• 드라이브 ㆍ 컨트롤
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• 제15권1호
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• pp.38-49
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• 2018

This research describes the development model and testing of a hybrid damper which can be applicable to a vehicle suspension. The hybrid damper is devised to improve the performance of a conventional passive oil damper using a magneto-rheological (MR) accumulator which consists of a gas accumulator and a MR device. The level of damping is continuously variable by the means of control in the applied current in a MR device fitted to a floating piston which separates the gas and the oil chamber. A simple MR device is used to resist the movement of floating piston. At first a mathematical model which describes all flows within the conventional oil damper is formulated, and then a small MR device is also devised and adopted to a mathematical model to characterize the performance of the device.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.748-751
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• 2010

로켓을 발사하기 위해서는 발사대에 로켓을 세워놓고 추진제와 고압가스 등을 충전한 다음 원격제어로 로켓을 발사하게 된다. 로켓 발사대로는 지상저장탱크에 고압으로 저장되어 있는 고압가스가 여러 종류의 압력조정기를 통과하여 운용압력으로 감압되어 공급된다. 로켓 발사시에는 발사통제실에서 원격으로 모든 운용이 이루어지기 때문에 압력조정기 전단에는 급격한 가스 공급이나 압력변동 등으로 인하여 운용압력을 벗어나거나 압력조정기가 파손되는 경우가 발생할 수 있다. 본 논문에서는 고압가스가 안정적으로 감압되어 발사대로 공급되기 위한 고압가스감압시스템 최적화 설계기법을 고찰하였다.

• 전기학회논문지
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• 제56권8호
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• pp.1424-1429
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• 2007

This paper presents a simple and reliable one-touch type multi-immunosensing lab-on-a-chip (LOC) detecting antibodies as multi-disease markers using electrochemical method suitable for a portable point-of-care system (POCS). The multi-stacked LOC consists of a PDMS space layer for liquids loading, a PDMS valve layer with 50 im in height for the membrane, a PDMS channel layer for the fluid paths, and a glass layer for multi electrodes. For the disposable immunoassay which needs sequential flow control of sample and buffer liquids according to the designed strategies, reliable and easy-controlled on-chip operation mechanisms without any electric power are necessary. The driving forces of sequential liquids transfer are the capillary attraction force and the pneumatic pressure generated by air bladder push. These passive fluid transport mechanisms are suitable for single-use LOC module. Prior to the application of detection of the antibody as a disease marker, the model experiments were performed with anti-DNP antibody and anti-biotin antibody as target analytes. The flow test results demonstrate that we can control the fluid flow easily by using the capillary stop valve and the PDMS check valves. By the model tests, we confirmed that the proposed LOC is easily applicable to the bioanalytic immunosensors using bioelectrocatalysis.

• 한국정밀공학회지
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• 제22권6호
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• pp.135-143
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• 2005

The shoes process management monitoring system for supporting SCM is developed in this study. This system consists of a monitoring program, a conveyer system, a pneumatic unit, a controller, an USB camera, and a server and a client computer. To operate the developed system easily, the monitoring program using LabVIEW in the Windows environment is developed. This program consists of 5 modules: production management, inventory control, media management, defective management, and communication management. The developed system has several advantages: reduced time for managing process work, decreased labor costs, effective operation, and continuous work without an operator. Nowadays advanced manufacturing companies are trying to find a way to check the performance of their production equipments and plants from remote sites. Thus, to manage the developed system from remote sites, communication network is constructed. In order to evaluate the performance of the monitoring system, experiments were performed. The experimental results showed that the developed system provided a reliable performance and a stable communication.

• 한국기계가공학회지
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• 제19권12호
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• pp.80-86
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• 2020

With the exception of welding activities, it is forbidden to use electricity in shipyards, owing to safety concerns such as the possibility of fire, explosions, and short circuits. In this paper, an automatic chamfering machine using pneumatics is proposed for use in such environments. Customers specify their requirements and the machine derives the corresponding theoretical design conditions. The proposed machine was used to perform 3D modeling, and its suitability and performance were confirmed via cutting experiments of the manufactured device. Two types of sensors may be used in this system: contact and non-contact. In the case of the contact type, an end-stop switch that can recognize the end of the material is installed, and when the machine reaches the end of the material, the end-stop switch is operated to cut off the air pressure. In the non-contact type, four sensors were used: photonic, ultrasonic, metal detection, and encoder. The use of the four sensors was repeated 30 times, and the average error determined. Thus, the optimum sensor was identified.

• Advances in nano research
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• 제10권3호
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• pp.271-280
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• 2021

The present work deals with an investigation on longitudinal wave propagation in nanobeams made of graphene sheets, for the first time. The nanobeam is modelled via a higher-order shear deformation theory accounts for both higher-order and thickness stretching terms. The general nonlocal strain gradient theory including nonlocality and strain gradient characteristics of size-dependency in order is used to examine the small-scale effects. This model has three-small scale coefficients in which two of them are for nonlocality and one of them applied for gradient effects. Hamilton supposition is applied to obtain the governing motion equation which is solved using a harmonic solution procedure. It is indicated that the longitudinal wave characteristics of the nanobeams are significantly influenced by the nonlocal parameters and strain gradient parameter. It is shown that higher nonlocal parameter is more efficient than lower nonlocal parameter to change longitudinal phase velocities, while the strain gradient parameter is the determining factor for their efficiency on the results.

• Nuclear Engineering and Technology
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• 제56권3호
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• pp.922-932
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• 2024

This paper presents the design features and preliminary design analysis results of the Wielenga Innovation Static Salt Reactor (WISSR). The WISSR incorporates features that make it both flexible and inherently safe. It is based on innovative technology that controls a nuclear reactor by moving molten salt fuel into or out of the core. The reactor is a low-pressure, fast spectrum transuranic (TRU) burner reactor. Inherent shutdown is achieved by a large negative reactivity feedback of the liquid fuel and by the expansion of fuel out of the core. The core is made of concentric, thin annular fuel chambers containing molten fuel salt. A molten salt coolant passes between the concentric fuel chambers to cool the core. The core has both fixed and variable volume fuel chambers. Pressure, applied by helium gas to fuel reservoirs below the core, pushes fuel out of a reservoir and up into a set of variable volume chambers. A control system monitors the density and temperature of the fuel throughout the core. Using NaCl-(TRU,U)Cl₃ fuel and NaCl-KCl-MgCl₂ coolant, a road-transportable compact WISSR core design was developed at a power level of 1250 MWt. Preliminary neutronics and thermal-hydraulics analyses demonstrate the technical feasibility of WISSR.

• Composites Research
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• 제27권2호
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• pp.47-51
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• 2014

본 논문은 기존의 유/공압 및 전기식 모터를 대체할 수 있는 경량, 고성능 지능소자 구동기를 설계/제작하고 이를 소형 무인비행체의 조종익 시스템에 적용 가능성을 연구한 것이다. 또한 압전 복합재료 작동기에 대한 성능평가를 수행하였으며, 유니모프 및 바이모프 형태의 작동기를 제작하여 각각의 작동 특성을 확인하였다. 이와 같은 성능시험 평과 결과를 통해 바이모프 형태의 작동기가 하중 유무와 무관하게 선형적인 받음각 변화를 가짐을 알 수 있었다. 이러한 지능소자 구동 시스템은 소형 로봇, 유도무기 및 MAV, UAV의 조종익 제어 시스템으로 사용될 수 있는 가능성을 확인하였다.

• 항공우주기술
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• 제1권1호
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• pp.141-146
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• 2002

로켓 추진에 의한 동력 비행 중 비행체의 자세제어를 위해, 대기권내 비행에 있어서는 공력비행 조정익으로 조종할 수 있으나 공기가 희박한 높은 고도나 대기권 밖에서의 비행은 추력벡터제어에 의존할 수밖에 없다. 추력벡터제어 방법으로 현재 여러 가지 장치가 개발되어 사용되고 있는데 본 연구는 로켓이 비행하는 동안 김발에 의해 연결된 로켓엔진 전체를 움직여 엔진에서 발생한 추력의 방향을 조종하여 로켓의 자세를 제어하는 김발엔진구동 추력벡터제어방식에 대한 내용을 다루었다. 로켓에 적용 가능한 김발엔진 구동장치로는 전기유압식, 전기기계식, 공압식 장치 등이 있으나 큰 동력이 요구되는 시스템에서는 대부분 출력 대 무게비가 높은 전기유압식 구동장치가 사용된다. 본 연구에서는 KSR-III의 추력벡터제어를 위해 사용되는 전기유압식 김발엔진 서보구동시스템을 상세모델링하였고 이에 기초하여 시뮬레이션을 수행하였다. 그리고 시뮬레이션 결과와 실제 시스템을 대상으로 시험한 결과를 비교하여 모델을 검증하였다.

• 한국추진공학회지
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• 제25권3호
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• pp.127-137
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• 2021

발사대시스템은 다양한 설비로 구성된다. 이들 설비를 원격 운용하는 발사관제시스템은 제어 알고리즘 개발과 검증에 많은 시간과 노력이 소요된다. 알고리즘 검증은 소프트웨어 제작자가 시험절차서에 기반한 시뮬레이션 상태 값을 입력하고, 알고리즘 흐름에 따라 출력 결과를 확인하는 과정을 통해 이루어진다. 이러한 검증 과정은 반복적으로 수행되므로 작업 오류를 쉽게 유발할 수 있다. 본 논문에서는 작업 오류의 최소화와 검증 기간 단축이 가능한 스크립트 시험절차서 기반의 효율적인 자동화 검증 방법을 제안하며, 발사대의 고압가스 공급설비와 전자식 유공압패널설비 제어 알고리즘 검증시험에 적용한 결과를 제시한다.