GTE550‑EFI Direct‑Drive 2‑Stroke EFI Gasoline Engine

  1. Lightweight Direct‑Drive Design: No clutch assembly, dry weight only 17.5 kg. Optimized weight‑reduction design delivers outstanding power‑to‑weight ratio for UAV engine installations.
  2. Precise 2‑Stroke EFI System: Electronic fuel injection ensures stable fuel supply under variable altitude and temperature conditions, lowers overall fuel consumption for long‑hour drone missions.
  3. High Power & Thrust Output: Produces peak power of 50HP (37 kW) at 7300 rpm and maximum thrust up to 72.4 kg, ideal for heavy‑lift commercial UAV platforms.
  4. Built‑in Onboard Generator: Delivers DC28.5V 1000W output at 5500 rpm, provides reliable power supply for payloads, sensors and other airborne accessories on the UAV.
  5. Heavy‑Duty Cylinder Construction: Aluminum alloy cast cylinder block with Ni‑SiC electro‑plated inner wall, great wear resistance and extended service life for continuous drone operation.
  6. Wide Practical RPM Band: Working RPM covers 1200‑7000 rpm, fully adapts to hover, climb and cruise flight states for different industrial drone applications.
  7. Simple Electric Start System: 22.2V (6S) electric start enables easy startup operation, eliminating manual pull‑start complexity.
  8. Customizable Engineering Support: As a professional supplier, we support customized development for mounting interfaces, parameters and auxiliary components to fit customers’ unique drone integration projects.

Product Overview

GTE550‑EFI is a 550cc four‑cylinder 2‑stroke electronic fuel injection gasoline engine with direct‑drive configuration, built for civil heavy‑payload UAV and commercial aviation platforms. Without clutch mechanism, this drone gasoline engine achieves significant weight reduction. It adopts capacitor discharge ignition together with mature EFI control unit for dependable continuous‑run performance. The integrated generator meets high onboard power demand for various payload devices. Our factory can carry out custom modification to satisfy diverse aircraft installation and performance requirements. UAV gasoline engine

Main Technical Specifications

ItemSpecifications
Displacement550cc (137.5cc*4)
RPM Operating Range1200‑7000 rpm
Recommended Propeller30×25, 32×20, 33×20 (Two‑blades)
Max Power50HP (37kW) @7300rpm
Generator OutputDC28.5V, 1000W @5500rpm
Ignition SystemCapacitor discharge ignition
Fuel Consumption480g/kW.h
Starting Mode & VoltageElectric start, 22.2V (6S)
Cylinder BlockAluminum alloy casting, inner wall electroplated Ni‑SiC
Dry Engine Weight17.5 kg
Max Tensile Thrust72.4 kg @5760 rpm
Required Fuel95# gasoline + Fully synthetic 2‑stroke lubricating oil
Fuel‑Oil Mix RatioGasoline : Lubricating oil = 35 : 1

Performance Characteristic

At 5760 RPM, this UAV engine delivers peak thrust of 72.37 kg and torque of 46.4 N·M. Thrust and torque increase steadily across the 1200‑6000 rpm operating zone. Thanks to direct‑drive structure, power transmission loss is minimized. It offers responsive power output suitable for heavy‑payload civil UAV during hovering, climbing and cruise flight.

Application Scenarios

This direct‑drive 2‑stroke EFI gasoline engine is well‑suited for multiple civil‑focused projects:

Heavy‑payload commercial UAV platforms

Long‑endurance industrial inspection drones

Cargo transport UAV power solution

Large‑size civil drone system integration

Custom light aviation power projects

Customized development service is available. We can adjust parameters, mounting interfaces and auxiliary structures according to customer‑specific integration requirements.

FAQ

What fuel and lubricant should I use for the GTE550‑EFI direct‑drive drone gasoline engine?

A: Please use 95‑grade gasoline mixed with fully synthetic 2‑stroke lubricating oil. The mixing ratio is 35:1 (gasoline to lubricating oil). Avoid mineral‑based two‑stroke oil, as it will accelerate internal component wear and shorten engine service life.

What are the main benefits of direct‑drive UAV engine compared with clutch‑type versions?

A: Direct‑drive design removes clutch components, reducing total engine weight and power transmission loss. It features simpler mechanical structure, fewer wearing parts and lower maintenance cost. This configuration is preferred for weight‑sensitive UAV projects.

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