发明名称 ACTUATING SYSTEM FOR A MOVABLE AIRCRAFT ENGINE NACELLE ELEMENT, SUCH AS A THRUST REVERSER COVER
摘要 This system for actuating at least one aircraft nacelle element comprises at least two actuators (A1, A2, A3) kinematically linked together, a main hydraulic (or electric) generation circuit (1) able to operate at least one (A1) of the two actuators, and a secondary electric (or hydraulic) generation circuit (13) able to operate the other actuator (A3).
申请公布号 US2012090311(A1) 申请公布日期 2012.04.19
申请号 US201013375383 申请日期 2010.06.23
申请人 LE COQ VINCENT PIERRE GERMAIN;MORADELL-CASELLAS PIERRE;MAALIOUNE HAKIM;DESCAMPS ALEXANDRE;AIRCELLE 发明人 LE COQ VINCENT PIERRE GERMAIN;MORADELL-CASELLAS PIERRE;MAALIOUNE HAKIM;DESCAMPS ALEXANDRE
分类号 F15B13/00 主分类号 F15B13/00
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