• Journal of Aerospace System Engineering
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• v.16 no.3
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• pp.84-92
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• 2022

The electro-hydrostatic actuator (EHA) recently has been used in flight control fields for aircraft because of its benefits of minimizing oil leakage and weight, improving safety, and etc. while independently operating the hydraulic power source and eliminating complex hydraulic piping. The aircraft of which EHA is installed inside, has the thermal management issue of EHA, because of its limited cooling source as compared with the aircraft which installs the traditional central hydraulic system. So, the thermal analysis model which predicts the thermal characteristics of EHA, is required to resolve this thermal management issue. In this study, an oil circulation circuit inside the hydraulic power module comprised of hydraulic pump and electrical motor for EHA was applied. This is for the purpose of developing the internal rotary group of hydraulic power module, which operates under the conditions of high rotation speed and hydraulic pressure. After formulating an appropriate thermal analysis model, the thermal analysis results with oil cooled or no oil cooled hydraulic control module were compared and reviewed, for the purpose of predicting the thermal characteristics of EHA.

• Proceedings of the KAIS Fall Conference
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• 2011.12b
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• pp.421-424
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• 2011

연비절감 및 조향감 향상을 위한 EHPS 시스템은 엔진 동력 기반의 HPS(Hydraulic Power Steering)시스템과는 달리 탈 엔진형 조향 기술로써 동력원인 BLDC 모터, 고압펌프 일체형 모듈, 상용 HPS 시스템의 기본 유압회로, 조향계 시스템 및 BLDC 모터를 제어하고 최적 조향력을 생성하기 위한 로직이 포함된 ECU로 구성되며. 주요구성 모듈은 펌프부, 모터부, 제어부로 분류된다. 본 논문에서는 펌프부의 외접형 Gear펌프의 시제품 제작하였고 구동토크 측정실험의 Data를 통해 기존 EHPS용 Gear펌프와 비교평가를 하였다.