Turbojet engine

SW55B

Product technical parameters


  • Thrust:5.5kg


  • Diameter:69.5mm


  • Length:175.2mm


  • Weight:535g


  • Speed range range:60000~170000


  • Total weight:780g


  • Rated exhaust Max Temp:780℃


  • Fuel consumption:≤230g/min


  • Fuel used: Aviation kerosene


  • Lubricating oil:3%~5%


  • Maintenance cycle: 25H

  • Power line

  • Throttle line

  • Signal line

  • GSU

  • Brushless Fuel Pump

  • ECU(V3)

  • Filter

  • Switch Valve


Engine startEngine operationStarting motor
Pump Voltage0.8-2.0VRPM ACC15Eject time0.4S
RPM Start Up Ramp100RPM DEC15Ejection Low Volt4.5V
Pump Start Up Ramp3Idle RPM range60000~170000Run Voltage4V
Hotspot voltage6.6VMax Temp≤1000℃Cooling5000rpm
Ignition oil valve40~60Voltage≥10V  
Ignition speed3000Shut down and restartClose  
Preheating speed12000Restart the ignition voltage6.6V  
Clutch disengagement speed35000Oil pump restriction13V  

    Independently developed brushless starting motor

    It has the advantages of stable output, reliable operation and long life

    RPM:97,000

    Self-developed fuel pump

    Compact structure and small size, precision design and occupy small space

    4 mm Oil in   4 mm Oil delivery

    Bus control

     Using only one bus to transmit data signals,

     More stable communication between the engine and the control system

     The connection is more convenient and concise

    Independent development of ECU control system

    With fixed Speed range control function, air engine Restart function

    32  Bit element high-Speed range chip

    Focus on the domestic development of micro and small aircraft engines


    • Research and development design


    • Intelligent manufacturing


    • Supply chain management

Contact

  • Tel:86-0312-2202266
  • Email:info@swiwin.com
  • Web:http://www.swiwin.com
  • Add:No. 66 Jianye East Road, High-tech district,Baoding,Hebei,China
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