Electric actuator
for aircraftelectro-optical

Electric actuator - ITT - for aircraft / electro-optical
Electric actuator - ITT - for aircraft / electro-optical
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Characteristics

Type
electric
Applications
for aircraft
Other characteristics
electro-optical
Torque

2.1 Nm
(1.549 ft.lb)

Description

Opto-Electronic Actuator Product Description ITT Aerospace Controls’ patented Opto Electronic Actuator (OEA) uses optical, non-contact, position sensing with solid state switching and incorporates an electrically isolated output shaft. The Opto-electronic switches and a solidstate H-bridge motor drive replace the older electromechanical position sensing and motor drives (relays and micro-switches) used in other typical actuator designs. The Opto Electronic actuator’s Isolated Output Shaft eliminates the possibility of electrical energy being passed through the output shaft and creating a safety hazard. Specifications - Patented Optical Switching - Patented Output Shaft Electrical Isolation - 25 in-lb Rated Load - Endurance Life to 100,000 Cycles and Rated Load - FAR 25.981 and SFAR88 Compliant - Low Weight - Low Power Consumption - Operates from 18 to 36 VDC Power Sources - Manual Override Clutch Standard - Environmentally Sealed - EMI/RFI Filtering Standard

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.