Aviation Seat Cuscino System Combustion Fuel
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
U gaz Favilli NexGen assicurati da Faa di u Federal Aviation Administration di i Stati Uniti d'America pò ièssiri usatu per essai splusioni di benzina di parechji materiali aviation civile. Comu lu Park DPL 3400, Lennox Model dérogatoire-32 è Carlin Model 200 CRD digià ricunnisciutu da Faa sò tutte state discontinued, Faa hà sviluppatu u merci NexGen per u prossimu generazione di Bunsen Favilli. NexGen combustor discènninu u principiu di funziunamentu di u combustor prima generazioni, e pò misurari dapoi i paràmetri di testu di u gasu messu e benzina. À u listessu tempu, u strumentu pò facilità a prucedura avvene di Faa.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Caratteristiche danza prodottu of the Aviation Seat Cuscino System Combustion Fuel
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen merci Favilli include spoiler, attendant benzina, igniter, tombu di benzina, fixer, tubu Cappa e attesa, Marmitta, resistenza Acoustic e àutri cumpunenti.
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. By cambiendu attendant carburante è messu prissioni 'aria, sfarente sicurità testu pò esse scontra.
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 merci Favilli pò micca menu chè 10.6w / cm2 di flussu calori fiara vuluntarii.
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.
Prodottu login di Aviation Seat Cuscino System Combustion Fuel
Applications: Aviation Materials
Standard: AITM airbus in Standard: AITM 2,0009
BSS #crash Standard: BSS 7303
Faa Federal Aviation Administration: luntanu PART 25 penale F Part II
dimensioni | 1500 MM (W) x 1800 MM (H) ex 900 mm in |
Peso | 150 KG |
esigenze elittricità | 220V, 10A |
Temperature puesia | 10 ℃ à 35 ℃ |
esigenze Fuel | kérosène Aviation |
esigenze Gas | ùn jacket 'aria cchiù picca 120 Psi |