• Title/Summary/Keyword: B767-300

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The Study of the Turbulence Effect during In-cruise-flight of Aircraft by FDR(Flight Data Recorder) (비행자료기록(FDR)을 통한 순항비행 중의 항공기 비행요란 현상에 대한 연구)

  • Kim, I.Y.;Song, B.H.;Shin, D.W.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.10 no.1
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    • pp.45-56
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    • 2002
  • This study is performed to analyze the turbulence effect by the analysis of the parameters related with flight data of FDR(Flight Data Recorder). In the analysis, the SSFDR(Solid State Flight Data Recorder) flight data of B747-400 and B767-300 model aircraft was selected. Through this study, we verified that turbulence interfere with flight safety because it is modifiable to flight situation and condition of aircraft.

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Research for the Chemical Emergency Oxygen Supply and Lighting System for Aircraft Passengers (항공기 승객용 화학적 비상산소 공급 및 조명시스템에 대한 연구)

  • Kim, Young-In
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.30 no.2
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    • pp.55-60
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    • 2022
  • A PSU (passenger service unit) is mounted on passenger seats in a cabin on an aircraft and consists of a crew call lamp, a reading lights, an information display lamp, an emergency oxygen generator, and an emergency oxygen mask. It is a safety device for providing convenience to passengers and providing oxygen to passengers in an emergency. This paper is a study on emergency oxygen supply systems and light systems of aircraft PSUs and a control device was developed to operate the system by analyzing the B767-300 aircraft's PSU circuit diagram. And the temperature generated by the B777-200ER aircraft's emergency oxygen generator was also measured by operating it directly. Through this, precautions for explaining the operation of an oxygen mask in an emergency were described and improvements were presented. Data acquired in these research processes can be used in the future to develop aircraft PSU (passenger service unit) and emergency oxygen generators.

A Study on the Characteristics of a 400W, 7.9~8.4GHz Double-Slot Coupled-Cavity Traveling-Wave Tube (400W, 7.9~8.4GHz 이중슬롯 결합공진기 진행파관 증폭기 특성 연구)

  • Kim, Hyoung-Jong;Kim, Hae-Jin;Choi, Jin-Joo;So, Jun-Ho
    • Journal of the Korea Institute of Military Science and Technology
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    • v.12 no.6
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    • pp.760-767
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    • 2009
  • This thesis focuses on the study of high-power, coupled-cavity traveling-wave tube(CCTWT) for radar applications. The CCTWT employed a reentrant double-slot staggered RF cavity structure. Computational analysis of the X-band, double-slot staggered structures is carried out through the use of HFSS code, which solves Maxwell's equations fully in three-dimensions. The non-linear, large-signal performance of CCTWTs are predicted from numerical simulations using a three-dimensional particle-in-cell code, MAGIC3D. With beam voltage set to 12.7~13kV and beam current at 300mA, the CCTWT produces a saturated radiation power of 350~430W, corresponding to an electronic efficiency of 8.9~11.2% and a gain of 23.7~24.2dB within a frequency range of 7.9~8.4GHz.

Effect on the Wake Flow according to Various length of Rectangular Cylinder in a Parallel Arrangement (병렬구조를 가진 장방형 실린더의 길이가 후류 유동에 미치는 영향)

  • Choe, Sang-Bom;Cho, Dae-Hwan
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.20 no.6
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    • pp.760-767
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    • 2014
  • An experimental study is carried out to investigate the effect of jet stream in the gab of rectangular cylinders with different length in a parallel arrangement by using PIV method in a circulating water channel. The height(h) of the rectangular cylinder and the gap between the cylinder is 10mm, and the width(B) which is 300mm. The length of the model for flow direction was applied to 30mm, 60mm, 90mm & 120mm, The aspect ratio of a model on the basis of height(H=30mm) is 1, 2, 3 and 4. Reynolds number $Re=1.4{\times}10^4$, $Re=2.0{\times}10^4$, $Re=2.9{\times}10^4$ based on the height(H) of model for the distance of tidal distributions as of water depth have been applied during the whole experiments. The measurement area was set to 5H rear of the cylinder. As a result, Vortex size in the wake area were increased as velocity increased. and high aspect ratio increased through-flow velocity component in the near wake. Velocity deficit increased highly after near-wake area and low aspect ratio.