• 항공우주시스템공학회지
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• 제16권6호
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• pp.129-137
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• 2022

최근 항공기용 구동기는 전기식 구동기의 높은 정밀도 및 유지관리의 용이성 등으로 인해 기존 유압 중심의 기계시스템에서 전기구동 중심(More/All Electric)으로 기술이 변화하고 있다. 따라서 항공기의 전기 전동기 고장은 치명적인 결함을 넘어 인명피해로도 이어질 수 있다. 전기 전동기의 고장진단은 항공기의 안전성을 보장하는데 필수적인 요소이다. 이에 따라 효율적이고 적절한 고장진단이 요구되며 이러한 고장진단 기술 연구가 활발히 이루어지고 있다. 본 논문에서는 전기 전동기 중 영구자석 동기전동기의 고장 유형과 고장진단 기술 동향에 대해 소개하고 분석한다.

• 전기학회논문지P
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• 제56권2호
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• pp.90-98
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• 2007

More and All-Electric Aircraft (AEA) carry many loads with varied functions. In particular, there may be large pulsed loads with short duty ratio, which can affect the normal operation of other loads. In this paper, a bi-directional converter with inductive storage is used as a voltage bus conditioner (VBC) to mitigate voltage transients on the bus. In addition, the constant frequency hysteresis control technique for a VBC is presented. A simple and fast prediction of the hysteresis band-width is implemented by the phase-lock loop control, keeping constant switching frequency. This technique offers the excellent dynamic response in load or parameter variation. The control performance is illustrated by simulated results with the SABER package, The proposed hysteresis control results in the shortest and the smallest excursions.

• 한국추진공학회지
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• 제14권6호
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• pp.89-102
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• 2010

본 논문에서는 항공우주분야의 구동장치와 여러 산업분야에서 응용되고 있는 미래 지향적 구동기의 기술에 대한 사항과 발전방향에 대해 연구하였다. 특히, 항공기 비행조종면 구동장치의 경우 기존에는 기계식 링키지나 무게 대비 출력이 높은 유 공압 구동기가 많이 사용되었으나 최근에는 대부분의 항공기에서 사용 중인 Fly-By-Wire 시스템과 더 나아가 'More Electric', 'All Electric' 시스템으로의 변화가 이루어지고 있다. 전기식 유압구동기와 전기식 구동장치의 경우 효율이나 안전성 그리고 비용적인 측면에서 우수하기 때문에 근래에 지속적인 개발이 진행되고 있다. 또한, 최근에는 구동기의 무게와 정밀도 그리고 응답속도의 향상을 위해 신소재를 이용한 새로운 분야의 구동기들이 개발되고 있다. 따라서 본 연구를 통해서 차세대 항공우주분야 구동장치와 신개념 구동기들의 세부기술 및 발전방향을 제시하고자 한다.

• 한국항공운항학회지
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• 제26권4호
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• pp.116-121
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• 2018

According to the incresement of aging aircraft, Republic of Korea Air Force (RoKAF) conducted a teardown inspection of aircraft's EWIS (electrical wiring interconnection system) to determine the status of deterioration and the influence of failure occurrences due to it. The inspected aircraft were the retired fighter jets that had been used for more than 40 years. By analyzing defect type and the defect tendency, RoKAF can establish the necessary measures for the usage extension of their fleet and furthermore, the analysis results can be used as a basic data for the preparation of it's aircraft aging. EWIS inspection was done throughout careful visual inspection technique by removing all the ducts and pipes located in the fuselage and wings. For the aircraft wiring where no damage was found, the elongation tests were performed to determine the deterioration of wiring according to the location of the aircraft. The connectors, which is the main cause of intermittent failure, were completely disassembled and inspected for internal damage such as corrosion, abrasion, and traces of foreign objects. The detected defects were classified into 4 severity levels based on the type of damage, and the classified defects were weighted according to the criticality which may affects to it's system to establish the action plan.

• Journal of Welding and Joining
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• 제18권1호
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• pp.52-58
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• 2000

Spot welding, namely a kind of electric resisting welding has been used widely in field of automobile and aircraft industries because of easiness to apply. Specimens used in this study was a mild steel of 1.2mm thickness and the electrode was a Cu-Cr alloy of 6mm diameter. The surface sheared of specimens after testing of tensile shear was observed by SEM(scanning electron microscope) after ultrasonic cleaning for 10min., and microstructures and grain size of all specimens were measured with using of O.M.(Optical microscope). By the means of measurement and observations of tensile shear load, fatigue strength and share surface, the weldability of spot welding was evaluated. When tensile shearing testing, fracture starting point in all specimens was took place at the bond between HAZ(Heat affected zone) and nugget. With increasing in number of layers, fatigue strength was decreased. With increasing in electric current, grain size in the HAZ became more fine.

• 전기학회논문지P
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• 제60권1호
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• pp.13-18
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• 2011

More and all-electric aircraft (AEA) carry many loads with varied functions. In particular, there may be large pulsed loads with short duty ratios which can affect the normal operation of other loads. In this paper, a converter with spilt capacitors and an improved adaptive controller is used as the Voltage Bus Conditioner (VBC) with the reduced capacitive storage to mitigate the voltage transients on the bus. The proposed converter allows the smaller capacitive storage. Also, the proposed controller has the advantage of requiring only one sensor and performing both the functions of mitigating the voltage bus transients and maintaining the level of energy stored. Experimental results are presented which verify the control principles and demonstrate the practicality of the approach.