Aviation Seat Këssen Benzin Verbrennungsmotor System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
D'NexGen Loftfaart Brennstoff au vun Faà vun der Federal Aviation Administration vun der USA guttgeheescht kann fir Bensin Verbrennungsmotor Testen vum vill Loftfaart Materialien benotzt ginn. Wéi de Park DPL 3400, CRD Lennox Model OB-32 an Carlin Model 200 virdrun duerch Faà unerkannt hunn all agestallt gouf, huet de Faà NexGen au fir déi nächst Generatioun vun Loftfaart Brennstoff Brenner entwéckelt. NexGen combustor bestëmmten der Operatioun Prinzip vun der viregter Generatioun combustor, a kann präziist der Test Parameteren vun der Input Gas a Bensin moossen. An der selwechter Zäit, kann d'Instrument Zukunft Upgrade vun Faà erliichtert.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Produit leeschtungsplang Charakteristiken of the Aviation Seat Këssen Benzin Verbrennungsmotor System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen Loftfaart Brennstoff au ëmfaasst Spoiler, Brennstoff nozzle, igniter, Brennstoff Persounegare, fixer, Ventilatioun eraus an Réibau, zreck muss, akustesch Resistenz an aner Deeler.
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. Vun Zaïtgeescht Brennstoff nozzle an Loftdrock Input, kann verschidden Test Standarden erfëllt ginn.
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 Loftfaart Brennstoff au kann net manner wéi déi 10.6w / cm2 vun Flam Hëtzt Flux.
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.
Produit Parameteren vun Aviation Seat Këssen Benzin Verbrennungsmotor System
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
Faà Federal Aviation Administration: wäit PART 25 Betriebspläng F Part II
| Dimensiounen | 1500 mm (W) x 1800 mm (H) x 900 mm |
| Gewiicht | 150 kg |
| Stroum Ufuerderunge | 220V, 10A |
| entgoe Temperatur | 10 ℃ bis 35 ℃ |
| Brennstoff Ufuerderunge | Loftfaart kerosene |
| Gas Ufuerderunge | net manner wéi 120 ass keng Gefor Loft bekenne |
