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Towards the Enhancement of Aircraft Cargo Compartment

Towards the Enhancement of Aircraft Cargo Compartment Fire Detection System Certification using Smoke Transport Modeling Walt Gill and Jill Suo-Anttila Fire Science and Technology Department Sandia National Laboratories Albuquerque, NM David Blake Fire Safety Section FAA Technical Center

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Towards the Enhancement of Aircraft Cargo Compartment

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  1. Towards the Enhancement of Aircraft Cargo Compartment Fire Detection System Certification using Smoke Transport Modeling Walt Gill and Jill Suo-Anttila Fire Science and Technology Department Sandia National Laboratories Albuquerque, NM David Blake Fire Safety Section FAA Technical Center International Fire and Cabin Safety Research Conference November 2004 Sandia is a multi-program laboratory operated by Sandia Corporation, a Lockheed-Martin Company, for the United States Department of Energy under Contract DE-AC04-94AL85000.

  2. Experimental David Blake, Walt Gill, and Jill Suo-Anttila Model Development Jim Nelsen and Stefan Domino Graphical User Interface and Code Development Carlos Gallegos Technical Support Louis Gritzo, manager of the Fire Science and Technology Department Sandia National Laboratories Team Members

  3. Airlines, Air-Framers, Certifiers Robust and fast running Validated using FAA experiments Built on firm FAA knowledge base Modeling Smoke Transport in Aircraft Cargo Compartments • Goal: Develop a CFD-based simulation tool to predict smoke transport in cargo compartments • Improve the certification process • Identify optimum smoke detector locations • Specify sensor alarm levels • Identify most challenging fire locations • Reduce the number of flight tests • Fast running • Suitable for non-expert users • Experimental data for source term characterization from FAA experiments • Validated using FAA full-scale experiments

  4. Pre-Processor Analysis Module Post-Processor Software Design Graphical User Interface

  5. Pre-Processor Overview • Provide models for different aircraft • Boeing 707, 727, 747, etc. • User defined • Capabilities • Refine mesh • Enter fire(s) location and type • Enter ventilation velocities and locations • Enter compartment temperature and pressure • Add obstacles and recessed areas • Instantaneous visual feedback

  6. custom 707 or DC-10 Running a Simulation Compartment and Mesh Specification • Execute the Pre-Processor • Select the type of compartment • 707 • DC-10 • User Defined • Input the dimensions • Enter the mesh size - # of nodes

  7. Running a Simulation Created 707 and DC-10 Meshes • Automatically generated DC-10 mesh • Internal view of compartment • Automatically generated 707 mesh • Curvature captured by mesh • Right side of screen shows selected plane

  8. 1 3 2 Running a Simulation Recessed Area Specification • Advance to selected Y-plane • Select desired cells • Perform operation using buttons

  9. Recessed Area Obstacle Running a Simulation Obstacle Specification

  10. 2 Outlet 1 3 Fire Inlet Running a Simulation Ventilation and Fire Specification • Select cells • Enter type of cell (inlet, outlet, fire) – cell colored to denote type • Use table to enter ventilation properties • Fire properties in file

  11. 2 1 3 Running a Simulation Mesh Refinement Specification • Select the plane for refinement • Use refinement tool • Enter level of refinement Resulting Grid

  12. Running a Simulation Running the Analysis Code • Analysis - - - Run Analysis • Status monitored on screen

  13. Temp (K) computational grid cell on wall Smoke Transport Analysis Code • Curvature of compartment is resolved on grid • HRR, MLR are time varying inputs (as measured in FAA experiments) • Species tracking: presently soot, CO, and CO2 but addition of more or different species possible • Simulation time = 1 hour per minute of real time • Validated using FAA full-scale experiments

  14. Post-Processor • Allow users to manipulate data in a variety of ways • contour plots • time history of field variables • 3D smoke visualization in time

  15. Thermocouple temperature rise 0 - 60 seconds 0 -120 seconds 0 -180 seconds Light transmission 30 and 45 sec (ceiling and vertical) 60 sec (vertical - high, mid, low) 120 sec (vertical - mid and low) 180 sec (vertical - mid and low) Gas species concentration rises 0 - 60 seconds 0 -120 seconds 0 -180 seconds Code Validation Metrics Experimental ceiling temperature distribution at 60 sec Insert most recent movie of temperature distribution Computational temperature distribution at 60 sec

  16. 707 experiments completed Baseline – center fire Attached – sidewall fire Corner – corner fire Determined leakage ventilation had no impact on data All 707 experiments were conducted without ventilation DC-10 experiments Ventilation validation Status of FAA Full-Scale Validation Experiments Insert most recent movie of temperature distribution

  17. Interface described used to create mesh and run simulation Results and comparisons follow 707 Validation Simulations Insert most recent movie of temperature distribution Internal view (showing fire and recessed areas) of 707 computational domain 707 Baseline computational mesh

  18. Preliminary Validation – Temperature • Baseline 707 experiments • center fire • 40 thermocouples • Model including heat transfer to the ceiling and walls • h=7 W/m2K in model • Comparison • Trends captured • Magnitudes predicted away from fire • Magnitudes agree above fire better at early times Insert most recent movie of temperature distribution

  19. Preliminary Validation – Light Transmission • Baseline 707 experiments • center fire • 6 smoke meters • Comparison • Good agreement in trends and magnitudes Insert most recent movie of temperature distribution

  20. Future Activities • Continue validation of the smoke transport code • Finish code modifications • 707 validation comparisons • DC-10 validation comparison • Release of code to small user community • Includes theory and users manual • Tutorial at FCS conference • Revisions and final release of code (Summer ’05)

  21. The Fourth Triennial International Aircraft Fire and Cabin Safety Research Conference

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