SWIWIN SW400 Pro UAV ECU Latest Model MOQ 7
- Brand::SWIWIN
- Product Code: SW400 PRO
- Availability: In Stock
-
£4,825.56
SWIWIN SW400 Pro UAV ECU Latest Model
Swiwin SW400Pro Brushless 80kg Jet Turbine Engine for Professional with One Key AutoStart UAV Version
We have many SWIWIN turbines available. Have a look at our range of SWIWIN RC Jet turbines
Minimum Order Quantity: 7
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The SWIWIN SW400 Pro UAV ECU has these great features listed below:
Compact design
Compact design
32Bit auto restart ECU
Brushless starter
Brushless pump
RS-232 telemetry functions
Color screen data terminal
CNC compressor wheel
very fast throttle response
Best cost/performance 400N turbine
Thrust 400N
RPM Range 33,000 - 95,000
EGT 750C
Fuel Consumption 1000g/min
Fuel kero or diesel
Lubrication 5% kero/3% diesel
Start full autostart
Restart auto restart
Weight 3000g
Diameter 146mm
Length 342mm
Maintenance Interval 25 hours
How to control and use the engine:
1 Throttle signal :
The throttle adopts the pulse width (PWM) control mode, the pulse width is 1ms~2ms, 1ms corresponds to the minimum throttle (0%), 2ms corresponds to the maximum throttle (100%), and the pulse high brightness is 3.3 V and 5V (3.3V and 5V level are available), pulse bias is 0V.
2 Start switch
The start switch adopts the pulse width (PWM) control mode, the pulse width is 1ms~2ms, 1ms corresponds to off, 2ms corresponds to on, the pulse height is rated 3.3V and 5V (3.3V and 5V voltage average is available), pulse The incident is 0 V.
3 Telemetering data
1) The engine has a telemetering function, and data transmission is carried out through 232 standard serial, and the serial baud rate remains unchanged from 9600bps to 57600bps.
2) The communication protocol of telemetry data is open, and detailed communication protocol documentation is provided.
4) Telemetry data includes but is not limited to engine steering, engine throttle, fuel pump voltage, engine status, and error information. Record 1) Engine data data recording function, which can record data 2 hours before engine failure. 2) The content of the data record includes but does not include engine steering, engine throttle, fuel pump voltage, engine status, and error information. 3) Provide engine data analysis software for proper data analysis after flight.
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