发明名称 SYSTEM FOR DEFROSTING THE LEADING EDGE SHEATH OF AN AIR INLET HOOD FOR A TURBOENGINE
摘要 The system for defrosting the leading edge sheath of an air intake hood for a turboengine comprises a hot pressure air supply duct (60) and a protective shell (90) which are longitudinally rigid and rigidly fixed to the partition (5) of a caisson (10), wherein said protective shell (90) is slidable with respect to a sliding bearing (15) embodied in the partition (11) and said air supply duct (60) is connected to the protective shell (90) by an elastic wall (16) closing an insulating space (12) and enabling relative longitudinal movements to be carried out between the air supply duct (60) and the protective shell (90).
申请公布号 US2010200699(A1) 申请公布日期 2010.08.12
申请号 US20060993009 申请日期 2006.06.15
申请人 AIRBUS FRANCE 发明人 PORTE ALAIN
分类号 F02C7/047;B64D15/04;F02C7/28 主分类号 F02C7/047
代理机构 代理人
主权项
地址