• Title/Summary/Keyword: 활주로

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고속활주형어선의 종방향중심이 저항에 미치는 영향에 관한 연구

  • 이귀주;이조원
    • Proceedings of the Korean Society of Fisheries Technology Conference
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    • 2001.05a
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    • pp.79-80
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    • 2001
  • 본 연구는 고속 활주형선의 어선 적용을 위해 경제성 및 운항ㆍ조업성능 등을 고려하여 .자료조사를 수행하고 기본 치수를 선정하였으며, 본 연구의 목적은 선정된 우수선형의 실선적용을 위해 실해역에서 발생할 수 있는 여러 조건들을 가정하여 발생 가능한 문제들을 예측하고 이를 방지 또는 개선하는 데 있다. (중략)

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Estimation of Annual Runway Capacity for Jeju International Airport Considering Aircraft Delays (항공기 지연시간을 고려한 제주국제공항 활주로 연간용량 산정)

  • Park, Jisuk;Yun, Seokjae;Lee, Youngjong;Baik, Hojong
    • Journal of Korean Society of Transportation
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    • v.33 no.2
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    • pp.214-222
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    • 2015
  • Jeju International Airport has become the most delayed airport in Korea, due to increased demand in air passengers and unexpected local weather condition. Observing the demands continuously grow for a decade, the airport is expected to be saturated in the near future. As a part of effort to prepare effective and timely measure for this expected situation, airport planners seeks the annual runway capacity, i.e., the appropriate number of flight operations in a given year with tolerable delay. In practice, the FAA formula is frequently adopted for the capacity estimation. The method, however, has intrinsic issues: 1) the hourly capacity imbedded in the formula is not clearly defined and thus the estimated value is vulnerable to be subjective judgement, and 2) the formula doesn't consider aircraft delay resulted from runway congestion. In this paper, we explain a novel method for estimating the daily runway capacity and then converting to the annual capacity taking into account the aircraft delay. In this paper, average delay of aircraft was measured using microscopic air traffic simulation model. Daily capacity of the runways were analyzed based on the simulation outputs and the method to assess the yearly capacity is introduced. Using a microscopic simulation model named TAAM, we measure the average aircraft delay at various levels of flight demand, and then estimate the practical daily runway capacity. The estimated daily and annual runway capacities of Jeju airport are about 460 operations a day which is equal to 169,000 operations year. The paper discusses how to verify the simulation model, and also suggests potential enhancement of the method.

A Case Study on the Application of Echelon Paving Method Using a 12m-Wide Screed Finisher on Flexible Airfield Pavements (광폭 Echelon 공법의 연성 활주로 포장 적용에 관한 사례 연구)

  • Jeon, Kook-Il;Choi, Heung-Sup;Bin, Cheol-Ho
    • 한국방재학회:학술대회논문집
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    • 2007.02a
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    • pp.353-356
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    • 2007
  • Asphalt pavements of the airport in service were monitored to construct new runway and taxiway and longitudinal cracks were found on the pavements. The sources of the longitudinal cracks were the low density which was caused by the longitudinal cold joint with asphalt Pavement constructions and the excessive loads of aircraft. Therefore, the echelon paving method using a 12m-wide screed finisher was used to eliminate longitudinal cracks. When the echelon paving is used, construction of the longitudinal joint is changed so that the compaction of the unconfined edge of the first lane is delayed until the second lane is placed. In conclusion, the use of this construction method results in the density of the longitudinal joint being equal to that of the adjacent mat.

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New range measurement method between aircraft and runway (항공기와 활주로 사이의 새로운 거리측정방법)

  • Lee, Hyeon-Cheol
    • Current Industrial and Technological Trends in Aerospace
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    • v.7 no.2
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    • pp.115-120
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    • 2009
  • Description in this paper is a system for new range measurement method between an aircraft and runway with circular mark in landing runway. The system includes an altimeter and a camera installed on the aircraft, and a circular mark placed on a landing runway. The camera installed on the aircraft must be oriented toward in front of the aircraft, and configured to detect the shape of the circular mark in image information form and a flight control computer configured to calculate the angle between the aircraft and the ground, the ground range between the aircraft and the circular mark, and the slant range between the aircraft and the circular mark with the altitude information measured by the altimeter. This system configured to control the automatic landing of the aircraft with this information.

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Comparisons of Resistance Characteristics of the High-speed Planing Craft with Respect to the Number of Bottom Steps (선저 스텝개수에 따른 고속 활주형선의 저항특성 비교)

  • Park, Chung-Hwan
    • Journal of Navigation and Port Research
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    • v.32 no.8
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    • pp.583-588
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    • 2008
  • The planing craft is designed specifically to achieve comparatively high speed on the surface of the water. In general, the stepped hull craft has effect improvement in speed and fuel-efficiency because of the reduction of total resistance by a small wetted surface area without corresponding stepped hull craft. In this paper, the high speed stepped hull crafts with respect to the number of bottom steps were performed to compare the effect of resistance performance using at-sea model-test method. In conclusion, the stepped hull craft with twin-step was proved to be effective to reduce the total resistance.

Study on the Transvers Step Application Location of High Speed Planning Hull by Numerical Analysis (수치해석을 통한 고속활주선의 횡방향 Step적용 위치에 관한 연구)

  • Kim, Byung-Jae;Kim, Sang-Won;Park, Geun-Hong;Lee, Gyoung-Woo;Cho, Dae-Hwan;Seo, Kwang-Cheol
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2017.11a
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    • pp.234-235
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    • 2017
  • In order to improve the frictional resistance of existing high-speed planning hull, a step-like linear transformation has been researched which forms an air layer on the bottom. However, there is a lack of research on the proper position to confirm the effect of Running Attitude and step on each position. In this study, we confirmed the change of the Running Attitude, the effect of the step and the change of the frictional resistance when the step was applied in the longitudinal location.

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A Study on Improvement in the Resistance Performance of Planing hulls by Hull Shape Optimization (고속활주선의 선형 최적화를 통한 저항성능 개선에 관한 연구)

  • Kim, Sunbum
    • Journal of the Korea Society for Simulation
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    • v.27 no.2
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    • pp.83-90
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    • 2018
  • This paper describes the method of hull shape optimization to improve the resistance performance of planing hulls when a reference hull shape and its principal dimensions are given. First, the planing hull of precedent research is adopted as the reference hull and an optimization problem is formulated by defining hull shape parameters. The search space of this research is discretized for computing cost and DPSO(Discrete binary version of Particle Swarm Optimization) method is used to solve the optimization problem. As the result of optimization, the decrease of resistance is confirmed from the comparison between the reference hull's and the modified hull's planing performance from computational results.

A Study on Evaluating the Applicability of Trapezoidal-shaped Grooves to Airport Runways (사다리꼴 형상 그루빙의 공항 활주로 적용성 평가 연구)

  • Cho, Nam-Hyun;Kim, Dong-Chul;Phi, Seung-Woo;Shin, Joong-Ha
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.29 no.4
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    • pp.78-87
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    • 2021
  • This study is to evaluate the applicability and performance of trapezoidal-shaped grooves on domestic airport runways. For this, the constructability, drainage performance, and friction resistance characteristics of trapezoidal-shaped grooves compared to square-shaped grooves were evaluated through test construction on pavement at Incheon Airport. As a result of the test construction, the trapezoidal-shaped grooves satisfies the required geometry standards and tolerance, and secured a macrotexture that was 25% improved compared to the square-shaped grooves. It was confirmed that trapezoid-shaped grooves secured drainage performance of more than 7-9%, and surface friction performance improved compared to existing grooves when the surface of the pavement was wet as the test speed increased in the dry state. In addition, after trapezoidal-shaped grooves was installed on the RWY 16R/34L of Incheon Airport, the friction coefficient was 0.84, which satisfies the design level of the new runway surface of 0.82 at the test speed.