发明名称 Fire barrier protection for airplanes comprising graphite films
摘要 A fire barrier system for use in aircraft, ship or offshore drilling platform comprises a flexible graphite sheet. Methods of providing fire barrier protection in an aircraft, ship or offshore drilling platform comprise installing the described fire barrier system in the aircraft, ship or offshore drilling platform. Additionally, the fire barrier system when installed in the aircraft, ship or offshore drilling platform is described.
申请公布号 US9272169(B2) 申请公布日期 2016.03.01
申请号 US201012807717 申请日期 2010.09.13
申请人 KANEKA CORPORATION 发明人 Ono Kazuhiro;Nishikawa Yasushi;Inada Takashi
分类号 A62C2/00;A62C2/06;A62C3/08;A62C3/10;B63B3/68;E02B17/00;E04B1/94;B32B5/18;B32B9/00;B32B9/04;B32B15/20;B32B27/18;B32B27/38;B63B43/00 主分类号 A62C2/00
代理机构 Kagan Binder, PLLC 代理人 Kagan Binder, PLLC
主权项 1. A method of providing fire barrier protection in an aircraft comprising a) providing a fire barrier system for use in aircraft comprising a flexible graphite sheet, and b) installing the fire barrier system in the aircraft; wherein the flexible graphite sheet is a continuous film of graphite that has been prepared from a starting material polymer sheet that has been heated to a high temperature for a time sufficient to transform the polymer sheet into a flexible graphitized polymer sheet, and the flexible graphitized polymer sheet has a thermal conductivity in the plane direction of 300 W/mK or more and an Oxygen permeability and/or Hydrogen permeability of less than 5×101 cc/m2·day.
地址 Osaka JP