发明名称 AIRCRAFT WINDOW AND AIRCRAFT
摘要 A window body constituting a window of an aircraft includes an electromagnetic shield film, and a conductive paint is applied to an outer perimeter edge face of the window body. A fixing member secures the window body to an airframe with a gasket seal and a window frame interposed therebetween. The fixing member has a first bonding surface on which a conductive film is formed. The first bonding surface is in direct contact with the gasket seal. An electrical path is formed through the electromagnetic shield film, the conductive paint, the gasket seal, the fixing member, and the window frame.
申请公布号 US2014319276(A1) 申请公布日期 2014.10.30
申请号 US201414323654 申请日期 2014.07.03
申请人 Mitsubishi Aircraft Corporation 发明人 YOKOI Takashi
分类号 B64C1/14;B60J10/00;B64D45/00 主分类号 B64C1/14
代理机构 代理人
主权项 1. A window of an aircraft attached to an opening formed in an airframe of the aircraft, comprising: a window body; a window frame that is made of a conductive material and surrounds an outer perimeter part of the window body; a gasket seal that is made of a conductive rubber material, at least a portion of the gasket seal being held between the outer perimeter part of the window body and the window frame; and a fixing member that is made of a conductive material and secures the window body to the airframe with the gasket seal and the window frame interposed therebetween, wherein the window body comprises a window panel having light transmissibility, and an electromagnetic shield film that is made of a conductive material and laminated on the window panel, a conductive paint is applied to an outer perimeter edge face of the window body, the fixing member has a first bonding surface in direct contact with the gasket seal, a conductive film is formed on the first bonding surface of the fixing member, and an electrical path is formed through the electromagnetic shield film, the conductive paint, the gasket seal, the fixing member, and the window frame.
地址 Aichi JP