UAV SOLUTIONS

Define the mission. Build the power-system brief.

Organise aircraft and operating requirements before comparing published data and opening an engineering discussion.

01 / MISSION CONTEXT

01

Long-endurance operations

A project-context category for requirements discussion.

02

Mapping and surveying

A project-context category for requirements discussion.

03

Infrastructure inspection

A project-context category for requirements discussion.

04

Cargo or utility platforms

A project-context category for requirements discussion.

05

Experimental and development aircraft

A project-context category for requirements discussion.

02 / SELECTION INPUTS

What defines engine selection

A single power, displacement or thrust value is insufficient to confirm compatibility.

03 / FROM REQUIREMENT TO REVIEW

01Define mission
02Capture aircraft inputs
03Compare published data
04Review integration constraints
05Plan ground testing
06Confirm through responsible flight validation

04 / PUBLISHED DATA

Four models for comparison

FieldZT-T170ZT-T222DLE170DLE222
ConfigurationTwin-cylinder, air-cooled, two-stroke gasoline engineFour-cylinder, air-cooled, two-stroke gasoline engineTwin-cylinder two-stroke gasoline engineFour-cylinder two-stroke gasoline engine
Displacement170 cc222 cc170 cm³222.5 cm³
Rated power18.1 hp / 13.3 kW20.9 hp / 15.3 kW10.77 kW @ 7,500 rpm11.76 kW @ 7,523 rpm
Engine weight3.93 kg4.86 kg3,620 g4,860 g
Propeller data30 × 12 / 32 × 1032 × 10 / 32 × 12 / 34 × 1030 × 12 / 32 × 1032 × 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

ENGINEERING SUPPORT

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