• 제목/요약/키워드: Thrust density

검색결과 133건 처리시간 0.032초

테이프 피더 내장 공압 액추에이터에 대한 신뢰성 평가에 관한 연구 (A Study on the Reliability Analysis for the High Precision Pneumatic Actuator within Tape Feeder)

  • 최진화;전병철;조명우;강성민;이수진
    • 한국공작기계학회논문집
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    • 제15권4호
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    • pp.63-68
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    • 2006
  • This research presents the reliability analysis of the pneumatic actuator within the tape feeder that is used to transfer the correct force to linked parts during l.0E+7 cycles. First, the degradation analysis for thrust and air leakage is executed to obtain the failure data of a product based on its performance over time. Second, once the parameters has been calculated using the weibull 2-parameter distribution and MLE(Maximum Likelihood Estimation), information related to life such as reliability, failure rate, probability density function is estimated. Finally, MTTF(Mean Time To Failure) and $B_{10}$ life of actuators are calculated. MTTF means the mean life at the confidence level and $B_{10}$ life refers to the time by which 10% of the product would fail. In this study, failure causes and solutions are examined using the reliability analysis.

세포 운동 가시화를 통한 상처 치유 과정 내 경계 이동의 규명 (Identification of boundary migration during the wound healing through the visualization of cell migrations)

  • 정현태;이재성;신현정
    • 한국가시화정보학회지
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    • 제18권2호
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    • pp.10-17
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    • 2020
  • The curvature of wound boundaries has been identified as a key modulator that determines a type of force responsible for cell migration. While several studies report how certain curvatures of the boundary correlate with the rate at which the wound closes, it remains unclear how these curvatures are spatiotemporally formed to regulate the healing process. We investigated the dynamic changes in the boundary curvatures by visualizing cell migration patterns. Locally, cells at the convex boundary continuously move forward with transmitting kinetic responses behind to the cells away from the boundary, and cells at the concave boundary exhibit dramatic contracting motion, like a purse-string, when they accumulate enough negative curvatures to gain the thrust toward the void. Globally, the dynamics of boundary geometries are controlled by the diffusive flow of cells driven by the density gradient between the wound area and the cell layer.

슬러리와 젤 추진제의 기술개발 동향 (Technical Review of Slurry and Gelled Propellant)

  • 정병훈;고승원;황갑성;한정식;홍명표
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.168-171
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    • 2007
  • 슬러리와 젤 추진제에 대한 최근기술동향과 주요기술을 분석하였다. 선진국에서는 1950년대부터 연구를 통하여 이러한 추진제가 가진 높은 비추력과 밀도, 우수한 취급성, 안전성, 그리고 추력조절 가능성과 같은 장점을 확인하였다. 추진제의 유변특성, 분무/연소 현상, 그리고 추진제 특성을 고려한 추진시스템 설계 등이 활발히 연구 되었다. 이 추진제는 군용 전술미사일 추진기관외에 민수용으로 램제트, 펄스폭발 엔진과 차세대 추진방식인 복합엔진에도 적용을 목표로 개발되고 있다.

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ADN 단일 추진제 기반 1N 급 추력기 시스템 개발 (Development of 1-N class Thruster System based on ADN Monopropellant)

  • 김진철;최우주;조영민;전종기;김태규
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.406-408
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    • 2017
  • Ammonium dinitramide (ADN) 저독성 단일 추진제 기반의 1N 급 추력기 및 시험장치 개발을 수행하였다. ADN은 기존에 인공위성용 추력기에 사용되고 있는 하이드라진 대비 취급이 용이하고 밀도, 비추력과 같은 물리적 특성이 우수한 물질이다. 이러한 특성으로 인해 ADN은 친환경 추진제로 주목받고 있다. 본 논문에서는 ADN 단일 추진제의 성능시험을 위한 1 N급 추력기 및 측정설비를 설계하였다. 설계 및 실험을 위한 추진제의 조성은 Methanol:$H_2O$:ADN 각각을 11.2:25.4:63.4로 설정하여 진행하였다.

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공심 코일형 리니어 DC 모터의 설계 및 동특성 해석 (Design and Dynamic Analysis of Air-core Coil type Linear DC Motor)

  • 강규홍;홍정표;김규탁;하근수;정중기;임태빈
    • 대한전기학회논문지:전기기기및에너지변환시스템부문B
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    • 제49권3호
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    • pp.165-171
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    • 2000
  • This paper proposes a technique to design of air-core type Linear DC Motor(LDM) by using Equivalent Magnetizing Current(EMC) method and has performed its dynamic analysis. The magnetic flux density differ in accordance with airgap position due to difference of mechanical and magnetic air gap length and the coil shape has an influence on the thrust. Therefore, the analysis of magnetic field due to the magnets is carried out by EMC. The phenomena according to the various coil various coil shape under the same Magneto Motive Force(MMF) has been analyzed and its result is applied to the design process. The appropriateness of the proposed technique is confirmed by Finite Element Method(FEM) and its dynamic analysis is carried out from the coupling of the electrical circuit equation and mechanical kinetic equation.

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Spray Characteristics of the Rocket Oxidizer-rich Preburner Injection System

  • Yang, Joon-Ho;Choi, Seong-Man;Han, Young-Min
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.255-259
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    • 2008
  • This paper presents the spray characteristics of the oxidizer rich preburner injector which can be used in the high-thrust rocket system. We designed the basic shape of the liquid-liquid coaxial swirl injector for the rocket oxidizer rich preburner injection system. To understand the spray angle variation with the high pressure environment, the spray visualization in the high pressure chamber was preformed. Also we measured the droplet velocity, the Sauter Mean Diameter(SMD), the volume flux and the number density with the PDPA system by using water in atmospheric pressure. The results show that the spray angle is reduced by increasing ambient pressure and maximum droplet velocity is shown from a nozzle tip and then the droplet velocity decreases as a spray moves to the downstream. The SMD decreases on the axial distance from 20 mm to 50 mm but it increases over 50 mm. That is due to the increasing number of collision with each droplet and interaction with ambient air on going downstream direction.

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연료전지 추진 멀티콥터의 사이징 계산 방법에 관한 연구 (Study on Sizing Calculation Method of Fuel Cell Propulsion Multirotor)

  • 이동근;안국영;김영상
    • 한국수소및신에너지학회논문집
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    • 제32권6호
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    • pp.542-550
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    • 2021
  • As the application of multirotor grows, the demands for multirotor that can fly longer and load more are increasing. Hydrogen has a high energy density, so it can satisfy these demands when used in multirotor. In order to design hydrogen fueled multirotor that satisfies the desired flight time and payload, it is important to calculate the specifications of a fuel cell, battery, and hydrogen storage system. This paper contains detailed information on various energy systems used in multirotor and fuel cell powered multirotor research trends. This study proposed a sizing calculation method that meets the target flight time and payload using thrust and power equations. It has been explained how the two equations derive the particular specifications. The specifications of the multirotor were derived by assuming a payload of 50 kg and a flight time of 1 hour. In addition, the effects of the values of the fuel cell, hydrogen storage system, and motor propeller were analyzed.

제천(提川) 서남부(西南部) 옥천대(沃川帶) 지역(地域)에 대(對)한 중력탐사연구(重力探査硏究) (Gravity Survey on the Southwestern Area of Jechǒn in the Okchǒn Zone)

  • 민경덕;박혜심
    • 자원환경지질
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    • 제22권2호
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    • pp.91-102
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    • 1989
  • The gravity measurement has been conducted at 61 stations with an interval of about 500 to 1,000 m along two survey lines of about 47 Km between $Chungju-Jech{\check{o}}n$ and $Salmi-D{\check{o}}cksanmy{\check{o}}n$ in order to study on the subsurface geologic structure and structural relation between $Okch{\check{o}}n$ Group and Great Limestone Group of $Chos{\check{o}}n$ Supergroup. The Bouger gravity anomalies were obtained from the reduction of the field observations, and the distribution patterns of the basement and subsurface geologic structure were interpreted by means of the Fourier-Series and Talwani method for two-dimensional body. The depth of Conrad discontinuity varies from 12.7 Km to 15.7 Km, and vertical displacements along the Osanri and Bonghwajae faults are 1.0 Km and 1.5 Km, respectively between Chungju and $Jech{\check{o}}n$. The depth of Conrad discontinuity varies from 13.8 Km to 15.4 Km, and vertical displacement along the Bonghwajae fault is 0.5 Km between Salmi and $D{\check{o}}cksanmyon$. The basement is widely exposed at several places between Chungju and $Jech{\check{o}}n$. In the unexposed area between Osanri and $W{\check{o}}lgulri$, its depth is from 1.5 Km to 2.1 Km. It is displaced downward along the Osanri and Bonghwajae faults by 0.8 Km and 0.6 Km, respectively, and is displaced upward along the Dangdusan fault by 1.6 Km. On the other hand, the depth of the basement varies abruptly by the Sindangri, Jungwon, Kounri, and Bonghwajae faults between Salmi and $D{\check{o}}cksanmy{\check{o}}n$, and it is from 2.8 Km to 3.2 Km around $Salmimy{\check{o}}n$, from 1.6 Km to 2.5 Km between the Sindangri and Bonghwajae faults, 3.0 Km near Koburangjae, and 2.5 Km at $Doj{\check{o}}nri$. The high Bouguer gravity anomalies are due to the accumulation of $Okch{\check{o}}n$ Group and $Jangs{\check{o}}nri$ Metamorphic Complex whose density is higher than the basement exposed between Sondong and Osanri, and imply the existance of Bonghwajae Metabasite or hornblende gabbro of high density distributed along the Bonghwajae fault in the vicinity of Koburangjae. The low Bouguer gravity anomalies resulted form the fracture zone associated with fault or rock of low density imply the existance of the Osanri, Bonghwajae, Dangdusan faults and $Daed{\check{o}}cksan$ thrust between Chungju and $Jech{\check{o}}n$, the uplift of the basement by the Sindangri, Jungwon, Kounri, and Bonghwajae faults, and extensive distribution of Cretaceous biotite granites between Salmi and $Docksanmy{\check{o}}n$. The thickness of $Okch{\check{o}}n$ metasediments varies from 1.5 Km to 3.2 Km, and that of Great Limestone Group of $Chos{\check{o}}n$ Supergroup from 200 m to 700 m. It is interpreted that $Okch{\check{o}}n$ Group is in contact with Great Limestone Group of $Chos{\check{o}}n$ Supergroup by the fault zones of the Bonghwajae and $Daed{\check{o}}cksan$ faults, and the Bongwhajae fault is a thrust of high angle, by which the east of the basement is displaced downward 0.5 Km between Chungju and lechon, and 1.0 Km between Salmi and $D{\check{o}}cksanmy{\check{o}}n$.

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중력탐사에 의한 삼척-태백간의 지하지질 및 지질구조 연구 (Gravity Survey of the Subsurface Geology and Geologic Structure between Samcheog and Taebaek Area)

  • 민경덕;조광은
    • 자원환경지질
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    • 제28권1호
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    • pp.79-88
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    • 1995
  • The gravity measurment has been carried out at 48 gravity stations with intervals of 1.0~1.5 km along the survey line between Samcheog, Gosari and Taebaek to study subsurface geology and geologic structure in the northeastern part of the Ockchon zone. The Bouguer gravity anomaly values were obtained from the measured gravity values through the gravity corrections. The subsurface geology and geologic structure were interpreted quantitatively by means of the Fourier series method and Talwani method for 2.5 dimensional body. In the study area, the depth of Conrad discontinuity is about 10 km at Samcheog, northeastern end of the survey line, and it is increased rapidly to about 12.5 km at Miro, 15 km at Gosari and 15.5 km at Dongjeom, southwestern end of the survey line, respectively. The depth of the basement of the Ockchon zone exposed at Samcheog is increased smoothly to about 2 km at 5 km from Samcheog along the survey line, and is exposed again in the area between Singiry and Gosari. Beyond Gosari its depth is increased to about 1.7 km, and displaced 2.3 km downward by Osipcheon fault near Dogyeri and 0.5 km by Baeksan thrust near Cheolam, respectively. Many V-shaped low Bouguer gravity anomalies resulted from the fracture zone associated with faults imply the existence of Osipcheon fault and several inferred faults. The low Bouguer gravity anomaly zone between Tongdong and Dongjeom is caused by Jurassic gneissose granite. A local high Bouguer gravity anomaly at 35 km along the survey line from Samcheog is interpreted by the effect of iron deposit of high density existed at subsurface. The thickness of Great Limestone Group varies from 0.5 km to 1.4 km, that of Pyeongan Supergroup from 0.4 km to 0.9 km, and that of Yangdeog Group is about 0.3 km. The thickness of Jurassic gneissose granite varies from 1.5 to 3.0 km.

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원심모형실험을 이용한 주문진 표준사 지반내 알루미늄 모형 터널 복공의 역학적 거동에 관한 연구 (Analysis of the Structural Behaviours of Aluminum Tunnel Lining in Joomunjin Standard Soil by Centrifugal Model Tests)

  • 김택곤;김영근;박중배;이희근
    • 터널과지하공간
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    • 제9권2호
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    • pp.114-130
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    • 1999
  • 최근 들어 노후화 터널 및 시공불량의 원인으로 결함이 발생하여 시공이후에 라이닝이 제기능을 발휘하지 못하여 보수, 보강, 심지어 재시공되는 사례가 발생하고 있어 이에 대한 역학적 거동 분석의 필요성이 제기되고 있다. 본 연구에서는 100G(G : 중력가속도)까지의 원심모형실험(centrifuge)을 실시하여 몇몇 라이닝들의 역학적 거동을 분석하였다. 이를 위해 강사기 (sand rainer)를 이용하여 평균적으로 상대밀도 86% 주문진 표준사 지반을 작성하였으며, 이 때 평균 정지토압계수는 평균 0.39로 나타났다. 원심모형실험의 토피 대 터널 높이비는 3으로 설정하였으며, 라이닝 재료로서 알루미늄을 이용하여, 천단부 및 어깨부 배면공동, 천단두께부족, 무인버트, 측벽결함 라이닝을 제작하여, 각종 센서로부터 라이닝 원주변형률, 휨모멘트, 축력, 라이닝토압, 지중토압, 지표침하를 계측 및 분석하였다.

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