1 / 18

Presented by: Bill Leach, Code 4.3.5.1 NAVAIR Fire Protection Team Leader

RETROFIT OPPORTUNITY FOR HFC-125 IN AIRCRAFT ENGINE SYSTEMS Presented 19 November 1998 to: The International Aircraft Fire and Cabin Safety Research Conference. Presented by: Bill Leach, Code 4.3.5.1 NAVAIR Fire Protection Team Leader. NAVY RESPONSIBLE USE POLICY. Stockpile

lel
Télécharger la présentation

Presented by: Bill Leach, Code 4.3.5.1 NAVAIR Fire Protection Team Leader

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. RETROFIT OPPORTUNITY FOR HFC-125IN AIRCRAFT ENGINE SYSTEMSPresented 19 November 1998 to:The International Aircraft Fire and Cabin Safety Research Conference Presented by: Bill Leach, Code 4.3.5.1 NAVAIR Fire Protection Team Leader

  2. NAVY RESPONSIBLE USE POLICY • Stockpile • Halon Usage Factors & Aircraft Attrition Rates • Minimize Use • Recycle • Reduce Non-Fire Discharges & False Alarms • Alternative R&D • Corporate Efforts • TDP: Technology Development Program • NGP: Next Generation Program • Navy Efforts • Gas Generator Technology • Water Mist Technology

  3. NAVAIR HALON POLICIES • In-Service Aircraft (Pre - 1993) • U.S. DOD Halon Stockpile • New Aircraft Programs (Post - 1993) • Non-Halon System • No Reliance on Stockpile

  4. NAVAIR HALON POLICIES • Old Retrofit Solution: • None Needed • None Available • New Retrofit Opportunity: • Enhanced (and Growing) Pressures on Stockpile • Unexpected Forward Fit Solution (F/A-18E/F) HIGH POTENTIAL FOR RETROFIT SOLUTION

  5. FORWARD FIT SOLUTION (F/A-18E/F) • E/F Specification Requirement • No Halon • Better than or equal to C/D System • C/D System: 5.5 # of Halon 1301 • Same Bottle Compartment as C/D • No Growth Provision for New Agent Cylinder • E/F Solution: HFC-125 (~ 6 pounds) F/A-18E/F Solution Seems to Contradict Industry Knowledge

  6. HALON ALTERNATIVE TECHNOLOGY DEVELOPMENT PROGRAM • 1992 Start, 4 Year Effort • DOD Program w/ FAA Participation • Only “Corporate” Effort to Identify Chemical Alternative for Halon • Extinguishing Performance; Toxicity; Material Compatability; Agent Stability; Availability • TDP Answer: HFC-125 Predictions of 200 - 300% System Growth Required

  7. F/A-18E/F PATH TO SUCCESS Technology Development • Baseline: Gas Generator • Thermal Extremes • Insensitive Munitions • Resulted in High Risk F/A-18E/F • Alternate Agents • Gas Generator • CF3I • Dry Chemical • HFC-125 Solution • New Baseline: HFC-125 • Four Nozzle Distribution • Equal to or Better than Halon

  8. F/A-18E/F TESTING • Detailed Airflow Analyses • High Fidelity Engine Nacelle Simulator • Agent Distribution Testing • Optimize Plumbing Scheme • Fire Testing • Baselined to Halon Defeat Point • Relight Condition • Confirm Equivalence with Halon

  9. F/A-18E/F TEST ARTICLE

  10. HFC-125 EVALUATED DISTRIBUTION OPTIONS 1998 HOTWC

  11. ENGINE AFT Nozzle Placement(s) “Agent” “Agent” ( HALON ) 5.5 lb min @ 600 psi ( HFC-125 Improved Distribution) “Agent” E/F 4 Nozzle To AMAD (Outb”d) 5.6 lb @ 600 psi

  12. GENERAL SYSTEM INSTALLATION FIREX BOTTLE

  13. 15 HALON 1301(5.5#) 6.3# Improve Performance HFC-125 10 5.6# Baseline “Fire Out” Time ~ (Sec) 5 Target Min Improve Distribution 0 EMD LRIP EMD LRIP3Noz 4Noz HFC-125 TEST RESULTS Optimized HFC-125 is Competitive With HALON 1301

  14. F/A-18E/F TEST RESULTS • HFC-125 System Proven to Meet or Exceed Halon Performance • HFC-125 Always Put Out the Fire • Several HFC-125 Test Points with No Relight • Defined System Details for Production • Optimized 4 Nozzle Arrangement • 6.0 # Agent Minimum • 600 psi Nitrogen (Maintain Cold Temp Performance) • HFC-125 System Selected to Enter Qualification Testing (End FY99)

  15. HFC-125 • 1998 F/A-18E/F Engine Testing

  16. HFC-125 DESIGN EQUATIONS • Application • Any New Use of HFC-125 • Requirement: Concentration • Guidance: Mass • Some Level of Conservatism • Option to Design Equations • Fire Testing • Less Agent Likely • Smaller, Lighter Solution for New Aircraft • Retrofit Possible

  17. FIRE PROTECTION TRUTHS • Halon 1301 is a Very Efficient Fire Extinguishing Chemical • HFC-125 is a Less Efficient Fire Extinguishing Chemical than Halon 1301 • Halon 1301 Discharge Plumbing is Very Inefficient (Most In-Service Aircraft) • By Addressing the Plumbing, HFC-125 Systems Can Be Made As Efficient as Halon 1301 Systems System Equivalence is the True Goal!

  18. FIRE PROTECTION TRUTHS • HFC-125 is a Retrofit Option, NOT A DROP-IN! • Agent Discharge Plumbing Must be Optimized • Detailed Airflow Analyses • Agent Concentration Measurement • Fire Testing • Even Better Retrofit Opportunity on Helos and Other Cross-Plumbed Systems • Redundant Halon Bottles (Primary & Secondary) • Couple Bottles for Single Discharge • 200% Growth Immediately Attainable • Possibility of Meeting Design Equations

More Related