Ground Based Fuel Tank Inerting - PowerPoint PPT Presentation

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Ground Based Fuel Tank Inerting

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Quiescent Full-Scale Testing has Indicated that Inerting of the B-747 SP in the ... Three Proposed Concepts, then Design and Fabricate a Part for Kit Installation ... – PowerPoint PPT presentation

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Title: Ground Based Fuel Tank Inerting


1
An Overview of FAA Fuel Inerting Research
March 12th-13th, 2002International Systems Fire
Protection Working GroupSeattle, Washington
2
Vertical Mixing / Temperature Effects
  • Quiescent Full-Scale Testing has Indicated that
    Inerting of the B-747 SP in the Optimal Deposit
    Method Developed with the Plywood Model can be
    Problematic
  • Inerting Efficiency Different from Test to Test
  • Measured Strong Vertical Effects in one Full
    Length Bay
  • Bottom of Bay Lags Behind Top of Bay on Most
    Tests
  • Complicated by the Fact that Sample System only
    Samples from Top
  • Observed Stratification of Inert Gas at Least
    Once with No Temperature Variation Between the
    Inert Gas and the Ullage
  • Developed Deposit Gas Heat Exchanger to Study
    Temperature Effects
  • Developed Inerting Efficiency Coefficient to
    Compare Tests
  • Back Calculate VTEs between 1.2 and 2.0 to reach
    8 O2 with 95

3
Full-Scale B-747 SP Inerting Data
4
Inerting Efficiency
  • Due to Sample Lag Dont have a Good Picture of
    Inerting in the Tank During Test
  • Sample Biased Due to Location of Sample Ports
  • Know Beginning Point (20.9) and End Point After
    Run ACMs
  • Want to Approximate the Progression of Tank
    Oxygen Concentration During the Testing
  • Use Generic Inerting Equation to Develop
    Efficiency Factor K
  • Solve for K and Redimensionalize to Get a Curve
    for Each Test Result
  • Did Several Tests with Different Temperature NEA

5
Full-Scale B-747 SP Inerting Data
6
Ancillary Equipment Development
  • Cross-Flow Reduction Device
  • Wrote and Distributed RFQ to Qualified
    Contractors for Developing a Cross-Flow Reduction
    Device for a B-747 SP
  • Three Phase Development to Optimize One of Three
    Proposed Concepts, then Design and Fabricate a
    Part for Kit Installation
  • OBGI Deposit System
  • FAA Developing a Method for Distributing the OBGI
    System Gas by Using Scale Plywood Tank Testing
  • RFQ for Development and Prototype in mid March

7
Flammability Survey of B-747 SP
  • Measured Heating and Flammability Parameters in
    CWT of Full-Scale Test Article During Typical
    Ground Operation with Low Fuel
  • Inert Tank Before Each Ground Sit (During Test)
  • Target Different Temperature Days (Relatively
    Constant Ambient Temperature) with Mild Weather
  • Run ACMs for 3 Hours to Make Cabin Comfortable
  • Thermocouples in Pack Bay, Ullage, and Fuel (and
    Sump) as well as On Walls, Floor, and Ceiling
  • All Data Obtained on Cool and Warm Days
  • Need Heat of Summer and Cold of Winter Data

8
B-747 SP Flammability Data
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