Product Description
Multi Fuel Engine 11.76KW(16hp) QX-16
Multi Fuel Engine 5.8KW(8hp) QX-8
40kg Thrust Turbojet CTJ-16
CH-5 UAV Engine
200Kg Thrust Turbojet Engine ZKXH-200
6.4kg Micro Turbojet Engine TJ60 |
Engine form: two-stroke horizontally opposed twin cylinder
Cooling method: air cooling
Displacement: 170cc
Actual compression ratio: 8.0:1
Speed range: 2000rpm~7500rpm
Maximum power: 11.76KW (16hp) / 7500rpm
Minimum fuel consumption rate: ≤300g/KW.h
Fuel: vehicle diesel, jet fuel, gasoline
Oil supply method: low pressure air-assisted direct injection in the atomizing cylinder
Machine weight: 6.3kg (including ECU, wiring harness, etc.)
Power to weight ratio: 1.87KW/kg
Ignition method: electronic ignition
Lubrication method: electronically controlled oil pump, consumption-type distributed independent lubrication
Lubricating oil consumption: maximum load>70g/h cruising condition>45g/h
Engine start altitude: 5000m
ceiling: 7000m
First overturn period TBO: 300h
Total engine life: 500h
Working temperature: -30ºC~+60ºC
Start mode: external handheld start (start time≤10s)
Engine form: two-stroke single-cylinder
Cooling method: air cooling
Displacement: 85cc
Actual compression ratio: 8.0:1
Speed range: 2000rpm ~ 7500rpm
Maximum power: 5.8KW (8hp) / 7500rpm
Minimum fuel consumption rate: ≤300g/KW.h
Fuel: vehicle diesel, jet fuel, gasoline
Oil supply method: low pressure air-assisted direct injection in the atomizing cylinder
Weight of the whole machine: 3.5kg (including ECU, wiring harness, etc.)
Power to weight ratio: 1.66KW/kg
Ignition method: electronic ignition
Lubrication method: electronically controlled oil pump, consumption-type distributed independent lubrication
Lubricating oil consumption: maximum load 70g/h cruising condition>45g/h
Engine start altitude: <5000m
ceiling: 7000m
First overturn period TBO: 300h
Total engine life: 500h
Working temperature: -30ºC~+60ºC
Start mode: external handheld start (start time≤10s)
Technical data
Dimensions
Length: 345mm
Diameter: 158mm
weight
Dry mass: 23kg
Performance
Takeoff thrust: ≥0.42kN
Cruising thrust (H=0, Ma0.3): ≥0.28kN
fuel consumption
Take-off state: 156kg/(kN h)
Life: 20h
600kW drone heavy fuel engine Main product features:
Boxer 8 cylinders ,4-stroke
Suitable for heavy fuel: diesel, RP- 3/RP-5
Light-weight design, high power-to-weight ratio
No attenuation altitude 4000m, the limit altitude is 10000m
Low fuel consumption, long-endurance
TBO time > 2000h
Fuel:Diesel, Jetfuel(RP- 3/RP- 5);
Boxer 8 cylinders,Liquid-cooled, 4-stroke, High pressure common rail, TCI
Maximum continuous power/Speed:805hp/4000rpm
Minimum fuel consumption:213g/kW·h
Weight(dry):Air version 515kg, face version 650kg
Length x widthx height:712×706×643mm (Integrated intake manifold status) 712×706×588mm(Split inlet manifold status)
Main uses:Apply to heavy load long endurance UAV, light helicopter, navigation fixed-wing aircraft, light leisure sport aircraft etc and range extenders.
Thrust:6.4kg / 64N / 13lbs
Weight (inc starter):850g
Diameter:90mm
Length(inc starter):230mm
Max RPM:140000/min
Idle RPM:40000/min
Fuel Consumption(per minute):245ml/ 6.9oz/ 196g
Max Exhaust Gas Temp:750ºC
Continuous Working Time:2h
Maintenance Interval:20h
Starting System:auto startup
Ignition Methods: fuel oil
Available Fuel:kerosene,diesel,LPG
Check at every level: from production to testing
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ATTENTION:
1. You must know before buying the product: If you don't understand, consult before buying:
2. Before buying the product, you must determine the needs, configuration, and cabinet requirements:
3. Is the transformer quoted according to the original drawing or the actual customer requirements:
4. For the transportation of special large items, please consult the freight instructions, and consult the customer service in advance for invoice requirements:
5. Customer-exclusive customized products do not support return and exchange services, regular stock is confirmed
Audited Supplier 
Engine form: two-stroke single-cylinder
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