Analysis of a boeing 747 aircraft fuel tank vent system

被引:0
|
作者
Jensen, DL [1 ]
机构
[1] JENTEC, Lawndale, CA 90260 USA
来源
JOURNAL OF AIRCRAFT | 2001年 / 38卷 / 05期
关键词
D O I
10.2514/2.2867
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This monograph presents an analysis of a 747 aircraft fuel vent system. The system is comprised of several fuel tanks feeding into a single vent tube. The analysis consisted of formulating equations that govern the venting and heating of the center tank. Flow losses along each section of the vent system were applied to correct the ideal flow from the center fuel tank. These equations were programmed for solution on a digital computer. Results were computed for a flight from Athens, Greece, to New York with a 5-hour delay on the ground before taking off again from New York. The heating caused by air conditioning and bleed air from the engines on the ground during the long delay caused vaporization of fuel and increased the density of the air-fuel vapor. The result was very sluggish venting and "choked" flow producing a significant overpressure, at 13,000 ft altitude, sufficient to fail some component of the center tank. This was a precursor event leading to serious consequences. The analysis supports a hypothesis of overpressure as the cause of the Trans World Airlines Flight 800 accident and shows that heating caused by air conditioning contributed to the sequence of events.
引用
收藏
页码:828 / 834
页数:7
相关论文
共 50 条
  • [41] Characteristics of stable oxygen concentration in aircraft fuel tank catalytic inerting system
    Shao L.
    Yang W.
    Zeng X.
    Hu H.
    Chen Q.
    Peng Y.
    He J.
    [J]. Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2023, 55 (04): : 56 - 63
  • [42] Modeling of fuel in aircraft crashworthiness study with auxiliary fuel tank
    Bin Rayhan, Saiaf
    Pu, Xue
    Xi, Huilong
    [J]. INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2023, 173
  • [43] Tracking Performance Analysis of a Distributed Recoverable Boeing 747 Flight Control System Subject to Digital Upsets
    Gray, W. Steven
    Wang, Rui
    Gonzalez, Oscar R.
    Chavez-Fuentes, Jorge R.
    [J]. 2010 AMERICAN CONTROL CONFERENCE, 2010, : 548 - 554
  • [44] Directly measured cabin pressure conditions during Boeing 747-400 commercial aircraft flights
    Kelly, Paul T.
    Seccombe, Leigh M.
    Rogers, Peter G.
    Peters, Matthew J.
    [J]. RESPIROLOGY, 2007, 12 (04) : 511 - 515
  • [45] Analysis of Boeing 737 aircraft towing accidents
    Chen, Shu-wen
    Liu, Hui
    Li, Fu-hai
    [J]. ENGINEERING FAILURE ANALYSIS, 2017, 80 : 234 - 240
  • [46] Multifunctional fuel cell system in an aircraft environment: An investigation focusing on fuel tank inerting and water generation
    Keim, Martin
    Kallo, Josef
    Friedrich, K. Andreas
    Werner, Claudia
    Saballus, Martin
    Gores, Florian
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 29 (01) : 330 - 338
  • [47] Analysis of inerting index when inerting capability of aircraft fuel tank was degraded
    Lü X.
    Yao S.
    Du M.
    [J]. Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (05): : 1067 - 1074
  • [48] Analysis on oxygen volume fraction control index in aircraft fuel tank inerting
    Zhou P.
    Liu W.
    Liu W.
    [J]. Liu, Weihua (liuwh@nuaa.edu.cn), 1856, Beijing University of Aeronautics and Astronautics (BUAA) (35): : 1856 - 1865
  • [49] Design Bionic Structure and Analysis of Kinematics for Aircraft Fuel Tank Inspection Robot
    Gao, Qingji
    Wang, Weijuan
    Niu, Guochen
    [J]. ADVANCES IN MECHATRONICS AND CONTROL ENGINEERING, PTS 1-3, 2013, 278-280 : 594 - 598
  • [50] Computational Tool for Aircraft Fuel System Analysis
    Department of Aeronautics Engineering, University of São Paulo - USP, São Carlos, São Paulo, Brazil
    不详
    不详
    14813-000, Brazil
    [J]. 1600,