WJH FAA Technical Center John W. Reinhardt

Slides:



Advertisements
Similar presentations
Subcontractor Electrical Safety & NFPA 70E
Advertisements

1. 2 Earthquake effects on health care facilities 2.
Halon Replacement for Airplane Cargo Compartments What it Takes Fourth Triennial International Fire and Cabin Safety Research Conference Lisbon, Portugal.
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center
Cargo Compartment Minimum Performance Standards for Gaseous Total Flood Agents FAA Technical Center Fire Safety Section, AAR-422 John Reinhardt Website:
BRIEF OVER VIEW OF THE MINIMUM PERFORMANCE STANDARD FOR ENGINES describes geometry for a fixture loosely representing an aircraft engine nacelle describes.
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration.
Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, AAR-440 Bldg.
Recent Simulator Activity Baseline Testing –Fire testing performed during the first week of May 2000 –Agent testing performed during the third and fourth.
R.G.W. Cherry & Associates Limited International Aircraft Fire and Cabin Safety Research Conference Slide 1 – Lisbon November 2004 International Aircraft.
DEVELOPMENT OF A MINIMUM PERFORMANCE STANDARD FOR HAND HELD FIRE EXTINGUISHERS AS A REPLACEMENT FOR HALON 1211 ON CIVILIAN TRANSPORT CATEGORY AIRCRAFT.
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration.
WJH FAA Technical Center John W. Reinhardt
Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, AAR-440 Bldg.
NexGen Burner Update International Aircraft Materials Fire Test Working Group Meeting October 21, 2009 Atlantic City, NJ.
DRI THE DEVELOPMENT OF DITCHING and WATER IMPACT DESIGN LIMITS PRESENTED AT INT’L CABIN SAFETY CONFERENCE NOVEMBER 15-17, 2004 LISBON, PORTUGAL DYNAMIC.
William Cavage AAR-440 Fire Safety Branch Wm. J
Student Book © 2004 Propane Education & Research CouncilPage Placing Appliances into Initial Operation Knowing the proper techniques and.
Program: Respiratory Therapy Course: Introduction to Respiratory Sciences Lesson: Gas Physics Handle Gas Cylinders With Care.
© Siemens Industry, Inc Confidential / Drive Your Business Forward Ignite the Power of New Products and Partnerships Siemens Fire Partner Summit.
Contact: Drift from boom sprayers 1. PDPA laser based droplet characterisation To measure and.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Task Group Session on Revised.
Jet-A Vaporization In an Experimental Tank Part II: Experimental Results at Atmospheric and Sub-Atmospheric Pressures Robert Ian Ochs Rutgers, The State.
N.F.P.A. 13R Justin Bohlmann FIR-204.
DOH Survey Citation Update; What’s New, What’s Hot, What’s Not!
Cargo Bay Fire Protection with a Fuel Tank Inerting System William Cavage AAR-440 Fire Safety Branch Wm. J. Hughes Technical Center Federal Aviation Administration.
Mr. D. Cannoletta - Environmental Control System Department Mr. E. Riegel - Environmental Control System Department ENVIRONMENTAL CONTROL SYSTEM CABIN.
Standard for the Organization and Deployment of Fire Suppression Operations, Emergency Medical Operations, and Special Operations to the Public by.
Interstate Aviation Committee IAC’s Approach to Development of the Global Design Code.
Class C Cargo Compartment ULD Suppression Agent Penetration Test
Integration of Hydronic Thermal Transport Systems with Fire Suppression Systems ASHRAE Winter Meeting 2001 WALTER M. JANUS, PE URS Corp., Washington, DC.
FIREPROOF AND FIRE RESISTANT MATERIALS Federal Aviation Administration Project Manager: J. Reinhardt William J. Hughes Technical Center Airport and Aircraft.
Engine Nacelle Halon Replacement, FAA WJ Hughes Technical Center Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration.
Fuel Tank Inerting Joint Airbus/FAA, A320 Flight Tests
Full Scale Battery Fire Test Plan
Federal Aviation Administration RTCA Update 0 RTCA Update Federal Aviation Administration International Aircraft Materials Fire Test Working Group Bremen,
John Reinhardt FAA Fire Safety Section, AAR-422. BULK LOAD FIRESCONTAINERIZED FIRES FLAMMABLE LIQUIDS FIRE AEROSOL CAN EXPLOSION SIMULATION “Minimum Performance.
ALTERNATIVE AGENT UPDATE Louise C. Speitel Fire Safety Branch AAR-440 FAA W.J. Hughes Technical Center Atlantic City International Airport, NJ
Federal Aviation Administration Status of Research & Testing to Replace Halon Extinguishing Agents in Civil Aviation Fire Safety Team FAA Wm. J. Hughes.
Presented to: International Aircraft Systems Fire Protection Working Group. Atlantic City, NJ By: Dave Blake. FAA Technical Center. Atlantic City, NJ.
3M™ Novec 1230™ Fire Protection Fluid
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration.
Federal Aviation Administration Aircraft Ducting 0 Federal Aviation Administration International Aircraft Materials Fire Test Working Group Savannah, GA.
Cargo Bay Fire Protection with a Fuel Tank Inerting System
Federal Aviation Administration Halon 1211 Stratification/ Localization in Aircraft Louise Speitel Fire Safety Branch FAA Wm. J. Hughes Technical Center.
Jet Fuel Vaporization and Condensation: Modeling and Validation Robert Ochs and C.E. Polymeropoulos Rutgers, The State University of New Jersey International.
Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, ATO-P (formerly.
Presentation to Transport Canada November 2008 – Fire & Cabin Safety Research Integrated Fire Protection Systems – Update.
Halon Contamination SIB R1 Deletain Rémi Powerplant Installation & Fuel Systems Certification Directorate Novembre 2011.
Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, AAR-440 Bldg.
Chapter 8 Final Construction Final construction in the SDLC Construct and test programs Construct and test the database Obtain additional hardware Prepare.
October 30-31, 2002 International Aircraft Systems Fire Protection Working Group Atlantic City, NJ Inerting of a Scale 747SP Center Wing Fuel Tank During.
Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, AJP6320 Bldg.
CERN: The ATRAP Experiment. Preview Overview of the ATRAP Experiment  History  Ongoing work  Goals Presentation of my jobs and projects.
Federal Aviation Administration Status of Research & Testing to Replace Halon Extinguishing Agents in Civil Aviation Douglas Ingerson Louise Speitel Constantine.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Task Group Session on Revised.
MULTI-COMPONENT FUEL VAPORIZATION IN A SIMULATED AIRCRAFT FUEL TANK C. E. Polymeropoulos Department of Mechanical and Aerospace Engineering, Rutgers University.
R.G.W. Cherry & Associates Limited #1 INTERNATIONAL AIRCRAFT SYSTEMS FIRE PROTECTION WORKING GROUP MEETING AN INTEGRATED FIRE PROTECTION SYSTEM.
Aircraft Cargo Compartment Fire Detector Certification. David Blake FAA Technical Center Atlantic City, NJ 3 rd Triennial International Fire and Cabin.
Hot /Cold Aisle Containment  Traditional Data Center/Telco designs are changing significantly!
Presented by John Lewandowski and Mike Larabel Inspection, Testing, and Maintenance of Kitchen Hood Systems Michigan Fire Inspectors Society Winter Educational.
Presented to: By: Date: Federal Aviation Administration Engine Nacelle Halon Replacement International Aircraft Systems Fire Protection Working Group Douglas.
Carbon Dioxide System Design
David Blake FAA Technical Center Atlantic City Airport, NJ Phone: International Aircraft Systems Fire.
Presented to: International Aircraft Materials Fire Test Working Group By: Robert Ochs Date: Wednesday, October 21, 2009 Federal Aviation Administration.
Water Mist Systems Chapter 6. Objectives Evaluate water mist as a potential halon replacement Discuss the applications for water mist systems Compare.
Protecting your Energy Storage System
Presented by Harry C. Elinsky, Jr. Filtech, Inc.
Decree of the Ministry of Interior 3rd August 2015 The “so called” Italian Fire Prevention Code - IFC: S6 – Fire Control and Suppression provisions.
ADVANCED FIRE PROTECTION DELUGE SYSTEM (AFPDS)
Presentation transcript:

WJH FAA Technical Center John W. Reinhardt Fire Safety Section, AAR-440 Atlantic City Int’l Airport, New Jersey 08405 609.485.5034

OBJECTIVES To determine the critical parameters required to scale a water mist system combined with nitrogen, used as an aircraft cargo compartment fire suppression system that have met the MPS.

CONSIDERATION The scaling consideration of the water mist/N2 fire extinguishing system is for cargo compartments of volume sizes of 719 ft3 (298 in x 125 in x 42 in) and 6252 ft3 (590 in x 164 in x 80 in).

ADOPT NFPA 750 – STANDARD ON WATER MIST FIRE PROTECTION SYSTEMS This NFPA document was prepared by the Technical Committee on Water Mist Fire Suppression Systems and acted on by the National Fire Protection Association, Inc. on November 1999. It was issued by the Standards Council on January 2000, with an effective date of February 11, 2000 In developing this standard, the committee addressed system components and hardware, system types, installation requirements, design objectives, hazard classifications, calculations, water supplies, atomizing media, plans, documentation, acceptance criteria, and maintenance considerations NFPA 750 represents a significant advancement in water mist technology and the knowledge base associated with its application.

SCALING APPROACH Characterize the WMS/N2 system that passed the MPS tests using the NFPA 750 standard and other techniques Use defined system parameters and transpose them to different scale cargo compartment, paying close attention to the vertical plane (z-axis). Adjust system as needed in scaled compartment to provide same critical parameters values.

CHARACTERIZATION OF WATER MIST NFPA 750 Section A-5-2 (Appendix A) System Flow Rate System Operating Pressure General Water Requirements Nozzle Characteristics Nozzle Spray Characteristics Nozzle Installation Parameters Activation Device General Design Parameters

CHARACTERIZATION OF WATER MIST (CONT.) NFPA 750 Section A-2-6.1 (Appendix A) Will characterize FAA’s WMS/N2 system using the recommended method to determine the cumulative volumetric distribution of water droplets NFPA 750 Section B-1 (Appendix B – Water Mist Droplet Size Characterization and Measurement) If the equipment is available, will characterize FAA’s WMS/N2 system using one of the following techniques: optical imaging, diffraction, or Doppler refraction (Sauter Mean Diameter, Dv0.10).

CHARACTERIZATION OF WATER MIST (CONT.) Water collection (mass flow) on a 18” by 18” pan located on the fire zone at 36” above the cargo compartment floor in order to determine water availability.

NITROGEN MEASUREMENT The measurement of the nitrogen volumetric concentration, in the scaled cargo compartment, will be achieved by determining the oxygen volumetric concentration in the hypoxic condition (using gas analyzers). COMPUTER MODELING Task group member recommended usage of computer modeling techniques to facilitate scaling analysis using critical characterized parameters. It may be used If provided by task group member.

STATUS The characterization of the FAA’s WMS/N2 has been initiated using the NFPA 750 standard. Test fixtures to determine water mass in the fire zone is under construction Searching for a Phase Doppler Particle Analyzer or similar equipment to measure particle size distribution and velocity of the mist on the fire zone. Anyone who owns one and is willing to share the equipment please contact John Reinhardt at 609-485-5034 or john.reinhardt@faa.gov