DLE430

DLE430 Twin-Cylinder Inline Two-Stroke Engine

DLE430

DL430 Twin-Cylinder Inline Two-Stroke Engine can be used for UAVs, ultra-light experimental aircraft, etc.

DLE430 Product Image 1

DLE430 Product Image 2

DLE430 Product Image 3

Technical Specifications

Detailed product specifications and performance indicators

Technical Parameters

Bore

70mm

Stroke

56mm

Displacement

430.8cc

Compression Ratio

Theoretical 11∶1, Actual 6.5∶1

Reduction Ratio

2.55

Power

42HP at 6800 RPM

Static Thrust

110kg

Max RPM

7000 RPM

Idle RPM

1000 RPM

Spark Plug

14mm DLE-8

Spark Plug Gap

0.6MM

Carburetor

DLE Self-priming

Fuel

Gasoline 93#, 97#

Fuel Mixed Oil

2T FD Grade, Fully Synthetic

Oil Mixing Ratio

50 : 1

Transmission Oil

Gear Oil, 85W-140EP API-GL5 GL6 SAE 140 EP

Ignition System

Dual DC Capacitor Discharge Ignition, 12V Power Supply, 5W/each

Generator Power

Permanent Magnet Generator 14.5V, 90W

Starter Motor Current

35A

Rotation Direction

Clockwise (Facing Propeller)

Cooling

Fan Cooling

Weight

Engine: 27kg, Exhaust Pipe: 4.1kg, Total Weight: 32.25 kg

Recommended Propeller

1.5M Variable Pitch Carbon Fiber Propeller

Product Dimensions

Precise engineering diagrams for installation planning. Click to enlarge

DLE430 Dimension Diagram 1

DLE430 Dimension Diagram 2

DLE430 Dimension Diagram 3