• Structural Monitoring and Maintenance
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• 제1권3호
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• pp.293-308
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• 2014

In the aeronautical environment, numerous regulatory and communication protocols exist that cover interconnection of on-board equipment inside the aircraft. Developed and implemented by the airlines since the 1960s, these communication systems are reliable, strong, certified and able to contact different sensors distributed throughout the aircraft. However, the scenario is slightly different in the structural health monitoring (SHM) field as the requirements and specifications that a global SHM communication system must fulfill are distinct. The number of SHM sensors installed in the aircraft rises into the thousands, and it is impossible to maintain all of the SHM sensors in operation simultaneously because the overall power consumption would be of thousands of Watts. This design of a new communication system must consider aspects as management of the electrical power supply, topology of the network for thousands of nodes, sampling frequency for SHM analysis, data rates, selected real-time considerations, and total cable weight. The goal of the research presented in this paper is to describe and present a possible integration scheme for the large number of SHM sensors installed on-board an aircraft with low power consumption. This paper presents a new communications system for SHM sensors known as the Bi-Instruction Link Bi-Operator (BILBO).

• 대한산업공학회지
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• 제37권4호
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• pp.390-399
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• 2011

Generally the life-cycle cost of complex systems composed of several sub systems or equipments such as train, aircraft weapon systems is spent much more during operation and maintenance phase than development phase. The maintenance cost for maintaining the availability and extending the life span of systems comprise a large proportion of systems operation cost. The cycle of preventive maintenance affects operation and maintenance cost a lot. In this study we introduce a way minimizing life-cycle cost of systems by calculating more reliable preventive maintenance period than the results of previous study using systems reliability data considered the reliability and failure effect ratio of sub-systems or components. We can solve the preventive maintenance period problem known as NP-Hard as quick as possible by using modified genetic algorithm than using other models introduced in previous study.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2008년도 추계학술대회 논문집
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• pp.1487-1493
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• 2008

Railway vehicle is very important to implement the effective maintenance in proper to prevent any failure during operation period. Many railway authorities are making efforts to maintain the railway vehicle through scientific and systematic procedure. To achieve this, Reliability Centered Maintenance(RCM) is partially applied. The efficiency of RCM has proven and its terminology was familiar with nuclear power, military and chemical plant etc. since the commercial aircraft's industries has introduced the maintenance program based on the target of reliability. The application of RCM on railway vehicle can be utilized with systematic analysis method to select the best effective maintenance period and action to prevent the failures by selecting the equipment affecting the its safety and reliability. This paper is presented that the procedure of adequate and effective maintenance for railway vehicle by comparing among the related standards in example IEC60300-3,11, MIL-STD-2173, and technical documents or papers. In accordance with above result, RCM procedure is proposed to apply effectively for maintenance of railway vehicle. That is, (1) Analysis of data and Calculation of criticality per equipment (2) Selection of equipment to analyze (3) Analysis of failure mode and effect (4) Evaluation of maintenance method and period (5) Optimization of maintenance program through renewal of maintenance method and period.

• Journal of Positioning, Navigation, and Timing
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• 제9권2호
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• pp.125-129
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• 2020

In this paper, Zero velocity UPdaTe (ZUPT) is implemented on the navigation system of Remotely Piloted Aircraft for GNSS denied environment. RPA's navigation system suffers from lack or loss of satellite signal while maintenance or ground test inside a hangar. Although some of the hangars install GPS repeaters for indoor tests, the anti-jamming equipment with array antenna blocks the repeater signal regarding them as hostile jamming signal. With ZUPT, an aircraft navigation system can be tested free from the divergence of navigation solution without line-of-sight satellites. The designed ZUPT aided centralized Kalman Filter is implemented on the Embedded GPS&INS and simulated with Captive Flight Test data. The simulation result shows stable navigation solution without GNSS updates.

• 한국군사과학기술학회지
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• 제2권2호
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• pp.83-91
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• 1999

Dynamic characteristic of manufacturing stage is understood and the utilization of each machine is maximized by developing on-line dynamic CAPP system to consider the overloads in the aircraft part manufacturing line. In this paper, a scheme of production planning and scheduling system was proposed through inspection about some predeveloped CAPP system. Developed production planning and scheduling system included process planning module. After precise inspection of some FMS line schema at domestic heavy industry, optimized FMS line was applied to aircraft part manufacturing and repairing factory. By virtue of considering overloads of factory and machine through on-line dynamic CAPP system, the utilization of resources is maximized and manufacturing lead time is minimized.

• 한국국방경영분석학회지
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• 제16권1호
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• pp.113-129
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• 1990

This paper presents the simulation model to decide the mean size of cannibalization aircraft (MSCA) under steady state when an airbase makes use of cannibalization to support the spare parts of an airfleet. In this model, the essential factors such as mission requirements, mission time, failure time, repair time, repair capability, inventory policy, cannivalization rule are considered. The model is constructed with above factors and actual airbase operating rules for a basis. Because of the tangled interdependencies among the each factors, it is inevitable to construct the model by the simulation technique. The mission and support system of the airbase is considered as a closed queueing network with a finite number of unit The troubled aircrafts are repaired in accordance with the priorities that are determined by their repair times. The illustrative example of the model, using the actual data of xx-airbase, is presented. The model would be a useful tool not only to determine the MSCA and the size of scheduled maintenance aircraft but to evaluate the NORS (not operationally ready supply) rate and the availability of an airfleet.

• 항공우주시스템공학회지
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• 제13권5호
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• pp.65-71
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• 2019

본 논문에서는 성능개량사업의 일환으로 설계 정보가 제공되지 않은 노후 항공기의 블레이드 형상 신규 안테나를 항공기 외부 주요 부위에 장착 시, 이에 대한 피로 수명을 입증하는 방법을 검토하고 정리하였다. 각 항공기 제조사 및 설계 조건에 따라 피로 수명을 입증하는 여러가지 방법들이 존재하며, 본 연구에서는 관련 규정과 항공기 산업체들의 예를 통하여 안테나가 장착된 항공기 동체의 해당 부위에 피로 수명 예측과 손상 허용 범위를 계산하였다. 이 계산 결과를 통해서 노후 항공기 주요 부위에 신규로 장착된 안테나 주변 구조물에 대한 피로 수명을 평가하고 손상 허용에 따른 정비 주기 및 관련 기준들을 설정하였다.

• 한국융합학회논문지
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• 제9권10호
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• pp.277-283
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• 2018

본 논문은 항공전자 부분품의 기능시험을 위해 사용하는 전용 자동시험체계(ATS)를 범용 자동시험체계로 TPS를 이식하는 연구이다. 항공전자 부분품의 성능시험을 위해 사용하는 전용 자동시험체계는 적게는 수천만원에서 많게는 수백억원에 이르는 고단가로, 항공전자 정비 사업을 영위하는 국내 기업에서는 초기 투자비용에 많은 어려움이 있어 사업 확장의 장애 요인이 되고 있다. 이러한 이유로, 본 논문에서는 전용 자동시험체계를 사용하는 정비대상품인 A항공기에 사용되는 발전기 내의 Wire-Harness를 범용 자동시험체계로 사용하도록 TPS를 이식하는 절차에 대해 연구하였다. 제안한 연구를 통해 전용에서 범용으로 TPS 이식 후 평가 및 검증을 수행한 결과 100% 성능검증을 확인하였으며, 이것은 절차의 표준화를 거쳐 무한한 확장 가능성이 있어 적은 투자로 항공전자 MRO사업의 확장을 원하는 국내 기업들에 큰 도움을 줄 수 있을 것이다.

• 한국추진공학회지
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• 제22권4호
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• pp.117-124
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• 2018

미국과 유럽은 대형 항공기 산업을 선도하고 있으며, 아시아-태평양 지역에서는 물동량이 증가하면서 운송산업과 정비산업이 크게 발전할 것으로 전망된다. 또한, 일본과 중국은 중소형 항공기 분야에서 설계 제작국에 진입하였으며, 후발국가의 정비산업도 경쟁이 더욱 가속되고 있다. 향후 10년간 세계의 항공기 정비산업은 연평균 3.4%로 성장하고, 엔진 정비산업은 7%씩 성장할 것으로 전망된다. 본 논문을 통하여 고부가가치를 창출할 수 있는 기술집약형 항공엔진 정비산업 육성 방안을 제시하고자 한다.

• 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.