Aviation Seat cushion Suluh System durukan
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
The NexGen burner suluh aviation disatujuan ku FAA tina Federal Aviation Administration Amérika Sarikat bisa dipaké pikeun nguji durukan suluh tina loba bahan aviation. Salaku Taman DPL 3400, Lennox Modél OB-32 sarta Carlin Modél 200 CRD saméméhna dipikawanoh ku FAA geus kabeh geus dilanjutkeun, FAA geus ngembangkeun éta burner NexGen keur generasi saterusna burners suluh aviation. NexGen combustor adopts prinsip operasi tina combustor generasi saméméhna, sarta akurat bisa ngukur parameter test tina gas asupan jeung suluh. Dina waktu nu sarua, instrumen bisa mempermudah pamutahiran kahareup 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 Performance produk of the Aviation Seat cushion Suluh System durukan
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen suluh aviation burner ngawengku spoiler, nozzle suluh, igniter, rail suluh, fixer, tube ventilasi jeung cangkang, saringan, résistansi akustik sareng komponenana lianna.
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. Ku ngarobah nozzle suluh na input tekanan hawa, standar test béda bisa patepung.
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 suluh aviation burner bisa nyadiakeun teu kurang ti 10.6w / cm2 aliran seuneu panas.
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 tina Aviation Seat cushion Suluh System durukan
Applications: Aviation Materials
Standar: AITM Airbus Standar: AITM 2,0009
BSS Boeing Standar: BSS 7303
FAA Administrasi Aviation Federal: tebih bagian 25 Appendix F Part II
| dimensi | 1500 mm (W) x 1800 mm (H) x 900 mm |
| beurat | 150 KG |
| syarat listrik | 220V, 10A |
| hawa ambient | 10 ℃ nepi ka 35 ℃ |
| syarat suluh | minyak tanah aviation |
| syarat gas | teu kurang ti 120 PSI compressor hawa |
