发明名称 TURBOJET NACELLE
摘要 FIELD: aircraft engineering.SUBSTANCE: claimed nacelle comprises air intake, mid and rear sections. Mid section is composed of airframe that makes the nacelle outer aerodynamic integrity. Said airframe is rigidly jointed the adjoining fixed structure and can be detached therefrom.EFFECT: decreased weight of nacelle components.11 cl, 6 dwg
申请公布号 RU2569503(C2) 申请公布日期 2015.11.27
申请号 RU20130102783 申请日期 2011.06.17
申请人 AIRCELLE;SNECMA 发明人 HURLIN HERVE;DEZEUSTRE NICOLAS;KERBLER OLIVIER;GALLET FRANCOIS;DESJOYEAUX BERTRAND
分类号 B64D29/06 主分类号 B64D29/06
代理机构 代理人
主权项
地址