Osu Prigiuneru Release Rate Tester
OSU Heat Release Rate Tester Stainless Steel Combustion Test Chamber Equipped
Nantu à u prodottu di Osu hHeat Release Rate Tester
The OSU heat release rate tester approved by FAA of the Federal Aviation Administration of the United States was originally designed by Smith of Ohio State University in 1972, and later became a FAA designated combustion test instrument for testing the heat release rate of Aeronautical materials. The test standards are FAR Part 25 Appendix F Part IV, Airbus AITM 2.00. 06, Boeing BSS 7322.
caratteristiche danza di Osu Prigiuneru Release Rate Tester
1. Stainless steel combustion test chamber with 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. Equipped with fully automatic pneumatic sample propulsion device and shielding door device;
5. Equipped with upper burner and movable lower burner;
6. Rotor flowmeter can be used to adjust the gas flow rate of upper and lower burners.
7. Equipped with movable T-type calibration burner device and flow controller;
8. Mass flow controller is applied to thermopile temperature calibration automatically.
9. Water-cooled heat flow meter is equipped with cooling mode to measure the heat radiation flux of the fire surface.
10. The air temperature control device can provide constant temperature and flow air for the test chamber.
11. The orifice flowmeter is used to measure the flow pressure entering the test bin.
12. Equipped with data acquisition system and heat release standard test software.
Prodottu login of OSU Heat Release Rate Tester
| Size | 760mm (W) x 1850mm x (H) x 850mm (D) |
| Peso | 218KG |
| esigenze elittricità | 220 V, 35 Amps |
| Temperature puesia | 10 ℃ à 35 ℃ |
| Gas ausiliari | Constant Temperature è Constant Gas Current |
| a gas Combustion | methane |
| Standard | AITM 2,0006, BSS 7322, luntanu PART 25 penale F Part IV |
| Travaux | Materials Aviation |
