• Title/Summary/Keyword: 경량항공기

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Technical Development Trend and Analysis of Futuristic Personal Air Vehicle (미래형 개인용 항공기 기술개발 동향 및 분석)

  • Yi, Tae-Hyeong;Kim, Keun-Taek;Ahn, Seok-Min;Lee, Dae-Sung
    • Current Industrial and Technological Trends in Aerospace
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    • v.9 no.1
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    • pp.64-76
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    • 2011
  • The current development trend and status of a personal air vehicle, known as the novel concept of a transportation that combines a personal car with a light general aviation aircraft, is summarized to investigate its feasibility as a future transportation. In the paper, the development programs of a personal air vehicle such as AGATE, PAVE, SATS and NGATS are first summarized, and then the design, technical development and testing activities of Terrafugia's Transition and Moller International's M400 Skycar, which will be commercialized in a short time, are reviewed. Based on the assessment of technical issues with those vehicles, the key technologies for the future development of the personal air vehicle are suggested with two basic requirements of safety and mobility.

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The analysis of the LSA Airpark of Metropolitan Area (수도권 지역 경량항공 이착륙장 분석)

  • Shin, Dai-Won;Kim, Woong-Yi
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.22 no.1
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    • pp.44-50
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    • 2014
  • In this study, we surveyed the operating status of the LSA Airpark in Metropolitan Area of Korea, and compared the Airfield Facilities Manual for the Air Leisure. We analyzed the problems of the closure and the currently used of the LSA Airpark, through site visits. We presented the re-usability for the closure LSA Airpark, the improvements for the currently used of the LSA Airpark.

PET / Cellulose Composite의 물성연구

  • 강영구;천영기
    • Proceedings of the Korean Institute of Industrial Safety Conference
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    • 2003.05a
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    • pp.418-421
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    • 2003
  • 경량ㆍ고강도 기능성 Composite는 경량구조재료로 차량, 항공기, 선박 및 각종 설비의 안전구조재로 그 용도가 다양하게 사용되고 있다. 특히 폐플라스틱을 이용한 경량구 조재는 가격 경쟁력이 높고 또한 환경 및 자원 재활용 측면에서 관심이 고조되고 있다. 고강도, 안전성 확보를 위해 사용가능한 폐플라스틱 소재로는 가공성이 용이한 폐Polyethylene(PE), 폐Polypropylene(PP), 폐Polyethyleneterephthalate(PET) 등을 주원료로 가공되나, 기계적 특성이 저하되어 이의 개선을 위해 여러 가지 형태의 충진재의 혼합을 통해 개선하고자 하는 연구가 진행되어 왔다.(중략)

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소형 프로펠러 경항공기 복합재 날개의 구조설계에 관한 연구

  • 공창덕;강명훈;정종철
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2000.04a
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    • pp.37-37
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    • 2000
  • 복합재료는 높은 무게비 강도 및 강성뿐만 아니라 우수한 재료 특성 때문에 경량화와 구조적 안전성이 요구되는 항공기의 구조재로서 사용이 증대되고 있다. 소형 민용항공기는 구조적 안전성과 함께 제작과 정비, 유지보수의 용이성이 중요시된다. 본 연구에서는 복합재료를 구조재로 사용하였을 때의 성능변화와 경량화 등을 검토하기 위하여 기존의 알루미늄 합금을 이용하여 설계된 소형 프로펠러 경항공기 날개의 구조재로서 복합재료를 사용하여 재설계하였다. 날개의 기본 구조는 스킨, 스파, 웹으로 구성된 상자형 단면으로 설계하였으며 날개의 구조재로서 탄소/에폭시를 사용하여 상용 유한요소해석코드인 NISAII를 이용하여 굽힘, 좌굴 등의 응력해석을 수행하였고 기존 설계된 날개와의 성능비교를 위하여 알루미늄 합금으로 설계된 날개를 모델링하여 해석한 결과와 비교하였다. 비교결과 구조재로 탄소/에폭시를 사용하여 설계된 날개가 무게비 성능면에서 더 우수함을 확인하였다.

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A Study on the Autofrettage Analysis in Single and Compound Cylinders (단일 및 복합실린더에서 자긴가공 해석에 관한 연구)

  • Shim, Woo-Sung;Kim, Jae-Hoon;Lee, Young-Shin;Cha, Ki-Up;Hong, Suk-Kyun
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.4
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    • pp.7-15
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    • 2008
  • In manufacturing aircraft, safety and lightness of structure are important factors. Utilizing autofrettage technique, these benefits can be obtained. This technique is most frequently applied to a single cylinder. However, the Bauschinger effect reduces the benefits of autofrettage process Therefore, there is increasing interest in the use of compound cylinder that combine shrink fit and autofrettage. In this paper, single and compound cylinders that has same geometry were considered. It was found that compound cylinder which was autofrettaged has lower tangential hoop stress and plastic strain than single cylinder at bore. This means a reduction in the impact of the Bauschinger effect after shrink-fitting which produces the beneficial bore hoop stress.

Ground Test and Performance Evaluation of Miniaturized AHRS for Small-Scale UAV (소형무인항공기를 위한 소형 경량 AHRS의 지상시험 및 성능 평가)

  • Roh, Min-Shik;Song, Jun-Beom;Song, Woo-Jin;Kang, Beom-Soo
    • Journal of Advanced Navigation Technology
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    • v.15 no.2
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    • pp.181-188
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    • 2011
  • A small UAVs(Unmaned Aerial Vehicles) have limited by the payload capacity which requires miniaturization of a navigation system. In this paper, the performance of the lightweight and small sized AHRS(Attitude Heading Reference System), which is self-developed, is evaluated at low acceleration environment. The designed AHRS adopts the commercial low-cost MEMS sensors. A quaternion-based attitude calculation method, which eliminates singularity with relatively simple algebra, is used. In an attitude correction algorithm, the Kalman filter is used with accelerometers and magnetometers combined. The fabricated AHRS is also evaluated with reference to a COTS(Commercial Off-The-Shelf) AHRS which reports a number of successful applications to a small UAVs. The test results show that the measurements from the fabricated AHRS provide proper attitude output data with acceptable amount of differences(horizontal axis 0.5$^{\circ}$, vertical axis 1.5$^{\circ}$) in test environment.

CFRP 적층쉘의 고속 관통실험에 따른 에너지 흡수특성

  • 조영재;김영남;양인영
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.62-62
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    • 2004
  • 최근 신소재인 선진 복합 재료 중 탄소 섬유 강화 플라스틱(이하 CFRP라고 한다. )은 비강도, 비강성이 높기 때문에 경량화가 요구되는 여러 분야, 즉 항공기, 인공위성, 원자로, 자동차 산업분야, 조선 산업분야 등 널리 사용되고 있다. 경량화가 요구되는 분야에 사용되는 구조 부재의 형상은 평판보다는 다양한 형태의 곡면 형상을 뛰는 챌(Shell)의 형상을 갖는다. 또한 이러한 구조물에 충격이 가해 졌을 때 곡면을 갖는 구조물의 충격_응답 및 파괴형태는 평판과는 다른 양상을 보인다.(중략)

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The Legal Theory on the Civil Execution against Aircraft (항공기 집행에 관한 법리)

  • Kwon, Chang-Young
    • The Korean Journal of Air & Space Law and Policy
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    • v.30 no.2
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    • pp.83-153
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    • 2015
  • As our economy grows and the number of aircraft increase, the number of civil execution against aircraft cases are likely to increase as well in the future. The purpose of this article is to present the legal theory on the civil execution against aircrafts by drawing on the legal theory on the civil execution against vessels which constitute a relatively large number of cases thus observed. The provisions of the civil execution against immovables or vessel, shall basically apply mutatis mutandis to the civil execution against aircraft or light aircraft. The civil execution against ultra-light flying devices or a foreign aircraft shall be executed in conformity with the civil execution against movables. There are a compulsory auction, an auction to execute a security right to aircraft, and an auction under the right of retention, etc. in the civil execution against an aircraft. A compulsory execution against an aircraft means an execution carried out by a creditor against a debtor's aircraft to obtain satisfaction of claims for the purpose of payment of money. The court of execution of a compulsory execution against an aircraft shall be the district court having jurisdiction over the airport of stoppage or storage of such aircraft at the time of seizure. The forums of execution of a compulsory execution against an aircraft shall be exclusive forums. When a court has rendered an order on commencing an auction, it shall order an execution officer to receive a certificate of the aircraft's registration and other documents as required for its operation, and to submit them to the court. A court may revoke the procedures for a compulsory auction when an execution officer fails to obtain a transfer of the aircraft's registration certificate, etc. and the location of the aircraft is not evident, not later than an elapse of 2 months from the date on which an order on commencing an auction has been rendered. In the case where it is deemed that there exists a business-related need or other based on proper reasoning, the court may permit the aircraft's operation, upon the motion submitted by the debtor. In this case, there shall be a consent from the creditor, the highest bidder, the next highest bidder and successful bidder. A court may, upon a motion submitted by the creditor, make the dispositions required for observing and preserving the aircraft. When a debtor has submitted the documents under subparagraph 2 or 4 of the Article 49 of the Civil Execution Act, and furnished the guarantee equivalent to the claims of the execution creditors and the creditors demanding a distribution and to the costs for execution, before a declaration of bid, the court shall, upon request, revoke other procedures than those for distribution. The provisions of a obligatory auction against vessel or aircraft and an auction to execute a security right to real estate or vessel, shall apply mutatis mutandis to an auction to execute the security right to aircraft. In an auction to execute the security right to aircraft case, an executive title is not necessary. An executory exemplification is not necessary in an application for an auction to execute the security right to aircraft. A court should examine the existence of security right and claim secured. No order on commencing an auction procedure shall be issued with non-existence or invalidity of the security right and absence or extinguishment of the claim secured. Furthermore, these prohibitions are the reason of a decision on non-permit for sale, the court overlooked these prohibitions, and the decision on a permit for sale became final and conclusive, the successful bidder who paid the price and registered of ownership could not acquire ownership of the aircraft sold. A court may render a ruling to put plural aircrafts up for a blanket auction, only when they are in restraint and related matter (Supreme Court Order 2001Ma3688 dated on August 22, 2001). A righter of retention on aircraft may file a request for an auction against the aircraft. The provisions of an auction to execute a security right to aircraft shall apply mutatis mutandis to the formal auction. Airport facility fee and an aircraft are not in restraint and related matter, so an airport management corporation does not hold the right of retention on the aircraft (Supreme Court Decision 2011Da29291 decided on April 10, 2014). In an auction in accordance with the right of retention, all encumbrances (e.g., mortgages) on the sold aircraft shall be extinguished by a sale under the legal conditions for sale. Not only creditors who have claims for preferential payment but also general creditors could demand for distribution. The precedence of the claim of the right of retention on aircraft and that of general creditor's claims are equal.

The Development of The Simulation Environment for Operating a Simultaneous Man/Unmanned Aerial Vehicle Teaming (유/무인 항공기 복합운용체계 검증을 위한 시뮬레이션 환경 구축)

  • Gang, Byeong Gyu;Park, Minsu;Choi, Eunju
    • Journal of Aerospace System Engineering
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    • v.13 no.6
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    • pp.36-42
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    • 2019
  • This research illustrates how the simulation environment for operating the simultaneous man/unmanned aerial vehicle teaming is constructed. X-Plane program, HILS for the ducted fan aircraft (unmanned) and CTLS (manned aircraft) with communication devices are interfaced to simulate the basic co-operational flight. The X-plane and HILS can allow operators to experience the maned and unmanned aircraft operation in the airspace on the ground in turn they can perform various simulated missions in advance before the actual flight. For the test purpose, the data link between man/unmanned aircraft and ground control station is examined using C Band and UHF radio channels by the manned aircraft.