Letalstvo sedežne blazine goriva Zgorevanje sistem
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
NexGen gorilnik letalsko gorivo, ki ga FAA Zvezne uprave za letalstvo Združenih držav odobri se lahko uporablja za testiranje izgorevanjem goriva številnih letalskih materialov. Kot Park DPL 3400, Lennox Model OB-32 in Carlin Model 200 CRD FAA prej pripoznana bili vsi prekinjeni, je FAA razvil NexGen gorilnik za naslednjo generacijo gorilnikov letalskega goriva. NexGen gorilec sprejema načelo delovanja prejšnje generacije gorilniku, in lahko natančno merjenje preskusne parametre vhodnega plina in goriva. Ob istem času, lahko instrument olajša prihodnje nadgradnjo FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Delovne lastnosti izdelka of the Letalstvo sedežne blazine goriva Zgorevanje sistem
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen gorilnik letalsko gorivo vsebuje spojler, šoba za gorivo, vžigalno, železniškega goriva, fiksirne, prezračevalne cevi in lupino, dušilnik, akustični odpornost in druge komponente.
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. Lahko S spreminjanjem šobe goriva in dovod zraka pod pritiskom, je treba izpolniti različne testne standarde.
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 gorilnika letalsko gorivo lahko najmanj 10.6w / cm2 toka plamensko toplote zagotoviti.
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.
Izdelek parametri za Letalstvo sedežne blazine goriva Zgorevanje sistem
Applications: Aviation Materials
Standardne: AITM Airbus Standardne: AITM 2,0009
BSS Boeing Standardni: TVS 7303
FAA Zvezna uprava za letalstvo: FAR DEL 25 DODATEK F Part II
| dimenzije | 1500 mm (š) x 1800 mm (H) x 900 mm |
| Utež | 150 kg |
| zahteve za električno energijo | 220V, 10A |
| Sobna temperatura | 10 ℃ do 35 ℃ |
| zahteve za gorivo | letalski kerozin |
| zahteve za plin | najmanj 120 PSI kompresor |
