LX-WP-40 is a typical axial flow single-stage radial compression small jet engine. Through CNC high-precision machining of components and unique assembly technology, ultra-high thrust-to-weight ratio and stable and excellent operating results are achieved. The price performance ratio is unparalleled in the world.
LX-WP-40 is 100% independently developed by our company. Our company has 20 years of experience in manufacturing machinery, industry exploration and experience accumulation. In such a premise, LX-WP-40 has excellent performance, incomparable
cost performance, extremely high quality.
More detailed information about LX-WP-40:
Thrust: ≥40kgf
Specific fuel consumption at maximum speed: ≤0.152 kg/Nh
Maximum exhaust temperature: ≤780ºC
Fuel: JP-4/petroleum/ Jet A1
Lubricant oil: Aeroshel Turbine Oil 90
Fuel pump integration: Now external, built-in can be developed
Integrated valve: External EPV
Time required to reach maximum speed:<40s
Start time (time required to reach idle):<30s
Start temperature: -8°C to +50°C
Minimum working ambient temperature: -35ºC
Maximum working ambient temperature: 50ºC
Maximum working altitude: 10,000 meters
Maximum working speed: 1000 kilometers/hour
Engine diameter (mm): 202
Engine length (mm): 336
Engine weight (Kg): 3.45±0.2
Maximum speed (RPM): 98000
Minimum speed (RPM): 30000
The engine should be able to run normally at full speed (maximum thrust) for at least 20 minutes.
Service life: 7 years or 50 hours (20 one hour flight cycles) or 60 starts
Voltage: 28V
Maximum instantaneous current: ≤30A
Maximum continuous current: ≤2.5A
Communication protocol: Both RS232 and Can bus transmission are possible
Telemetry data includes: engine speed, throttle valve instruction feedback, pump voltage, pump speed, engine temperature, ECU
temperature, ECU voltage, engine status, error message
Instruct: start, stop, chill-down, safety stop
ECU control unit:The ECU control unit consists of an aluminum-encapsulated control box, oil pump, valves and their connecting wires. The control unit is connected to the engine main engine through a connecting line to implement control.
Technical features:
1) The unique combustion system design allows the engine to generate strong thrust at lower exhaust temperatures, with a small.
volume, light weight, and high thrust to weight ratio.
2) Reliable bearing lubrication system design improves the service life of the engine.
3) Simple and reliable ignition system design, with optional oil and gas ignition options.
4) High acceleration performance, taking no more than 12 seconds from idle to maximum thrust.
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