发明名称 Safety device for restarting windmilling turbojet
摘要 <p>A turbojet (1) has a fan (2) and compressor driven respectively by low pressure turbine and high pressure turbine through the coaxial shafts (3,4). The shafts are interconnected, to compensate rotation speed in normal operation of turbojet. A braking system (6) slowdown or blocks a differential (5) having an annular gear (7) rotating about the shafts, when turbojet shuts down.</p>
申请公布号 EP1270903(A1) 申请公布日期 2003.01.02
申请号 EP20020291410 申请日期 2002.06.07
申请人 SNECMA MOTEURS 发明人 FRANCHET, MICHEL;HEBRAUD, GUY
分类号 F02C3/113;F02C7/262;F02C7/264;F02C7/275;F02K3/06;(IPC1-7):F02C7/262 主分类号 F02C3/113
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