发明名称 Aircraft engine flame barrier - has inner pressurisable silicone pipe, felt barrier interlayer and fibre-reinforced rubber-impregnated outer layer
摘要 <p>Fire barrier for aircraft has an inner, elastic pipe which can be pressurised by feed of pressure medium, and which is surrounded by a flameproof yieldable interlayer. This in turn is surrounded by a resistant outer layer. Preferably the inner pipe consists of a fibre-reinforced silicone elastomer. The interlayer is a yieldable felt flame barrier. The outer layer is resistant, rubber-impregnated glass fibre sheathing, which may also be rubber-coated. The intermediate layer may also be of metal, asbestos or quartz fibres. The barrier prevents fire spreading at the boundary surface between the airframe and an engine.</p>
申请公布号 IT1029588(B) 申请公布日期 1979.03.20
申请号 IT19740053130 申请日期 1974.09.20
申请人 ROLLS ROYCE 1971 LTD 发明人
分类号 B64D;(IPC1-7):64D/ 主分类号 B64D
代理机构 代理人
主权项
地址