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A method of providing fuel to an engine or manifold air refueling aircraft

机译:一种向发动机或歧管空中加油机提供燃料的方法

摘要

A method in an aircraft (100) to provide fuel to at least one of a motor (105) and a manifold air refueling in flight, the method comprising: at least partially filling a first set of tank (120) with fuel a fuselage (102) of the aircraft by the flow of fuel through a manifold inlet / outlet dual purpose (671) at least partially filling a second set of tank (121) with fuel in the aircraft fuselage by the fuel flow through the manifold inlet / outlet dual purpose (671), removing fuel from the first tank assembly (120), while fuel from the first tank assembly (120) is removed by withdrawing second fuel tank assembly (121), and transfer the removed fuel first and second sets of at least one tank and engine manifold aerial refueling through manifold inlet / outlet double pro pósito (671) where the manifold inlet / outlet dual purpose (671) is configured to transfer fuel from, and provide fuel to the first and second sets of tank.
机译:飞机(100)中的一种向飞行中的电动机(105)和歧管空气加油中的至少一个提供燃料的方法,该方法包括:用机身至少部分填充第一组油箱(120)的燃料( 102)的飞机通过流经歧管入口/出口两用的燃料流(671)至少部分地通过飞机流经双歧管入口/出口的燃料在第二组油箱(121)中填充飞机机身中的燃料目的(671),从第一燃料箱组件(120)去除燃料,同时通过抽出第二燃料箱组件(121)去除第一燃料箱组件(120)的燃料,并转移去除的燃料的第一组和第二组至少一个油箱和发动机歧管通过双歧管进气口/出口(671)进行空中加油,其中歧管进气口/出口双重用途(671)配置为从第一组和第二组油箱传输燃料并提供燃料。

著录项

  • 公开/公告号ES2456940T3

    专利类型

  • 公开/公告日2014-04-24

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号ES20120183085T

  • 发明设计人 HOWE MARK E.;

    申请日2004-11-15

  • 分类号F16K31/20;B64D37;B64D37/04;B64D39;

  • 国家 ES

  • 入库时间 2022-08-21 15:55:05

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