Engine Nacelle Halon Replacement - PowerPoint PPT Presentation

About This Presentation
Title:

Engine Nacelle Halon Replacement

Description:

engine nacelle halon replacement presentation contents review equivalence data to date discuss progress regarding observed over-pressures discuss status reviewing ... – PowerPoint PPT presentation

Number of Views:87
Avg rating:3.0/5.0
Slides: 21
Provided by: DougIn4
Category:

less

Transcript and Presenter's Notes

Title: Engine Nacelle Halon Replacement


1
Engine Nacelle Halon Replacement
2
PRESENTATION CONTENTS
  • REVIEW EQUIVALENCE DATA TO DATE
  • DISCUSS PROGRESS REGARDING OBSERVED
    OVER-PRESSURES
  • DISCUSS STATUS

3
REVIEWING EQUIVALENCE DATA TO DATE
Agent Ventilation configuration Fire Threat Equivalent Concentration (v/v) FIXED DURATION/OBSOLETE VALUES IN BRACES
HFC-125 High JP8 spray 17.5 16.9
HFC-125 High JP8 pool 7.6 9.6
HFC-125 Low OIL spray 16.4 (a) 15.8
HFC-125 Low JP8 pool 8.1 (a) not determined
CF3I High JP8 spray 5.6 5.8
CF3I High JP8 pool Incomplete
CF3I Low OIL spray 7.2 (a,b) 7.2
CF3I Low JP8 pool Incomplete
(a) Bracketing method used to find mass equivalent (a) Bracketing method used to find mass equivalent (a) Bracketing method used to find mass equivalent (a) Bracketing method used to find mass equivalent
(b) Partial result, JP8 verification incomplete as of November 2005 (b) Partial result, JP8 verification incomplete as of November 2005 (b) Partial result, JP8 verification incomplete as of November 2005 (b) Partial result, JP8 verification incomplete as of November 2005
4
REVIEWING EQUIVALENCE DATA TO DATE
OTHER REPORTED or CALCULATED CONCENTRATIONS
Agent Fuel Peak, Critical or Design Concentration (v/v) REFERENCE
CF3I PROPANE 6.5 (p) NFPA 2001, TABLE A-3-4.3
CF3I JP8 SPRAY 3.2 (c) NIST SP890, V.2, TBL 10, p.115
CF3I JP8 POOL 6.8 (c) NIST SP890, V.2, TBL 10, p.115
CF3I OIL 7.2 (d) FAATC none work in progress...
HFC-125 METHANE 14.7 (p) NFPA 2001, TABLE A-3-4.3
HFC-125 PROPANE 15.7 (p) NFPA 2001, TABLE A-3-4.3
HFC-125 PROPANE ?12.6 (p) NIST SP890, V.2, FIG. 41, p.78
HFC-125 JP8 SPRAY 8.7 (c) NIST SP890, V.2, TBL 10, p.115
HFC-125 JP8 POOL 12 (c) NIST SP890, V.2, TBL 10, p.115
HFC-125 JP8 SPRAY, LoVent 25.4 (d) AFRL-VA-WP-TR-1999-3068
HFC-125 JP8 SPRAY, HiVent 18.2 (d) AFRL-VA-WP-TR-1999-3068
HFC-125 JP8 17.5 (d) FAATC none work in progress...
5
OVER-PRESSURE BEHAVIOR BRIEF OVERVIEW
  • IN 2004, TWO HALON REPLACEMENT CANDIDATES WERE
    OBSERVED TO PRODUCE OVER-PRESSURE PHENOMENA
    SUBSEQUENT TO REIGNITION WITHIN THE TEST FIXTURE
    FLOW PATH
  • 2-BTP
  • HFC-125
  • HFC-125 2-BTP APPEARED TO ACT AS A FUEL IN SOME
    INSTANCES
  • THE PHENOMENA WAS NOT 100 RELIABLE
  • INVESTIGATION REQUIRED DUE TO FREQUENT OCCURRENCE
  • OUTCOMES
  • 2-BTP WITHDRAWN FROM CONSIDERATION
  • ENVIRONMENTAL BEHAVIORS FOR HFC-125 DURING
    OVER-PRESSURE EVENTS WILL BE RECORDED IN
    NEAR-TERM TESTING TO PERMIT FUTURE
    DECISION-MAKING ACTIVITY

6
OVER-PRESSURE BEHAVIOR SCHEMATIC ORIENTATION
RETURN
7
OVER-PRESSURE BEHAVIOR DUCT INTERFACE IMAGE
8
OVER-PRESSURE BEHAVIOR ACTIVITIES/PLANS TO DATE
  • INSTRUMENTATION IS INSTALLED IN TEST FIXTURE
    RED DUCT TO CAPTURE ENVIRONMENTAL BEHAVIORS
    DURING OVER-PRESSURE EVENTS
  • 4 THERMOCOUPLES TO MONITOR TEMPERATURES IN RED
    DUCT
  • 2 PRESSURE TRANSDUCERS TO RECORD STATIC PRESSURE
  • 4 PHOTOCONDUCTIVE PHOTODIODES TO DETECT FLAME
  • DUCT INTERFACE CAN BE ISOLATED FROM TEST BAY
  • MINIMIZED THE IMPACT ON THE VENTILATION STREAM
    ASSOCIATED WITH DUCT INTERFACE ISOLATION
  • PERFORMING ANALYTICAL EVALUATIONS OF THE DUCT
    INTERFACE
  • BERNOULLI VELOCITY MEASUREMENTS
  • 1ST LAW OF THERMODYNAMICS
  • WILL RECORD ENVIRONMENTAL BEHAVIORS NEAR-TERM
  • FIRE TESTING WITH NO AGENT, HALON 1301, HFC-125
  • OIL JP8 (??) SPRAY FIRES
  • DUCT INTERFACE OPEN CLOSED

9
OVER-PRESSURE TELEMETRY PLACEMENT
10
OVER-PRESSURE TELEMETRY BEHAVIORS/OPEN DUCT
INTERFACE
11
OVER-PRESSURE TELEMETRY BEHAVIORS/CLOSED DUCT
INTERFACE
12
OVER-PRESSURE BEHAVIOR ANALYTICAL EVALUATION
BERNOULLI VELOCITY ANALYSIS
  • RECORD STATIC PRESSURE IN RED DUCT AT 2 LOCATIONS
  • 21 INCHES FROM INLET 7 INCHES OFF DUCT WALL
    (21/7)
  • 16 INCHES FROM INLET 4 INCHES OFF DUCT WALL
    (16/4)
  • ALL FLOWS WERE THE SAME TEMPERATURE
    NON-COMBUSTING
  • WORKED WITH STREAM LINES FROM TEST BAY INTO RED
    DUCT SMOKE TRAIL OBSERVATIONS INDICATED
  • 21/7 WAS IN THE FLUCTUATION BETWEEN THE TEST BAY
    EDUCTION FLOW THE TEST SECTION EJECTA
  • 16/4 WAS IN THE TEST BAY EDUCTION FLOW SOLELY
  • VELOCITIES (mass flows identified in parentheses
    are based on an assumption that speed is an
    average value for the annular surface area of the
    duct inlet where test bay air is entering i.e.
    QAV A0.31 m2)
  • 21/7
  • T_bay 13C, V 3 m/s (mdot ? 1.1 kg/s)
  • T_bay 26C, V 2.9 m/s (mdot ? 1.1 kg/s)
  • 16/4 T_bay 26C, V 3.3 m/s (mdot ? 1.2 kg/s)

13
OVER-PRESSURE BEHAVIOR ANALYTICAL EVALUATION
BERNOULLI VELOCITY ANALYSIS
14
OVER-PRESSURE BEHAVIOR ANALYTICAL EVALUATION
15
OVER-PRESSURE BEHAVIOR ANALYTICAL EVALUATION
1ST LAW OF THERMODYNAMICS
  • CONTAINED DUCT INTERFACE WITHIN A CONTROL VOLUME
    (CV)
  • NON-COMBUSTING FLOW CONDITIONS
  • ESTIMATING MASS FLOW FROM THE TEST BAY INTO RED
    DUCT
  • THE PROBLEM IS UNDER-SPECIFIED
  • THE CV WAS MODELED FOR VARIABLE INPUTS TO
    OBSERVE BEHAVIOR OVER A RANGE OF CONDITIONS
  • HEAT TRANSFER TO THE BAY ASSUMED NEGLIGIBLE
  • WORK 0
  • MASS FLOW FROM THE TEST SECTION IS REASONABLY
    SIMILAR ACROSS THE AMBIENT CONDITIONS TO TREAT AS
    A CONSTANT VALUE (1 lbm/s /- 0.1 lbm/s 0.45
    kg/s /- 0.05 kg/s)

16
OVER-PRESSURE BEHAVIOR ANALYTICAL EVALUATION
1ST LAW OF THERMODYNAMICS
17
OVER-PRESSURE BEHAVIOR ANALYTICAL EVALUATION
1ST LAW OF THERMODYNAMICS
18
OVER-PRESSURE BEHAVIOR ANALYTICAL EVALUATION
JUMP TO TEST FIXTURE SCHEMATIC
1ST LAW OF THERMODYNAMICS
TEST BAY 29C
19
OVER-PRESSURE BEHAVIOR SUMMATION TO DATE
  • TEST FIXTURE IS READY FOR TESTING IN OPEN
    CLOSED DUCT INTEFACE CONFIGURATIONS
  • ANALYSIS OF VENTILATION AT DUCT INTERFACE NEARING
    COMPLETION
  • SPEEDS FOR RED DUCT TEST BAY FLOWS HAVE
    NEGLIGIBLE IMPACT ON CALCULATIONS FOR TEST BAY
    MASS FLOWS
  • ONLY WHEN AIR TEMPERATURE DIFFERS BETWEEN TEST
    SECTION TEST BAY
  • NEGLIGIBLE IMPACT ILLUSTRATED BY CALCULATED
    CURVES IN THE REASONABLE REGION OF BULK
    TEMPERATURE FOR THE RED DUCT FLOW
    (150-200F/65-93C)
  • THE GREATEST SENSITIVITY TO THE FLOW SPEEDS
    EXISTS WHEN THE 3 MASS FLOWS ARE THE SAME
    TEMPERATURE
  • ESTIMATING 1 kg/s OR LESS ENTERING RED DUCT FROM
    THE TEST BAY VIA THE INTERFACE
  • FUEL/AIR RATIOS TO BE CALCULATED

20
CURRENT STATUS
  • NEED TO COMPLETE
  • HFC-125 OVER-PRESSURE CHARACTERIZATION
  • WORKING ON FUEL-AIR RATIO INFORMATION FOR JP8,
    OIL, HYDRAULIC FLUID
  • TEST PLAN REQUIRES FINALIZATION
  • CF3I EQUIVALENCE TESTING
  • JP8 POOL, HIGH LOW VENTILATION
  • JP8 SPRAY, LOW VENTILATION
  • COLD-SOAK HFC-125 PROOF (FIRE) TESTS
  • WRITE/PUBLISH REPORT MPSE
  • WILL CONSOLODATE WORDS FORMING MPSE PASS AROUND
    TO TASK GROUP FOR COMMENT
  • MPSE TO BE APPENDIX MATERIAL IN FINAL REPORT
  • REPORT BODY TO DESCRIBE HISTORY LESSONS LEARNED
  • DRAFT REPORT DUE SEP 2006
Write a Comment
User Comments (0)
About PowerShow.com