首页> 外国专利> INFLATABLE AIRFOIL SYSTEM HAVING REDUCED RADAR AND INFRARED OBSERVABILITY

INFLATABLE AIRFOIL SYSTEM HAVING REDUCED RADAR AND INFRARED OBSERVABILITY

机译:雷达和红外可观察性降低的可充气翼型系统

摘要

A method and apparatus for operating an airfoil system. A gas may be generated. The gas may be sent into an inflatable airfoil system comprising an inflatable air foil and a section. The inflatable airfoil may have an inner end and an outer end in which the inflatable airfoil may be comprised of a number of materials that substantially pass electromagnetic waves through the inflatable airfoil. The section may have a number of openings in which the inner end of the inflatable airfoil may be associated with the section. The section may be configured to be associated with a fuselage. The number of openings may be configured to provide communications with an interior of the inflatable airfoil. The section with the number of openings may be configured to reduce reflection of the electromagnetic waves encountering the section.
机译:一种用于操作翼型系统的方法和设备。可能会产生气体。气体可被送入包括可膨胀的空气箔和部分的可膨胀的翼型系统中。可充气翼型件可以具有内端和外端,其中,可充气翼型件可以由基本上使电磁波通过可充气翼型件的多种材料组成。该部分可具有多个开口,可膨胀翼型的内端可在其中与该部分相关联。该部分可以被配置为与机身相关联。多个开口可以被配置为提供与可充气翼型的内部的连通。具有多个开口的部分可以被构造成减少遇到该部分的电磁波的反射。

著录项

  • 公开/公告号US2014255189A1

    专利类型

  • 公开/公告日2014-09-11

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201414250385

  • 发明设计人 KEVIN REED LUTKE;AARON JONATHAN KUTZMANN;

    申请日2014-04-11

  • 分类号B64C3/30;

  • 国家 US

  • 入库时间 2022-08-21 16:10:27

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