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Aviation piston engine with electronic fuel injection x400
Unknown BrandSKU: 60862

Aviation piston engine with electronic fuel injection x400

Two-stroke horizontally opposed 4-cylinder piston aircraft engine.

$8,081.40

USD · Volume pricing available

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Export Compliance

9A012
ECCN Code9A012
ClassificationUnmanned Aerial Vehicles, Drone Systems
Control Basis
NSMTRS
DestinationsWorldwide except embargoed/sanctioned destinations
Customer TierVerified B2B Buyer (KYC + End-User Statement)
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I. Main characteristics

  • Model: x400 EFI[cite: 2]
  • Type: two-stroke horizontally opposed 4-cylinder piston aircraft engine[cite: 2]
  • Cooling method: air[cite: 2]
  • Lubrication method: oil mist (mixed lubrication system)[cite: 2]
  • Working volume (cubic capacity): 400 cc cm (400 cc)[cite: 2]
  • Minimum stable speed: ≤ 1200 rpm[cite: 2]
  • Maximum power: 48 hp / 35 kW at 6400 rpm[cite: 2]
  • Specific fuel consumption:
    • 1) Cruise mode: ≤ 380 g/(kWh)[cite: 2]
    • 2) Maximum power mode: ≤ 480 g/(kWh)[cite: 2]
  • Fuel: gasoline with an octane rating of 92 and higher (mixture ratio with oil for two-stroke engines 50:1)[cite: 2]
  • Resource (Service life):
    • 1) Time to first overhaul (TBO): ≥ 250 h[cite: 2]
    • 2) Total resource: ≥ 500 h[cite: 2]

II. Weight and dimensions

  • Engine net weight: 15 kg (including engine block, intake and exhaust components, electronic injection control unit)[cite: 2]
  • Dimensions (L×W×H): 370 × 320 × 280 mm[cite: 2]

III. Fuel supply and control

  • Fuel supply system: electronic fuel injection (EFI)[cite: 2]
  • Control method: capable of receiving commands from the control computer (or integrated on-board computer) and adjusting engine speed accordingly; capable of transmitting to the control computer parameters of throttle position, speed, intake temperature, cylinder temperature, exhaust gas temperature, etc.[cite: 2].

IV. Startup and power generation

  • The engine has an electric start function:
    • 1) Number of starting attempts: the engine must start successfully within 3 attempts[cite: 2].
    • 2) Low Temperature Starting: The engine can be started in low temperature conditions down to -40°C (use of the included preheating equipment is acceptable)[cite: 2].
  • Generation power: ≥ 2 kW[cite: 2].

V. Environmental Conditions (Adaptability)

  • Operating temperature: -50°C to +55°C (start at -40°C, auxiliary heating possible)[cite: 2].
  • Storage temperature: -50°C to +65°C[cite: 2].
  • Relative Humidity: (95±5)% (at 30°C ~ 60°C)[cite: 2].
  • Vibration: ≥ 2g (15Hz ~ 500Hz ~ 15Hz)[cite: 2].
  • Shock loads: vertically ≥ 20g, along the transverse and longitudinal axes ≥ 15g[cite: 2].
  • Low pressure: Capable of withstanding low pressure conditions equivalent to an altitude of 7000 m[cite: 2].
  • Salt fog: is resistant to salt spray[cite: 2].
  • Mold: is resistant to mold fungi[cite: 2].
  • Rain: Provides protection from moderate rain[cite: 2].
  • Application altitude: capable of starting and operating normally in high mountain conditions at an altitude of up to 5000 meters[cite: 2].

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