ZT-1280cc 107HP UAV Engine

ZT-1280cc 107HP UAV Engine

The ZT-1280cc is an automotive-grade, high-reliability 1280mL (1.5L) inline 4-cylinder aviation piston engine engineered for next-generation heavy-lift industrial UAVs, tactical VTOL platforms, and light experimental aircraft. Utilizing a naturally aspirated induction system combined with a Dual Overhead Camshaft (DOHC) architecture and 4 valves per cylinder, this gasoline propulsion powerhouse unleashes a commanding 107HP (78.5kW) at 5500rpm and a massive peak torque of 145N·m. Outfitted with an advanced multi-point electronic fuel injection (MPI) system and an all-aluminum alloy structure, the ZT-1280CC sets a new benchmark for thermal efficiency, fuel economy, and persistent power delivery in high-end commercial aviation.
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Product Specifications

1. Precision Inline 4-Cylinder DOHC Architecture

Designed for exceptional mechanical balance and smooth power delivery, the ZT-1280CC adopts an Inline (L) 4-cylinder layout with 4 valves per cylinder (16 valves total). Driven by a high-efficiency Dual Overhead Camshaft (DOHC) valvetrain and featuring a 10:1 compression ratio, the engine optimizes gas exchange dynamics, providing a sustained maximum net power of 75kW and a stable piston linear speed of 15.77 m/s under continuous high-load flight regimes.


2. Advanced Multi-Point Injection & Fuel Flexibility

Say goodbye to altitude-induced tuning issues. The engine integrates a sophisticated Multi-Point Electronic Fuel Injection system that meters fuel dynamically based on real-time atmospheric conditions. Optimized for high-altitude operational stability and superior fuel economics, it runs flawlessly on standard 92 Octane Gasoline (92#) while complying with stringent China V (国V) environmental emission standards.


3. All-Aluminum Alloy Construction & High-Torque Outputs

To ensure an outstanding power-to-weight ratio without sacrificing structural durability, both the cylinder head and cylinder block are precision-cast from high-strength aluminum alloy. The engine exhibits a wide and robust torque band, generating a peak torque of 145N·m between 3500-4500rpm, ensuring remarkable climbing ability, prompt throttle response, and massive payload hauling capacity for fixed-wing cargo aircraft.


4.Technical Specifications

Technical Property ItemVerified Specification Value
Product Model / DisplacementZT-1280cc / 1280 mL (1.5L)
Engine TypeAviation Piston Engine
Max Power Output107 hp / 78.5 kW @ 5500 rpm
Maximum Net Power75 kW
Maximum Torque145 N·m @ 3500 - 4500 rpm
Induction SystemNaturally Aspirated
Cylinder ArrangementInline layout / "L" type
Number of Cylinders4
Valves per Cylinder4 (16 Valves Total)
Compression Ratio10:1
Valvetrain MechanismDOHC
Fuel Type / Fuel GradeGasoline / 92# Octane
Fuel Delivery SystemMulti-Point Electronic Fuel Injection
Cylinder Head MaterialHigh-strength Aluminum Alloy
Cylinder Block MaterialHigh-strength Aluminum Alloy
Emission StandardChina V / National V
Piston Linear Speed15.77 m/s


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