Fire Suppression in Class-E Cargo Compartments · Fire Suppression in Class E Cargo Compartments...

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Federal Aviation Administration 1 Fire Suppression in Class E Cargo Compartments November 2012 Fire Suppression in Class-E Cargo Compartments Presentation By: Fire Safety Team: ANG-E211 F.A.A. William J. Hughes Technical Center Atlantic City Int’l Airport, NJ

Transcript of Fire Suppression in Class-E Cargo Compartments · Fire Suppression in Class E Cargo Compartments...

Page 1: Fire Suppression in Class-E Cargo Compartments · Fire Suppression in Class E Cargo Compartments ... • Zone based Water mist ... Fire Suppression in Class E Cargo Compartments

Federal Aviation Administration

1 Fire Suppression in Class E Cargo Compartments

November 2012

Fire Suppression in Class-E Cargo Compartments

Presentation By:

Fire Safety Team: ANG-E211

F.A.A. William J. Hughes Technical Center

Atlantic City Int’l Airport, NJ

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Federal Aviation Administration

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November 2012

Objective

Test a variety of Fire Suppression Options

• Oxygen Starvation

• Aerosol based agents

• Fire Containment Covers (FCC)

• Medium Expansion Foams

• Zone based Water mist systems

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Federal Aviation Administration

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November 2012

Test Article

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Federal Aviation Administration

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Federal Aviation Administration

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Composite Test Article

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Federal Aviation Administration

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Tests Conducted

Test Container Composite Container

Full Load Half load Full Load Half Load

Oxygen Starvation X X X X

Aerosol Based Suppression Agent

X X X X

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Federal Aviation Administration

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Test Procedure: Oxygen Starvation

• The air exchange rates of each container was measured prior to testing.

• Ignition box was lit in the front left corner of the container. (Worst case scenario)

• Observe ceiling temperatures and oxygen concentration over a period of 4 hours.

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Federal Aviation Administration

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November 2012

Test Procedure: Aerosol Suppression

• Ignition box was lit in the front left corner of the container. (Worst case scenario)

• The agent was triggered manually when the internal ceiling temperature reached 200°F. (Failure point in a Lexan based AAY)

• Observe ceiling temperatures and oxygen concentration over a period of 4 hours.

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Federal Aviation Administration

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November 2012

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Federal Aviation Administration

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Observations: Oxygen Starvation

• Air exchange rates in the test and composite container were approximately 26 cfm and 5 cfm respectively.

• Temperatures within the test container suggest failure.

• Test container also shows an upper bound of air exchange rate at which oxygen starvation could starve a fire.

• The composite container effectively deprived the fire while being able to withstand the initial surge in high temperatures.

• There was a flashover in the composite container once the doors were opened at the end of the test.

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Federal Aviation Administration

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Federal Aviation Administration

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Observations: Aerosol suppression

• The aerosol agent in combination with oxygen starvation successfully suppressed the fire.

• ~85% of the boxes were undamaged.

• There was no flashover at the end of the test.

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Federal Aviation Administration

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Federal Aviation Administration

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Significance of Fire Suppression in Tandem with Oxygen Starvation

• The agent extinguishes the fire in the container.

• Oxygen starvation allows the aerosol to remain within the container to maintain an inert environment.

• There is a smaller probability of a flashover when the container is opened.

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Federal Aviation Administration

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Fire Containment Covers

Test Setup • 114 cardboard boxes

filled with 2.5 lbs of shredded paper used as fire load.

Test Criteria • Test will be considered

a failure if any thermocouple placed 4” away from the FCC exceeds 400°F

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Federal Aviation Administration

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Federal Aviation Administration

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Federal Aviation Administration

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Federal Aviation Administration

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Observations: FCC

• Both FCC covers failed to the standards of ISO 14186.

• The FCCs were able to contain the fire within itself.

• The FCCs displayed a behavior that was explained as “offgassing”. When the temperature inside the FCC rose, the material on the FCC decomposed to release a gas that spontaneously combusted on the external surface of the FCC. This did not affect the performance of the cover, but could lead to failing the ISO standard.

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Federal Aviation Administration

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Medium Expansion Foam

Objective:

• To determine the expansion ratio of ANSUL foam with and without using a medium foam expansion nozzle.

• To obtain the same expansion ration as mentioned above without using the nozzle and using an inert gas to drive the foam.

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Federal Aviation Administration

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Medium Expansion Foam: Setup

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Federal Aviation Administration

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Zone Based Water Mist System

Objective:

• To determine the effectiveness of a water mist system as a viable fire suppression system in a Class-E cargo deck.

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Federal Aviation Administration

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Zone Based Water Mist System

• The DC-10 cargo deck has been rebuilt to perform fire testing within.

• Ducting systems are being installed to replicate air exchange rates similar to a real world scenario.

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Federal Aviation Administration

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Future Work

• Conduct tests to determine a worst case scenario fire load that contains lithium batteries.

• Conduct tests with medium expansion foam driven by an inert gas in the test container.

• Conduct tests with zone based water mist systems on a standard fire load and on lithium battery fires in the main cargo deck.