• Composites Research
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• v.18 no.4
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• pp.52-58
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• 2005

A cyclocopter propelled by the cycloidal blade system, which can be described as a horizontal rotary wing, is a new concept of VTOL vehicle. In this paper, optimized structure design is carried out for the aerodynamically optimized cyclocopter rotor system. Database is obtained fer design variables such as stacking sequence (ply angles), number of plies and spar locations through MSC/NASTRAN and optimum values are determined by RSM and some other optimizing processes. For the rotor system including optimized blade and composite hub m, the maximum stress by static analysis is within the failure criteria. And the rotor system is designed for the purpose of avoiding possible dynamic instabilities by inconsistency between frequencies of rotor rotation and some low natural frequencies of rotor.

• Tribology and Lubricants
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• v.29 no.6
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• pp.397-402
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• 2013

This study examined the tribological characteristics of the drive shaft and axle system in vehicles. The first drive shaft example contained end play for a CV joint that transferred part of the transmission power to the wheel. The joint part of the drive shaft was deformed because of reduced durability due to wear. Thus, vibrations caused the body to shake and become unbalanced when the drive shaft transferred the power. The second example was the cross-section of a shaft that connected the slip-connection of the propeller shaft on the input side to the yoke flange of the output side; the durability was reduced because of corrosion. End play caused by wear between the bearing and cross-section shaft appeared to cause shaking. In the third example, a grease leak reduced lubrication and thus caused damage to the hub bearing and inside the knuckle. The failure was produced by sticking. The fourth example had noise produced by the gear and gear transfer. This was due to the backlash of the pinion and few ring gears for the differential gear. Therefore, drive shaft and axle systems must be thoroughly checked and managed to minimize and reduce failure phenomena.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.23 no.5
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• pp.646-652
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• 1999

Detailed characteristics of the mean flow field inside the rotor of a multiblade fan with scroll are presented in this paper by measurements and visualizations. The measurements were taken with a five-hole probe and conformed by smoke test. How field is distinguished clearly in 3 regions with respect to the flow directions. The first region is near the exit of scroll where the fluid flows the opposite direction to the rotation of rotor. The second is opposite side of the scroll exit where the fluid flows the same direction to the rotation of rotor. The third is the region where the fluid flows toward the blades directly with the largest values comparatively. The strongest recirculation is happened in the second region, and the weakest one is in the third region. This complex configuration makes the flow field highly non-uniform and may cause to generate a noise and ineffective flow efficiency.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2019.11a
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• pp.216-217
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• 2019

As the shipping market deteriorates, shipping companies seek to realize economies of scale by promoting the enlargement of container ships. Container terminal operators are increasingly adopting automated equipment and systems in order to quickly provide services and attract traffic. As such, the competition for each terminal to become a hub port is intensifying. Increased automation of advanced container terminals improves productivity and efficiency In the meantime, Korea remains semi-automated. Therefore, the relevant subject survey through SPSS 23.0 program for analysis of recognition difference, We will check the awareness among stakeholders for the smooth introduction.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2013.10a
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• pp.841-844
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• 2013

This paper suggests methods to drive motor and dsPIC30F2010 microprocessor software design for the Wheel Hub Motor that is incorporated into a hub of the wheel and drives it directly. The minimum function of dsPIC30F2010, system clock, PWM, I/O, communication, applicable to hub motor control are explained and tested. The algorithm including PI control method was implemented to the system by using dsPIC30F2010 microprocessor functions.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.8 no.6
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• pp.1126-1134
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• 2004

This research is targeted on developing an advancing model for 4 provinces of Jeollabuk-Do, Jeollanam-Do, Gangwon-Do, and Jeju Island that are relatively underdeveloped in regard to various infrastructures, on causing balanced development of this country (South Korea) by making those provinces undertaking a part of growth power in the next generation, and accordingly, on helping this country (South Korea) to emerge as a heart of north-east countries in economy. This research at first focuses on Jeollabuk-Do as considering the geographical and economical characteristics, has an effort to contrive an advancing model of culture-information industry, and then, if successfully souled down, is enlarged to the other underdeveloped provinces in developing advancing models.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.2
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• pp.115-120
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• 2014

In this study, a module is developed for modeling and analyzing dynamic behavior of a wind turbine using RecurDyn, which is a commercial multi-body dynamics software developed by FunctionBay, Inc. The wind turbine consists of tower, nacelle, hub and blades. Tower and blades are regarded as flexible bodies for considering elastic effect using beam theory and spring force. In this paper, a constant speed wind was assumed and aerodynamic force is modeled using BEM theory. Dynamic analysis applying this aerodynamic force is carried out. To verify the validity of analysis results, these results are compared to those of GH-Bladed which is a commercial software for analyzing wind turbine system distributed by Garrad Hassan.

• Proceedings of the Korea Information Processing Society Conference
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• 2015.10a
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• pp.471-474
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• 2015

최근 사물인터넷이 빠른 속도로 발전할 것으로 예측됨에 따라서, 서비스들은 사용자들에게 제공되기 위해서 작은 디바이스부터 거대한 디바이스들간의 임베디드 디바이스의 발전과 센서 허브와 같은 보조 프로세서의 발전을 통해, 서로 연결되고 있으며, 사용자들을 위해 지금보다 더 정확하고 신뢰할 수 있는 맞춤형 사물인터넷 서비스를 제공하기 위한 개발의 필요성이 대두되고 있다. 효과적인 서비스 구축을 위한 기법들로 하위 디바이스 계층의 수준과 상위 어플리케이션 계층의 수준을 서로 구분 지을 수 있도록 서비스 지향형 컴퓨팅 방식을 사용하는 여러 계층 구성의 계층적 추상화 접근 방법이 소개되고 있지만, 사용자들에게 더 정확하고 신뢰할 수 있는 서비스를 구축하는 것은 여전히 다양한 이슈가 존재한다. 본 논문에서는 서비스 객체의 단방향 그래프 구성 기법을 적용하여, 효과적이고 신뢰할 수 있는 사물인터넷 서비스 구성을 위하여 서비스 오브젝트를 단방향 그래프 자료구조로 구성한 새로운 형태의 IoT 미들웨어 구조를 제안한다. 또한, 새로 제안된 미들웨어 구조상에서의 사용자의 사용 시나리오 및 시스템 성능상의 이점을 분산 시뮬레이션을 통하여 증명한다.

• Journal of the Korea Institute of Military Science and Technology
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• v.24 no.3
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• pp.255-263
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• 2021

This paper investigates numerically the effect of rotor hub vibratory load components on the airframe vibration responses of high-speed compound unmanned rotorcraft (HCUR) using a lift-offset coaxial rotor, wings, and two propellers. The rotor hub vibratory loads are predicted using a rotorcraft comprehensive analysis code, CAMRAD II, and the airframe vibration responses are calculated by a finite element analysis software, MSC.NASTRAN. It is shown that the vibratory hub pitch moment of a lift-offset coaxial rotor is the most dominant component for both the longitudinal and vertical vibration responses at four specified locations of the airframe.

• Design & Manufacturing
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• v.16 no.3
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• pp.16-21
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• 2022

In order to reduce the weight of parts and materials for the development of high-efficiency engines in accordance with the strengthening of automobile fuel efficiency regulations, the existing casting material is changed to a iron plate material, and plastic processing and turning operations are performed to lighten the weight and reduce the manufacturing cost. Among the pulley components applied to the damper pulley, the HUB product was manufactured by plastic machining instead of the existing casting process, and the inspection standardized for automating the inner diameter and parallelism measurement of the turning result of the new hub part with improved quality, and the inspection system for this Development of design and operation software to automate the inspection of the inner diameter and parallelism of the hub was described. The representative specifications of the development equipment are a hub inner diameter 22mm inspection system, a three-point inspection system with a parallelism of 0.15mm on the top.