ZT-T730cc 730cc Heavy-Lift UAV Engine

ZT-T730cc 730cc Heavy-Lift UAV Engine

The ZT-T730cc is an industrial-grade, heavy-duty 730cc two-stroke propulsion system utilizing an advanced 4-cylinder horizontally opposed layout form. Specially engineered to meet the extreme demands of heavy-payload tactical logistics, long-endurance cargo drones, and large fixed-wing agricultural aircraft, it delivers an exceptional 63.5hp (47.3kW) maximum power output. Boasting a massive 270kg maximum take-off weight (MTOW) capacity and producing up to 75kg of static thrust at low altitudes, the ZT-T730CC introduces unmatched structural resilience, minimal vibration frequencies, and persistent operational reliability for advanced commercial and industrial aviation missions globally.
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Product Specifications

1. Premium 4-Cylinder Layout & Smart Ignition

Featuring an innovative horizontally opposed 4-cylinder layout form, this engine dramatically mitigates low-frequency vibration across a broad speed range of 2000-7500rpm. It integrates an opposed two-cylinder synchronous ignition mechanism with an intelligent CDI automatic angle igniter that performs automatic switching at 500 rpm, ensuring buttery-smooth idle performance and seamless throttling.


2. Aerospace-Grade Materials & Forged Components

Built for extended lifespans under grueling thermal stress, the engine block features a cast aluminum alloy cylinder wall treated with a premium ceramic nickel-silicon hardened coating. The piston utilizes precision oval grinding and top-tier aluminum alloy casting. The entire internal structure is driven by an ultra-robust, seven-piece forged combination crankshaft assembly designed to absorb massive torque impacts.


3. Optimized Fuel Systems & Massive Power Generation

The propulsion system offers two fuel delivery architectures: standard dual diaphragm-type all-around carburetors (built without traditional choke/injector nozzles) running at 17L/h, or an advanced high-altitude ECU EFI electronic fuel injection suite reducing fuel consumption to just 12L/h. With an optional integrated high-power onboard generator (800W / 2000W), it seamlessly powers high-draw avionics, heavy-duty servos, and mission payloads.

4.Technical Specifications

Technical Property ItemVerified Specification Value
Displacement730 cc
Maximum Power63.5 hp / 47.3 kW
Layout FormHorizontally opposed, 4 cylinders
Engine StrokeTwo-stroke
Speed Range2000 - 7500 rpm
Static Thrust @ 100m75 kg
Static Thrust @ 1800m70 kg
Maximum Take-off Weight270 kg
Recommended Propellers32*20; 30*23; 30*25
Bore × Stroke66 mm × 54 mm
Lubrication Ratio30:1 (Gasoline to two-stroke oil mix)
Ignition SystemCDI Automatic Angle Ignition
Firing OrderOpposed two-cylinder synchronous ignition, auto-switch at 500 rpm
Cylinder EngineeringCast aluminum alloy, with ceramic nickel-silicon hardened coating on the inner wall
Piston CompositionOval grinding, aluminum alloy casting
Crankshaft ArchitectureForging, seven-piece set
Carburetor SpecTwo diaphragm-type all-around carburetors, without choke/injector nozzles
Optional Generator Output800 W / 2000 W
Fuel Consumption - Carburetor17 L/h
Fuel Consumption - EFI Version12 L/h
Core Weight18.5 kg
Dimensions ( L*W*H)420 × 410 × 370 mm
Factory OptionsExhaust pipe, Starter, Generator


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