ZT-T730CC 730cc Heavy-Lift UAV Gasoline Engine | EFI & Carburetor Versions, Electric Start with Optional Generator

  1. High-power 4-cylinder horizontally opposed two-stroke UAV gasoline engine, peak output up to 63.5hp/47.3kW, supporting maximum take-off weight of 270kg heavy-lift industrial drones
  2. Dual fuel supply options: EFI electronic fuel injection version cuts fuel consumption to 12L/h; carburetor version suits low-budget industrial drone assembly
  3. Ultra-low vibration boxer layout, intelligent automatic angle CDI ignition, stable idle and smooth throttle response for long-hour continuous flight missions
  4. Aerospace-grade reinforced structure: ceramic nickel-silicon coated cylinder liner & 7-piece forged crankshaft, strong heat and torque resistance for harsh aerial working environments
  5. Integrated electric start design, optional 800W/2000W onboard generator to power heavy avionics, survey cameras and multi-functional mission payloads
  6. Large static thrust output: 75kg thrust at 100m altitude, 70kg thrust at 1800m, perfectly matched with large agricultural fixed-wing and long-endurance cargo drones

Product Overview

The ZT-T730CC heavy-lift drone gasoline engine is an industrial-grade two-stroke propulsion system built for commercial aerial operations, excluding tactical military use scenarios. Adopting a mature horizontally opposed 4-cylinder layout, this UAV engine is specially optimized for heavy-payload cargo delivery drones, large agricultural spraying fixed-wing aircraft, long-distance aerial mapping and environmental monitoring UAV platforms.

Compared with single/twin-cylinder drone gasoline engines of the same displacement, its symmetrical opposed cylinder structure effectively offsets low-frequency vibration within the full speed range (2000–7500rpm), avoiding equipment jitter interference to high-precision survey payloads. With verified maximum static thrust of 75kg near sea level and a 270kg MTOW limit, it balances power output, fuel economy and service life to meet the long-cycle operation demands of global commercial aviation users.Drone gasoline engine

Core Structural & Performance Highlights

Balanced 4-Cylinder Boxer Layout & Intelligent Ignition

The horizontally opposed four-cylinder layout eliminates unbalanced vibration common in single-row engines. It equips a synchronous dual-opposed cylinder CDI automatic angle ignition module, which automatically switches ignition timing at 500rpm. This design ensures steady idle speed without stall risk and linear throttle adjustment during climbing, cruising and descending flights, greatly improving flight safety for heavy-load UAVs.

Aerospace Durable Forged & Coated Components

All load-bearing core parts are upgraded with aviation manufacturing standards:

Cylinder block: Cast aluminum alloy with inner wall ceramic nickel-silicon hard coating, anti-wear and heat-resistant, extending continuous working life

Piston: High-purity aluminum alloy blank with precision oval grinding, reducing friction loss under high-speed operation

Crankshaft: Integrated seven-piece forging assembly, capable of enduring instant torque impact during full-throttle takeoff and steep climbing

Dual Fuel System & Custom Power Generation Module

Two independent fuel supply solutions are available to match different altitude and cost demands:

Diaphragm carburetor version: No traditional choke structure, fuel consumption 17L/h, suitable for plain low-altitude agricultural and delivery UAV projects

ECU EFI electronic injection version: Intelligent real-time oil supply adjustment for high-altitude thin air environments, fuel consumption reduced to only 12L/h, obvious endurance improvement

Custom optional high-power generator module: 800W or 2000W output options, which can continuously supply power to heavy servo actuators, LiDAR mapping pods, thermal imaging cameras and long-distance data transmission equipment without extra external power batteries.

Full Technical Specification Table

Specification ItemVerified Parameter Value
Total Displacement730 cc
Maximum Power Output63.5 hp / 47.3 kW
Cylinder ArrangementHorizontally opposed 4-cylinder
Engine Cycle TypeTwo-stroke air-cooled
Working RPM Range2000 – 7500 rpm
Static Thrust (100m Altitude)75 kg
Static Thrust (1800m Altitude)70 kg
Maximum Take-off Weight Supported270 kg
Recommended Propeller Sizes3220; 3023; 30*25
Bore × Stroke66 mm × 54 mm
Fuel-Oil Mix Lubrication Ratio30:1 (Gasoline : Two-stroke synthetic oil)
Ignition ModeCDI automatic angle advance ignition
Firing Control LogicOpposed twin-cylinder synchronous ignition, auto timing switch at 500rpm
Cylinder Inner Wall TreatmentCast aluminum alloy + ceramic nickel-silicon hard coating
Piston CraftPrecision oval grinding aviation aluminum alloy casting
Crankshaft CraftIntegrated seven-piece forging structure
Standard Carburetor ConfigurationDual diaphragm universal carburetors (choke-free design)
Optional Onboard Generator Power800 W / 2000 W
Fuel Consumption (Carburetor Model)17 L/h
Fuel Consumption (ECU EFI Model)12 L/h
Net Core Engine Weight18.5 kg
Overall Outer Dimensions (LWH)420 × 410 × 370 mm
Factory Optional AccessoriesExhaust pipe assembly, electric starter, power generator set

Wide Commercial Application Scenarios

This multi-purpose UAV gasoline engine is widely applied in civilian industrial aerial fields only:

Large agricultural fixed-wing drones: Crop pesticide spraying, seed sowing, farmland nutrient mapping

Long-endurance cargo delivery UAVs: Rural mountain logistics, island material transportation, emergency disaster relief material delivery

Aerial survey & mapping platforms: Topographic mapping, mine resource survey, water conservancy pipeline inspection

Environmental monitoring aircraft: Forest fire patrol, river water quality sampling, wildlife habitat observation

Civil engineering inspection power: High-voltage line patrol, bridge structure safety detection, wind turbine blade inspection

FAQ (2 Exclusive Questions for Independent Station Conversion)

Q1: What are the differences between the carburetor version and ECU EFI version of this 730cc UAV gasoline engine, and how to choose the suitable one?

A: The carburetor model has lower overall procurement cost, with a fuel consumption of 17L/h, stable performance in areas below 1000m altitude, ideal for plain-area agricultural drones and short-distance cargo UAVs. The ECU EFI electronic injection version supports adaptive fuel supply under high altitude and low air pressure, fuel consumption is reduced to 12L/h, greatly extending flight endurance, which is more suitable for plateau mountain survey UAVs and long-hour monitoring missions. If your operation area is above 1500m altitude or you have strict endurance requirements, the EFI version is recommended.

Q2: Can the optional 2000W generator of ZT-T730CC drone gasoline engine drive multi-payload equipment such as LiDAR and thermal imaging cameras at the same time?

A: Yes, the 2000W high-power generator supports simultaneous power supply of multi-type high-power mission payloads including LiDAR scanning pods, infrared thermal cameras, long-distance digital transmission modules and heavy steering servos. The built-in voltage stabilizing module can avoid current fluctuation interference to precision detection equipment during engine speed changes. If you only carry basic mapping cameras and small servos, the 800W generator option can fully meet daily operation demands to control extra costs.

Packing & Factory Supply Information

All ZT-T730CC UAV engines are packed with shockproof foam and export-grade wooden cases to avoid collision damage during ocean and air transportation. The factory supports bulk wholesale, OEM customized labeling and matching accessory packages (exhaust pipe, starter, generator set). We provide complete operation manuals, maintenance guides and one-year core component warranty service for all orders. If you need test data sheets, dimension drawings or customized technical adjustments, please contact our sales team to get detailed supporting documents.

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