Aviation Wurin zama matashi Fuel konewa System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
A NexGen jirgin sama man fetur kuka amince da FAA ta Tarayya sufurin jiragen sama Administration na Amurka za a iya amfani da man fetur konewa gwaji na da yawa jirgin sama kayan. Kamar yadda Park DPL 3400, Lennox Model Likitan mata-32 da kuma Carlin Model 200 CRD baya gane ta FAA sun duk aka katse, FAA ya ci gaba da NexGen kuka ga na gaba ƙarni na jirgin sama da man fetur burners. NexGen combustor rungumi dabi'ar aiki manufa na baya tsara combustor, kuma zai iya daidai auna gwajin sigogi na shigar da gas da kuma man fetur. A lokaci guda, da kayan aiki na iya tallafa a nan gaba inganci na FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Samfurin Performance halaye of the Aviation Wurin zama matashi Fuel konewa System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen jirgin sama man fetur kuka hada da batawa, man bututun ƙarfe, igniter, man dogo, fixer, samun iska tube da kuma harsashi, zanen wuya, Ft Irfan juriya da kuma sauran gyara.
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. Ta canza man fetur bututun ƙarfe da kuma iska matsa lamba shigar, daban-daban gwajin nagartacce za a iya hadu.
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 jirgin sama man fetur kuka iya samar da wani kasa da 10.6w / cm2 na harshen wuta zafi kwarara.
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.
Samfurin sigogi na Aviation Wurin zama matashi Fuel konewa System
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
FAA Tarayya sufurin jiragen sama Administration: FAR SASHE 25 RATAYE F Part II
| girma | 1500 mm (W) x 1800 mm (H) x 900 mm |
| Weight | 150 KG |
| da wutar lantarki da bukatun | 220V, 10A |
| yanayi zazzabi | 10 ℃ zuwa 35 ℃ |
| Fuel bukatun | jirgin sama kananzir |
| gas bukatun | babu kasa da 120 psi iska kwampreso |
