항공기의 도어 댐퍼용 교축 오리피스의 설계

다국어 초록 (Multilingual Abstract)

In this study the flow rate-to-pressure difference characteristics of short-tube type damping orifices for an aircraft door damper were investigated by CFD analyses and experiments. As the design parameters of the damping orifice its diameter, inlet and outlet angle, tube length and the viscosity of the working fluid were taken into consideration. The results showed that the discharge coefficient of the orifices are dependant on the inlet and outlet angle and the oil viscosity, while their length plays an little significant role. Although the short-tube type damping orifice was employed to induce a turbulent flow, their discharge coefficient decreases rapidly as the oil viscosity gets higher than 50cSt. Therefore, in order to determine the orifice size, satisfying the working temperature range of the door damper, the oil viscosity as well as the friction force on the damper piston should be kept within proper values. For the verification of the CFD analysis results the actual performance of a door damper was measured and compared with them.

목차 (Table of Contents)

• Abstract
• 기호 설명
• 1. 서론
• 2. 항공기용 도어 댐퍼의 이론 모델
• 3. 댐핑 오리피스의 성능 분석
• 4. 실험
• 5. 결론
• 후기
• 참고문헌