Osu Far Appendix F to Part 25 Aviation Parts Heat Release Rate Tester

• After-sales Service: Response on Customers′ Questions Within 12 Hours.
• Warranty: 12 Months
• Reference Standards: Far 25.853 Part IV, Boeing Bss 7322, ASTM E906
• Model NO.: OSU
• Test Specimen: Aviation Parts, Aviation Materials
• Type: Fire Testing Equipment
• Combustion Gas: Methane
• Auxiliary Gas: Constant Temperature and Constant Current Gas
• Dimension: 760mm (W) X 1850mm X (H) X 850mm (D)
• Weight: 218kg
• Display: Digital
• Operation Mode: Automatic
• Language: English
• Data Print: Built-in Printer
• Power Supply: 220V, 50Hz
• Delivery: by Sea
• OEM Service: Available
• Training and Installation: Available
• Transport Package: Packed in The Plywood Cases
• Specification: 220kg
• Trademark: Delta
• Origin: China Mainland
• HS Code: 9031809090
• Production Capacity: 10 Sets / Month
• Package Size: 120.00cm * 250.00cm * 130.00cm
• Package Gross Weight: 300.000kg

Product Description

OSU FAR Appendix F to Part 25 Aviation Parts Heat Release Rate Tester

Introduction:
The OSU FAR Appendix F to Part 25 Aviation Parts Heat Release Rate Tester is mainly composed of an adiabatic outer box, an electric heating radiation device, an ignition device, and a constant temperature and current device.

During the test, air passes through the enclosure at a constant flow rate from the inlet, and the data acquisition system records the air inlet and outlet temperatures as well as the box wall temperature, and calculates the heat release rate based on the energy per unit of exposed surface.
OSU heat release rate tester can also determine toxic gases such as CO, CO2, NOx, HCN, Hbr, HCL, etc. by adding an FTIR Fourier infrared flue gas toxicity testing device.

Standard:
• FAR 25.853 Part IV: Heat release rates by materials and products when exposed to one level of radiant heat Airbus AITM 2.0006.
• Boeing BSS 7322.
• ASTM E906: Standard Test Method for Heat and Visible Smoke Release Rates for Materials and Products Using a Thermopile Method SUPERSEDED.

Main Features:
1. The OSU FAR Appendix F to Part 25 Aviation Parts Heat Release Rate Tester adopts a stainless steel combustion test chamber with a high-temperature glass observation window;
2. The heat radiation source is 4 Glowbars heating rods, which can provide 35KW/M2 heat radiation flux.
3. Two independent PID temperature controllers are used for heating temperature control.
4. The OSU heat release rate tester is equipped with a fully automatic pneumatic sample propulsion device and shielding door device;
5. It has an upper burner and a movable lower burner;
6. A rotor flow meter can be used to adjust the gas flow rate of upper and lower burners.
7. The OSU heat release rate tester is equipped with a movable T-type calibration burner device and flow controller;
8. Mass flow controller is applied to thermopile temperature calibration automatically.
9. The Water-cooled heat flow meter is equipped with a cooling mode to measure the heat radiation flux of the fire surface.
10. The air temperature control device can provide constant temperature and flow of air for the test chamber.
11. The orifice flowmeter is used to measure the flow pressure entering the test bin.
12. The OSU heat release rate tester is equipped with a data acquisition system and heat release standard test software.

Specification:

Item Name	OSU FAR Appendix F to Part 25 Aviation Parts Heat Release Rate Tester
Size	760mm (W) x 1850mm x (H) x 850mm (D)
Weight	218KG
Electricity requirements	220 V, 35 Amps
Ambient temperature	10 ºC to 35 ºC
Auxiliary Gas	Constant Temperature and Constant Current Gas
Combustion gas	Methane
Standard	ASTM E906, BSS 7322, FAR PART 25 APPENDIX F Part IV
Applications	Aviation Materials