Aviation Seat Cushion Fuel Combustion Ratio
Aviation Seat Cushion Fuel Combustion System
Product Introduction of Aviation Seat Cushion Fuel Combustion System
USTOR probatus est cibus NexGen aviation per FAA in Aviation Administration Foederatum de Civitatibus Foederatis Americae adhiberi potest combustione fuel probatio fidei aviation plures materiae. Ut Park DPL MMMCD, OB cum Levinius-Model XXXII Carlin Model CC CRD, et ante omnia sunt agnita FAA in luce subtracto, FAA has developed in NexGen habens turibulum in generatione altera, aviation cibus cremetis. NexGen combustor gerit prioris generatio est operatio a principle combustor et metimur verius potest ad gas test parametri initus atque cibus. Idem instrumentum esse faciliorem futura roadable upgrade.
Fuel combustion test of seat cushion on aircraft can be carried out by cooperating with seat cushion test frame and dynamic running device.
Euismod characteres productum of the Aviation Seat Cushion Fuel Combustion Ratio
1. The conical cylinder of burner is made of corrosion resistant and high temperature resistant alloy.
2. NexGen aviation cibus habens turibulum includit depopulator est cibus COLLUM: igniens, cibus, blasphemant: fixer, tubo spiramento, et pellem completum, muffler, porus acusticus compulit ad alia components.
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. et aer CERVIX mutantur cibus pressura input, signis diversis test potest occurrit.
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 cibus habens turibulum potest providere minus quam 10.6w / cm2 calor flammae fluxus.
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.
Productum parametri de Aviation Seat Cushion Fuel Combustion Ratio
Applications: Aviation Materials
Latin: AITM SCATEBRA Airbus transeunte Latin: AITM 2,0009
BSS Boeing Latin: BSS (VII)CCCIII
FAA Foederatum Aviation Administration: XXV retro ORDO UNCTIONIS INFIRMORUM II F
| dimensiones | MD mm (W) X mm MDCCC (H) x mm CM |
| pondus | CL KG |
| electricity iudicium | 220V, 10A |
| Ambientium, temperatus | X ℃ ad XXXV ℃ |
| fuel necessitates | ad prunam et aviation |
| opus gas | non minus quam CXX PSI caeli compressor |
