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A method of arranging a buoyancy system on an aircraft, a buoyancy system for an aircraft and an aircraft

机译:一种在飞机上布置浮力系统的方法,一种用于飞机的浮力系统以及一种飞机

摘要

The method involves connecting a cover (20) to a compartment of an aircraft (1) by an extensible connection element (25) in order to enable the cover to be retained and to be moved transversely while a float (15) is inflating. The cover is fastened to connection element by a reversible fastener element. The cover is connected to the compartment by the connection element. The float is fastened to an internal wall defining the compartment. An independent claim is included for a buoyancy system for aircraft.
机译:该方法包括通过可延伸的连接元件(25)将盖子(20)连接到飞机(1)的机舱,以便在浮子(15)充气时使盖子能够被保持并横向移动。盖通过可逆的紧固件元件紧固到连接元件。盖通过连接元件连接到隔室。浮子被紧固到限定隔室的内壁。飞机的浮力系统包括独立索赔。

著录项

  • 公开/公告号IL229641D0

    专利类型

  • 公开/公告日2014-03-31

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号IL20130229641

  • 发明设计人

    申请日2013-11-26

  • 分类号A01G;

  • 国家 IL

  • 入库时间 2022-08-21 15:57:56

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