Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, AJP6320 Bldg.

Slides:



Advertisements
Similar presentations
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center
Advertisements

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.
1 Simulator Status, FAA WJ Hughes Technical Center Completed since the April 1999, Seattle meeting : –Simulator Inlet : A 22 foot long, 22 inch diameter.
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.
WJH FAA Technical Center John W. Reinhardt
William Cavage AAR-440 Fire Safety Branch Wm. J
IASFPWG – Seattle, WA Fuel Tank Ignition Experiments at Reduced Oxygen Concentrations International Aircraft Systems Fire Protection Working Group.
Advanced Thermodynamics Note 6 Applications of Thermodynamics to Flow Processes Lecturer: 郭修伯.
Jet-A Vaporization In an Experimental Tank Part II: Experimental Results at Atmospheric and Sub-Atmospheric Pressures Robert Ian Ochs Rutgers, The State.
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.
Limiting Oxygen Concentration of Aviation Fuels Federal Aviation Administration 0 0 Limiting Oxygen Concentration of Aviation Fuels Steve Summer Project.
An Update on FAA Fuel Tank Ullage Modeling
Presented to: International Aircraft Systems Fire Protection Working Group By: Date: April 2-3, 2008 Federal Aviation Administration Next-Generation Oil.
Class C Cargo Compartment ULD Suppression Agent Penetration Test
Aircraft Cargo Compartment Fire Detection David Blake FAA William J. Hughes Technical Center Atlantic City Airport, NJ Phone:
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.
NFPA 31 Standard for the installation of Oil- Burning Equipment
Federal Aviation Administration Burnthrough Update International Aircraft Materials Fire Test Working Group Meeting June 17, 2009 Köln, Germany.
Federal Aviation Administration Federal Aviation Administration 1 Presentation to: Name: Date: Federal Aviation Administration AMHS Security Security Sub-Group.
Federal Aviation Administration 0 Composite Wing Tank Flammability April 2-3, Composite and Aluminum Wing Tank Flammability Comparison Testing Steve.
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.
FAA R&D Efforts Leading to Fuel Tank Inerting
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
Presented to: By: Date: Federal Aviation Administration Forced-flow Fire Testing with “cold”-soaked FK International Aircraft Systems Fire Protection.
Federal Aviation Administration Handheld Advisory Circular Update Louise Speitel Fire Safety Branch FAA Wm. J. Hughes Technical Center Atlantic City International.
Presented to: By: Date: Federal Aviation Administration Burnthrough Test Method for Aircraft Thermal/Acoustic Insulation: Burner Replacement Investigation.
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration.
Federal Aviation Administration Measuring Ullage Oxygen Concentration November 17-18, Measuring Oxygen Concentration in a Fuel Tank Ullage Federal.
Reticulated Foam Advantages: 100% protection Passive System
IAMFTWG March 1-2, 2011 – Savannah, GA, USA Robert I. Ochs, FAA Fire Safety Team AJP-6322 Federal Aviation Administration Burnthrough and NexGen Burner.
Presented to: IAMFTWG, Renton, WA By: Robert Ochs Date: March 3, 2010 Federal Aviation Administration NexGen Burner for Seat Cushion Fire Testing.
Federal Aviation Administration Aircraft Ducting 0 Federal Aviation Administration International Aircraft Materials Fire Test Working Group Savannah, GA.
Background Numerous FAR’s mandate fire protection in aircraft powerplant fire zones Parts 23, 25, 27, 29, 33… FAR Part 1 Section 1.1 – Definitions and.
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.
Federal Aviation Administration 0 Composite Wing Tank Flammability November 20, Composite and Aluminum Wing Tank Flammability Comparison Testing.
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.
OBIGGS Sizing Data for Transport Canada Trade Study William Cavage AAR-440 Fire Safety Branch Wm. J. Hughes Technical Center Federal Aviation Administration.
Modeling Smoke Transport in Aircraft Cargo Compartments Jill Suo-Anttila ‡, Stefan Domino †, Walt Gill ‡, Paul DesJardin ‡, and Lou Gritzo ‡ ‡ Fire Science.
Presentation to Transport Canada November 2008 – Fire & Cabin Safety Research Integrated Fire Protection Systems – Update.
Federal Aviation Administration Wiring Test 0 Federal Aviation Administration Pat Cahill AJP-632; Fire Safety Team Wm. J. Hughes Technical Center Federal.
Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, AAR-440 Bldg.
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration.
October 30-31, 2002 International Aircraft Systems Fire Protection Working Group Atlantic City, NJ Inerting of a Scale 747SP Center Wing Fuel Tank During.
Federal Aviation Administration 0 Composite Wing Tank Flammability May 19 th, Composite and Aluminum Wing Tank Flammability Comparison Testing Steve.
Federal Aviation Administration 0 Composite Wing Tank Flammability May 20, Composite and Aluminum Wing Tank Flammability Comparison Testing Steve.
Federal Aviation Administration Status of Research & Testing to Replace Halon Extinguishing Agents in Civil Aviation Douglas Ingerson Louise Speitel Constantine.
MULTI-COMPONENT FUEL VAPORIZATION IN A SIMULATED AIRCRAFT FUEL TANK C. E. Polymeropoulos Department of Mechanical and Aerospace Engineering, Rutgers University.
IASFPWG – Atlantic City, NJ Limiting Oxygen Concentration (LOC) Work Update International Aircraft Systems Fire Protection Working Group Atlantic.
Federal Aviation Administration Slide Evacuation Test Method TSO C69A 0 Slide Evacuation Test Method TSO C69A Federal Aviation Administration International.
Presented to: By: Date: Federal Aviation Administration Engine Nacelle Halon Replacement International Aircraft Systems Fire Protection Working Group Mr.
David Blake FAA Technical Center Atlantic City Airport, NJ Phone: International Aircraft Systems Fire Protection.
Presented to: International Aircraft Systems Fire Protection Working Group. London, UK By: Dave Blake. FAA Technical Center. Atlantic City, NJ.
Engine Nacelle Halon Replacement, FAA, WJ Hughes Technical Center Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration.
Presented to: By: Date: Federal Aviation Administration Engine Nacelle Halon Replacement International Aircraft Systems Fire Protection Working Group Douglas.
IASFPWG – Atlantic City, NJ Nitrogen Inerting Requirements – A Lit. Review International Aircraft Systems Fire Protection Working Group Atlantic.
RETROFIT OPPORTUNITY FOR HFC-125 IN AIRCRAFT ENGINE SYSTEMS Presented 19 November 1998 to: The International Aircraft Fire and Cabin Safety Research Conference.
Wing Tank Flammability Testing William Cavage Steven Summer AAR-440 Fire Safety Branch Wm. J. Hughes Technical Center Federal Aviation Administration International.
Federal Aviation Administration Aircraft Ducting 0 Federal Aviation Administration International Aircraft Materials Fire Test Working Group Atlantic City,
Steve Griffith February 28th, 2017
Component Availability Effects
Presentation transcript:

Point of Contact :Doug Ingerson Department of Transportation Federal Aviation Administration WJ Hughes Technical Center Fire Safety Branch, AJP6320 Bldg 205 Atlantic City Int'l Airport, NJ USA tel: fax: web page: Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 Engine Nacelle Halon Replacement

Slide #2 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 PRESENTATION CONTENTS  REVIEW EQUIVALENCE DATA TO DATE  HFC-125 SIMULATION  MINIMUM PERFORMANCE STANDARD TESTING - NOVEC 1230  DISCUSS STATUS

Slide #3 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 REVIEWING EQUIVALENCE DATA TO DATE Agent Ventilation configuration Fire Threat Equivalent Concentration (%v/v) HFC-125 High JP8 spray17.5 JP8 pool7.6 Low OIL spray16.4 (a) JP8 pool8.1 (a) CF3I High JP8 spray5.6 JP8 poolIncomplete Low OIL spray7.2 (a, b) JP8 poolIncomplete (a) Bracketing method used to find mass equivalent (b) Partial result, JP8 verification incomplete as of November 2005

Slide #4 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 REVIEWING EQUIVALENCE DATA TO DATE AgentFuel Peak, Critical or Design Concentration (%v/v) REFERENCE CF3I PROPANE6.5 (p)NFPA 2001, TABLE A JP8 SPRAY3.2 (c)NIST SP890, V.2, TBL 10, p.115 JP8 POOL6.8 (c)NIST SP890, V.2, TBL 10, p.115 OIL7.2 (d)FAATC; none; work in progress... HFC-125 METHANE14.7 (p)NFPA 2001, TABLE A PROPANE15.7 (p)NFPA 2001, TABLE A PROPANE  12.6 (p) NIST SP890, V.2, FIG. 41, p.78 JP8 SPRAY8.7 (c)NIST SP890, V.2, TBL 10, p.115 JP8 POOL12 (c)NIST SP890, V.2, TBL 10, p.115 JP8 SPRAY, LoVent25.4 (d)AFRL-VA-WP-TR JP8 SPRAY, HiVent18.2 (d)AFRL-VA-WP-TR JP817.5 (d)FAATC; none; work in progress... OTHER REPORTED or CALCULATED CONCENTRATIONS

Slide #5 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006  HFC-125 CAN SIMULATE THE DISTRIBUTION OF HALON 1301 IN ENGINE NACELLE COMPARTMENTS  TECHNICAL NOTE PUBLISHED  DOT/FAA/AR-TN99/64, “Simulating the Distribution of Halon 1301 in an Aircraft Engine Nacelle With HFC-125”  INCLUDES BIBLIOGRAPHICAL REFERENCES  EXPLAINING THE PHYSICAL REASONING  TEST CASES  ADDITIONAL TEST CASE INCLUDED  DESCRIBES PROCEDURE TO UTILIZE THIS SIMULATION  TECH NOTE DID NOT ADDRESS AGENT STORAGE TEMPERATURE FOR COLD SOAK EVALUATION DURING CERTIFICATION TESTING  JAKOB (Ja) NUMBER USED TO ADDRESS THIS SHORTFALL HFC-125 SIMULATION

Slide #6 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006  JAKOB (Ja) NUMBER (1) :  A MEASURE OF THE FRACTION OF A LIQUID THAT FLASHES TO VAPOR WHEN DEPRESSURIZED INSTANEOUSLY  Ja IS A RATIO OF :  THE DIFFERENCE IN ENTHALPY OF A LIQUID BETWEEN ITS NORMAL BOILING POINT & “AMBIENT” TEMPERATURE  HEAT OF VAPORIZATION AT THE NORMAL BOILING POINT  IN LIEU OF EVALUATING THE HEAT CAPACITY BY INTEGRATION, THE NUMERATOR CAN BE DETERMINED BY THERMODYNAMIC TABLE (1) Womeldorf, C.A. & Grosshandler, W.L., “Fire Suppression System Performance of Alternative Agents in Aircraft Engine & Dry Bay Laboratory Simulations”, NIST SP890, November 1995, Vol. 2, p.591 HFC-125 SIMULATION

Slide #7 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006  TO MATCH THE HFC-125 TEMPERATURE TO -65°F (-54°C) HALON 1301  DETERMINE Ja OF HALON 1301 AT “AMBIENT” = -65°F (-54°C)  INSTANT DEPRESSURIZATION OCCURS WITHIN PLUMBING  PLUMBING WILL TEND TOWARD THE AGENT STORAGE TEMPERATURE  USE THIS Ja AND SOLVE FOR THE PROPER HFC-125 STORAGE TEMPERATURE  THERMODYNAMIC INFORMATION IS AVAILABLE FROM THE MANUFACTURER (DuPONT)  REMAINING PORTIONS OF THE SIMULATION PROTOCOL SHOULD BE FOLLOWED  FILL THE HALON 1301 BOTTLE WITH A MASS OF HFC-125 = 77% OF THE HALON MASS  CAPTURE THE GAS DISTRIBUTION TEST AS AN HFC-125 TEST  EVALUATE THE HFC-125 BEHAVIOR AS YOU WOULD HALON 1301 HFC-125 SIMULATION

Slide #8 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 HFC-125 SIMULATION  EXAMPLES FOR USING HFC-125 AS A SIMULANT AND OBTAINING APPROVAL FOR THE HALON 1301 NACELLE FIRE SUPPRESSION SYSTEM  FAA/BOEING, SEPTEMBER 2003  BOEING ER  GE B  USAF/LOCKHEED MARTIN AEROSPACE, SPRING 2006  C-5 ( background on program at )  GE CF6-80C2

Slide #9 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 MINIMUM PERFORMANCE STANDARD TESTING - NOVEC 1230  RUNNING NOVEC 1230 AGAINST THE MINIMUM PERFORMANCE STANDARD FOR ENGINE NACELLE/APU COMPARTMENTS (MPSe)  TESTING STARTED 11APRIL2006  AIRBUS, SIEMENS, & 3M SUPPORTING THE PROJECT  INTENDED AIRFRAME : AIRBUS A350  IF SUCCESSFUL, OTHER AIRBUS AIRFRAMES MAY BE CONSIDERED FOR THIS MATERIAL  INERTING GAS CONCENTRATION DATA FOR NOVEC 1230  REFERENCE NFPA 2001 (2004 EDITION), TABLE A  METHANE (CH 4 ) = 8.8%v/v  PROPANE (C 3 H 8 ) = 8.1%v/v

Slide #10 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 MINIMUM PERFORMANCE STANDARD TESTING - NOVEC 1230  NACELLE TASK GROUP WILL BE ASKED IN THE NEAR FUTURE FOR COMMENTARY REGARDING THE SPECIFICATION OF THE AGENT DISCHARGE DURATION  SPECIFICATION IS BASED LOOSELY ON HALON 1301 & CLOSELY ON HFC-125 & CF3I BEHAVIORS  DURATION = 1.0 +/- 0.5 SEC FROM STORAGE PRESSURE TO 100 PSIG  THE INTENT OF THE SPECIFICATION WAS/IS TO :  KEEP THE TEST METHODOLOGY SIMILAR OVER TIME  TO PREVENT LARGE DISPARITY FROM HALON PERFORMANCE  WORK WITH BROMOTRIFLUOROPROPENE (2-BTP) IN 2004 :  SUGGESTED A CONFLICT WITH THE SPECIFICATION  CONFLICT DID NOT REQUIRE RESOLUTION  CONFLICT AGAIN APPEARS WITH NOVEC 1230

Slide #11 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 MINIMUM PERFORMANCE STANDARD TESTING - NOVEC 1230 AGENT INJECTION ~ 10 FEET TEST SECTION INLET AIR FLOW APPROACH DUCT ~ 55 FEET FIREX PRESSURE TRANSDUCER HOT WIRE ANEMOMETER (HWA) ~ 15 FEET 3 HP (2.2 kW) ELECTRIC BLOWER SPRAY FIRE ZONE DIAMETER~2 FEET DIAMETER~3 FEET ID~2 FEET / OD~4 FEET

Slide #12 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 MINIMUM PERFORMANCE STANDARD TESTING - NOVEC bar = 14.5 psi 1 m = 3.28 ft QUANTITIES DISCHARGED : => 3.6 lbf HALON 1301 => 8.8 lbf NOVEC 1230 NOTE VARIATION : => IN DISCHARGE DURATION => OF HWA BEHAVIOR (FIRE?!)

Slide #13 Federal Aviation Administration ~ WJ Hughes Technical Center Fire Safety Branch, AJP6320 ~ Atlantic City Int’l Airport, NJ USA International Aircraft Systems Fire Protection Working Group Gatwick/London, United Kingdom – 19-20April2006 CURRENT STATUS  NEED TO COMPLETE :  NOVEC 1230 MPSe TESTING  DRAFT MPSe & OBTAIN COMMENT FROM TASK GROUP  HFC-125 OVER-PRESSURE CHARACTERIZATION  CF3I MPSe TESTING  WRITE/PUBLISH REPORT & MPSe  MPSe TO BE APPENDIX MATERIAL IN FINAL REPORT  REPORT BODY TO DESCRIBE HISTORY & LESSONS LEARNED  DRAFT REPORT DUE SEP 2006