Aviation Seat Bantal bakar System Combustion
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
The NexGen burner bahan bakar aviation disetujoni dening FAA Federal Aviation Administration Amerika Serikat bisa digunakake kanggo testing pangobongan bahan bakar saka bahan-bahan aviation. Minangka Park DPL 3400, Lennox Model OB-32 lan Karlin Model 200 CRD sadurunge dikenali dening FAA wis kabeh wis mandheg, FAA wis dikembangaké ing burner NexGen kanggo generasi sabanjure Burners bahan bakar aviation. NexGen combustor adopts asas operasi saka combustor generasi sadurunge, lan kanthi bisa ngukur paramèter test saka gas input lan bahan bakar. Ing wektu sing padha, instrument bisa nggampangake upgrade mangsa FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Ciri Performance Product of the Aviation Seat Bantal bakar System Combustion
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen bahan bakar aviation burner kalebu spoiler, nozzle bahan bakar, igniter, alur bahan bakar, fixer, tabung ventilasi lan Nihan, saringan, resistance akustik lan komponen.
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. Kanthi ngganti nozzle bahan bakar lan input online meksa, standar test beda bisa ketemu.
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 bahan bakar aviation burner bisa nyedhiyani ora kurang saka 10.6w / cm2 saka aliran semangat panas.
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.
Product paramèter saka Aviation Seat Bantal bakar System Combustion
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
FAA Administrasi Aviation Federal: Tebih PART 25 Lampiran F Part II
| Ukuran | 1500 mm (W) x 1800 mm (H) x 900 mm |
| bobot | 150 KG |
| syarat listrik | 220V, 10A |
| suhu sekitar | 10 ℃ kanggo 35 ℃ |
| syarat bahan bakar | kerosene aviation |
| syarat gas | ora kurang saka 120 PSI kompresor udara |
