OSU Heat Release Rate Tester
OSU Heat Release Rate Tester Stainless Steel Combustion Test Chamber Equipped
Produk inligting van OSU hHeat Release Rate Tester
Die OSU hitte vrylating koers tester deur FAA van die Federal Aviation Administration van die Verenigde State van Amerika goedgekeur is oorspronklik ontwerp deur Smith van Ohio State University in 1972, en later 'n FAA aangewese verbranding toets instrument vir die toets van die hitte vrylating koers van Lugvaartkundige materiaal. Die toets standaarde is agterkant 25 Bylaag F Deel IV, Airbus AITM 2.00. 06, Boeing BSS 7322.
Prestasie eienskappe van OSU Heat 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.
Produk parameters of OSU Heat Release Rate Tester
grootte | 760mm (W) x 1850mm x (H) x 850mm (D) |
gewig | 218KG |
elektrisiteit vereistes | 220 V, 35 Amps |
Omgewingstemperatuur | 10 ℃ tot 35 ℃ |
hulp Gas | Konstante temperatuur en konstante Huidige Gas |
verbranding gas | metaan |
Standard | AITM 2,0006, BSS 7322, agterkant 25 BYLAAG F Deel IV |
aansoeke | Aviation Materials |