ELECTRIC ACTUATION FOR FLIGHT & ENGINE CONTROL: …

SAE-ACGSC Mtg 99 Slide 1 ELECTRIC ACTUATION for FLIGHT & ENGINE CONTROL: Evolution & 2, 2007 Boulder Meeting ELECTRIC ACTUATION FOR FLIGHT & ENGINE CONTROL: EVOLUTION & CHALLENGESAmit KulshreshthaMoog CHARRIERH ispano-SuizaSAE-ACGSC Mtg 99 Slide 2 ELECTRIC ACTUATION for FLIGHT & ENGINE CONTROL: Evolution & 2, 2007 Boulder Meeting Rationale for ELECTRIC Powered ACTUATION in Aircraft Reduced Weight ELECTRIC Powered ACTUATION allows the aircraft certification with 3 or, 2 ELECTRIC & 2 Hydraulic compared to conventional aircraft requiring 3 ELECTRIC & 3 Hydraulic A weight saving of ~ 1000 A380 and 400 Lbs for F-35 has been attributed to ELECTRIC ACTUATION due to savings from additional Hydraulic Systems.

MECHANICAL TRANSMISSION SENSOR INTERFACE AUX POWER 28 VDC ELECTRONICS MOTOR CONTROL UNIT (EMCU) CONTROL ELECTRONICS 115/230 VAC, Var Freq BIT & MONITOR ELECTRONICS POSITION / VELOCITY COMMAND EHM Mode device Ram Manifold Electronics Motor Accumulator Pump ELECTRIC DRIVE Electro-Mechanical Actuator (EMA) Electro-Hydro-Static Actuator …

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  Mechanical, Electro, Actuator, Mechanical actuator

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