| Customization: | Available |
|---|---|
| Transport Package: | Box |
| Origin: | China |
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| EEJ-20(J70) EEJ-40 EEJ-23 Micro Jet Engine |
|
Model |
EEJ-20 |
|
Maximum thrust(daN) |
19 |
|
Maximum speed(rpm) |
120,000 |
|
Specific fuel consumption at Maximum speed (kg/daN·h) |
1.73 |
|
Max outer diameter(mm) |
110 |
|
Total Length(mm) |
304 |
|
Weight(kg) |
1.77(without oil pumps and ECU) |
|
Exhaust temperature at Maximum speed(°C) |
760 |
|
Idle speed(rpm) |
32,000 |
|
Idle thrust(daN) |
0.5 |
|
Fuel consumption in idle speed(ml/min) |
200 |
|
ground start air start(if needed) |
electric ignitor/motor start fireworks ignitor/wind milling start fireworks ignitor/powder start
|
|
fuel |
95%kerosene +5%jet engine oil |
|
open oil system |
95%kerosene +5%jet engine oil |
|
TBO bearing (hours) |
25 |
|
Maximum flight altitude(m) |
8000 |
|
Maximum flight Mach Number |
0.8 |
|
Ground start envelope |
4,000m/-30°C |
Model:EEJ-40
Maximum thrust(daN):39.2
Maximum speed(rpm):96,000
Specific fuel consumption at Maximum speed (kg/daN·h) :1.71
Exhaust temperature at Maximum speed(°C):850
Max outer diameter(mm):147
Total Length(mm):385
Weight(kg):3.65(excluding oil pump and ECU)
Idle speed(rpm):30,000
Idle thrust(daN):1.3
Fuel consumption in idle speed(ml/min) :271
ground start air start(if needed):electric ignitor/motor start;
pyro ignitor/wind milling start
fuel:95%kerosene +5%jet engine oil
open oil system:95%kerosene +5%jet engine oil
TBO bearing imported/made in China(hours):25/12.5
Maximum flight altitude(m):8000
Maximum flight Mach Number:0.8
Ground start envelope:2,600m/-25°
Product model: EEJ-23
Maximum thrust (DN): 23
Maximum speed (rpm): 132,000
Maximum speed fuel consumption rate (kg/DN hour): 1.4
Maximum speed exhaust temperature (Celsius): 780
Diameter*total length (mm): 132*366
Weight (kg): 3.0 (excluding oil pump and ECU) 3.3 (including oil pump and ECU)
Slow speed (rpm): 40,000
Slow thrust (DN): 2
Slow fuel consumption (ml/min): 100
Starting method: electric start + oil ignition/propane gas ignition
Fuel: 95% aviation kerosene + 5% Pegasus No. 2 turbojet lubricant
Open lubrication: 95% aviation kerosene + 5% Pegasus No. 2 turbojet lubricant
Engine repair life imported bearing/domestic bearing (hours) : 50/25 (tentative)
Total life (hours) 200 (under normal use)
Maximum flight altitude (m): 8000
Maximum flight Mach number: 0.8
Ground start envelope: 4,000m/-30ºC
Product maturity: small batch supply to customers
Remarks: The maximum working state working time does not exceed 3 minutes, and the maximum working state is reached when any one of the engine speed, thrust and exhaust temperature reaches the maximum.
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