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중소형 무인기 브레이크 시스템용 복합형 지능재료펌프 설계
이종훈,황재혁,양지연,주용휘,배재성,권준용,Lee, Jonghoon,Hwang, Jaihyuk,Yang, Jiyoun,Joo, Yonghwi,Bae, Jaesung,Kwon, Junyong 항공우주시스템공학회 2015 항공우주시스템공학회지 Vol.9 No.3
In this study, the design of compound smart materials hydraulic pump that can be applied to a small-medium size UAV having a limited space envelope and weight has been conducted. Compound Smart Material Pump(CSMP) proposed in this paper is composed of a pressurize pump and a flow pump for supplying the high pressure and fluid displacement to overcome the disadvantages of the piezoelectric actuator which has a small strain. Though this compound smart material pump has been designed as small size and lightweight as possible, it can sequentially supply the sufficient large flow rate and pressure required for the brake operation. For the design of CSMP, about 2,700 kg (6,000 lb) class fixed wing manned aircraft was selected. Based on the established requirements, the design of the CSMP have been done by strength, vibration, and fluid flow analysis.