Aviyasyon Syèj Kousen gaz Konbisyon Sistèm
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
Ka NexGen gaz avyasyon brûler a ki te apwouve pa FAA nan Administrasyon an Aviyasyon Federal nan peyi Etazini a dwe itilize pou fè tès ki degaje konbisyon gaz nan materyèl avyasyon anpil. Kòm Park DPL nan 3400, Lennox ki gen konpòtman egzanplè OB-32 ak Carlin ki gen konpòtman egzanplè 200 CRD deja rekonèt pa FAA gen tout te sispann, FAA te devlope brûler a NexGen pou jenerasyon kap vini an brûler gaz aviyasyon. NexGen konbustyon adopte prensip la operasyon nan konbustyon nan moun k'ap viv koulye anvan yo, e yo ka avèk presizyon mezire paramèt yo egzamen sou gaz la opinyon ak gaz. An menm tan an, enstriman an ka fasilite ajou nan lavni nan FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Karakteristik Pwodwi Pèfòmans of the Aviyasyon Syèj Kousen gaz Konbisyon Sistèm
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen brûler gaz avyasyon an gen ladan beke, bouch gaz, ignitron, tren gaz, fiksateur, tib vantilasyon ak koki, mòflè, rezistans acoustic ak lòt konpozan.
3. Equipped with fuel pressure gauge, fuel solenoid valve, fuel temperature detection device, air pressure regulating valve, air temperature detection device;
4. Equipped with a gas and air temperature control device ice bath with a volume not less than 2 x 0.14 m3, the fuel temperature can be controlled.
5. Pa chanje bouch gaz ak D 'presyon lè a, nòm ofisyèl tès diferan ka satisfè.
6. The burner covers the fuel pipeline and fuselage with insulation blanket.
7. The flame temperature provided by NexGen aviation fuel burner is not less than: 2000 +50;
8. NexGen brûler gaz avyasyon ka bay pa mwens pase 10.6w / cm2 nan koule chalè flanm dife.
9. Module unit of NexGen burner support system;
10. Powder coated steel frame, including an integrated digital ruler;
11. Calibrable weighing unit;
12. Movable seat cushion test device, movable drip collecting tray;
13.Seven ceramic-encapsulated, metal sheaths and grounded K-type (nickel-chromium-nickel-aluminium) thermocouples with a diameter of 1.6 mm should be used for calibration. Their conductors should have an external diameter of 0.254 mm, a cross-sectional area of 0.0507 mm2 and a resistance of 361_/km (American wire gauge 30 AWG). The thermocouple should be fixed on an angle steel bracket to form a thermocouple comb so that it can be placed on the sample bracket during calibration.
14. The heat radiation flux sensor is equipped with a cooling device and installed on a fixed bracket.
Pwodwi paramèt nan Aviyasyon Syèj Kousen gaz Konbisyon Sistèm
Applications: Aviation Materials
Creole: AITM èrbus Creole: AITM 2,0009
BSS Boeing Creole: BSS 7303
FAA Federal Administrasyon Aviyasyon: FAR PATI 25 APENDIS F Pati II
| Dimansyon | 1500 mm (W) x 1800 mm (H) x 900 mm |
| Pwa | 150 KG |
| elektrisite kondisyon | 220V, 10A |
| tanperati anbyen | 10 ℃ a 35 ℃ |
| kondisyon gaz | avyasyon kewozin |
| kondisyon gaz | pa mwens pase 120 PSI COMPRESSOR lè |
