Aviation Rooj Cushion Roj Combustion System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
Lub NexGen aviation roj burner kev pom zoo los ntawm FAA ntawm Tsoom Fwv Teb Chaws chaw ua dav hlua Administration ntawm lub tebchaws United States yuav siv tau rau cov roj combustion kuaj ntawm ntau aviation cov ntaub ntawv. Raws li cov tiaj ua si DPL 3400, Lennox Model OB-32 thiab Carlin Model 200 CRD yav tas los paub los ntawm FAA tau tag nrho cov tau txiav, FAA tau tsim lub NexGen burner rau cov tiam tom ntej ntawm chaw ua dav hlua roj burners. NexGen combustor adopts lub lag luam hauv paus ntsiab lus ntawm yav dhau los tiam combustor, thiab muaj peev xwm kom meej ntsuas lub xeem tsis muaj lub tswv yim roj thiab roj. Nyob rau tib lub sij hawm, lub twj paj nruag yuav pab txhawb lub neej yav tom ntej txawj tej yam ntxiv ntawm FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Khoom Performance yam ntxwv of the Aviation Rooj Cushion Roj Combustion System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen aviation roj burner muaj xws li spoiler, roj nozzle, igniter, roj tsheb nqaj hlau, fixer, cua raj thiab plhaub, yam khoom uas kom lub tsheb tsis nrov, acoustic kuj thiab lwm yam.
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. Los ntawm kev hloov roj nozzle thiab cua siab tawm tswv yim, sib txawv xeem qauv yuav tau ntsib.
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 aviation roj burner yuav muab tsis muaj tsawg tshaj li 10.6w / cm2 ntawm nplaim tshav kub txaus.
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.
Khoom tsis ntawm Aviation Rooj Cushion Roj Combustion System
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
FAA Federal Aviation Administration: DEB FEEM 25 COV LUS QHIA NTXIV F Part II
| Qhov ntev | 1500 hli (W) x 1800 hli (H) x 900 hli |
| Nyhav | 150 KG |
| Hluav taws xob uas yuav tsum tau | 220V, 10a |
| ambient kub | 10 ℃ 35 ℃ |
| Roj uas yuav tsum tau | aviation kerosene |
| Gas yuav tsum | tsis muaj tsawg tshaj li 120 psi cua compressor |
