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SYSTEMS AND METHODS FOR AIRCRAFT REFUELING

机译:飞机改签的系统和方法

摘要

In an example, an indication system (134) includes a plurality of light sources (236) communicatively coupled with a control system (370). The indication system (134) can be used with a refueling system (120), including a hose (122) for supplying fuel to a receiver aircraft (112). Each light source (236) is configured to simultaneously emit visible light and infrared light, and is operable at a dim setting and a bright setting. The control system (370) receives refueling data (360) from the refueling system (120). The refueling data (360) includes position data (364) indicating a position of the receiver aircraft (112) relative to the refueling system (120). The control system (370) is configured to, when the refueling data (360) indicates that the position of the receiver aircraft (112) is in a refueling range (132), activate at least one refueling light source (242) of a plurality of refueling light sources (242) at the bright setting and activate a remainder of the refueling light sources (242) at the dim setting.
机译:在一个示例中,指示系统(134)包括与控制系统(370)通信地耦合的多个光源(236)。指示系统(134)可以与加油系统(120)一起使用,该加油系统(120)包括用于向接收飞机(112)供应燃料的软管(122)。每个光源(236)被配置为同时发射可见光和红外光,并且可在暗淡设置和明亮设置下操作。控制系统(370)从加油系统(120)接收加油数据(360)。加油数据(360)包括位置数据(364),该位置数据指示接收机飞机(112)相对于加油系统(120)的位置。控制系统(370)被配置为,当加油数据(360)指示接收飞机(112)的位置在加油范围(132)中时,激活多个中的至少一个加油光源(242)。在明亮的设置下加油光源(242)的亮度,并在暗的设置下激活其余的加油光源(242)。

著录项

  • 公开/公告号EP3381810A1

    专利类型

  • 公开/公告日2018-10-03

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20180160125

  • 发明设计人 CHANG KEVIN JULIAN;WALSH TIMOTHY J.;

    申请日2018-03-06

  • 分类号B64D39;

  • 国家 EP

  • 入库时间 2022-08-21 13:16:07

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