THE COMMUNICATION OF LANDING CONDITIONS
    11.
    发明申请
    THE COMMUNICATION OF LANDING CONDITIONS 有权
    登陆条件通信

    公开(公告)号:US20090267798A1

    公开(公告)日:2009-10-29

    申请号:US11464642

    申请日:2006-08-15

    IPC分类号: G08B21/00 B60T8/32

    摘要: The invention discloses differing embodiments of methods, aircraft, and apparatus for communicating the braking conditions of a runway. In one embodiment, braking information may be determined from a first aircraft which has landed on the runway. The braking information may be communicated to air traffic control and/or a second aircraft. Communication of the braking information may take place utilizing an Automatic Dependent Surveillance Broadcast system (ADS-B) and/or other type of automatic networking system.

    摘要翻译: 本发明公开了用于传达跑道制动条件的方法,飞行器和装置的不同实施例。 在一个实施例中,可以从已经降落在跑道上的第一飞机确定制动信息。 制动信息可以被传送到空中交通管制和/或第二飞行器。 制动信息的通信可以利用自动相关监视广播系统(ADS-B)和/或其他类型的自动联网系统进行。

    Determination of runway landing conditions
    12.
    发明授权
    Determination of runway landing conditions 有权
    确定跑道着陆条件

    公开(公告)号:US07586422B2

    公开(公告)日:2009-09-08

    申请号:US11461880

    申请日:2006-08-02

    IPC分类号: G08B21/00

    摘要: The invention discloses differing embodiments of methods, aircraft, and apparatus for determining the landing conditions of a runway. In one embodiment, braking data may be collected from an aircraft which has landed on the runway; a braking performance measurement of the aircraft may be calculated based on the braking data; and a normalized braking performance measurement may be determined based on the braking performance measurement. The invention may be utilized to predict the expected braking performance of various types of aircraft on the runway. The invention may provide landing performance information to a broad host of users, and/or may be used as a basis for the development of a new aviation standard for the reporting of runway braking action.

    摘要翻译: 本发明公开了用于确定跑道着陆条件的方法,飞行器和装置的不同实施例。 在一个实施例中,可以从已经降落在跑道上的飞机收集制动数据; 可以基于制动数据来计算飞行器的制动性能测量; 并且可以基于制动性能测量来确定归一化的制动性能测量。 本发明可以用于预测跑道上各种类型的飞机的预期制动性能。 本发明可以向广泛的用户主体提供着陆性能信息,和/或可以用作开发用于报告跑道制动动作的新的航空标准的基础。