OSU brzinu oslobađanja toplote Tester
OSU Heat Release Rate Tester Stainless Steel Combustion Test Chamber Equipped
Informacije o proizvodu za OSU hHeat priopćenju Rate Tester
Brzinu oslobađanja tester OSU topline odobren od strane FAA Savezne administracija za avijaciju SAD-a je originalno dizajnirao Smit Ohio State University 1972. godine, a kasnije je postao FAA određen sagorijevanje test instrument za testiranje brzina oslobađanja toplote Aeronautical materijala. Standarde testiranja su daleko Dio 25 Dodatak F Dio IV, Airbus AITM 2.00. 06, Boeing BSS 7322.
Karakteristike performansi OSU brzinu oslobađanja toplote 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.
Proizvod parametri of OSU Heat Release Rate Tester
Veličina | 760mm (Š) x 1850mm x (H) x 850mm (D) |
težina | 218KG |
potreba za električnom energijom | 220 V, 35 Amps |
temperatura okoline | 10 ℃ do 35 ℃ |
Pomoćni plin | Konstantna temperatura i Constant Current Gas |
sagorijevanje plina | metan |
standard | AITM 2,0006, BSS 7322, FAR Dio 25 DODATAK F Dio IV |
Aplikacije | avijacija Materijali |