Transcript
Page 1: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

HEAT RELEASE RATE Updates

2014 June Materials MeetingSwitzerland

Materials Working Group

Michael Burns, FAA Tech Center

June, 2014

Page 2: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

Heat Release Rate Test ApparatusJune 2014

AGENDA

OSU

• Orifice Meter Discussion

(Static Pressure Taps)

CHAPTER HR UPDATE (HR2)

• Combined Supplement with Test method

Page 3: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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:

Page 4: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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

Page 5: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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

Page 6: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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

Page 7: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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

Page 8: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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)

Page 9: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

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

Page 10: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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

Page 11: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

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

Page 12: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

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

Page 13: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

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

Page 14: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

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%

Page 15: HEAT  RELEASE RATE  Updates 2014 June Materials Meeting Switzerland

Federal AviationAdministration

Heat Release Rate Test ApparatusJune 2014

QUESTIONS?

What is full of holes, but can still hold a lot of water?Answer: Sponge


Recommended