• Title/Summary/Keyword: Personal Air Vehicle(PAV)

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미래형 항공교통수단의 개발전망과 기회 - PAV(Personal Air Vehicle)를 중심으로 -

  • Lee, Gi-Sang
    • The Journal of Aerospace Industry
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    • s.70
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    • pp.70-93
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    • 2008
  • 산업의 고도화에 따라 시간을 절약하고 공간을 활용하기 위한 방법으로서, 보다 큰 항공기, 보다 빠른 항공기에 대한 요구가 꾸준히 제기된다. 최근 불거진 지구온난화에 대한 이슈는 모든 산업의 초점을 친환경으로 돌려고 있어서, 항공기산업의 경우에도 예외 없이 보다 친환경적이고, 연료 효율적인 항공기개발에 집중하고 있다. 또한, 과거에 비해 자유의지가 강조되는 현재에는 보다 이용이 간편한 개인용 항공기의 출현이 요구되고 있어 이 분야에 대한 연구도 활발히 진행 중이다. 이에 따라 많은 국가들이 각각의 요구에 따라 초대형여객기(VLCT), 차세대 초음속여객기(HSCT), 그린항공기, 개인 자가용 항공기(PAV) 등의 형태로 개발을 서두르고 있으며, 일부 분야는 이미 상용화를 눈앞에 두고 있다. 특히 PAV의 수요는 향후에 자동차 시장의 일부를 대체할 것으로 예상되는 만큼 선진국들은 수요자의 요구에 따라 발 빠르게 대응하여 PAV에 대한 투자를 아끼지 않고 있다. 따라서 본 연구에서는 미래형 항공교통수단의 개발전망과 동향을 분석함으로써 앞으로 우리나라 항공기산업의 발전방향에 대한 시사점을 도출하고자 하였다. 특히 틈새 시장으로서의 PAV 분야의 개발동향과 전망을 살펴봄으로써, 동 분야에 대한 연구개발과 투자를 통한 우리나라 항공기산업의 발전기회를 모색해 보고자 하였다.

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Current Status and Development Direction of Advanced Air Mobility ICTs (Advanced Air Mobility ICT 기술 현황 및 발전 방향)

  • B.J. Oh;M.S. Lee;B.K. Kim;Y.J. Jeong;Y.J. Lim;C.D. Lim
    • Electronics and Telecommunications Trends
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    • v.38 no.3
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    • pp.1-10
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    • 2023
  • In this study, the status of global advanced air mobility (AAM) was investigated to derive information and communications technologies (ICTs) that should be prepared according to directions of domestic AAM development. AAM is an urban air traffic system for moving from city to city by electric vertical take-off and landing or personal aircraft. It is expected to establish a three-dimensional air traffic system that can solve ground traffic congestion caused by the rapid global urbanization. With the full-scale commercialization of AAM solutions, high-density air traffic is expected, and with the advent of the personal air vehicle (PAV), the flight space usage is expected to expand. Therefore, it is necessary to develop a safe AAM service through early research on core ICTs for autonomous flight.

Conceptual Design and Development Test of an Unmanned Scaled-down Quad Tilt Prop PAV (쿼드 틸트 프롭형 PAV 무인 축소모델 개념설계 및 개발시험)

  • Byun, Young-Seop;Song, Jun-Beom;Kim, Jae-Nam;Jeong, Jin-Suk;Song, Woo-Jin;Kang, Beom-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.1
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    • pp.37-46
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    • 2014
  • This paper describes the conceptual design and development test procedure of a unmanned scaled-down personal air vehicle(PAV) with drive and flight dual mode capability. Trade studies on operational requirements led to the suggestion of a quad tilt prop platform which has nacelle tilt capability with multi rotor configuration. Motors for propeller propulsion and driving mechanism were integrated into a single nacelle, then they were implemented by nacelle tilt mechanism for conversion between the drive and the flight modes. Primary design parameters and initial specifications were confirmed through conceptual design, then functional tests were performed with the test platforms for the drive and the flight modes.

A Study on the Urban Air Mobility(UAM) Operation Pilot Qualification System

  • Kim, Su-Ro;Cho, Young-Jin;Jeon, Seung-Mok
    • International Journal of Internet, Broadcasting and Communication
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    • v.14 no.1
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    • pp.201-208
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    • 2022
  • As around the world, ground and underground transportation capacity is reaching its limit, centering on urban areas. As urban traffic becomes congested, time and cost are astronomical, and environmental destruction caused by urban pollution is becoming increasingly serious. As a way to solve this problem, the means of flying over the air are in the spotlight as the next generation of future transportation, and the concept of urban air mobility (UAM, Urban Air Mobility) is defined as systematic planning. The development of an electric-powered vertical take-off (eVTOL) aircraft that obtains electric power through a battery using a personal aerial vehicle (PAV) as a means of transportation has accelerated. As the aircraft development of new technology aircraft in the evtol method is actively carried out, the need to prepare systems such as aircraft certification standards, pilot qualification systems, and qualification management is emerging. The Federal Aviation Administration (FAA) and the European Union Aviation Safety Agency (EASA), which lead international standards, announced new special technical conditions and temporary regulations SCVTOL-01, respectively. However, the pilot qualification system for operating the uam aircraft has not yet been clearly announced. Therefore, this paper analyzes the recently announced FAA regulations and EASA regulations to identify differences and directions in perspectives on UAMs and study the existing vertical take-off and landing aircraft (VTOL) pilot qualification system to present directions for qualification classification.

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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Comparison of the Free-Fall Impact Force Applied to a Multicopter PAV According to External Airbag Folding Method (외부 에어백 폴딩 방식에 따른 자유 낙하 충돌 시 멀티콥터형 개인용 항공기에 가해지는 충격력 비교)

  • Jang, Yoon Ho;Kim, Jeong
    • Journal of Aerospace System Engineering
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    • v.16 no.1
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    • pp.28-39
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    • 2022
  • With the development of small multicopter PAV (Personal Air Vehicle), it is necessary to develop safety-related devices for manned rotorcraft. In this study, we assumed that an external airbag can be installed in a small multicopter PAV, and using LS-DYNA's Airbag Folding Application, we performed a free-fall collision analysis by modeling the airbag shapes consisting or Roll, Zigzag, and Sigma. There was no significant difference in the final airbag deployment time of the three models. However, when it collides with the ground during deployment, the Sigma fold type external airbag had the fastest deployment speed, applying the most impact force to the PAV, while the Roll fold type external airbag applied the smallest impact force to the PAV.

Analysis of Operational Concept Development Guide, Process and A Case Study (운용개념 개발 가이드와 프로세스 분석 및 작성 사례 연구)

  • Park, Joongyong
    • Journal of the Korean Society of Systems Engineering
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    • v.9 no.1
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    • pp.13-23
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    • 2013
  • Operational Concept Descriptions or Document(OCD) shall be developed to understand stakeholder's desire for to-be-delivered system. But there is little study on methodology of OCD generation and many developers do not understand importance of OCD in Korea. According to Nicole Roberts' industry(18 U.S. companies and organizations) survey, only 30% of system development projects had OCD, too. Researchers and developers have opposing views regarding the generation of an OCD. Many researchers believe that the development and use of operational concepts at the start of large projects is essential. Alternatively, developers may view the OCD as a burden to the development process rather than an enabler due to the extensive documentation requirement. In this paper a couple of OCD guidelines were investigated to clarify how to build a CONOPS effectively and what to include. Finally, OCD for rotorcraft based Personal Air Vehicle System(PAVS) was developed as a case study. In the future, a template for generating OCD appropriate to Korean environment could be proposed.

Preliminary Conceptual Design of a Multicopter Type eVTOL using Reverse Engineering Techniques for Urban Air Mobility (도심항공 모빌리티(UAM)를 위한 역설계 기법을 사용한 멀티콥터형 eVTOL의 기본 개념설계)

  • Choi, Won-Seok;Yi, Dong-Kyu;Hwang, Ho-Yon
    • Journal of Advanced Navigation Technology
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    • v.25 no.1
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    • pp.29-39
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    • 2021
  • As a means of solving traffic congestion in the downtown of large city, the interest in urban air mobility (UAM) using electric vertical take-off landing personal aerial vehicle (eVTOL PAV) is increasing. eVTOL configurations that will be used for UAM are classified by lift-and-cruise, tilt rotors, tilt-wings, tilted-ducted fans, multicopters, depending on propulsion types. This study tries to perform preliminary conceptual design for a given mission profile using reverse engineering techniques by taking the multicopter type Airbus's CityAirbus as a basic model. Wetted area, lift to drag ratio, drag coefficients were calculated using the OpenVSP which is an aerodynamic analysis software. The power required for each mission section of CityAirbus were calculated, and the corresponding battery and motor were selected. Also, total weight was predicted by estimating component weights of eVTOL.

Requirement Analysis of Efficiency, Reliability, Safety, Noise, Emission, Performance and Certification Necessary for the Application of Urban Air Mobility (UAM) (도심항공 모빌리티(UAM) 적용에 필요한 효율, 신뢰성, 안전성, 소음, 배기가스, 성능 및 인증의 요구도 분석)

  • Yun, Ju-Yeol;Hwang, Ho-Yon
    • Journal of Advanced Navigation Technology
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    • v.24 no.5
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    • pp.329-342
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    • 2020
  • In this paper, we analyzed the requirements for the application of UAM, a new concept to solve the traffic congestion in large cities. First, the current domestic and foreign status of research and development related to UAM was investigated and the pros and cons and the time required for each mission radius were analyzed for various configurations of aircraft being commercialized. In addition, in order to analyze the market acceptance of the UAM, the individual's consciousness and reliability requirements were identified and safety requirements were analyzed through accident rate data for each aircraft type. Because it operates in a densely populated urban area, requirement analyses on noise and exhaust, which are environmental factors that can affect the community were performed, and requirements related to aircraft performance, certification standards, and airworthiness standards of FAA and EASA were also analyzed.

A Study of Model-Based Aircraft Safety Assessment (모델기반 항공기 안전성평가에 관한 연구)

  • Kim, Ju-young;Lee, Dong-Min;Lee, Byoung-Gil;Gil, Gi-Nam;Kim, Kyung-Nam;Na, Jong-Whoa
    • Journal of Aerospace System Engineering
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    • v.15 no.5
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    • pp.24-32
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    • 2021
  • Personal Air Vehicle (PAV), Cargo UAS (Cargo UAS), and existing manned and unmanned aircraft are key vehicles for urban air mobility (UAM), and should demonstrate compatibility for the design of aircraft systems. The safety assessment required by for certification to ensure safety and reliability should be systematically performed throughout the entire cycle from the beginning of the aircraft development process. However, with the increasing complexity of safety critical aviation systems and the application of state-of-the-art systems, conventional experience-based and procedural-based safety evaluation methods make ir difficult to objectively assess safety requirements and system safety. Therefore, Model-Based Safety Assessment (MBSA) using modeling and simulation techniques is actively being studied at domestic and foreign countries to address these problems. In this paper, we propose a Model-Based Safety Evaluation framework utilizing modeling and simulation-based integrated flight simulators. Our case studies on the Traffic Collision Availability System (TCAS) and Wheel Brake System (WBS) confirmed that they are practical for future safety assessments.