• EDISON SW 활용 경진대회 논문집
• /
• 제6회(2016년)
• /
• pp.23-26
• /
• 2016

Gurney Flap은 자동차의 스포일러 부분에 장착되는 고속주행용 Flap으로써 항공기에는 제한적으로 사용되고 있다. 매우 짧게 설치되는 특성이 있기 때문에 Flap의 길이를 항공기의 기준으로 10%로 증가시켜 Flap으로써의 역할을 확인해 보고자 실험을 진행하였다. Gurney Flap을 장착한 형상 3가지 모두 기본형의 NACA0012형상보다는 양력과 항력이 모두 증가하는 형상을 보였다. 양항비의 경우는 항력의 증가로 인해서 NACA0012에 비해서 모두 감소하는 것으로 나타났다. Gurney Flap은 고양력장치로 사용하기에는 다소 무리가 있지만, Dogfight와 같이 고항력장치를 사용하는 경우에는 좋은 성능을 기대할 수 있다.

• 한국산업융합학회 논문집
• /
• 제26권6_2호
• /
• pp.1083-1095
• /
• 2023

Recently, the demand for low-voltage, high-capacity ESS is rapidly increasing due to the revitalization of the e-mobility industry, which is mainly powered by electricity. In addition, the demand for portable power banks is rapidly increasing due to the revitalization of leisure industries such as camping and fishing. The ESS with this structure consists of a small number of series cells and many parallel cells, resulting in a system with a large rated current. Therefore, the number of power devices for cell balancing configured in series is small, but a balancing device with a large current capacity is required. Construction of a constant temperature device in such a low-voltage, high-current ESS is difficult due to economic issues. The demand for an active balancing system that can solve the passive balancing heating problem is rapidly increasing. In this paper, propose a power feedback fly-back topology that can solve the balancing heating problem. The characteristic of the proposed topology is that a series-connected voltage sharing voltage is used as the input of the flyback converter, and the converter output is connected to one transformer. In this structure, the converter output for cell voltage balancing shares magnetic flux through one high-frequency transformer, so the cell voltage connected to the converter automatically converges to the same voltage.

• 전력전자학회:학술대회논문집
• /
• 전력전자학회 2018년도 전력전자학술대회
• /
• pp.480-481
• /
• 2018

본 논문에서는 대용량 에너지저장 시스템을 효율적으로 구성 및 운용하기 위해 배터리 군을 여러 군으로 분리하고, 각 군을 Half-bridge 전력변환기와 결합한 새로운 토폴로지를 제안한다. 또한 제안된 스위칭방식에 의해 넓은 입력 범위에서 충 방전할 수 있으며, 배터리의 SOC 추정이 용이하게 할 수 있어 직렬로 연결된 배터리 군의 SOC 밸런싱 제어가 가능하게 하였다. 또한 시뮬레이션을 통하여 제안된 방식의 타당성을 검증 하였다.

• 항공우주기술
• /
• 제9권1호
• /
• pp.78-83
• /
• 2010

본 연구에서는 높은 양력을 얻기 위하여 플랩 형상 최적 설계를 시도하였다. 플랩 형태는 플랩 중에서 가장 효율이 좋은 파울러 플랩(fowler flap)이다. 플랩 설계는 최적화 기법을 활용하여 진행하였고 최적화의 초기 형상은 general aviation airfoil과 Wentz 등이 개발한 플랩이다. 최적화 방법으로는 반응면 기법 (Response Surface Method)이 사용되었으며, Hicks-Henne 형상함수가 사용되었고, GA(W)-1 익형과 fowler flap이 조합된 형상의 유동장에 대하여 Navier-Stokes 해석을 수행하였다. 상용 최적화 프로그램인 Visual-Doc, 격자 생성 프로그램인 Gambit/Tgrid, 그리고 유동해석에는 Fluent를 이용하였다. 플랩의 윗면 형상과 gap에 대한 최적화를 수행하여 착륙조건에서의 양력이 증가하였다. 초기 형상과 최적화된 형상의 공력특성 변화를 관찰하기 위하여 항우연의 1m 풍동에서 시험을 수행하였다. 최적화된 형상은 대체로 예측치와 비슷한 경향을 보이나, 이른 실속이 관찰되었다. 또한, 날개와 플랩 간의 간격을 설계치보다 좁혀 줌으로써 양력특성이 향상됨을 알 수 있었는데, 이는 설계시 사용된 난류 모델의 영향이라 판단된다.

• 대한조선학회논문집
• /
• 제36권1호
• /
• pp.22-29
• /
• 1999

선박의 고속화에 따라서 선체를 부양시키거나 자세를 제어하기 위하여 높은 양력을 발생시키는 장치의 필요성이 증대하게 되었다. 뿐만 아니라 해양오염방지를 위하여 IMO 등의 국제기구에서는 대형 신조선에 대하여 충분한 조종성능을 확보할 것을 권장하고 있어서 높은 양력을 발생시키는 타의 필요성이 증대하게 되었다. 높은 양력을 얻는 문제는 항공분야에서 오래 전부터 핵심적인 문제로 다루어져 왔으며 그중 대표적인 것이 Coanda장치이다. 방형비척계수가 크고 길이-폭비가 작은 저속비대선에서는 통상적인 타를 부착한 경우에 높은 양력을 얻기 어려우므로 플랩이 부탁된 타를 선정하고 이에 Coanda장치를 도입하였을 때 성능이 향상되는 것을 선형시험수조에서 실험적으로 확인하고자 하였다.

• 한국산업융합학회 논문집
• /
• 제23권5호
• /
• pp.853-863
• /
• 2020

As the battery ages, the internal resistance of the battery increases, so the loss due to the internal resistance increases at the same charging current, causing the battery temperature to rise, which further accelerates battery aging. Therefore, it is necessary to optimize the charging conditions according to the aging of the battery or the current charge amount, and to accurately estimate this, estimation of the parameters of the equivalent circuit is most important. This paper proposes a new measurement technique that can measure the internal resistance of a battery by analyzing a specific high frequency voltage and current applied to the battery. In addition, in order to test the validity of the proposed measurement technique, the current charging amount was estimated based on the measured internal resistance, and the terminal voltage of the constant current charging mode was automatically set and operated. As a result, good results were obtained regardless of the battery voltage. If this equipment is installed in the charging device, it is believed that it will be of great help in the stability management of the aging reusable battery.

• 항공우주시스템공학회지
• /
• 제10권4호
• /
• pp.11-16
• /
• 2016

본 논문에서 채널 안내로를 비행하는 가변스팬 날개의 공력특성에 관한 실험연구를 수행하였다. NACA 0012익형을 가진 가변스팬 날개를 제작하였으며 선형서보모터를 사용하여 작동시켰다. 날개의 가로세로비, 지면효과, 날개와 펜스사이의 거리가 날개의 공력특성에 미치는 영향을 조사하였다. 연구결과 지면 및 펜스 모두 항공기 날개의 양력을 증가시켰으며 지면효과와 달리 펜스는 날개의 항력에 큰 영향을 미치지 않았다. 가변스팬 메커니즘이 플랩사용이 제한되는 상황에서 효과적인 고양력 장치로 사용가능할 것으로 판단된다.

• 한국전기전자재료학회논문지
• /
• 제34권1호
• /
• pp.21-26
• /
• 2021

Single-layer graphene is grown directly on Ti-buffered SiO2 at 100℃. As a result of the AFM measurement of the Ti buffer layer, the roughness of approximately 0.2 nm has been improved. Moreover, the Raman measurement of graphene grown on it shows that the D/G intensity ratio is extremely small, approximately 0.01, and there are no defects. In addition, the 2D/G intensity ratio had a value of approximately 2.1 for single-layer graphene. The sheet resistance is also 89 Ω/□, demonstrating excellent characteristics. The problem was solved by using graphene and a lift-off patterning method. Low-temperature direct-grown graphene does not deteriorate after the patterning process and can be used for device and micro-patterning research.

• 한국진공학회:학술대회논문집
• /
• 한국진공학회 2014년도 제46회 동계 정기학술대회 초록집
• /
• pp.489.2-489.2
• /
• 2014

The planar type flexible piezoelectric energy harvesters (PEH) based on PbZr0.52Ti0.48O3 (PZT) thin films on the flexible substrates are demonstrated to convert mechanical energy to electrical energy. The planar type energy harvesters have been realized, which have an electrode pair on the PZT thin films. The PZT thin films were deposited on double side polished sapphire substrates using conventional RF-magnetron sputtering. The PZT thin films on the sapphire substrates were transferred by PDMS stamp with laser lift-off (LLO) process. KrF excimer laser (wavelength: 248nm) were used for the LLO process. The PDMS stamp was attached to the top of the PZT thin films and the excimer laser induced onto back side of the sapphire substrate to detach the thin films. The detached thin films on the PDMS stamp transferred to adhesive layer coated on the flexible polyimide substrate. Structural properties of the PZT thin films were characterized using X-ray diffraction (XRD) and scanning electron microscopy (SEM). To measure piezoelectric power generation characteristics, Au/Cr inter digital electrode (IDE) was formed on the PZT thin films using the e-beam evaporation. The ferroelectric and piezoelectric properties were measured by a ferroelectric test system (Precision Premier-II) and piezoelectric force microscopy (PFM), respectively. The output signals of the flexible PEHs were evaluated by electrometer (6517A, Keithley). In the result, the transferred PZT thin films showed the ferroelectric and piezoelectric characteristics without electrical degradation and the fabricated flexible PEHs generated an AC-type output power electrical energy during periodically bending and releasing motion. We expect that the flexible PEHs based on laser transferred PZT thin film is able to be applied on self-powered electronic devices in wireless sensor networks technologies. Also, it has a lot of potential for high performance flexible piezoelectric energy harvester.

• Journal of Biosystems Engineering
• /
• 제39권3호
• /
• pp.158-165
• /
• 2014

Purpose: The objective of this paper was to compare test standards regarding the performance and safety of agricultural tractors to identify the differences in test conditions, measurement tolerances, and test procedures. Based on the comparison, some recommendations were proposed for possible revisions or improvements to current tractor test standards. Methods: The test standards and codes of major standards development organizations (SDOs), such as the Organization for Economic Cooperation and Development (OECD), the International Organization for Standardization (ISO), the American Society of Agricultural and Biological Engineers (ASABE), EC type approval, and the board of actions of the Nebraska Tractor Test Laboratories (NTTL), were selected and analyzed. Comparison of the test standards: The ISO provides references for fuel and lubricants for tractor tests, and the OECD provides additional measurements for calculating fuel consumption characteristics during the power take-off (PTO) tests. The ISO, EC type approval, and the ASABE provide PTO protective device and the safety requirements. During drawbar power tests, seven transmission ratios are selected for fully automatic transmissions, according to the OECD. In case of hydraulic lift tests, ISO 789-2 and OECD Code 2 advise the use of a static lift force, while SAE J283 advises the use of additional dynamic lift capacity tests for a better representation of in-field operations. The OECD, the ISO, and EC type approval determine the seat index point (SIP), whereas the ASABE determines the seat reference point (SRP) for roll-over protective structure (ROPS) tests. Diversified measurement tolerances were among the braking performance test standards. The European Union (EU) has developed daily limits for vibration exposures with adaptations from ISO 2631-1. Electromagnetic compatibility evaluations are emerging of high-efficiency tractors due to the long-term conformance to electromagnetic emissions and interferences. Comparisons of tractor test standards discussed in this paper are expected to provide useful information for tractor manufacturers and standards development personnel to improve the performance and safety test standards of tractors.