Продукт Performance мүнөздөмөлөрү  of the Aviation сизчи отундун күйүү системасы

1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. генэ күйүүчү жаздыргыч кыйратуучуну, күйүүчү май куюуучу шланганы байлап, igniter, отун темир жол, кемтиксиз, желдетүү түтүктү жана жер кыртышын, глушитель, акустикалык каршылык жана башка компоненттерди камтыйт.
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. шланганы жана аба басымы киргизүүнү өзгөртүү менен, ар кандай тест стандарттары сакталган болот.
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. генэ күйүүчү жаздыргыч жок жалын жылуулук агымынын 10.6w / см2 аз камсыз болот.
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.