Avjazzjoni Seat cushion Fjuwil Sistema Kombustjoni
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
Il NexGen berner fjuwil għall-avjazzjoni approvata mill-FAA tal-Federal Aviation Administration tal-Istati Uniti jistgħu jintużaw għall-ittestjar kombustjoni tal-fjuwil ta 'materjali avjazzjoni ħafna. Peress li l-DPL Park 3400, Lennox Mudell OB-32 u Carlin Mudell 200 DRK rikonoxxuti qabel mill-FAA kollha ġew tkomplewx, FAA żviluppat il-burner NexGen għall-ġenerazzjoni li jmiss ta 'berners tal-karburant tal-avjazzjoni. NexGen combustor jadotta l-prinċipju operazzjoni ta 'l-combustor ġenerazzjoni preċedenti, u jistgħu jitkejjel b'mod preċiż il-parametri tat-test ta' l-gass input u l-fjuwil. Fl-istess ħin, l-istrument jista 'jiffaċilita l-upgrade futur ta' FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Karatteristiċi tar-rendiment tal-prodott of the Avjazzjoni Seat cushion Fjuwil Sistema Kombustjoni
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen berner fjuwil għall-avjazzjoni jinkludi spoiler, iż-żennuna tal-karburant, tagħmir tat-tqabbid, bil-ferrovija tal-fjuwil, Fixer, tubu ventilazzjoni u qoxra, silencer, reżistenza akustiċi u komponenti oħra.
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. Billi tinbidel żennuna fjuwil u l-input pressjoni ta 'arja, l-istandards tat-test differenti jistgħu jiġu sodisfatti.
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 berner fjuwil għall-avjazzjoni jistgħu jipprovdu mhux inqas minn 10.6w / cm2 tal-fluss tas-sħana fjamma.
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.
Prodott parametri ta Avjazzjoni Seat cushion Fjuwil Sistema Kombustjoni
Applications: Aviation Materials
standard: AITM Airbus Standard: AITM 2.0009
BSS Boeing Standard: BSS 7303
FAA Amministrazzjoni Federali tal-Avjazzjoni: FAR PARTI 25 APPENDIĊI F Parti II
| dimensjonijiet | 1500 mm (W) x 1800 mm (H) x 900 mm |
| piż | 150 KG |
| rekwiżiti elettriku | 220v, 10A |
| temperatura ambjentali | 10 ℃ għal 35 ℃ |
| rekwiżiti tal-fjuwil | pitrolju avjazzjoni |
| ħtiġijiet tal-gass | ebda kompressur arja anqas minn 120 PSI |
