Aviation Seat Cushion Fuel Combustion System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
De NexGen loftfeart fuel burner goedkard troch FAA fan de Federale Aviation Administration fan 'e Feriene Steaten kin brûkt wurde foar branje ferbaarning testen fan in protte aviation materialen. As it Park DPL 3400, Lennox Model OB-32 en Carlin Model 200 CRD earder werkend troch FAA hawwe allegear al staakt, FAA hat ûntwikkele de NexGen burner foar de folgjende generaasje fan de fleanderij brânstof burners. NexGen combustor oannimt de eksploitaasje prinsipe fan de foarige generaasje combustor, en kin sekuer mjitten de test parameters fan de ynfier gas en brânstof. Tagelyk, it ynstrumint kin fasilitearje de takomst fernijing fan FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Produkt Performance skaaimerken of the Aviation Seat Cushion Fuel Combustion System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen loftfeart fuel burner omfiemet spoiler, brânstof nozzle, igniter, brânstof spoar, Fixer, ventilation buis en shell, muffler, akoestyske ferset en oare komponinten.
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. Troch it feroarjen fan brânstof mûlestik en loft druk ynput, ferskillende test standerts kinne foldien wurde.
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 loftfeart fuel burner kin foarsjen net minder as 10.6w / cm2 fan flam waarmte flow.
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.
Produkt parameters of Aviation Seat Cushion Fuel Combustion System
Applications: Aviation Materials
Standert: AITM Airbus Standert: AITM 2,0009
BSS Boeing Standert: BSS 7303
FAA Federal Aviation Administration: FAR DIEL 25 Taheakke F Part II
| Ofmjittings | 1500 mm (W) x 1800 mm (H) x 900 mm |
| Gewicht | 150 KG |
| elektrisiteit easken | 220V, 10A |
| Omjouwingstemperatuer | 10 ℃ to 35 ℃ |
| Fuel easken | aviation kerosine |
| gas easken | net minder as 120 PSI lucht compressor |
