• 제목/요약/키워드: aircraft industry

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경비행장 개발 및 입지선정에 관한 연구 (A Study on Development and Site selection of an AIRFIELD)

  • 박상용
    • 항공우주정책ㆍ법학회지
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    • 제30권2호
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    • pp.3-36
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    • 2015
  • 2014년말 기준 항공레포츠 동호인은 약 13만명, 경항공기 356대, 경량항공기 200대, 초경량비행장치 636대에 이르고 있으며, 항공레포츠 산업은 향후 생활수준 향상에 따라 급격히 발전할 유망 레저산업으로 부상하고 있다. 또한 초경량비행장치, 특히 무인비행장치를 활용한 사용사업도 지속적으로 증가하는 추세에 있으며, 향후 이들 장치를 활용한 관광, 레저 사업자 서비스에 대한 수요도 증가할 것으로 전망된다. 본 논문은 경항공기, 경량항공기 및 초경량비행장치 관련 지속적인 수요 증가에 대비하여 경항공기, 경량항공기 및 초경량비행장치 산업 활성화를 위한 "경(소형)비행장 개발의 표준화"를 통한 개발 방안에 대한 연구를 목적으로 하였다. 정부에서 제시하고 있는 항공레저산업의 활성화를 위해서는 전국에 경비행장을 많이 건설하여 운영할 수 있는 인프라를 제공해야 하지만, 각 지자체와 기관들은 앞 다투어 경항공기 비행장 건설에 나서고 있으나, 현실적으로 개발이 된 곳은 많지 않다. 정부차원에서도 경비행장 입지를 위한 연구를 진행한 바 있으나, 후보지만 검토하였고, 실제 건설에 대한 타당성을 수행하고 있지 못하다. 만일 실제로 건설이 된다면, 이러한 비행장의 입지가 과연 적합한지에 대해서는 타당성 검토를 통해 다시 한 번 검증 받게 될 것이다. 그리고 기존 연구보고서들과 관련 문서를 통해 입지선정 요소를 도출해내고, 전문가의 설문을 통해 경비행장의 입지선정 요소들을 분석해 내고자 하였다. 연구모형은 AHP분석을 위해 계층화 형태로 정하였는데, 선행연구 검토를 토대로 가중치를 정하여, 경비행장 입지선정요소에 대하여 2단계 구성을 기술/운영적 요소, 경제/정책적요소로 선정하였다. 그리고 3단계로 기술적 요소, 운영적 요소로 구성하였다. 마지막 단계로는 총 11개 (기상조건, 장애물 제한표면 조건, 공역조건, 운항절차, 소음문제, 환경문제, 시설의 이용성, 건설 및 투자비용, 지역경제 기여도, 접근성, 산업연계성)의 하위요소들을 선정하여 구성하였다. 경항공기 비행장 입지선정 요소 가중치 설문은 본 분야의 전문가 집단인 항공 운항, 관제 등의 교수 및 기장, 교관, 관제사, 정비사 등 전문가 70명을 대상으로 실시하였다. 일관성 지수는 CI=0.02로 일관성이 있는 것으로 나타났다.

중심성 분석을 이용한 2018년 판보로 국제 에어쇼 참가업체 기술동향 분석 (Analysis Results in Technical Trends of 2018 Farnborough International Airshow via Centrality Analysis)

  • 황재교;박재우;고용신;이창범;황재식
    • 한국산학기술학회논문지
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    • 제20권8호
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    • pp.164-173
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    • 2019
  • 본 연구에서는 전 세계 3대 에어쇼 중의 하나인 "FIA(Farnborough International Airshow, 판보로 국제 에어쇼)"의 참여기관/업체를 대상으로 네트워크 분석을 활용하여 항공우주분야 기술동향을 분석하였다. 판보로 국제 에어쇼는 전 세계 주요 항공관련 민간 및 방산 업체와 각국 정부 및 군 관계자가 참여하여 항공우주산업분야에 대한 최신 기술을 선보이는 중요한 행사로서, 2018 FIA에서는 총 112개 국가에서 1,500여 업체(기관)가 참여하였다. 본 연구에서는, 항공우주분야 기술관련 45개 국가, 1,108개 업체를 대상으로 223개의 기술 분류 카테고리를 통해 네트워크 분석 중 하나인 키워드 기반의 중심성 분석을 수행하였다. 분석결과, 전 세계적 우주항공 분야의 핵심기술은 "Machining"으로 조사되었다. 하지만 지역(국가) 별로 분류되는 핵심기술은 다소 다른 경향을 보여주고 있었는데, 유럽(EU)과 영국의 경우 "Machining", 아시아의 경우 "Aircraft Components", 미국의 경우 "Engine Components/controls"가 식별되었다. 우리나라의 경우에는 관련 기관/업체 수의 부족으로 뚜렷한 중심 기술이 식별되지 않았다. 본 연구의 결과가 우주항공분야 기술기획 및 연구 방향성 제시를 위한 참고자료로서 활용 될 수 있으며, 또한 국내 관련 업체의 수출 진흥을 위한 국외 주요 기술 분야를 제시하는데 유용하게 활용되리라 기대한다.

Effect of Joint Reformation on Adhesive Strength of 6061 Aluminum Alloy to Polycarbonate Lap Structures

  • D. W. Seo;Kim, H. J.;J. K. Lim
    • International Journal of Korean Welding Society
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    • 제4권1호
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    • pp.53-60
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    • 2004
  • Adhesive-bonded joints are widely used in the industry. Recently, applications of adhesive bonding joints have been increased extensively in automobile and aircraft industry. The strength of adhesive joints is influenced by the surface roughness, adhesive shape, stress distribution, and etc. However, the magnitude of the influence has not yet been clarified because of the complexity of the phenomena. In this study, as the fundamental research of adhesive bonding joints, the effects of adhesive shape and loading speed on bonding strength properties and durability of aluminum to polycarbonate single-lap joints were studied. To evaluate the effect of adhesive shape, several modified shapes were used, and loading speeds were varied from 0.05 to 5mm/min. As a result, the load distribution showed a brittle fracture tendency. The trigonal edged single lap and bevelled lap joints showed the higher strength than the plain single lap, trigonal single lap, joggle lap and double lap joints in same adhesive area. The fractures of trigonal single lap and trigonal edged single lap joints that had the higher strength level were shown as the mixture type of the cohesive and interfacial-failure, mostly joggle lap joints that had the lower strength level were shown as the adhesive-failure.

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도로건설 현장에서의 드론 운용방안 (Drone Operation Plan at Road Construction Site)

  • 성상민;윤부열;송미화;조준상
    • 한국산업융합학회 논문집
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    • 제23권5호
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    • pp.709-716
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    • 2020
  • Recently, the drone's equipment development and software technology have dramatically improved. With such developments, the applicability is increasing in various fields that require rapid geospatial information, and in practice, regulations and systems have been established, and the fields in use are increasing. Also, in Korea, corporations and public institutions are actually using and researching drones in fields such as aircraft development, communication technology development, construction site use, and surveying. However, there are no fields where drones are actually used in road construction sites. Therefore, in this study, to utilize drones that have been actively used in the civil engineering and construction fields for road construction, we investigated the current status of the Korea Highway Corporation's field drone use research and classified the possibility of drone introduction by road construction. Finally, a method of using drones at road construction sites was proposed to prepare a method for using drones at road construction sites.

에폭시 접착제 접합구조물의 강도향상을 위한 접착부 형상설계 (Shape Design of Adhesive Joints for Strength Improvement of Epoxy Adhesive Structures)

  • 서도원;김효진;임재규
    • 대한기계학회논문집A
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    • 제28권6호
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    • pp.783-790
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    • 2004
  • Adhesive-bonded joints are widely used in the industry. Recently, applications of adhesive bonding joints have been increased extensively in automobile and aircraft industry. The strength of adhesive joints is influenced by the surface roughness, adhesive shape, stress distribution, and etc. However, the magnitude of the influence has not yet been clarified because of the complexity of the phenomena. In this study, as the fundamental research of adhesive bonding joints, the effects of adhesive shape and loading speed on bonding strength properties and durability of aluminum to polycarbonate single-lap joints were studied. To evaluate the effect of adhesive shape, several modified shapes were used, and loading speeds were varied from 0.05 to 5 mm/min. As a result, the load-displacement distribution was shown a brittle fracture tendency. The trigonal edged single lap and bevelled lap joints showed the higher strength than the plain single lap, trigonal single lap, joggle lap and double lap joints in same adhesive area. The fractures of trigonal single lap and trigonal edged single lap joints that had the higher strength level were shown as the mixture type of the cohesive and interfacial-failure, mostly joggle lap joints that had the lower strength level were shown as the adhesive-failure.

고주파열처리를 적용한 캠 샤프트 소재의 피로균열진전 특성 (Characteristics of Fatigue Crack Growth for Camshaft Material Applied to High Frequence Induction Treatment)

  • 이현준;박성호;박원조
    • 한국해양공학회지
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    • 제23권3호
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    • pp.46-52
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    • 2009
  • Nowadays, many components in automobile, aircraft, offshore structure and industry require lightness and high strength. However, since developments of advanced materials have limitations, it mainly is applying to method of surface hardening. This study offered research about camshaft that is one among engine important component. The material used in this study is 0.53% carbon steel as structure material of camshaft, splineshaft, coupling, pulley, driveshaft et cetera. Camshaft is processed using mainly carbon steel, and receives wear and fatigue by special quality high speed of parts. Therefore, camshaft need surface hardening to improve camshaft's fatigue life and increase durability of engine. This study compare to residual stress and martensite microstructure created by high frequency induction treatment, and these results lead to the conclusion of fatigue crack growth characteristics.

접착부 형상이 알루미늄/폴리카보네이트 접합재의 강도에 미치는 영향 (Effect of Adhesive Shape on the Strength of Aluminum/Polycarbonate Joint)

  • 서도원;김효진;최준용;;임재규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.1039-1044
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    • 2003
  • Adhesive-bonded joints are widely used in the industry. Recently aircraft applications of adhesive bonding joints have been increased extensively in automobile and air industry. Because adhesives which are available for structural applications have been developed a lot and understanding of adhesive bonding has been improved so much. In this study, as the fundamental research of design of adhesive bonding joints, this study considers specimen shape are affect strength and durability of Al/Polymer lap joints. In this research, cross head speed difference were concerned to evaluate their effects on the adhesive strength. Cross head speed makes a change 0.05mm/min, 0.5mm/min, 5mm/min. The result is load-displacement diagram showed brittleness fracture tendency. Fracture tendency that is shown enough on stress distribution of trigonal single lap joint and trigonal edged single lap joint occur the inside of adhesive.

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중복안정성 확보를 위한 항공전자 소프트웨어 설계방안 연구 (A Study on the Avionics Software Design for Redundancy)

  • 임성신;조한상;김종문;송재일
    • 항공우주시스템공학회지
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    • 제8권2호
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    • pp.21-26
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    • 2014
  • The aircraft manufacturers are constantly driving to reduce manufacturing lead times and cost at the same time as the product complexity increases and technology continues to change. Integrated Modular Avionics (IMA) is a solution that allows the aviation industry to manage their avionics complexity. IMA defines an integrated system architecture that preserves the fault containment and 'separation of concerns' properties of the federated architectures. In software side, the air transport industry has developed ARINC 653 specification as a standardized Real Time Operating System (RTOS) interface definition for IMA. It allows hosting multiple applications of different software levels on the same hardware in the context of IMA architecture. This paper describes a study that provided the avionics software design for separation of fault and backup of core function to reduce workload of pilot with cost efficiency.

The Study on EU ETS (欧盟航空减排交易体制评析) -From the Perspective of China-

  • Qin, Huaping
    • 항공우주정책ㆍ법학회지
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    • 제26권1호
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    • pp.127-145
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    • 2011
  • European Union unilaterally included the emissions from aviation activities into EU ETS on 19 November 2008 by amending Directive 2003/87/EC. According to the Directive all the emissions(mainly against the CO2) from aviation activities shall be subject to the regulation of EU ETS from 2012. For the period from 1 January 2012 to 31 December 2012, the total quantity of allowances to be allocated to aircraft operators shall be equivalent to 97% of the historical aviation emission s. From 1 January 2013, the allowances will be reduced to 95%. The allocation of allowances which may be applied by each operator with free of charge will be reduced from 85% to 82% from 1 January 2012 to 1 January 2013. Since the Directive will affect every country's airline industry more or less, the nations and international organizations respond variously. The controversial focus is that whether EU has the right to unilaterally include the emissions from international aviation activities into EU ETS. This article firstly analyzes the effect caused by EU ETS to China's airline industry, and then studies the legality of the action of EU subject to current positive international law, and finally draws the conclusion that EU enjoys no such right to unilaterally include the emissions from international aviation activities.

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CNC선반 C축 밀링 원호가공에서 절삭조건이 표면 거칠기에 미치는 영향 (Effect of Surface Roughness on Cutting Conditions in CNC lathe C-Axis Milling Arc Cutting)

  • 신국식
    • 한국기계가공학회지
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    • 제13권4호
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    • pp.99-105
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    • 2014
  • The domestic airline industry undertakes the production of finished products by assembling existing self-described components via a design process which involves assembly and production steps, after which many of the finished products are exported. However, high reliability and stability must be guaranteed, because customers require high-precision components at the time of manufacturing. In the aircraft parts industry, the mass production of high-value-added parts is limited. Therefore, a small production scale depending on the part is used, as many types of conventional CNC lathe machines with X-axis and Z-axis as well as Z-axis and C-axis CNC milling are used. The parts also rely on high-pressure air to increase production. The most important factors are good stability during processing, as high-precision parts are required, as noted above. It was found that as the C-axis rotation speed increased, the diameter of the cutting tool decreased with a decrease in the surface roughness, while the workpiece rotation speed increased with an increase in the surface roughness.