Halon Replacement For Airplane Portable Fire Extinguishers D6668 Madden 0511 BTP
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Halon Replacement for Airplane Portable Fire Extinguishers Progress Report BOEING is a trademark of Boeing Management Company. Copyright © 2009 - 2011 Boeing. All rights reserved. International Aircraft Systems Fire Protection Working Group Conference Köln, Germany May 11-12, 2011 Mike Madden Objective Provide a progress report on development of BTP (2-bromo-3, 3, 3trifluropropene), a promising new environmentally safe Halon replacement fire extinguishing agent 2 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Agenda Halon Replacement Dates Steps to Commercialization BTP Performance Agent Summary Fire Extinguisher Installation BTP Risks BTP Near-term Steps Summary 3 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Halon Replacement Dates New Design (New TC Application) Current Production Proposed Requirement Lavatory Handheld Propulsion/ APU Cargo EC Cutoff Date 2011 2014 2014 2018 ICAO 2011 2016 2014 NA UL Standard NA 2014 NA NA EC End Date (incl. retrofit) 2020 2025 2040 2040 ICAO UL Standard 2011 2016 NA NA NA 2014 NA NA Notes: EC dates were adopted in March 2010 and published August 18, 2010; to be effective December 31 of the stated year. ICAO proposed halon replacement “resolution” adopted at ICAO General Assembly Meeting on October 6, 2010. Amendments to Annexes 6 & 8 in-work. Underwriters’ Laboratory Standard 1093 to be withdrawn September 2014. COPYRIGHT © 2009 - 2011 THE BOEING COMPANY 4 Steps to Commercialization Cup burner testing - 2002 Initial toxicity tests (Ames, cardiotox…) - 2002 2D ODP, GWP and atmospheric lifetime - 2004 Prototype extinguisher, near drop-in replacement for Boeing 1211 extinguisher - 2009 UL 711 5B pan fire tests - 2009 UL 711 cold temperature pan fire test - 2009 FAA MPS AR-01/37 hidden fire tests - 2009 3D model analysis of ODP and GWP - 2010 FAA MPS AR-01/37 seat fire toxicity tests - 2011 ASTM flammability tests (per NFPA 704) - 2011 Airplane material compatibility tests - 2011 Synthesis of BTP for toxicology testing - 2011 Publication of 3D ODP scientific paper Complete toxicology testing PBPK testing and modeling Provide PBPK data to FAA for inclusion in AC 20-42D and FAA/AR-08/3 Additional BTP properties testing US EPA TSCA inventory listing US EPA SNAP approval EU REACH approval 3.25” diameter bottle UL 2129 fire extinguisher bottle tests and UL listing 5 ASTM standard for BTP COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Performance Initial BTP toxicity test results Item Comments Ames (mutagenic test) No effects noted Human Lymphocyte (chromosomal aberration) No effects noted Cardiotoxic Dog Inhalation NOAEL .5% LOAEL 1.0% Preliminary Limit Test (5% for 30 minutes) Some potential anesthetic effects noted Data from J Grigg & A Chattaway, “The Evaluation of Bromotriflouropropene as a Halon 1211 Replacement”, NIST SP 984, June 2002 http://www.fire.nist.gov/bfrlpubs/fire02/PDF/f02114.pdf 6 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Performance Passed UL 711 5B and UL 2B cold temperature fire tests, December 2009 7 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Performance Passed FAA MPS AR-01/37 hidden fire tests at UL, December 2009 8 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Performance Passed FAA MPS AR-01/37 seat fire toxicity tests, February 2011 9 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Performance FAA MPS seat fire toxicity test results: Agent HF 1-Minute Average (200 ppm limit) Test Number BTP Halon 1211 2011 tests Halon 1211 1999 tests HF 4.5-Minute Average (100 ppm limit) Agent Used (pounds) Discharge Time (seconds) 1 47.8 23.9 1.85 3.2 2 65.7 34.5 1.76 3.8 3 88.2 47.7 1.55 2.9 1 20.5 11.7 .64 2.1 2 20.4 11.0 .64 2.4 3 25.8 14.6 .57 2.0 1 9.28 6.01 1.2 6 2 21.04 13.87 .8 4.5 3 19.83 12.92 .96 4.7 Data from FAA test data sheets BTP HF levels below the MPS requirements, and FE-36 and FM-200 levels COPYRIGHT © 2009 - 2011 THE BOEING COMPANY 10 BTP Performance Passed NFPA 704 required flammability tests, March 2011 Test Results ASTM D92 Flash point (Cleveland open cup) None, vapor extinguished flame ASTM E659 Auto ignition Temperature No ignition ASTM E681 Upper and lower flammability limits Non-flammable ASTM D6668 Flammability rating F=0 NFPA 704 flammability rating of zero 11 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Performance Passed Boeing aircraft materials compatibility testing, March 2011 Non-corrosive to standard aircraft metals No effect on standard aircraft plastics No effect on standard seals or sealants No effect on standard aircraft interior materials BTP is compatible with typical aircraft materials 12 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Performance 3-D Modeling of BTP by Dr Wuebbles and Ken Patten of University of Illinois (UIUC) completed Dec 22, 2010 Whole Atmosphere Community Climate Model (WACCM) version 3.5.48. Based on BTP emissions over land areas between 30N and 60N latitude: Very short lived compound - 7 days. Oxidizes in troposphere, where bromine is rained out. 0.0028 ODP. 0.005 GWP (100 year). “BTP should be environmentally safer than other likely choices of agents” Dr. Wuebbles 13 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Agent Summary Agent Halon 1211 BTP Halotron 1 (HCFC Blend B) 3 FE-36 (HFC-236fa) FM-200 (HFC-227ea) 1. UL 711 Agent Weight (#) Total Weight Rating (#) 5 BC 2.5 3.93 Dimensions (H x W x D) ODP GWP (100 year) 17 x 4.8 x 3.25 7.91 1890 1 0.00282 15.75 x 5 x 3.5 (3D -model) 0.0052 5 BC 3.75 5.6 5 BC 5.5 9.3 15 x 5 x 4.25 0.01 1 77 1 5 BC 4.75 9.5 15.9 x 8 x 4.5 0 9820 1 5 BC 5.75 9.8 16.6 x 6.5 x 4.4 0 3580 1 World Meteorological Organization Report No. 52 – “Scientific Assessment of Ozone Depletion: 2010.” (Note that Halotron ODP was rounded up from 0.0098). http://ozone.unep.org/Assessment_Panels/SAP/Scientific_Assessment_2010/index.shtml 2. University of Illinois at Urbana-Champaign Report “2-Bromo-3,3,3-Triflouropropylene Ozone Depletion Potentials and Global Warming Potentials” dated December 22, 2010, author Kenneth Patten and Donald Wuebbles. (Note that ODP/GWP values vary depending on the assumed geographical distribution of BTP release. The latitudes considered include the U.S. and EU). 3. HCFC -123 (primary constituent of Halotron 1) is subject to US production phase-out in 2015. Supply will be limited to recycling after 2015 unless HCFC-123 is removed from the Montreal Protocol, or the Clean Air Act is 14 amended. COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Agent Summary Global Warming Potential (GWP) of Agents 12000 9820 GWP (100 year) 10000 8000 6000 3580 4000 2000 1890 0.005 77 BTP Halotron 1 0 Halon 1211 FE-36 FM-200 15 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Agent Summary Seat Fire Toxicology Test Results HF 1 Minute Average 120 HF (ppm) 100 80 Test #1 60 Test #2 Test #3 40 20 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY FM-200 FE-36 Halotron 1 BTP Halon 1211 0 16 Agent Summary Seat Fire Toxicology Test Results HF 4-1/2 Minute Average 80 70 HF (ppm) 60 50 Test #1 40 Test #2 30 Test #3 20 10 FM-200 FE-36 Halotron 1 BTP Halon 1211 0 17 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Agent Summary LOAEL & NOAEL of Agents 16 14 %V/V 12 10 LOAEL 8 NOAEL 6 4 2 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY FM-200 FE-36 Halotron 1 BTP Halon 1211 0 18 Agent Summary Size and Weight Comparison of Handheld Fire Extinguishers Size/Weight Relative to Halon 1211 3 2.5 2 Size Weight 1.5 1 0.5 0 Halon 1211 BTP Halotron 1 FE-36 FM-200 19 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Fire Extinguisher Installation Validation fit-check of 3.5” diameter BTP fire extinguisher was conducted on Boeing production models Diameter of existing production bottle used for BTP prototype caused Interference on 737 models Boeing is developing a 3.25” diameter bottle of the same volume Halon BTP Halotron 20 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Fire Extinguisher Installation Example of a 737 installation (bracket is removed) 21 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Fire Extinguisher Installation Example of a 737 installation 22 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Fire Extinguisher Installation Example of a 777 installation 23 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Near-term Steps Submit paper on 3D atmospheric modeling (ECD 3Q11) Toxicology testing (ECD 2Q13) • Primarily subchronic, reproductive toxicity, PBPK, irritation 24 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Risks Must pass all toxicity tests prior to SNAP/REACH approval. Low volume production cost of BTP is high compared to Halon and alternatives. Expanding BTP market beyond airplane use will lower cost. Boeing considers the higher price acceptable for the following reasons: •Allows retrofit of existing airplanes with minimal impact to airlines •Allows production incorporation with minimal cost and impact •Provides a long term industry solution that is safe for the environment •It is airplane safety equipment 25 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY BTP Risks Per AC20-42D - Halon 1211, Halotron 1, and BTP are unsafe for use in Boeing airplane flight decks and other small volumes. AC 20-42D, Chapter 4.4b(3), (4) states that concentrations may be adjusted to account for stratification…a report will be published at the FAA Technical Center with method to adjust safe-use concentrations. The report providing necessary guidance to show compliance has not been developed or released. Need to reconvene the Handheld Working Group and develop guidance material based on stratification testing 26 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Summary BTP does not have the environmental, size, or weight issues of existing FAA approved halon replacement fire extinguishers/agents. BTP is a promising, environmentally safe, drop-in replacement. • 3D model validated near zero ODP and GWP. • Passed UL 711 5B, 2B cold temperature, and FAA MPS tests. • Passed Boeing aircraft material compatibility tests. Boeing has funded toxicology testing and is working toward commercialization of BTP. Boeing’s goal is to replace Halon portable fire extinguishers just one time, and with an environmentally acceptable agent. 27 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY Questions? Contact: Mike Madden The Boeing Company Mike.r.madden@boeing.com 425-342-2517 28 COPYRIGHT © 2009 - 2011 THE BOEING COMPANY
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