• 항공우주정책ㆍ법학회지
• /
• 제35권1호
• /
• pp.153-180
• /
• 2020

본 연구는 우리나라의 자동차산업, 조선업 등 일부 중공업이 세계적으로 높은 수준의 생산규모와 기술수준을 달성한 것에 비해 상대적으로 발전이 저조한 항공기산업을 육성하기 위해서는 어떠한 법적, 정책적 사안의 개선이 필요한지에 대해 알아보는데 그 의의가 있다. 우리나라의 항공기산업이 여타 산업에 비해 저조한 성장세를 보이고 있는데 국가 경제규모를 비롯하여 관련 산업의 발달 수준, 항공기 기술 수준, 항공기 제조 수요 등의 변수를 적절히 사용할 수 있는 시장구조를 구축하지 못했기 때문이라고 볼 수 있다. 대부분의 산업은 경쟁체제의 시장구조 하에 민간이 주도하여 성장하지만, 항공기산업과 같은 중공업은 막대한 규모의 초기 투자비용과 높은 기술력, 충분한 양의 수요를 확보하여야만 최소한의 경제성을 유지할 수 있기에 불완전경쟁체제의 시장구조 하에 정부가 주도하여 성장하는 것이 일반적이다. 이에 우리나라의 항공기산업은 군 수요를 중심으로 하는 군용 항공기를 개발하고 양산하는 것에 집중되어 있었으나, 미국과의 BASA(Bilateral Aviation Safety Agreement; 상호항공안전협정)를 체결함으로써 분위기의 반전을 도모하였다. 이에 차세대 중형항공기 개발 사업을 추진하기 위한 예비타당성 조사까지 2010년에 수행되었으나 컨소시움 대상인 캐나다의 Bombardier사와 입장 차이로 인해 무산되고, 현재는 한국항공우주산업(KAI)이 단독으로 Bombardier사의 Q400 면허생산을 추진 중이며 그마저도 순탄치 않다. 이처럼 개발에 난항을 겪고 있는 중대형 민간 항공기에 비해 KAI와 항우연 등에서 민수용 헬기를 비롯하여 무인항공기, 유인항공기의 무인화 기술을 성공적으로 개발하고 있다. 또한 무인항공기 분야는 세계적으로 독점적인 영향력을 행사하고 있는 제조사가 아직까지 마땅하지 않으므로 향후 항공기산업 육성을 위해 민간용 헬기 및 무인항공기 분야에 초점을 맞추어 정부 주도의 연구개발사업을 추진할 필요가 있다고 본다. 또한 KT-1과 T-50과 같은 군용항공기도 순조롭게 수출되고 있는 추세이며, 대한민국 내 항공기 제조에 관한 최대 수요자는 군이라는 점을 간과할 수 없으므로 민군겸용 개발(spin-up), 군용기술 개발 후 민간이전(spin-off), 민간기술 개발 후 국방 분야 활용(spin-on)이 가능하도록 국가연구개발사업과 국방연구개발 사업을 동시에 추진할 필요가 있다. 그러나 양 사업은 사업추진 방식과 전담부서, 기술료 제도에 있어 여러 차이점이 있다. 이에 본 연구를 통해 국가연구개발사업과 국방연구개발사업의 기술 소유권과 실시권, 그리고 기술료 제도에 대해 알아보았다. 그리고 해당 제도의 문제점을 확인하고 개선방안을 도출하였다.

• 한국기계가공학회지
• /
• 제12권6호
• /
• pp.132-141
• /
• 2013

Robotic Drilling Systems(RDSs) set the standard for the factory automation systems in aerospace manufacturing. With the benefits of cost effective drilling and predictive maintenance, RDSs can provide greater flexibility in the manufacturing process. The system can be easily adopted to manage very complex and time-consuming processes, such as automated fastening hole drilling processes of large aircraft sections, where it would be difficult accomplished by workers following teaching or conventional guided methods. However, in order to build an RDS based on a CAD model, the precise calibration of the Tool Center Point(TCP) must be performed in order to define the relationships between the fastening-hole target and the End Effector(EEF). Based on the kinematics principle, the robot manipulator requires a new method to correct the 3D errors between the CAD model of the reference coordinate system and the actual measurements. The system can be called as a successful system if following conditions can be met; a. seamless integration of the industrial robot controller and the IO Level communication, b. performing pre-defined drilling procedures automatically. This study focuses on implementing a new technology called iGPS into the fastening-hole-drilling process, which is a critical process in aircraft manufacturing. The proposed system exhibits better than 100-micron 3D accuracy under the predefined working space. Based on the proposed EEF fastening-hole machining process, the corresponding processes and programs are developed, and its feasibility is studied.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 1997년도 추계학술대회 논문집
• /
• pp.125-128
• /
• 1997

They use a Ball End-mill in order to manufacturing sculptured surface when making metal mold, mold, cars and aircraft. In the work of a Ball End-mill case, customers do not often satisfied with manufacturing precision. Eventually, they have to re-work for the purpose of meeting manufacturing precision. There are resulted in lots of loss, whereby, in terms of both time and costs. The reasons of tolerance reducing manufacturing precision are thermal strain, the surface is damaged because of increasing cutting force and tool wear, tool deflection etc.. We focus on, however, manufacturing precision caused due to deflection of tool.

• 한국기계가공학회지
• /
• 제11권3호
• /
• pp.68-72
• /
• 2012

Al2017 is typical Duralumin of self-hardening aluminum alloy. It is lightweight, formability and machinability so throughout the industries have widely used automobile, electronics, semiconductor and aircraft as material. A variety of CNC machine tool processing technology, scientific principles and experience have been studied in order to increase accuracy and productivity. Using a machining center is to constant amount of side step and cutting characteristics studied changing depth of cut, revolution per minute and feed rate.

• International Journal of Aeronautical and Space Sciences
• /
• 제12권1호
• /
• pp.84-91
• /
• 2011

A finite element analysis for the wing and landing gear of a composite target-drone air vehicle was performed. For the wing analysis, two load cases were considered: a 5g symmetric pull-up and a -1.5g symmetric push-over. For the landing gear analysis, a sinking velocity of 1.4 m/s at a 2g level landing condition was taken into account. MSC/NASTRAN and LS-DYNA were utilized for the static and dynamic analyses, respectively. Finite element results were verified by the static test of a prototype wing under a 6g symmetric pull-up condition. The test showed a 17% larger wing tip deflection than the finite element analysis. This difference is believed to come from the material and geometrical imperfections incurred during the manufacturing process.

• 한국항공운항학회지
• /
• 제13권1호
• /
• pp.43-49
• /
• 2005

There are several ways to mold the complex material, and it is divided to vacuum pack mold, compression mold, and hand lay up for a high molecular substance as a basic material. Moreover, it can be divided to general manufacturing (Single form) and mold manufacturing(Mold form) under normal temperature for Firefly. Firefly was manufactured with hand lay up and general manufacturing that using the foam core, glass fabric, and template without mold. However, mold manufacturing that is producing the surface by semi-sandwich using thin foam core and glass fabric then reinforce the inside with spar and rib is on developing. Mold manufacturing can make easy to production, standardize the quality, and possible to mass producing. In this paper, we present the mold producing process for canard aircraft "Firefly", and the problems and solutions during producing Firefly. Moreover, it complements the defect that the problems caused by master manufacturing error when produce several masters of a large part, and make the manufacturing process to be shortened by the replacement from the supplementary plate to the foam that is installed when producing lay up mold.

• Advances in aircraft and spacecraft science
• /
• 제1권2호
• /
• pp.219-232
• /
• 2014

This paper reports on an ongoing study investigating the feasibility of using an evolutionary method to develop the rules governing Self-Organised (SO) systems for use in swarms of unmanned aerial vehicles. In general, it is difficult to design swarm systems that follow explicit global behaviour. Unlike optimising a predefined objective function, the solution to the problem is the emergent behaviour in the SO systems which results from simultaneous interactions among agents and between agents and their environment. In this study, evolutionary algorithms are used to investigate their control and effectiveness in synthesising the weighting of different rules on SO emergent behaviour. Both homogeneous swarms and heterogeneous swarms were considered though the results provided are for a case study investigating the simplest problem a homogeneous swarm without mutation. Though simple this study does indicate the potential of the approach.

• 한국공작기계학회:학술대회논문집
• /
• 한국공작기계학회 2005년도 춘계학술대회 논문집
• /
• pp.473-476
• /
• 2005

Today's manufacturing industry is facing challenges from advanced difficult-to-machine materials (WC-Co alloys, ceramics, and composites), stringent design requirements (high precision, complex shapes, and high surface quality), and machining costs. Advanced materials play an increasingly important role in modem manufacturing industries, especially, in aircraft, automobile, tool, die and mold making industries. The greatly-improved thermal, chemical, and mechanical properties of the material (such as improved strength, heat resistance, wear resistance, and corrosion resistance), while having yielded enormous economic benefits to manufacturing industries through improved product performance and product design, are making traditional machining processes unable to machine them or unable to machine them economically. In this paper, mechanical characteristic evaluation test of fine powder type WC-Co alloy was accomplished to obtain clear data for miniaturized special die parts machining with high reliability and high quality.

• Journal of Welding and Joining
• /
• 제34권4호
• /
• pp.9-16
• /
• 2016

Metal parts are produced by conventional methods such as casting, forging and cutting, extrusion, etc. However, nowadays, with additive manufacturing (AM), it is possible to directly commercialize by means of stacking of equipment to the 3D drawing and use of high precision tools such as laser source. Thus, drawing of materials is an important aspect in delivering good products. AM deals with production of lighter aircraft parts and few more three-dimensional molds, it wish to manufacture special medical parts and want to steadily expand the new market area. The cost of related equipment and materials are still expensive and difficult to obtain on a mass production. However, the ability to make changes and lead the innovation in the paradigm of traditional manufacturing process is still effective. In this paper, we introduce metal AM and the principles of the related devices, metal powder production process, and their application.

• 한국기계가공학회지
• /
• 제14권4호
• /
• pp.85-91
• /
• 2015

Current world aircraft industry studies on the precision of the product are in active progress. Particularly in terms of improving the quality of processed products in terms of the surface roughness of the dimensional accuracy, fatigue strength, and corrosion resistance, which affect a lot of research on surface roughness, has been investigated. In this study of aluminum alloy, 7075 aircraft aluminum is used in a cutting CNC lathe machine for the cutting speed and feed rate according to the cutting experiments that were conducted. Additionally, the machine tool of the cooling method soluble cutting oil, insoluble cutting oil by cooling, and cooling the workpiece by cutting surface roughness will be investigated. Through the method and soluble cutting oil coolant cooled by the cutting speed increases, the value of surface roughness showed a regular result. Tool nose radius of 0.8 mm than 0.4 mm picture of when approximately 50 of the surface roughness values were less.