PGAPOWER E-34 Multi-Fuel EFI Engine (Global Warehouse)

According to the mission requirements, it can be installed in the weight class of UAVs under 25 kg. Using German technology and thanks to a carefully designed electronically controlled fuel injection system, the E-34 engine achieves precise control over the full speed range. The crankshaft design with three bearings reduces mechanical fatigue and ensures reliable operation of the power system. Compared with the previous piston engine of the same class, the fuel consumption is reduced by 10%-15%, which can make the UAV competent for long endurance work. In addition, the design of multi-fuel applications allows users to download different fuel data to the ECU without changing peripherals, so that the fuel can be changed in a very short time to meet the needs of special scenarios.

Cylinder working condition balance control

With engine overtemperature, overspeed protection control mechanism

Fast multi-fuel switching operation

Fixed speed control function

Wide temperature range adaptive control (-25 ° C to +50 ° C)

Ambient temperature and air pressure compensation

Serial port or PWM signal input control

Can implement engine heat management control

Specification Parameters:

Weight: 1.95kg

Working capacity: 34cc

Cylinder diameter: 38mm

Travel time: 30mm

MAX running speed: 9500RPM

Rated MAX power @6500RPM: 3.4HP(2.5kW)

Economic fuel consumption: 360-460g/kWh

Maintenance interval time: 150-200h

Mix fuel oil ratio: 45:1

Displacement: 34cc

Air cooling with FADEC control, Optional Liquid cooling

Max RPM & Power Output: 9500 RPM/3.4HP

Rated Power: 3.4HP: 2.5 KW/6500 RPM

Fuel Consumption: 360-460g/kWh

Dimension: 119 x 1656x 111 mm

Core weight: 1.95kg (including core engine, muffler, ECI, fuel pump

MTOH: 150-200

Features:

Designed for 20-55kg UAV

FADEC control

Live sensor for pressure, temperature, cylinder temperature

Protection function for engine temperature, over speeding

Multi fuels option applicable

Fixed RPM Control function

Temperature rang: -25C-50c

Compensation for pressure and surrounding temperature

Industrial port connection or PWM signal input

3 Bearing design for crankcase, lower fuel consumption

Note:

1. Engine weight (excluding exhaust pipe). Including ignition system, EFI controller, and fuel pump, the total weight of different configurations will be different

2, depending on the aircraft design and engine conditions.

3, depending on the conditions of use.

Available fuel types: Ethanol free 93-100 gasoline, aviation gasoline, aviation kerosene Jet-A1, JP-5,JP-8,TS-1.