• 한국유체기계학회 논문집
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• 제4권1호
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• pp.7-13
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• 2001

In developing a multistage compressor, the stage matching is one of the critical design issues. The mismatching can be often observed even if each stage has been proven good and then used as part of a compression system. A good matching among the stages can be achieved by changing various design parameters (i.e., passage cross sectional areas, blades angles, stagger angles, curvature, solidity, etc.). Therefore, designers need to find out what parameters must be changed and how much. In this study, a method to search the design parameters for optimum stage matching has been used based on an 1-D mathematical model of a compressor, which uses the data obtained from the preliminary test to identify the design parameters. This methodology is applied with a two-stage axial compressor, which was originally designed for a helicopter gas turbine engine. After identifying design parameters using preliminary test data, an optimization process has been employed to achieve the best matching between the stages (i.e., maximum efficiency of the compressor at its operation modes within a given range of the rotor speed under given restrictions for required stall margins and mass flow). 3-D flow calculations have been performed to confirm the usefulness of the corrections based on the 1-D mathematical model. Calculational results agree well with the experimental data in view of the performance characteristics. Some promising results were produced through the methodology proposed in this paper in conjunction with flow calculations.

• 디지털융복합연구
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• 제9권3호
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• pp.59-67
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• 2011

세계 항공산업은 디지털 기술의 발전과 더불어 지속적으로 성장하고 있다. 김포지역의 항공전자 시스템을 기반으로 하는 디지털 항공산업 발전방안을 수요적 측면, 제도적 측면, 산업구조적 측면에서 연구 하였다. 항공산업의 성장동력화를 위한 추진전략을 제시하고 전략 달성을 위하여 항공수요의 지속적 창출, 핵심 부품소재 육성 및 경쟁우위 디지털 기술력 확보, 제도 운용의 활성화를 위한 인프라 구축, 행정지원제도의 개선, 민 산 군 학 관의 정책조정기능 강화를 추진과제로 제안하였다. 연구를 수행한 결과 행정적, 산업적인 분야에서 관련 제도 등을 보완하면 항공정비산업과 헬기산업을 중심으로 김포지역의 디지털항공산업 발전이 가능하다는 결론을 도출 하였다.

• 항공우주시스템공학회지
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• 제17권4호
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• pp.110-117
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• 2023

본 논문에서는 회전익 항공기 통신·항법 안테나의 최적 위치와 체계 성능측정 방법에 대해 연구하였다. 통신·항법 안테나의 항공기 최적 장착 위치 선정을 위해 기체 형상 및 특성을 고려한 후 항공기 장착 안테나에 대한 복사패턴, 커플링 분석, 장비 운용 프로파일 및 안테나 종류별 분석을 수행하고, 분석결과에 따라 항공기에 장착된 안테나에 대한 지상시험 및 비행시험을 통해 VSWR 측정, 안테나 패턴시험을 순차적으로 수행하는 절차를 정립하였다. 본 논문에서 제안한 체계적인 성능 측정 방법 및 절차는 LAH(소형무장헬기)체계의 지상 및 비행시험을 통해 입증하였다.

• 한국추진공학회지
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• 제12권4호
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• pp.42-47
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• 2008

스마트무인기의 출력제어계통은 터보프롭 항공기와 유사한 피치 가버닝 개념으로 조종사가 엔진출력을 직접 조절하고 제어기는 프로펠러의 회전속도를 일정하게 유지하는 방식을 사용한다. PW206C 엔진은 회전익 항공기에 맞게 개발된 전자식엔진제어기를 갖춘 터보축 엔진으로 스마트무인기에서 요구되는 엔진제어개념과는 맞지 않는다. 따라서 엔진 출력을 전기식 작동기를 엔진의 출력조절레버에 연결하여 조절하는 수동방식을 사용한다. 본 논문에서는 엔진성능계산프로그램을 사용하여 엔진출력축속도, 비행고도 및 비행속도변화에 대한 엔진성능을 계산하여 각 비행조건에서의 출력조절레버각의 작동범위를 예측한다.

• Journal of Trauma and Injury
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• 제32권3호
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• pp.168-171
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• 2019

The treatment outcome remains poor of severe facial injuries because of the high risk of compromised airway or massive bleeding. We experienced two successful treatment cases of severe facial injury by the chainsaw. A 52-year-male had his face injured by the chainsaw during his work. He was transferred to the Level I trauma center using the Doctor-Helicopter. During his flight, bleeding control was tried and the information was given to the trauma surgeons before his arrival. His consciousness was alert and the vital signs were stable. The crushing wound, mandible open fracture, deep laceration of tongue, lip, neck and arterial bleeding were noted around his mandible. Nasotracheal intubation was performed under the bronchoscope-guided. Emergency operation (open reduction & internal fixation, primary repair with neurorrhaphy) was performed. At 30 hospital days, he was discharged with facial palsy on left mandibular area. A 30-year-male had his face injured by the chainsaw. He was transferred to our Level I trauma center from the local hospital. The deep-mutiple lacerations on right upper eyelid and forehead with the bony exposure were noted. The vital signs were stable and emergency operation was performed. He was discharged at 20 hospital days. Bone loss or tissue loss were not devastating than we expected even though the injury was occurred by the chainsaw. Aggressive treatment including airway manipulation or bleeding control and maximal opportunity of therapy are absolutely needed.

• International Journal of Naval Architecture and Ocean Engineering
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• 제13권1호
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• pp.734-745
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• 2021

In order to achieve a good and competitive FPSO design, the building cost and the motion performances are the two most critical and conflicting KPIs to be considered. In this study, the author's previous work (Lee, et al., 2021) on the optimization of an FPSO's hull dimensions with 1800 MBBLs storage capacity at Brazil field was extended using a multi-objective parametric optimization with the hull steel weight and the operability which are closely related to the building cost and the operational cost during the lifetime, respectively. For the purpose of more realistic and practical FPSO design, the constraints related to crew comfort and the safe helicopter take-off and landing operation were newly added. Also, the green water on deck was calculated accurately to check the suitability of the designed freeboard height using a newly developed real-time calculation module for the relative wave elevations. With aids of this updated optimization formulation, we presented multiple optimal FPSO dimensions expressed as a Pareto set which aids FPSO designers to conveniently select the practical and competitive dimensions. The excellence of the developed approach was verified by comparing the optimization results with those of FPSOs dimensioned for operation at West Africa and Brazil field.

• International Journal of Internet, Broadcasting and Communication
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• 제14권1호
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• pp.201-208
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• 2022

As around the world, ground and underground transportation capacity is reaching its limit, centering on urban areas. As urban traffic becomes congested, time and cost are astronomical, and environmental destruction caused by urban pollution is becoming increasingly serious. As a way to solve this problem, the means of flying over the air are in the spotlight as the next generation of future transportation, and the concept of urban air mobility (UAM, Urban Air Mobility) is defined as systematic planning. The development of an electric-powered vertical take-off (eVTOL) aircraft that obtains electric power through a battery using a personal aerial vehicle (PAV) as a means of transportation has accelerated. As the aircraft development of new technology aircraft in the evtol method is actively carried out, the need to prepare systems such as aircraft certification standards, pilot qualification systems, and qualification management is emerging. The Federal Aviation Administration (FAA) and the European Union Aviation Safety Agency (EASA), which lead international standards, announced new special technical conditions and temporary regulations SCVTOL-01, respectively. However, the pilot qualification system for operating the uam aircraft has not yet been clearly announced. Therefore, this paper analyzes the recently announced FAA regulations and EASA regulations to identify differences and directions in perspectives on UAMs and study the existing vertical take-off and landing aircraft (VTOL) pilot qualification system to present directions for qualification classification.

• 한국산학기술학회논문지
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• 제18권9호
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• pp.92-100
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• 2017

회전익 항공기의 MRA 조종로드는 메인로터의 회전면을 조절하여 항공기의 속도, 고도 및 방향을 조절해 주는 중요한 기능을 수행한다. 그러나 A 항공기 운용 중에 조종로드에 수분이 유입됨으로서 동계 운용 간 조종로드 내부가 결빙으로 파손되고 제작공정 간 불균일한 코팅으로 인한 부식이 발생되어 개선이 요구되었다. MRA 조종로드 상부 공간을 통하여 로드 내부로 수분이 유입되었고, 유입된 수분이 외부 온도의 영향으로 결빙 발생 후 팽창하는 과정에서 로드가 파손되었으며, 조종로드의 제작공정 간에는 도금처리 미흡으로 조종로드 내부에 부식이 발생하였다. 이러한 결함을 해결하기 위하여, 로드 내부로 수분이 유입되지 않도록 조종로드 상단 부분을 실링 처리하였고, 부식이 발생되지 않도록 제작공정 진입 전 내경부 부식 확인, 공정 이동 간 불순물 제거 및 방청유 적용 공정 추가, 균일한 두께 분포를 위한 내경부 2회 코팅 등을 반영하였다. 이를 검증하기 위해 개선품에 대한 방수시험과 염수분무시험 등을 통하여 방수와 부식방지 여부를 확인하였다. 본 논문에서는 이처럼 항공기 운용과정에서 발생한 MRA 조종로드 결함에 대한 현상과 원인 및 대책을 검토하고 개선 방안을 수립하여 이를 입증하였다. 이와 같은 방수 및 부식 방지 기술은 국내 회전익 항공기 개발 산업에 크게 기여할 것으로 판단된다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2012년도 추계학술대회 논문집
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• pp.190-195
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• 2012

Small-scaled Rotor Test facility(GSRTS, General Small-scaled Rotor Test Facility) in KARI could not use the test because facility aging and parts discontinued. Also in order to perform a joint international research, GSRTS modifications should be needed. So requirements of GSRTS modifications were established and according to the requirements, GSRTS modifications were conducted. Facility operation test, 6-component fixed balance calibration, Small-scaled OLS rotor performance test were performed to verify the results of GSRTS modifications. Reasonable results were obtained in comparison to calculation results. Then GSRTS ready was completed to conduct international collaborative research and wind tunnel test.

• 대한조선학회논문집
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• 제59권5호
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• pp.252-261
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• 2022

The present study concerns assessing the operability of a surface combatant, based on the Percent-Time-Operable (PTO). For validation of the seakeeping analysis in the regular waves, the model test is first conducted in a towing tank. The seakeeping analysis results in the regular waves are expanded to the irregular waves, considering the wave spectra around the Korean peninsula and in North Pacific. The seakeeping criteria of the surface combatant in transit, combat, replenishment operation, and survival condition are defined by the literature review. An annual operation scenario of the surface combatant in two operation areas, i.e., advance speed and wave direction, are combined with the seakeeping analysis results to assess PTO. The main constraints of operability of the surface combatant are identified as the pitch angle and vertical velocity at the helicopter deck.