• 한국정밀공학회지
• /
• 제17권2호
• /
• pp.73-79
• /
• 2000

The part-surface of mold or stamping-dies consists of a compound surface which consists of lots of composite surfaces, and may have various types of feature shapes including convex sharp edge (CSE). Those CSE features should be considered with care in machining the surface, which necessitates extraction of CSE curves on a compound surface. This work can be done rather easily for a solid model which has a complete topology information. In case of the compound surface without topology information, however, such CSE curves must be gathered through some geometrical calculations paying much computation time. In the paper, extracting CSE curves by the construction of a CSE region-map which can reduce time, and detecting various common edge types are presented.

• EDISON SW 활용 경진대회 논문집
• /
• 제5회(2016년)
• /
• pp.647-652
• /
• 2016

To reduce drag force at supersonic speeds, sharp leading edge is hugely efficient. It is, however, incompatible with leading edge shape to have fine aerodynamic characteristics at subsonic and transonic speeds. It is critical to reduce drag force for enhanced cruise performance and higher efficiency. An air superiority fighter, however, required to have high maneuverability for survivability, and sharp leading edge is not proper. Consequently, variable leading edge is demanded to reduce drag force significantly at supersonic speeds for cruise performance. Leading edge altering system is constructed with rigid material to improve possibility of realization, and minimized movement of its components in altering for reduce effects on flight. It is compared with bi-convex airfoil and NACA 65-006 airfoil, which have comparable maximum thickness. At Mach number 1.7 and zero angle of attack, supersonic mode of designed airfoil indicates approximately 17% higher drag coefficient than the bi-convex airfoil indicates, it is, however, 23% lower than the NACA 65-006 indicates. Also, subsonic mode of the designed airfoil shows fine aerodynamic characteristics in comparison with NACA 65-006 airfoil in subsonic and transonic speed range. In this regard, design of the airfoil achieved the object of this study satisfactorily.

• 센서학회지
• /
• 제14권6호
• /
• pp.374-380
• /
• 2005

Vibration sensors have a wide scope of applications in the field of monitoring systems that needs to perceive an undesirable physical vibration before a critical failure occurs in a system, and then costly unplanned repairs can be avoided. The conventional vibration sensors developed so far have many disadvantages, such as complex manufacturing process, bulkiness, high cost, less reliability and so on. This paper reports a simple-structured vibration sensor, which has been developed using a commercialized conductive ball and silicon bulk-micromachining technology. The sensor consists of a conductive ball placed in $600{\mu}m$-deep micromachined silicon groove, in which Au thin film has been patterned using a shadow mask technique. Prior to the formation of the Au thin film, the sharp convex corner was rounded for smooth meatl deposition on the non-planar surface at the edge of the groove. The measurement results of the fabricated vibration sensor demonstrate a stable response characteristic to low-frequency vibration range ($1{\sim}30{\;}Hz$).

• 대한의용생체공학회:의공학회지
• /
• 제25권2호
• /
• pp.137-144
• /
• 2004

심전도 신호에는 근 잡음과 전원잡음 둥의 잡음이 섞이는 경우가 많다. 이러한 잡음들은 심전도 신호의 주요 주파수 성분에 비하여 상대적으로 고주파 성분이지만 전체적으로 보면 주파수 스펙트럼이 중첩된다. 본 논문에서는 연속적으로 변하는 차단주파수를 가지는 시변 저역통과 디지털필터를 이용하여 원신호의 왜곡을 최소화하면서 잡음을 제거하는 신호처리 방법에 대하여 기술한다 이 필터는 차단주파수 제어기와 가변차단주파수 저역통과필터로 구성된다. 차단주파수 제어기는 잡음이 포함된 심전도 신호로부터 신호의 기울기를 이용하여 차단주파수 제어 신호를 생성한다. 가변차단주파수 저역통과필터의 구현을 위해서 본 논문에서는 컨벡스 조합 필터와 계수보간 필터로 불리는 새로운 두 가지 필터 설계방법을 제안하였으며, 이 두 가지 방법을 이용함으로써 저역통과필터의 차단주파수를 임의의 제한된 구간에서 연속적으로 변화시키는 것이 가능하였다. 고주파 잡음이 첨가된 심전도 신호에서 가변차단주파수 저역통과필터의 잡음 제거 능력이 우수함을 보였으며, 본 논문에서 제안된 가변차단주파수 저역퉁과필터는 심전도 신호의 전처리에 유용하게 사용되어질 것으로 판단된다. 특히, 제어된 환경이 아닌 일상생활 환경에서 심전도를 측정하는 재택건강관리 시스템에서 신호의 품질을 개선하는 데에 효과가 있을 것으로 기대한다.