Drone Generator New and Original

• Customization: Available
• Transport Package: Box
• Origin: China
• Model NO.: Drone generator

Product Description

Product Description

 

Drone generator 

Excellent thrust-to-weight ratio, low fuel consumption, integrated inspiration, ECU control, centrifugal compressor, annular combustion chamber, axial flow turbine and fixed output nozzle.
Maximum thrust: 392 N
Maximum fuel consumption: 0.043 Kg/N/h
Speed: 96000
Maximum diameter: 147 mm
Length: 385 mm
Net weight: 3.6 Kg
Fuel type: JET-A1 / JP5 / JP8
Lubricating oil type: 3cST or 5cST
Maximum fuel consumption applies to fuel with calorific value of 43/5MJ/Kg

 

Excellent thrust-to-weight ratio, low fuel consumption, integrated inspiration, ECU control, centrifugal compressor, annular combustion chamber, axial flow turbine and fixed output nozzle
Maximum thrust: 1250/1100 N
Maximum fuel consumption: 0.125/0.111 Kg/N/h
Speed: Idle: 30000 / Maximum: 57000~61000
Output power: 750 W
Maximum diameter: 272 mm
Length: 625 mm
Net weight: 22 Kg
Fuel type: JET-A1 / JP5 / JP8
Lubricating oil type: 3cST or 5cST
Maximum fuel consumption applies to fuel with calorific value of 43/5MJ/Kg

 

Twin cylinder horizontally opposed air-cooled, two-stroke gasoline engine with magneto ignition and mixed lubrication for push and pull installation.

Performance: 15 kW (20 ) at 7200 rpm

Bore: 66 mm

Stroke: 40 mm

Displacement: 274 cc

Crankcase: aluminum casting

Crankshaft: integral forging, split connecting rod, needle bearings

Piston: cam face, cast aluminum alloy

Cylinder: cast aluminum alloy, ceramic coating

Ignition system: solid state magneto ignition

Firing order: two cylinders

Carburettor: diaphragm carburettor

Starter: 12 V 300 W

Generator: 12 V 850 W

Weight: approx. 7.2 kg (magneto ignition)

Fuel: 100LL aviation gasoline, mixed oil ratio of 1:25 or 1:50

Twin cylinder horizontally opposed air-cooled, two-stroke gasoline engine with magneto ignition and mixed lubrication suitable for push and pull installation.

Performance: 15 kW (20 ) at 7200 rpm

Bore: 66 mm

Stroke: 40 mm

Displacement: 274 cc

Crankcase: aluminum casting

Crankshaft: integral forging, split connecting rod, needle bearing

Piston: cam face, cast aluminum alloy

Cylinder: cast aluminum alloy, ceramic coating

Ignition system: solid state magneto ignitio

Firing order: two cylinders

Carburettor: diaphragm carburettor

Starter: 12 V 300 W

Generator: 12 V 850 W

Weight: about 7.2 kg (magneto ignition)

Fuel: 100LL aviation gasoline, mixed oil ratio is 1:25 or 1:50

The MDR208 has the highest power-to-weight ratio compared to other rotary engines. It is specially designed and developed for use in small target drones or short-life disposable UAVs.

Type: Single rotor Wankel type spark ignition engine

Displacement: 208 cc

Performance: 28 kW (38 ) at 7800 rpm

Weight: Approx. 9.9 kg

Fuel consumption: 0.57 lb//hr - max power, 0.52 lb//hr - cruise

Vibration intensity: Radial vibration zero

Chamber cooling: Ram air

Rotor cooling: Ram air

Direction of rotation: Counterclockwise (from propeller mounting direction)

Ignition system: Non-contact magneto

Carburettor: Internal pressure diaphragm pulse fuel pump

Fuel type: Mogas or AVGAS (100 LL)

Lubrication: Separate fuel supply by constant flow metering pump

Spark plugs: 2 (NGK CR9EK)

Generator: 12 V 850 W

Propeller: 28 - 20