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The State of the Art and Application of Actuator in Aerospace  

Yoon, Gi-Jun ((주)한화 항공우주/기계연구소)
Park, Ho-Youl ((주)한화 항공우주/기계연구소)
Jang, Ki-Won ((주)한화 항공우주/기계연구소)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.14, no.6, 2010 , pp. 89-102 More about this Journal
Abstract
In this paper, a study on the future-oriented actuator introduces the future technology and future direction in aerospace and several industry fields. In particular, the mechanical linkage or hydraulic and pneumatic actuators which have the higher output-to-weight ratio have been used a lot in the past as the aircraft's flight control device. Most recently, Fly-By-Wire system has been used in aircraft and the flight control system has been changed in more electric and all electric systems. Electrohydraulic actuators and electric actuators have been developed continually, because they have better efficiency, safety and lower cost for the flight control system of aircraft. Also, to improve the weight condition, accuracy and response of actuator, new field actuators using new materials have been developed. In this paper we clearly proposed the actuator design and detailed technology development trend for next generation actuation system in aerospace and new field.
Keywords
Electro-Hydrostatic Actuator(EHA); Electro-Mechanical Actuator(EMA); Piezoelectric Actuator; Fly-By-Wire(FBW); Power By Wire(PBW);
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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