Aviation Seat Cushion Sistem Pembakaran Bahan Api
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
The NexGen pembakar bahan api penerbangan yang diluluskan oleh FAA Pentadbiran Penerbangan Persekutuan Amerika Syarikat boleh digunakan untuk ujian pembakaran bahan api banyak bahan-bahan penerbangan. Sebagai Taman DPL 3400, Lennox Model OB-32 dan Carlin Digital 200 CRD diiktiraf sebelum ini oleh FAA semua telah dihentikan, FAA telah membangunkan pembakar NexGen untuk generasi akan datang pembakar bahan api penerbangan. NexGen pembakar mengamalkan prinsip operasi pembakar generasi sebelumnya, dan tepat boleh mengukur parameter ujian gas input dan bahan api. Pada masa yang sama, suratcara boleh memudahkan naik taraf masa depan daripada FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Ciri-ciri prestasi produk of the Aviation Seat Cushion Sistem Pembakaran Bahan Api
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen pembakar bahan api penerbangan termasuk spoiler, muncung bahan api, igniter, rel bahan api, tukang pasang, tiub pengudaraan dan shell, muffler, rintangan akustik dan komponen lain.
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. Dengan menukar muncung bahan api dan input tekanan udara, standard ujian yang berbeza dapat dipenuhi.
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 pembakar bahan api penerbangan boleh memberikan tidak kurang daripada 10.6w / cm2 aliran api haba.
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.
Produk parameter daripada Aviation Seat Cushion Sistem Pembakaran Bahan Api
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
FAA Pentadbiran Penerbangan Persekutuan: FAR BAHAGIAN 25 LAMPIRAN F Part II
Ukuran | 1500 mm (W) x 1800 mm (H) x 900 mm |
Berat | 150 KG |
keperluan elektrik | 220V, 10A |
Suhu ambien | 10 ℃ untuk 35 ℃ |
keperluan bahan api | minyak tanah penerbangan |
keperluan gas | tidak kurang daripada 120 PSI pemampat udara |