Aviation Seat Cushion Fuel Combustion System
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
The NexGen avhiyesheni chinotsva burner yakatenderwa Faa of Federal Aviation Administration kuUnited States inogona kushandiswa huni combustion kuidzwa zhinji avhiyesheni zvinhu. Sezvo Park DPL 3400, Lennox Model Ob-32 uye Carlin Model 200 CRD kare kuzivikanwa Faa dzakavharwa zvose, Faa yava akakurukura NexGen burner inotevera chizvarwa avhiyesheni mafuta burners. NexGen combustor adopts nokushanda nhungamiro rapfuura chizvarwa combustor, uye anogona zvakarurama kuyera bvunzo parameters ose mazano gasi uye mafuta. Panguva iyoyowo, huchashandiswa anogona kugarwa remangwana ndiwedzere pamusoro 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 Performance unhu of the Aviation Seat Cushion Fuel Combustion System
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen avhiyesheni chinotsva burner zvinosanganisira pomuparadzi, mafuta kamwene, igniter, mafuta njanji, fixer, kufefetedza chubhu uye goko, mafuro, acoustic nemishonga nezvimwe zvinoriumba.
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 kuchinja huni kamwene uye mhepo kufurirwa chiyamuro, akasiyana muedzo mitemo inogona akasangana.
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 avhiyesheni chinotsva burner inogona kuva asingasviki 10.6w / cm2 zvomoto kupisa kuyerera.
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 parameters pamusoro Aviation Seat Cushion Fuel Combustion System
Applications: Aviation Materials
Standard: AITM Airbus Standard: AITM 2,0009
BSS Boeing Standard: BSS 7303
Faa Federal Aviation Administration: rwemberi 25 MASHOKO OKUWEDZERA F Part II
| miganhu | 1500 mm (W) X 1800 mm (H) x 900 mm |
| uremu | 150 KG |
| Electricity zvinodiwa | 220V, 10a |
| Ambient tembiricha | 10 ℃ kusvika 35 ℃ |
| Fuel zvinodiwa | avhiyesheni eparafini |
| Gas zvinodiwa | hapana asingasviki 120 PSI mhepo compressor |
