Kursiga barkin Aviation Shiidaalka sari System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
The gubi shidaalka diyaaradaha NexGen ansixiyey FAA Duulista Maamulka Federaalka ah ee Mareykanka waxaa loo isticmaali karaa baaritaanka sari shidaalka ka mid ah maaddooyinka badan duulista. Sida DPL Park ee 3400, Lennox Model OB-32 iyo Carlin Model 200 CRD hore aqoonsan FAA ayaa lagu joojiyo, FAA ayaa sameeyay gubi NexGen ee jiilka soo socda ee gubidda shidaalka diyaaradaha. NexGen combustor qaadanayaa ku mabda 'hawlgalka qarnigan hore combustor ah, oo si sax ah loo cabbiro karo oo xuduudaheedu imtixaanka gaaska talooyin iyo shidaalka. Isla mar ahaantaana, qalab ah loo fududeeyo karaa hagaajinta mustaqbalka ee FAA ah.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Sifooyinka Performance Product of the Kursiga barkin Aviation Shiidaalka sari System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen gubi shidaalka diyaaradaha ka mid ah Baabbi'iyihii, biiyaha shidaalka, Qaraxshe, rail shidaalka, jiheeye, tube hawo iyo qolof, iskaamiinto, iska caabin ah loomana baahno iyo qaybaha kale.
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. By beddelo biiyaha shidaalka iyo talooyin cadaadiska hawada, heerarka imtixaanka kala duwan loo fulin karo.
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 gubi shidaalka diyaaradaha aan ka yarayn 10.6w / cm2 socodka kulaylka olol ku siin kara.
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.
Product xuduudaheedu ee Kursiga barkin Aviation Shiidaalka sari System
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
inaysan muhiimadiisu Boeing Standard: inaysan muhiimadiisu 7303
FAA Maamulka Aviation Federaalka: FAR PART 25 LIFAAQA F Qaybta II
| Cabirka | 1500 mm (W) x 1800 mm (H) x 900 mm |
| miisaanka | 150 kg |
| shuruudaha korontada | 220V, 10A |
| heerkulka | 10 ℃ 35 ℃ |
| shuruudaha Shiidaalka | shito duulista |
| shuruudaha Gas | aan ka yarayn 120 PSI kombaresarada hawada |
