Zrakoplovstvo sjedala sustavu izgaranja goriva
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
NexGen avionsko gorivo plamenika odobrila FAA od Federal Aviation Administration SAD-a može se koristiti za ispitivanje izgaranja goriva mnogih zrakoplovnih materijala. Kao Park DPL 3400, Lennox model OB-32 i Carlin model 200 CRD prethodno priznata od strane FAA svi su prekinuti, FAA je razvio NexGen plamenik za sljedeću generaciju zrakoplovstva gorivo plamenika. NexGen Upaljivački usvaja načelo rada prethodne generacije za izgaranje, a može točno izmjeriti test parametre ulaznog plina i goriva. U isto vrijeme, instrument može olakšati buduću nadogradnju FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Radne značajke proizvoda of the Zrakoplovstvo sjedala sustavu izgaranja goriva
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen zrakoplovstva gorivo plamenika sadrži spojler, mlaznica za gorivo, upaljač, razvodnik goriva, popravljač, ventilacijski cijevi i ljuska, prigušivač, akustični otpornost i druge komponente.
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. Promjenom mlaznica za gorivo i ulaz tlaka zraka, različite ispitne norme mogu biti ispunjeni.
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 zrakoplovstva gorivo plamenika može osigurati najmanje 10.6w / cm2 protoka plamena topline.
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.
Proizvod parametri za Zrakoplovstvo sjedala sustavu izgaranja goriva
Applications: Aviation Materials
Standardni: AITM Airbus Standardni: AITM 2,0009
BSS Boeing Standardni: BSS 7303
FAA Federal Aviation Administration: FAR DIO 25 DODATAK F II dio
| Dimenzije | 1.500 mm (W) x 1800 mm (H) x 900 mm |
| Težina | 150 KG |
| zahtjevi za struju | 220V, 10A |
| Sobna temperatura | 10 do 35 ℃ ℃ |
| zahtjevi goriva | zrakoplovstva kerozin |
| zahtjevi za plin | ne kompresor manje od 120 PSI zrak |
