01 / MODEL
ZT-T170
High-output twin-cylinder gasoline propulsion
- Configuration
- Twin-Cylinder
- Displacement
- 170 cc
- Rated Power
- 18.1 hp / 13.3 kW
- Engine Weight
- 3.93 kg
ENGINEERING PROPULSION SYSTEMS / 01
Gasoline Engines for Fixed-Wing UAVs
Gasoline engines for UAV manufacturers, system integrators and giant-scale aircraft.
ZT-T170 · ZT-T222 · DLE170 · DLE222
Engineering Support · OEM Integration
01 / PROPULSION02 / OEM INTEGRATION03 / SELECTION
ENGINEERING EVALUATION
Published specifications.
Informed selection.
Compare approved specifications and evaluate each model against documented installation requirements.
FOUR-ENGINE PORTFOLIO
Clear choices.
Neutral guidance.
Four available engine models presented by configuration and approved technical data.
02 / MODEL
ZT-T222
High-output four-cylinder gasoline propulsion
- Configuration
- Four-Cylinder
- Displacement
- 222 cc
- Rated Power
- 20.9 hp / 15.3 kW
- Engine Weight
- 4.86 kg
03 / MODEL
DLE170
Twin-cylinder gasoline engine option
- Configuration
- Twin-Cylinder
- Displacement
- 170 cm³
- Rated Power
- 10.77 kW @ 7,500 rpm
- Engine Weight
- 3,620 g
04 / MODEL
DLE222
Four-cylinder gasoline engine option
- Configuration
- Four-Cylinder
- Displacement
- 222.5 cm³
- Rated Power
- 11.76 kW @ 7,523 rpm
- Engine Weight
- 4,860 g
ENGINE COMPARISON
Four engines.
Approved fields only.
| Field | ZT-T170 | ZT-T222 | DLE170 | DLE222 |
|---|---|---|---|---|
| Configuration | Twin-cylinder, air-cooled, two-stroke gasoline engine | Four-cylinder, air-cooled, two-stroke gasoline engine | Twin-cylinder two-stroke gasoline engine | Four-cylinder two-stroke gasoline engine |
| Displacement | 170 cc | 222 cc | 170 cm³ | 222.5 cm³ |
| Rated power | 18.1 hp / 13.3 kW | 20.9 hp / 15.3 kW | 10.77 kW @ 7,500 rpm | 11.76 kW @ 7,523 rpm |
| Engine weight | 3.93 kg | 4.86 kg | 3,620 g | 4,860 g |
| Propeller data | 30 × 12 / 32 × 10 | 32 × 10 / 32 × 12 / 34 × 10 | 30 × 12 / 32 × 10 | 32 × 10 / 32 × 12 / 34 × 10 |
ZT-T170
- Configuration
- Twin-cylinder, air-cooled, two-stroke gasoline engine
- Displacement
- 170 cc
- Rated power
- 18.1 hp / 13.3 kW
- Engine weight
- 3.93 kg
- Propeller data
- 30 × 12 / 32 × 10
ZT-T222
- Configuration
- Four-cylinder, air-cooled, two-stroke gasoline engine
- Displacement
- 222 cc
- Rated power
- 20.9 hp / 15.3 kW
- Engine weight
- 4.86 kg
- Propeller data
- 32 × 10 / 32 × 12 / 34 × 10
DLE170
- Configuration
- Twin-cylinder two-stroke gasoline engine
- Displacement
- 170 cm³
- Rated power
- 10.77 kW @ 7,500 rpm
- Engine weight
- 3,620 g
- Propeller data
- 30 × 12 / 32 × 10
DLE222
- Configuration
- Four-cylinder two-stroke gasoline engine
- Displacement
- 222.5 cm³
- Rated power
- 11.76 kW @ 7,523 rpm
- Engine weight
- 4,860 g
- Propeller data
- 32 × 10 / 32 × 12 / 34 × 10
ENGINE SELECTION
Engine Selection Guide
Compare engine configuration, displacement, rated power, engine weight, propeller requirements, available installation space and aircraft integration requirements.
Final engine selection should be based on complete aircraft performance calculations, installation constraints and flight testing.
Fuel consumption, service life and delivery timing: Contact engineering.
For projects in Russia, Eastern Europe and Central Asia, share the destination, operating conditions, available fuel and documentation requirements. Compatibility and delivery arrangements require confirmation.
Request guidance →ENGINEERING SUPPORT