Product Overview
SW60B micro turbojet engine is a medium-thrust civil miniature jet propulsion system independently designed by SWIWIN, serving as a cost-effective mid-size UAV engine and drone gasoline engine solution for medium industrial unmanned aircraft and high-performance hobby jet aeromodelling.
Our brand focuses on full-process independent research, intelligent precision manufacturing and standardized global supply chain management of civil micro aviation turbine power equipment. We provide compact, low-failure, easy-operating kerosene-powered propulsion solutions for global aeromodelling clubs, small commercial UAV manufacturers and university civil aerospace research labs.
Different from lightweight small-thrust SW55B and heavy large-thrust turbine models, SW60B adopts moderate 83mm diameter and 200mm overall length design to fit medium-size airframes with medium payload. It takes aviation kerosene as exclusive fuel with 3%–5% lubricant mixing requirement, matched with self-developed brushless starter, mini precision fuel pump and intelligent V3 ECU controller. The bus-type communication architecture greatly simplifies internal wiring layout of medium fixed-wing UAVs, and multi-dimensional real-time parameter monitoring effectively avoids over-temperature, overspeed and other flight faults for all civilian flight platforms.
Complete Official Technical Parameter Table
| Parameter Item | Standard Technical Data |
|---|---|
| Official Model | SW60B Micro Turbojet Engine |
| Rated Continuous Thrust | 6kg (60N) |
| Main Engine Net Weight | 800g |
| Outer Diameter | 83mm |
| Total Overall Length | 200mm |
| Stable Idle Rotational Speed | 50,000 RPM |
| Full Operating RPM Range | 50,000 ~ 150,000 RPM |
| Rated Maximum Exhaust Temperature | 750℃ |
| Upper Limit Fuel Consumption | ≤260g/min |
| Compatible Fuel Type | Aviation Kerosene |
| Lubricating Oil Mix Ratio | 3% ~ 5% turbine dedicated lubricant |
| Standard Maintenance Cycle | 25 continuous flight hours |
Independent R&D Core Component Introduction
Independent Brushless Starter Motor
Optimized internal magnetic circuit and wear-resistant bearing structure, stable torque output during cold startup of the UAV engine
Low vibration and low noise during long-time continuous operation
Extended service life after thousands of startup cycle aging tests, fully matching SW60B ignition logic
Standard maximum output speed up to 97,000 RPM to realize fast preheating and reliable ignition
Mini Precision SWP30S Fuel Pump
Ultra-small integrated compact structure, occupying minimal internal installation space of medium UAV airframes
High-precision internal gear assembly to realize even, stable fuel atomization delivery
Universal 4mm inlet and outlet pipe connectors, easy connection between fuel tank and engine combustion chamber
Real-time voltage adjustment linked with V3 ECU to balance fuel supply volume under different throttle gears, reduce total fuel consumption of this drone gasoline engine
Single-Bus Signal Communication Architecture
Only one data bus cable completes signal transmission between ECU, turbine main body, fuel pump and parameter display
Reduce messy internal wiring of medium fixed-wing UAVs and lower electromagnetic signal interference risks
Synchronously transmit real-time data including RPM, exhaust temperature, pump voltage and throttle position for full flight status monitoring
Simple plug-and-play wiring operation, friendly for amateur aeromodel users without professional circuit matching experience
V3 Generation Self-Developed ECU Control System
Equipped with high-performance 32-bit high-speed operation chip, ultra-fast data calculation and throttle response speed
Built-in fixed RPM lock control function: automatically stabilize rotation speed without continuous manual throttle adjustment
Integrate engine flameout protection and manual restart lock function to improve overall flight safety coefficient
Abundant expansion interfaces: 3S lipo power supply, telemetry data feedback, display screen access, PPM throttle signal input port
Built-in multi-dimensional fault self-detection including over-temperature, over-voltage and low-speed stall, effectively extend the service life of the UAV gasoline engine
Civil Commercial Application Scenarios
Mid-Size High-Performance RC Jet Aeromodelling
Premium medium-power UAV engine for intermediate jet model hobbyists and amateur aeromodelling competitions. The 6kg steady thrust and sensitive throttle response support agile high-speed cruising, vertical climbing and sharp bank turn flight actions, greatly upgrading flight experience of medium-size civil jet model aircraft.
Medium Load Civil Fixed-Wing UAVs
Serves as core drone gasoline engine power source for multiple medium-sized civilian unmanned aerial platforms:
Medium-range landform survey & remote sensing mapping UAVs with medium camera payloads
Medium-area agricultural crop inspection and moderate-volume pesticide spraying drones
Medium-distance river basin, forest and suburban air quality environmental monitoring fixed-wing UAVs
Civil aerial photography and sightseeing unmanned aircraft with medium takeoff weight
University Civil Aerospace Teaching & Lab Research
Perfect test power equipment for school aviation miniature jet propulsion teaching experiments and medium-size civil aircraft prototype R&D. Complete real-time parameter monitoring system provides accurate, repeatable test data for students and researchers engaged in micro turbine UAV engine technical research.
FAQ Section
What fuel and lubricant mixing ratio does SW60B UAV gasoline engine require?
A1: This micro turbojet only supports aviation kerosene as standard fuel. Operators need to mix 3% to 5% dedicated turbine lubricating oil into kerosene before each flight to protect internal rotors and bearings from wear.
What is the standard maintenance cycle of SW60B jet engine?
A2: The fixed maintenance cycle is 25 flight hours. After reaching the cycle standard, users need to disassemble and clean fuel filter, check fuel nozzle and rotor components, and replace worn consumable parts to guarantee long-term stable operation of the drone gasoline engine.
