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.

Slides:



Advertisements
Similar presentations
Objective - Develop a test method that is: Representative of Actual Conditions Repeatable and Consistent Obtainable by All Labs in All Parts of the World.
Advertisements

FAA Regulatory Information
Federal Aviation Administration Radiant Panel Updates 2014 June Materials Meeting Switzerland Materials Working Group Michael Burns, FAA Tech Center June,
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Test Results for Proposed Cargo.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Developing an In-flight Fire Condition.
Federal Aviation Administration Evacuation Slide Test Method: Round Robin 3 Results 0 Evacuation Slide Test Method: Comparison Test Results Federal Aviation.
NexGen Burner Update International Aircraft Materials Fire Test Working Group Meeting October 21, 2009 Atlantic City, NJ.
MAJOR REPAIRS AND ALTERATIONS
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Task Group Session on Revised.
BUNSEN BURNER BASICS. General Information Bunsen burners are used to provide a safe heat source during many laboratory experiments. Before using a Bunsen.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Discussion on Format of New Test.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Task Group Session on Revised.
IASFPWG – Ottawa, Canada Limiting Oxygen Concentration (LOC) Work Update International Aircraft Systems Fire Protection Working Group Ottawa, Canada.
Limiting Oxygen Concentration of Aviation Fuels Federal Aviation Administration 0 0 Limiting Oxygen Concentration of Aviation Fuels Steve Summer Project.
Federal Aviation Administration 0 Intermixing of Cells in Nickel-Cadmium Batteries for Aircraft Usage May 11, Intermixing of Cells in Nickel-Cadmium.
European Aviation Safety Agency IASFPWG May London Certification Directorate Slide 1 ISO2685 Revision Fire Testing For Propulsion Rémi DELETAIN.
Presented to: International Aircraft Systems Fire Protection Working Group By: Date: April 2-3, 2008 Federal Aviation Administration Next-Generation Oil.
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.
Federal Aviation Administration OSU & NBS Updates 2010 March Materials Meeting Boeing Facility - Renton, WA Materials Working Group Michael Burns, FAA.
Federal Aviation Administration Burnthrough Update International Aircraft Materials Fire Test Working Group Meeting October 21, 2008 Atlantic City, NJ,
Federal Aviation Administration (FAA) Presented by Jim Gardner, AFS-200 Proposed Amendment To Annex 6, Part I International Commercial Transport – Aeroplanes.
NFPA 31 Standard for the installation of Oil- Burning Equipment
International Aircraft Materials Fire Test Working Group Meeting
Federal Aviation Administration 0 FTFAM – Version 11 Update May 19 th, Fuel Tank Flammability Assessment Method – Version 11 Update Steve Summer.
Federal Aviation Administration RTCA Update 0 RTCA Update Federal Aviation Administration International Aircraft Materials Fire Test Working Group Bremen,
Federal Aviation Administration Burnthrough Update International Aircraft Materials Fire Test Working Group Meeting June 17, 2009 Köln, Germany.
Federal Aviation Administration 0 Composite Wing Tank Flammability April 2-3, Composite and Aluminum Wing Tank Flammability Comparison Testing Steve.
Presented to: International Aircraft Materials Fire Test Working Group – Köln, Germany By: Robert Ian Ochs Date: Wednesday, June 17, 2009 Federal Aviation.
Presented to: International Aircraft Systems Fire Protection Working Group. Atlantic City, NJ By: Dave Blake. FAA Technical Center. Atlantic City, NJ.
Review of Handbook Chapters Pat Cahill
Presented to: By: Date: Federal Aviation Administration Forced-flow Fire Testing with “cold”-soaked FK International Aircraft Systems Fire Protection.
Federal Aviation Administration Aircraft Wiring 0 Federal Aviation Administration International Aircraft Materials Fire Test Working Group Bremen, Germany.
Federal Aviation Administration RTCA Update 0 Federal Aviation Administration Pat Cahill AJP-632; Fire Safety Team Wm. J. Hughes Technical Center Federal.
Presented to: By: Date: Federal Aviation Administration In-Flight Burn- Through Tests Aluminum vs. composite materials Aircraft Systems Fire Working Grp.
Federal Aviation Administration Radiant Panel Test for Thermal/Acoustic Insulation 0 Federal Aviation Administration International Aircraft Materials Fire.
Federal Aviation Administration HRR 2 Development Task Group 2011 March Materials Meeting Savannah, GA Materials Working Group Michael Burns, FAA Tech.
Tim Marker FAA Technical Center Discussion of Test Method to Determine the Burnthrough Resistance of Thermal/Acoustic Insulation Materials.
IASFPWG – Seattle, WA Jet-A Vaporization Computer Model A Fortran Code Written by Prof. Polymeropolous of Rutgers University International Aircraft.
Federal Aviation Administration OSU & NBS Updates 2009 March Materials Meeting Materials Working Group Michael Burns, FAA Tech Center March 4 th & 5 th,
Federal Aviation Administration RTCA Update 0 Federal Aviation Administration Pat Cahill AJP-632; Fire Safety Team Wm. J. Hughes Technical Center Federal.
Enhanced Airworthiness Program for Airplane Systems (EAPAS) Presented by: Massoud Sadeghi FAA - Aging Systems Program Manager EAPAS Workshop November 2002.
Federal Aviation Administration OSU & NBS March Materials Meeting Materials Working Group Michael Burns, FAA Tech Center June 17 th & 18 th, 2008.
NexGen Fire Test Burner Update
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.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Update Handbook Chapters IAMFT WG, Cologne,
Federal Aviation Administration 0 Composite Wing Tank Flammability November 20, Composite and Aluminum Wing Tank Flammability Comparison Testing.
Federal Aviation Administration RTCA Update 0 Federal Aviation Administration Pat Cahill AJP-632; Fire Safety Team Wm. J. Hughes Technical Center Federal.
Federal Aviation Administration RTCA Update 0 RTCA Update Federal Aviation Administration International Aircraft Materials Fire Test Working Group Savannah,
Federal Aviation Administration Wiring Test 0 Federal Aviation Administration Pat Cahill AJP-632; Fire Safety Team Wm. J. Hughes Technical Center Federal.
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.
Tim Marker FAA Technical Center Burnthrough Task Group Report.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Task Group Session on Revised.
Federal Aviation Administration OSU & NBS Updates 2008 October Materials Meeting Materials Working Group Michael Burns, FAA Tech Center October 21 st &
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 International Aircraft Materials Fire Test Working Group Discussion of Full-Scale Testing of Leather.
Federal Aviation Administration 0 Composite Wing Tank Flammability May 11, Composite and Aluminum Wing Tank Flammability Comparison Testing Steve.
Federal Aviation Administration OSU & NBS Updates 2010 June Materials Meeting Koeln, Germany Materials Working Group Michael Burns, FAA Tech Center June.
Progress report of TFG 7 “Fire resistance test” Mar. 3rd, 2016 Korea Transportation Safty Authority (TS) Korea Automobile Testing & Research Institute.
Presented to: By: Date: Federal Aviation Administration International Aircraft Materials Fire Test Working Group Meeting Test Cell Airflow Study For Cargo.
Tim Marker Discussion of Burner Heat Flux Mapping for Proposed Insulation Burnthrough Test Standard FAA Technical Center.
Federal Aviation Administration Aircraft Ducting 0 Federal Aviation Administration International Aircraft Materials Fire Test Working Group Atlantic City,
Presented to: International Aircraft Materials Fire Test Working Group By: Robert Ochs Date: Wednesday, October 21, 2009 Federal Aviation Administration.
Thermocouple Considerations for fire testing
International Aircraft Materials Fire Test Working Group Meeting
AIRCRAFT FIRE REGULATIONS
Presentation transcript:

Federal Aviation Administration Next Generation Fire Test Burner for Powerplant Fire Testing Applications Steve Summer Federal Aviation Administration Fire Safety Branch http://www.fire.tc.faa.gov International Aircraft Systems Fire Protection Working Group Koeln, Germany May 11, 2011

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 Abbreviations Fireproof-- (1) With respect to materials and parts used to confine fire in a designated fire zone, means the capacity to withstand at least as well as steel in dimensions appropriate for the purpose for which they are used, the heat produced when there is a severe fire of extended duration in that zone; (2) With respect to other materials and parts, means the capacity to withstand the heat associated with fire at least as well as steel in dimensions appropriate for the purpose for which they are used. Fire resistant-- (1) With respect to sheet or structural members means the capacity to withstand the heat associated with fire at least as well as aluminum alloy in dimensions appropriate for the purpose for which they are used; and (2) With respect to fluid-carrying lines, fluid system parts, wiring, air ducts, fittings, and powerplant controls, means the capacity to perform the intended functions under the heat and other conditions likely to occur when there is a fire at the place concerned. No definition of test method, apparatus, or criteria Advisory material has been used to define these test parameters

Background Advisory Circulars and FAA Reports: Power Plant Engineering Report No. 3A, Standard Fire Test Apparatus and Procedure (For Flexible Hose Assemblies), Revised March 1978 Acceptable fire test burners listed in Appendix III: Lennox OB-32 (not available) Carlin 200 CRD (not available) Stewart-Warner HPR 250 (not available) Stewart-Warner FR-600 (not available) AC 20-135, Powerplant Installation and Propulsion System Component Fire Protection Test Methods, Standards, and Criteria, 2/6/90 Acceptable fire test burners listed in sec. 6c: Those listed in Appendix III of Powerplant Report 3A SAE 401 Burner adjusted to 9.3 BTU/ft2s (propane fueled burner) Propane and oxy-acetylene torch-standard and diverging nozzles

Background Advisory Circulars and FAA Reports (cont.): FAA Aircraft Materials Fire Test Handbook (4/2000) Chapter 11 specifies the oil burners listed above, plus Park DPL 3400 (not available) Chapter 12 specifies the oil burners above, including the Park DPL 3400 Chapter 12 Supplement, section 12.3.1 states: SAE AS401B Propane Burner is also acceptable provided the temperature profile and heat flux density conform to the specified requirements AC 33.17-1A, Engine Fire Protection, 8/3/09 References Powerplant Report 3A and AC 20-135 for acceptable burners

Background All of the specified oil burners are no longer commercially available Industry is left with the propane burner, which can be obtained and is typically preferred due to it’s consistency and ease of use Propane and jet fuel flames, despite having similar measured temperatures and heat flux, are fundamentally different Propane will provide a less severe flame than a jet fuel flame, due to the transparency of the propane flame vs. the opacity of the jet fuel flame As test components approach the flame temperature, they begin to re-radiate due to the high surface temperature Heat is lost readily from the hot surface through the transparent propane flame Heat is not lost through the opaque jet fuel flame Intent of regulations is to provide protection against an engine fire, which is a jet fuel flame, not a propane flame FAA Tech Center Fire Safety Team has been tasked by Transport Airplane Directorate to develop burner performance standards for the next-generation fire test burner for powerplant fire testing

Current Status New lab space being built up at the Fire Safety facilities for powerplant burner testing. Burner and associated calibration and test rigs are complete. Instrumentation, wiring and installation of burner is currently being worked on. Lab should be ready for testing within 4-6 weeks.

Planned Work – Powerplants Fire Test User Survey In conjunction with DGA and EASA, a detailed user survey has been created and will be released shortly on the Powerplants KSN website. This survey is aimed at providing authorities better insight as to how the various labs are operating/calibrating their burners and what parts of the test standards need clarification and/or modification. As part of the survey, user will be asked to conduct a sample test on a 24”x24” sheet of 2024 aluminum as the initial test in part of a larger round robin test program. When the survey is available, Powerplant Task Group members who are registered on the KSN site will receive an email with detailed instructions and a link to the survey.

Planned Work – Round Robin Testing Round Robin testing to be initiated with various labs and burners (Park DPL 3400, NexGen, and Propane). Materials to be tested include: Slug Calorimeter Sheet of copper with thermal absorptive coating, and thermocouple(s) on back face to determine heat flux 2024 Aluminum Sheet Metallic Firewall (steel) Composite Firewall Information will be posted on the Powerplants KSN site as soon as available to request participants.