• Title/Summary/Keyword: Flight Safety Critical Software

Search Result 12, Processing Time 0.016 seconds

Computational Investigation of Lightning Strike Effects on Aircraft Components

  • Ranjith, Ravichandran;Myong, Rho Shin;Lee, Sangwook
    • International Journal of Aeronautical and Space Sciences
    • /
    • v.15 no.1
    • /
    • pp.44-53
    • /
    • 2014
  • A lightning strike to the aircraft seriously affects the aircraft and its components in various ways. As one of the most critical threats to the flight safety of an aircraft, fuel vapour ignition by lightning can occur through various means, notably through hot spot formation on the fuel tank skins. In this study, a coupled thermal-electrical approach using the commercial software ABAQUS is used to study the effects of a lightning strike on aircraft fuel tanks. This approach assumes that the electrical conductivity of a material depends on temperature, and that a temperature rise in a material due to Joule heat generation depends on electrical current. The inter-dependence of thermal and electrical properties-the thermal-electrical coupling-is analyzed by a coupled thermal-electrical analysis module. The analysis elucidates the effects of different material properties and thicknesses of tank skins and identifies the worst case of lightning zones.

Design Study of Digital Map Architecture for AAV (미래형 항공기체(AAV)용 전자지도 아키텍처 설계 연구)

  • Kyung-Chul Choi;Ji-Hun Kim;Nak-Min Choi;Gyong-Hoon Baek
    • Journal of Advanced Navigation Technology
    • /
    • v.28 no.4
    • /
    • pp.393-399
    • /
    • 2024
  • The digital map computer for advanced air vehicles (AAV) must be high-performance, lightweight, portable, and modular. It should receive data on terrain, weather, and obstacles from external modules to display digital maps accurately. This necessitates robust communication capabilities with external devices via an Ethernet interface and the ability to output digital map visuals clearly through an high-defintion multimedia Interface (HDMI) or digital visual interface (DVI) interface. This paper presents the design of both hardware and software architecture that fulfills these critical requirements for an AAV digital map system. Additionally, it establishes the minimum specifications needed and verifies the suitability of the designed digital map computer through rigorous performance measurements and testing. By ensuring these standards, the digital map computer can reliably support the complex navigational needs of AAV, enhancing operational efficiency and safety.