• 제목/요약/키워드: vertical lift

검색결과 175건 처리시간 0.024초

타워를 포함한 6kW급 수직축 풍력발전기 구조진동해석 (Structure Dynamic Analysis of 6kW Class Vertical-Axis Wind Turbine with Tower)

  • 김동현;류경중;김요한;김성복;김광원;남효우;이명구
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2011년도 춘계학술대회 논문집
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    • pp.663-670
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    • 2011
  • In this study, the design and verification of 6kW class lift-type vertical-axis wind turbine (VAWT) has been conducted using advanced CAE technique based on computational fluid dynamics (CFD), finite element method (FEM), and computational structural dynamics (CSD). Designed aerodynamic performance of the VAWT model is tested using unsteady CFD method. Designed structural safety is also tested through the evaluation of maximum induced stress level and resonance characteristics using FEM and CSD methods. It is importantly shown that the effect of master eccentricity due to rotational inertia needs to be carefully considered to additionally investigate dynamic stress and deformation level of the designed VAWT system.

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역도 인상동작에 대한 근력의 기여도 분석 (Analysis of Muscle Contribution on Snatch Motion)

  • 강찬금;박은혜
    • 한국운동역학회지
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    • 제13권3호
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    • pp.265-276
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    • 2003
  • The objective of this research is to provide basic data for improving athletic performances, suggesting methods that can be utilized at games and coaching movements in the snatch, by analyzing the level of contribution of muscles to the movements of the snatch lift through three-dimensional imaging and EMG analysis between skilled and unskilled lifters. To this end, three high school students (the skilled group), three middle school student (the unskilled group) were selected; two digital video cameras and electromyography were used. The muscles measured by an EMG include gastrocnemius muscle, biceps femoris muscle, erector spinae, latissimus dorsi muscle, trapezius muscle, and brachioradialis. Based on the Ariel Performance Analysis System (APAS) program, the results of the analysis are summarized as follows. 1. In performing snatch pulls, the skilled lifters were found to simultaneously move the weight centers of the body and the barbell close to vertical, close to the shoulders in the pulling portion; in snatching and grabbing the barbell from a sited position, it was observed that the shorter the time for adjusting to change in the height of the barbell by using rotational inertia, the better it is to perform the movements. 2. The skilled lifters were observed to perform stable and efficient movements in grabbing the bar in a sited position, by moving the barbell and weight center of the body close to vertical and moving the shoulder joint under the bar fast. 3. The results of the EMG analysis of the entire movements from the snatching portion to the portion of grabbing the bar in a sited position show that when the skilled lifters lifted the barbell vertically during the pulling portion, their shoulder joints were extended to put more weight on biceps femoris muscle and brachioradialis; and in snatching and grabbing the bar from a sited position, it was found desirable to increase the myoelectrical activity of erector spinae in order to achieve a balance in the movements of the hip joint between font and rear, as the weight centers of the body and the barbell move higher. On the other hand, the unskilled lifters were found that in response to change in posture, they increase their muscular strength inefficiently in performing the movements throughout the entire lifting process.

철도차량 충돌에 의한 타고오름 탈선거동 예측을 위한 단일윤축 이론모델 개발 (Development of a Theoretical Wheelset Model to Predict Wheel-climbing Derailment Behaviors Caused by Rolling Stock Collision)

  • 최세영;구정서;유원희
    • 한국철도학회논문집
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    • 제14권3호
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    • pp.203-210
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    • 2011
  • 본 논문에서는 열차 충돌로 발생되는 충격으로 차축에 큰 수직하중 및 수평하중이 부과될 때 플랜지가 레일을 타고 오르는 탈선현상을 예측할 수 있는 단일 윤축의 이론적 탈선 모델을 연구하였다. 철도차량 충돌 시 크게 타고오름(wheel-climbing), 들려오름(lift-up), 전복(roll-over) 등과 이들의 복합유형탈선이 발생할 수 있다. 타고오름 및 복합 유형의 탈선은 세 가지(Climb-over, Climb/roll-over, Roll-over)로 정의할 수 있다. 본 논문에서는 충돌 후 탈선거동을 예측하기 위하여 타고오름 및 복합 유형 탈선에 대한 단일윤축 이론모델을 제안하고, 정의한 세 가지 탈선거동이 발생하기 위한 조건을 제시하였다. 타고오름 및 복합 유형의 탈선거동을 예측하기 위하여 제안된 단일윤축 이론모델의 타당성을 단순플랜지 형상 윤축모델을 사용한 동역학 시뮬레이션을 통하여 검증하고, 타당성을 보인다.

부력식 연직수문의 자유흐름 상태에서 하단방류 특성에 관한 실험적 연구 (An experimental study on the discharge characteristics of underflow type floating vertical lift gate at free-flow condition)

  • 한일영;최흥식;이지행;나성민
    • 한국수자원학회논문집
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    • 제51권5호
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    • pp.405-415
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    • 2018
  • 연직수문의 방류량 계산에 필요한 수리학적 변수는 유량계수, 수문개방고, 상류수심이다. 자동수문의 수문개방고는 나머지 변수에도 영향을 미치기 때문에, 운영 중 수문개방고의 거동을 예측하는 것은 정밀한 수문설계를 위해 매우 중요하다. 본 연구에서는 부력식 연직수문 모형을 대상으로 부력이론으로 계산한 수문개방고와 실험에서 방류 중에 측정한 값과의 관계로 부터, 임의의 상류수심에서 수문개방고를 예측할 수 있는 무차원 관계식을 도출하였다. 측정값이 계산 값과 차이가 나는 것은 동수압 하중에 의한 영향임을 압력계수를 이용하여 검증하였다. 유량계수는 수문개방율과의 무차원 관계식을 도출하였다. 도출된 관계식들을 홍수추적에 적용한 결과, 수문설계 시에는 동수압 하중으로 인한 수문개방 억제 효과를 충분히 고려하여야 하는 것으로 판단되었다.

수직이송 서비스가 가능한 한국형 PRT 운행제어시스템 개발 (Development of an Operation Control System of the Vertical Transferable Korean Personal Rapid Transit)

  • 김백현;엄주환;정락교;변윤섭;강석원
    • 디지털융복합연구
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    • 제12권10호
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    • pp.337-343
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    • 2014
  • PRT(Personal Rapid Transit)는 유형 또는 무형의 전용궤도에서 자동으로 승객의 요구에 따라 출발지에서 목적지까지 최적의 경로로 논스톱 운행하며, 높은 접근성과 프라이버시 보장 등 자가용 수준의 서비스 제공이 가능한 대중교통수단으로서, 최근 새로운 미래교통시스템으로 재조명받고 있다. 본 논문에서는 PRT 시스템의 연계 운행 효율성 극대화를 목표로 수직이송장치를 연동제어하는 PRT 운행제어시스템의 제어모듈 및 시뮬레이터의 설계 및 시험결과를 제시하였다. 수직이송장치부의 PLC는 운영제어센터 또는 역제어시스템과의 인터페이스를 위해 Modbus 프로토콜을 적용하여 설계되었으며, 원격제어시스템으로부터 명령을 전달받아 동작하는 자동모드와 수직이송장치에 설치된 센서검지 상태에 따라 독립적으로 동작하는 수동모드로 구성하였다. 또한, 실제 차량이 운행하는 환경에서 가상의 차량운행 시나리오를 적용하여 실제 차량과 가상 차량을 혼합하여 운행할 수 있는 3D 그래픽 기반 PRT 운영제어 시뮬레이터를 구현하였다.

On the development of the Anuloid, a disk-shaped VTOL aircraft for urban areas

  • Petrolo, Marco;Carrera, Erasmo;D'Ottavio, Michele;de Visser, Coen;Patek, Zdenek;Janda, Zdenek
    • Advances in aircraft and spacecraft science
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    • 제1권3호
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    • pp.353-378
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    • 2014
  • This paper deals with the early development of the Anuloid, an innovative disk-shaped VTOL aircraft. The Anuloid concept is based on the following three main features: the use of a ducted fan powered by a turboshaft for the lift production to take-off and fly; the Coanda effect that is developed through the circular internal duct and the bottom portion of the aircraft to provide further lift and control capabilities; the adoption of a system of ducted fixed and swiveling radial and circumferential vanes for the anti-torque mechanism and the flight control. The early studies have been focused on the CFD analysis of the Coanda effect and of the control vanes; the flyability analysis of the aircraft in terms of static performances and static and dynamic stability; the preliminary structural design of the aircraft. The results show that the Coanda effect is stable in most of the flight phases, vertical flight has satisfactory flyability qualities, whereas horizontal flight shows dynamic instability, requiring the development of an automatic control system.

Circular Hub타입 해상용 풍력발전기 개발에 관한 연구 (A Study on the Development of Circular Hub type offshore wind power generation)

  • 이병성;김남훈;오진석;김동현
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2010년도 춘계학술대회 초록집
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    • pp.183.2-183.2
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    • 2010
  • 본 개발에서의 해상용 풍력발전기는 크게 허브와 블레이드를 합한 상부 구조물, 전기 발전기와 연결 조인트의 중간구조물, 각종 제어 장치가 들어있는 제어박스로 나누어진다. 상부 구조물은 Circular Hub 타입의 Darrieus 형상으로 양력(lift)을 이용한 회전력이 발생하며, Circular Hub 타입은 기존의 허브와 블레이드를 연결하여주는 암(arm)에 의해 유발되는 항력토크를 최소화 하기 위한 신개념 형상설계가 이루어 졌으며, 저속에서 우수한 회전특성을 가진다. 이는 바람을 받아 기계적 에너지로 전환 하는 역할을 하며, 풍력발전기의 성능에 직접적인 영향을 미친다. 중간구조물의 전기발전기는, 상부에서 발생된 기계적 에너지를 이용하여 전기적 에너지로 전환 하는 역할을 수행한다. 이렇게 전환된 전기적 에너지는 하부의 제어박스를 거쳐서 해상용 부이(buoy)의 하단에 위치한 베터리 뱅크로 전달, 저장되어 부이에서 쓰이는 전력을 충당하게 된다. 한편 본 개발은 풍력발전기의 공력하중 해석과 로터블레이드의 설계, 풍력발전기의 구조, 진동해석, MPPT 제어컨트롤러와 Breaking controller, 풍동 및 차량시험을 통한 성능평가 및 분석 등의 순으로 개발을 수행하였다.

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Optimal Shape of Blunt Device for High Speed Vehicle

  • Rho, Joo-Hyun;Jeong, Seongmin;Kim, Kyuhong
    • International Journal of Aeronautical and Space Sciences
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    • 제17권3호
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    • pp.285-295
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    • 2016
  • A contact strip shape of a high speed train pantograph system was optimized with CFD to increase the aerodynamic performance and stability of contact force, and the results were validated by a wind tunnel test. For design of the optimal contact strip shape, a Kriging model and genetic algorithm were used to ensure the global search of the optimal point and reduce the computational cost. To enhance the performance and robustness of the contact strip for high speed pantograph, the drag coefficient and the fluctuation of the lift coefficient along the angle of attack were selected as design objectives. Aerodynamic forces were measured by a load cell and HWA (Hot Wire Anemometer) was used to measure the Strouhal number of wake flow. PIV (Particle Image Velocimetry) was adopted to visualize the flow fields. The optimized contact strip shape was shown a lower drag with smaller fluctuation of vertical lift force than the general shaped contact strip. And the acoustic noise source strength of the optimized contact strip was also reduced. Finally, the reduction amount of drag and noise was assessed when the optimized contact strip was applied to three dimensional pantograph system.

혐기성 소화조의 에너지 효율 향상을 위한 수직 왕복형 교반기 적용에 관한 연구 (A Study on the Effect of Energy Saving with Newly Implemented Vertical Circulating Tray Mixer in Anaerobic digester)

  • 주윤식;손건태;배영준;박정수;이승환
    • 상하수도학회지
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    • 제31권1호
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    • pp.13-19
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    • 2017
  • Relatively low efficiency in anaerobic digestion process is mainly caused by unproper mixing method. In this study, tray motion type agitator was applied in actual anaerobic digestion tank in order to improve the digestion efficiency, equalize the flow velocity distribution and energy saving. The impeller of tray motion type agitator was reciprocated vertically. Gas lift type agitator and tray motion type agitator appears almost same mixing efficiency include digestion rates. However, tray motion type agitator have shown that lower energy consumption compared to the conventional gas lift type agitator. Implementation of tray motion type agitator in the anaerobic digestion tanks contributed to the stabilization of mixing environment, efficiency and energy efficiency of the tank.

곤충의 호버링 비행을 구현하는 메카니즘의 설계 (Design of a Mechanism for Reproducing Hovering Flight of Insects)

  • 정세용;최용제
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2004년도 추계학술대회 논문집
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    • pp.826-831
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    • 2004
  • Recently, studies have been carried out to develop unmanned Micro Air Vehicles(MAVs) that can search and monitor inside buildings during urban warfare or rescue operations in hazardous environments. However, existing fixed-wing and rotary-wing MAVs cannot travel at extremely low or high speeds, hover in place, or change directions instantly. This has lead researches to search for other flight methods that could overcome those drawbacks. Insect flight principles and its applications to MAVs are being studied as an alternative flight method. To take flight, insects flap and rotate their wings. These wing motions allow for high maneuverability flight such as hovering, vertical take off and landing, and quick acceleration and deceleration. This paper proposes a method for designing a mechanism that reproduces hovering insect flight, the basis for all other forms of insect flight. The design of a mechanism that can reproduce the motion that causes maximum lift is proposed, the required specifications are calculated, and a method for reproducing hovering insect flight with a single motor is presented. Also, feasibility of the design was confirmed by simulation.

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