OSU Heat Release Rate Tester
OSU Heat Release Rate Tester Stainless Steel Combustion Test Chamber Equipped
Produkt informacion i OSU hHeat Release Rate Tester
Shkalla Lirimin OSU nxehtësisë kontrollor aprovuar nga FAA i Administratës Federale të Aviacionit e Shteteve të Bashkuara ishte projektuar fillimisht nga Smith e Ohio State University në vitin 1972, dhe më vonë u bë një instrument FAA caktuar provë me djegie për testimin e shkallës ngrohjes lirimin e materialeve Aeronautike. Standardet e testit janë shumë Part 25 Shtojca F Pjesa IV, Airbus AITM 2.00. 06, Boeing BSS 7322.
karakteristikat e performancës të OSU nxehtit 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.
Produkt parametrat of OSU Heat Release Rate Tester
madhësi | 760mm (W) x 1850mm x (H) x 850mm (D) |
peshë | 218KG |
kërkesat e energjisë elektrike | 220 V, 35 Amps |
temperatura e ambientit | 10 ℃ në 35 ℃ |
ndihmëse Gas | Temperatura konstante dhe Gas Constant aktuale |
gazit të djegies | metan |
standard | AITM 2,0006, BSS 7322, FAR PJESA 25 SHTOJCA F Pjesa IV |
Aplikimet | Materialet aviacionit |