Aviation Seat fom Fuel combustion System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
The NexGen ụgbọelu mmanụ ụgbọala burner mma site FAA nke Federal Aviation Administration nke United States ga-eji na mmanụ ụgbọala combustion ule nke ọtụtụ ụgbọelu ihe. Dị ka Park DPL 3400, Lennox Model Ob-32 na Carlin Model 200 CRD mbụ ghọtara site FAA niile e kwụsịrị, FAA azụlitewo na NexGen burner maka ọgbọ ọzọ nke ụgbọelu mmanụ ụgbọala burners. NexGen combustor adopts ọrụ ụkpụrụ nke gara aga ọgbọ combustor, na ike n'ụzọ ziri ezi tụọ ule afọ nke input gas na mmanụ ụgbọala. N'otu oge ahụ, bụ ngwá nwere ike ikwado n'ọdịnihu upgrade nke FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Product Performance e ji mara of the Aviation Seat fom Fuel combustion System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen ụgbọelu mmanụ ụgbọala burner agụnye nāpunara, mmanụ nozulu, igniter, mmanụ okporo ígwè, fixer, ventilashion tube na shei, mofla, now na-eguzogide ndị ọzọ mmiri.
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. Site na-agbanwe mmanụ ụgbọala nozulu na ikuku input, dị iche iche ule ụkpụrụ nwere ike zutere.
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 ụgbọelu mmanụ ụgbọala burner nwere ike inye dịghị ihe na-erughị 10.6w / cm2 nke ire ọkụ okpomọkụ eruba.
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 parameters nke Aviation Seat fom Fuel combustion System
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
FAA Federal Aviation Administration: nnọọ IKPEHE 25 ODIDE NTụKWASị Ihe F Part II
| akụkụ | 1500 mm (W) x 1800 mm (H) x 900 mm |
| ibu | 150 KG |
| eletrik chọrọ | 220V, 10a |
| ihere okpomọkụ | 10 ℃ 35 ℃ |
| mmanụ ụgbọala chọrọ | ụgbọelu kerosin |
| gas chọrọ | dịghị ihe na-erughị 120 PSI ikuku Compressor |
