उत्पादन कामगिरी वैशिष्ट्ये  of the एव्हिएशन आसन उशी इंधन ज्वलन प्रणाली

1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGEN विमानचालन इंधन बर्नर नाश करणारा, इंधन तोंड, igniter, इंधन रेल्वे, असलेला नागपूरचा बुकी, वायुवीजन ट्यूब आणि शेल रुमाल, अकौस्टिक प्रतिकार आणि इतर घटक आहेत.
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. इंधन तोंड आणि हवाई दबाव इनपुट बदलून, विविध चाचणी मानके भेटले जाऊ शकते.
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 विमानचालन इंधन बर्नर कमी ज्योत उष्णता प्रवाह 10.6w / CM2 पेक्षा प्रदान करू शकता.
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.