heat release rate updates 2014 june materials meeting switzerland
DESCRIPTION
HEAT RELEASE RATE Updates 2014 June Materials Meeting Switzerland. Materials Working Group. Michael Burns, FAA Tech Center. June, 2014. AGENDA. OSU Orifice Meter Discussion (Static Pressure Taps) Chapter HR Update (hr2) Combined Supplement with Test method. OSU:. - PowerPoint PPT PresentationTRANSCRIPT
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HEAT RELEASE RATE Updates
2014 June Materials MeetingSwitzerland
Materials Working Group
Michael Burns, FAA Tech Center
June, 2014
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Heat Release Rate Test ApparatusJune 2014
AGENDA
OSU
• Orifice Meter Discussion
(Static Pressure Taps)
CHAPTER HR UPDATE (HR2)
• Combined Supplement with Test method
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Heat Release Rate Test ApparatusJune 2014
• Protruding pressure taps (beyond the pipe inner wall) vs. surface pressure taps (flush with inner wall) may have a influence on pressure readings
• Could have an influence on total airflow
OSU:
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Heat Release Rate Test ApparatusJune 2014
Supplemental material moved to Test Method as follows: Added BTU/ft2*sec units
Environmental Chamber – Added Radiation Door Assembly Figure
Radiation Source
• Power Supply Capacity – 12 kVA is sufficient
• Diamond-Shaped Mask Mounting – ½ inch diameter machine screw
(approximately 4 inches in length)
• Mask Position – Approximately 3 inches from the reflector plate
• Mask shaft-head or nut only on side facing specimen
(no threads extending towards specimen)
HR2: HEAT RELEASE TEST METHOD
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Heat Release Rate Test ApparatusJune 2014
Thermopile Wiring
• Color coding differences - Chromel yellow/green; Alumel red/white
Upper Pilot Burner
• Caution Statement – Do not disturb burner position once set
• Flame Profile – To increase orange tip, reduce air from the mixture
Drill hole sizes added for:
• Upper Pilot Burner (#59 Drill)
• Air Distribution Plate (# 4 Drill)
• Second Stage Plate (# 28 Drill)
Drip Pan - Foil can be used to line the drip pan to facilitate cleaning after use
HR2: HEAT RELEASE TEST METHOD
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Heat Release Rate Test ApparatusJune 2014
Heat Flux Gauge (HFG)
• Cooling Water Tubing – Rigid due to the high temperatures
• Cleaning – Gently wipe with soft, water-dampened sponge
• Caution Statement – Damage done to the coating during the cleaning process will affect the measurement accuracy of the sensor
Specimen Preparation
• Added recommended specimen foil wrapping technique
• Foil trimming – no scoring or incisions permitted
• Spring Plate Pressure – Recommended applying equal pressure to specimens of equal thickness by inserting the specimen retaining rod in the same holes for each specimen tested
HR2: HEAT RELEASE TEST METHOD
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Heat Release Rate Test ApparatusJune 2014
Heat Flux Calibration Procedure (Corner)
• Caution Statement – Do not disturb burner position when rotating calibration fixture 90 degrees
• Added options for improving 4-corner uniformity:
Adjust power settings
Reposition globars - Hottest to coolest (bottom to top)
Move mask – Closer to or further from HFG
Move globars – Adjustment left or right
Reflector plate – Adjust slope (top and bottom)
Added Rounding, Accuracy and Units section
HR2: HEAT RELEASE TEST METHOD
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Heat Release Rate Test ApparatusJune 2014
Calculation of Calibration Factor Kh – Added example assuming 60 mV baseline; 7 mV rise for each change in flow
HR2: HEAT RELEASE TEST METHOD
Kh = 0.5879∗ሺF1 − F0ሻሺV1 − V0ሻ kW/mV
If:
Baseline Flow
(SLPM)
High Flow
(SLPM) Baseline
(mV)
High Flow (mV) Δ Flow Δ mV Kh
1 2 60 67 1 7 0.0840 1 3 60 74 2 14 0.0840 1 4 60 81 3 21 0.0840
Then: Kh = (Kh (1 → 2) + Kh (1 → 3) + Kh (1 → 4)) / 3 kW/mV Average Kh = 0.0840 kW/mV Cv = 0.0% (< 5% therefore calibration is valid)
Federal AviationAdministration
Heat Release Rate Test ApparatusJune 2014
Test Preparation
• Thermopile – Baseline mV observed daily as an indicator of developing problems
Variations in heat flux (heat flux gauge malfunction)
Defects in thermopile
Air leakage – Environmental chamber/lower plenum, exhaust stack or holding chamber door seal
Test Performance
• The use of an externally positioned mirror may assist in viewing upper pilot flames during testing
HR2: HEAT RELEASE TEST METHOD
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Heat Release Rate Test ApparatusJune 2014
Heat Release Rate – Added example for calculating HRR (Peak HRR)
HR2: HEAT RELEASE TEST METHOD
Heat Release Rate = ሺTestmV − BaselinemVሻ ∗ ቀ Kh0.02323 m2ቁ kW/m2
ሺTestmV − BaselinemVሻ ∗ ቀ Kh0.02323 m2ቁ kW/m²
If: BaselinemV = 60 [Average thermopile millivolt reading at baseline (mV)] TestmV = 81 [Thermopile millivolt reading at any point during test (mV)] Kh = 0.0840 [Calibration factor (kW/mV)] Then: Heat Release Rate = ሺ81 − 60ሻ ∗ ቀ0.08400.02323ቁ kW/m² = ሺ21ሻ ∗ ሺ3.62ሻ kW/m² = 75.93 kW/m²
Federal AviationAdministration
Heat Release Rate Test ApparatusJune 2014
Total Heat Release – Added example for calculating Total HR (2-Min. THR)
HR2: HEAT RELEASE TEST METHOD
σ ൫Test mV − Baseline mV൯ ∗ ൬ Kh0.02323 m2൰n−1t=0 x kW · min/m² If: n = 120 [Total number of data collection points in 2 minutes] x = 60 [Total number of data collection points in 1 minute] BaselinemV = 60 [Average thermopile millivolt reading at baseline (mV)] TestmV = 81 [Thermopile millivolt reading at any point during test (mV)] Kh = 0.0840 [Calibration factor (kW/mV)] Scan # Heat Release Rate T = 0 75.93 T = 1 75.93 . 75.93 . 75.93 . 75.93 T = 119 75.93 TOTAL 9111.0 Then: Total Heat Release (After 2 minutes) = (9111.0 / 60) kW · min/m² = 151.9 kW · min/m²
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Heat Release Rate Test ApparatusJune 2014
Test Report
• Laboratory
• Fully identify the material tested
• Graphically report the heat release rate (kW/m2) as a function of time (in seconds) for each test
• Maximum heat release rate and time (in seconds) it occurs during each test
• Total heat released during the first 2 minutes of each test
• Radiant heat flux to the specimen
HR2: HEAT RELEASE TEST METHOD
Federal AviationAdministration
Heat Release Rate Test ApparatusJune 2014
Test Report (Continued)
• Calibration factor Kh (kW/mV )
• Average mV baseline for each specimen tested
• Melting, sagging, delaminating, or other behavior that affected the exposed surface area or mode of burning that occurred and the time(s) at which such behavior occurred
• Total number of materials tested
• Total number of materials passed
HR2: HEAT RELEASE TEST METHOD
Federal AviationAdministration
Heat Release Rate Test ApparatusJune 2014
Requirements
• Quantity of Samples – Minimum of three samples must be tested and 80% or greater must pass
HR2: HEAT RELEASE TEST METHOD
Example
Total Samples Tested
Must Pass %
3 3 100%
4 4 100%
5 4 80%
6 5 83%
7 6 86%
8 7 88%
9 8 89%
10 8 80%
11 9 82%
12 10 83%
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Heat Release Rate Test ApparatusJune 2014
QUESTIONS?
What is full of holes, but can still hold a lot of water?Answer: Sponge