Vaalele aluga Nofoa System Combustion suauu
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
O le burner suauu vaalele NexGen faamaonia e FAA o le Malo o Vaalele Pulega o le Iunaite Setete e mafai ona faaaoga mo suauu combustion suʻega o le tele o mea tau vaalele. A o Park DPL 3400, Lennox Faataitaiga OB-32 ma Carlin Faataitaiga 200 CRD muamua aloaia e FAA ua le toe faaauauina uma, ua atiina ae FAA le burner NexGen mo le tupulaga e sosoo ai o vaalele burners suauu. Combustor NexGen faʻatamafaiina le faagaoioiga mataupu faavae o le combustor tupulaga talu ai, ma e mafai ona saʻo fuaina le suega le faataamilosaga o le sao o penisini ma suauu. I le taimi lava lea e tasi, e mafai ona faafaigofie ai le pepa faaletulafono le faaleleia lumanai o FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Uiga Faatinoga o Galuega oloa of the Vaalele aluga Nofoa System Combustion suauu
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. burner suauu vaalele NexGen aofia faaleaga, au suauu, igniter, suauu nofoaafi, fixer, ea faagaau ma le atigi, e pupuni ai, tetee acoustic ma isi vaega.
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. E ala i le suia o suauu au ma le ea sao o uunaiga, e mafai ona feiloai tulaga faatonuina tofotofoga eseese.
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. burner suauu vaalele NexGen mafai ona maua ai e le itiiti ifo nai lo 10.6w / cm2 o afi tafe vevela.
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.
Oloa tapulaa o le Vaalele aluga Nofoa System Combustion suauu
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
FAA Feterale Vaalele Faafoeina: MAMAO VAEGA 25 FAAOPOOPOGA F Vaega II
| fua | 1500 mm (W) x 1800 mm (H) x 900 mm |
| mamafa | 150 kilokalama |
| manaoga o le eletise | 220V, 10a |
| vevela Ambient | 10 ℃ e 35 ℃ |
| suauu manaoga | karasini vaalele |
| kasa manaoga | leai se compressor ea itiiti ifo nai lo le 120 PSI |
