Āhuatanga mahinga Hua  of the Aviation Seat urunga Fuel Pūnaha Te tahu

1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen rererangi wahie pūwera ngā kaipahua, wahie pupuha, igniter, wahie rail, fixer, ventilation ngongo, me te anga, puta auahi, resistance oro me ētahi atu wāhanga.
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. Mā te huri wahie pupuha me tāuru pēhanga hau, e taea te tutaki paerewa whakamātautau rerekē.
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;
Kahore iti iho i te 10.6w / cm2 o te rere wera mura taea 8. NexGen rererangi wahie pūwera whakarato.
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.