Maunakea noho Cushion wahie'ā System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
Ka NexGen maunakea wahie puhiʻino i apono ia e FAA o ka Pekelala maunakea noho kia'āina o ka Amerika Huipuia hiki ke hoʻohana no ka wahie'ā ikea ai o na mea he nui maunakea mea. E like me ka Park DPL 3400, Lennox Model OB-32 a me Carlin Model 200 CRD mua 'ike' ia e FAA i nā mea a pau, ua hele aku, FAA ua ulu ka NexGen puhiʻino no ka mea e hiki mai ana o ka hanauna o ka maunakea wahie burners. NexGen combustor apono i ka rula ana o ka mua o ka hanauna combustor, a hiki pololei ana i ka hoao ana kiko'î o ka hoʻokomo o kinoea a me ka wahie. I ka Ia manawa, i ka mea hiki ke kōkua i ka wā e hiki mai upgrade o FAA.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Product Auana ano of the Maunakea noho Cushion wahie'ā System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen maunakea wahie puhiʻino nā mea hao wale, wahie kīʻamo, igniter, wahie hoino aku, fixer, hoʻokomo ea şarkı a me ka iwi, a mea hoʻohāmau, acoustic ia'ku a me nā eiiiiiaiou.
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. Ma hoʻololi wahie kīʻamo a me ka lewa puʻe hoʻokomo o, kekahi ho'āʻo mau hae hiki ke halawai.
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 maunakea wahie puhiʻino hiki i i emi ma mua o 10.6w / cm2 o ka lapalapa ahi wela pele.
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 kiko'î o Maunakea noho Cushion wahie'ā System
Applications: Aviation Materials
Koo: AITM Airbus Koo: AITM 2,0009
BSS Boeing Koo: BSS 7303
FAA Federal maunakea kia'āina ': a hiki Mahele 25 i paiiaʻi F Part II
| Ana | 1500 mm o (W) m 1800 mm o (H) x 900 mm o |
| Weight | 150 KG |
| uila koi | 220V, 10A |
| Ambient wela | 10 ℃ i 35 ℃ |
| wahie koi | maunakea kerosene |
| kinoea koi | i emi iho malalo o 120 PSI ea mea'opihia |
