURA, Yuichi

    摘要: A flight control device performs flight control processing for causing a subject aircraft to fly. When a collision between the subject aircraft and a counterpart aircraft is predicted, the flight control device performs detection avoidance processing assuming that a risk of collision has been detected. In step S304 of the detection avoidance processing, the flight control device sets an order of priority of the subject aircraft and the counterpart aircraft for collision avoidance. When the order of priority of the counterpart aircraft is higher than the order of priority of the subject aircraft, it is assumed that the counterpart aircraft performs collision avoidance flight, and the flight control device (40) ends the detection avoidance processing without performing the collision avoidance flight. On the other hand, when the order of priority of the subject aircraft is higher than the order of priority of the counterpart aircraft, the flight control device changes a flight route of the subject aircraft to the collision avoidance route in step S404.