ZT-1480cc 197HP UAV Engine

ZT-1480cc 197HP UAV Engine

The ZT-1480cc is a top-tier, heavy-duty 1480mL (1.5L) inline 4-cylinder turbocharged aviation piston engine purpose-built for high-altitude tactical UAVs, large-scale logistics cargo drones, and light aviation aircraft. Harnessing a powerful turbocharger combined with Gasoline Direct Injection (GDI) and a Dual Overhead Camshaft (DOHC) valvetrain, this state-of-the-art powerplant delivers an astonishing 197HP (145kW) at 5600rpm. Boasting a massive low-end peak torque of 285N·m starting from just 1500rpm and built completely with a lightweight aluminum alloy block and cylinder head, the ZT-1480CC provides unparalleled power density, superior fuel economy, and absolute reliability for critical commercial aviation missions worldwide.
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Product Specifications

1. Forced Induction Turbocharging & Extreme Torque

Engineered to eradicate altitude-induced power loss, the ZT-1480CC incorporates an advanced Turbocharged induction system. It unleases a jaw-dropping peak torque of 285N·m across a wide 1500-4000rpm band, ensuring massive instantaneous pulling power, shorter take-off rolls, and unrivaled high-altitude climbing capabilities for heavy payload deployment.


2. Gasoline Direct Injection & DOHC Valvetrain

Equipped with an advanced Direct Injection fuel delivery architecture and a 10.5 compression ratio, fuel is atomized directly into the combustion chambers at ultra-high pressure. Guided by a precision Dual Overhead Camshaft (DOHC) valvetrain with 4 valves per cylinder (16 valves total), the engine achieves optimal thermal efficiency, maximizing net power to 130kW while keeping a stable piston linear speed of 15.68 m/s.


3. Lightweight All-Aluminum Design & Environmental Compliance

To achieve the optimal power-to-weight ratio crucial for aviation platforms, both the cylinder head and cylinder block are manufactured from premium high-strength aluminum alloy. Designed for modern sustainable aviation, it runs on standard 92 Octane Gasoline (92#) and fully complies with the highly stringent China VI environmental emission standards.


4. Technical Specifications

Technical Property ItemVerified Specification Value
Product Model / DisplacementZT-1480cc / 1480 mL (1.5L)
Engine TypeTurbocharged Aviation Piston Engine
Max Power Output197 hp / 145 kW @ 5600 rpm
Maximum Net Power130 kW
Maximum Torque285 N·m @ 1500 - 4000 rpm
Induction SystemTurbocharged
Cylinder ArrangementInline layout / "L" type
Number of Cylinders4
Valves per Cylinder4 (16 Valves Total)
Compression Ratio10.5:1
Valvetrain MechanismDOHC
Fuel Type / Fuel GradeGasoline / 92# Octane
Fuel Delivery SystemGasoline Direct Injection / GDI
Cylinder Head MaterialPremium Aluminum Alloy
Cylinder Block MaterialPremium Aluminum Alloy
Emission StandardChina VI / National VI
Piston Linear Speed15.68 m/s


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