• 제목/요약/키워드: Endurance performance

검색결과 355건 처리시간 0.028초

스마트무인기 축소형 비행체 개발 (Development of the Scaled Vehicle of Smart UAV)

  • 장성호;최성욱;구삼옥
    • 항공우주기술
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    • 제6권2호
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    • pp.236-244
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    • 2007
  • 스마트무인기의 기본 비행성능 파악과 비행제어 알고리즘의 검증을 위하여 40% 축소형 비행체를 개발하였다. 축소형 비행체는 실물기와 유사한 형태의 짐발 허브와 드라이브 장치를 채택하였으며 강제 공랭 방식의 왕복엔진을 장착하였다. 축소형 비행체 주요 부품에 대한 다양한 시험을 수행하였고 조립된 축소형 비행체의 지상시험 및 호버링 시험을 통하여 주요 성능과 기계적 내구성을 확인하였다.

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주행시험기를 이용한 차륜의 안전성 평가에 관한 연구 (A Study on Safety Evaluation of Wheel Using Roller Rig Tester)

  • 함영삼
    • 한국정밀공학회지
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    • 제32권7호
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    • pp.591-595
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    • 2015
  • The roller rig tester for safety performance evaluation of wheel derailment is a test facility which can give the test load condition to the test wheel, similar to the actual dynamic condition in actual running condition. This study describes the evaluation result on the durability of the resilient wheel equipped with the ring damper and the damping material, and installed in the half part of a full scaled bogie in combination with the primary spring when it rotates under the dynamic condition. The evaluation result on durability of resilient wheel after load test of 2 million cycles shows that the safety of wheel is not affected by the applied load in visual inspection and nondestructive test, however, in the bolt used for fastening the ring damper to the wheel the loosening was found. Accordingly the use of self-locking nut and washer is recommended.

해양레저용 발전기 방음케이싱 개발을 위한 소음 진동 측정 분석 (Noise and Vibration Measurements for Development Leisure Generator Soundproof)

  • 김용휘;이종명;하정민;장용호;최병근
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2014년도 추계학술대회 논문집
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    • pp.523-526
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    • 2014
  • Recently, all the generators needed of the boats are being imported, so our objective is to make a national production of soundproof generators. We have already built a marine soundproof generator and it has also been hrough an endurance test for its commercialization. This paper has the noise vibration measurements needed for maintaining its durability and performance. We concluded that the difference of the noise values with and without the case was of 11.4dB.

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자동차용 직선화 배기시스템의 피로내구 해석 및 평가 (Fatigue Durability Analysis and Evaluation for Straighted Type Exhaust System of Automobile)

  • 박세종;서호철
    • 한국자동차공학회논문집
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    • 제13권1호
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    • pp.147-152
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    • 2005
  • The exhaust system of automobile is faced with random or spectrum types of fatigue loads during usage life and so needs to be closely estimated for quality and performance to have enough certainty on design endurance lift during preliminary design process. Structural operation conditions, operation load history, property of material and manufacturing process etc. should be considered by performing experiment approach. Using the software program for predicting fatigue life quickly and exactly in preliminary design stage saves plenty of time and cost generated by fatigue tests. In this paper, fatigue life prediction was performed on the basis of fatigue analysis using MSC/FATIGUE and load data from field test and the life of development items was estimated and compared through the results.

직접분사식 소형 디젤엔진의 3D 유동특성 및 분절형 스틸 단조 피스톤의 최적화에 관한 연구 (A Study on the Optimization of Articulated Steel Forging Piston and 3D Analysis of Fluid Characteristics for Light Duty DI Diesel Engine)

  • 김현철;박종호
    • 한국자동차공학회논문집
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    • 제12권5호
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    • pp.25-31
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    • 2004
  • In order to prepare for the large power diesel vehicle, the current trend of advanced nations is to shift from the aluminum alloy piston to the steel piston. In this research, a steel forging piston which replaces the aluminum alloy piston is developed to improve the power performance of the diesel engine. The three dimensional flow and combustion analysis of the target engine is conducted. Using the result of the analysis, the piston is optimized, and a prototype of the articulated steel forging piston is built. The reliability of the piston has been evaluated through durability test using a Hydropuls Test Machine for 300,000 km.

반파정류를 이용한 형광램프용 전자식 스타터의 개발 (Development of an electronic starter using a half-wave rectifier for fluorescent lamps)

  • 이동호;송상빈;여인선
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 하계학술대회 논문집 F
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    • pp.2088-2090
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    • 1998
  • A low-cost electronic starter is developed to decrease ignition failure significantly through successive starting trial and to prevent overheating at the end of fluorescent lamp life. Moreover, it has an additional feature of being capable of ignition at the recovered lamp voltage without any circuit correction. The developed electronic starter is consisted of four parts - a half wave rectifier circuit, a timer circuit, a switching circuit and a protection circuit. The protection circuit made up of a transistor and capacitors utilizing capacitive characteristics, carries out successive starting trial and end-of-life protection. Lamp ignition is completed within 0.5 seconds with taking advantage of a high preheating current from the half-wave rectifier circuit. Nevertheless, its performance is proved to be very excellent through a standard switching endurance test.

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공동 현상 방지를 위한 버터플라이 밸브의 유동장 해석 (Numerical Analysis of Flows in Butterfly Valves to Prevent Cavitation)

  • 윤준용;이승준;김은석
    • 한국유체기계학회 논문집
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    • 제7권1호
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    • pp.9-16
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    • 2004
  • A three-dimensional numerical analysis was carried out on incompressible flows in butterfly valves by using commercial FLUENT/UNS code. Characteristics of complex flows including cavitation effect were investigated for different valve disk angles. The butterfly-valves that had different disk angles and different disk shapes were compared with each other in detail. This study focused on the flow analysis in the conventional butterfly valve and the newly designed butterfly valve in order to prevent cavitation. The newly designed valve shows great improvement on performance and endurance.

개인화기 총열 표면처리 및 시험에 관한 연구 (Study on Surface Treatment and Test over the Barrel of Small Arms)

  • 채제욱;김인우;이영신
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.722-727
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    • 2004
  • This paper includes the comparative study between Cr plating and nitriding process with an aim at improving corrosion, wear and maintainability for KNR(Korean Next Generation Rifle) 5.56mm barrel. The endurance test was conducted to compare the performance of standard barrel, Cr plating barrel and nitriding barrel. Main activities are described as follows; optimal Cr plating and nitriding process set-up for KNR 5.56mm barrel; durability test of each barrel(20,000 rounds); salt water immersion test; dispersion, initial velocity, inner diameter data acquisition. According to the results of this firing test, Cr plating barrel is superior to standard barrel and nitriding barrel in view of corrosion, wear and maintainability

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n/m 흐름작업의 Heuristic 기법에 관한 연구 (A Study on the Heuristic Algorithm for n/m Flow- Shop Problem)

  • 이근부
    • 산업경영시스템학회지
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    • 제5권6호
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    • pp.41-48
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    • 1982
  • This paper analyzed md developed flow - shop sequencing heuristic method. The essence of the heuristic approach is in the application of selective routine that reduce the size of a problem. The advantages of this approach are consistency. Speed, endurance and the ability to cope with more data and larger systems than is humanly possible, In recent years many heuristic procedures have been suggested for the flow - shop sequencing problem. Although limited comparisons of these procedures have been made, a full scale test and evaluation have not been reported previously. The maximum flow - time criterion is selected as the evaluation criterion is selected as the evaluation criterion of flow - shop's efficiency. The author evaluated these 3 heuristic method's performance. By the evaluation of the result, we can see that the modified methods produce a shorter maximum flow - time than the original methods.

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BADA를 활용한 4-D 경로 모델링법 개발 (Development of 4-D Trajectory Modeling using BADA)

  • 오은미;은연주;전대근
    • 한국항공운항학회지
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    • 제20권2호
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    • pp.1-6
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    • 2012
  • Four dimensional(4-D) trajectory modeling is conducted based on flight plan. The flight plan is divided into several segments which represent certain operating flight modes. Thrust, drag and fuel consumption rate of an aircraft are calculated using BADA provided by Eurocontrol. The trajectory is modeled with the rate of climb/descent calculated with Total-Energy Equation. The simulation results with a typical aircraft and its flight plan indicate that the trajectory modeled corresponds well with the suggested flight plan. The performance profiles including total endurance time and time history for speed, thrust, drag and fuel consumption were also appropriately generated.