PG50 Web

TEI-PG50
2-Stroke Gasoline
Aviation Engine

Designed for Unmanned Air Vehicles (UAV)

Developed through the superior design and manufacturing engineering capabilities, with the support of TUBITAK and technical infrastructure of TEI, and by utilization of national opportunities/facilities with maximum indigenousness, TEI-PG50 is a 2-stroke boxer type UAV gasoline engine, which is the first 2-stoke aviation engine of Turkey in its power class.

The TEI-PG50 engine for which the activities to proceed to the mass production stage continue at a rapid pace attracts attention with a maximum capacity of 50 (± 2) HP. TEI-PG50 engine has a best-in-class altitude capability with a ceiling altitude 30.000 ft.

Standing out with higher power/weight ratio and the higher power it generates compared to that of the current UAV intended for similar purposes, as well as the rapid technical and logistic support features it offers through the injection and ignition systems and the electronic engine control system, TEI-PG50 performs Its flights by TEI's experimental platform successfully.

TEI-PG50

The advantages compared to the existing UAV engines for the same intended purpose:

Higher power
High power/weight ratio
Electronic engine control unit
Electronic injection and ignition
Efficient combustion with double spark plug application
Fast technical, logistic support
~84% localized part
Pg50 V

 

Technical Specifications

Engine Configuration

2 Cylinder Boxer Engine

Displacement

0.5 L

Air Induction

Natural Aspiration

Fuel Supply

 ECU Controlled Injection

Maximum Power

(@6500 RPM) 50 HP (±2)  

Engine Cooling

Air Cooled

Fuel

AVGAS 100 LL

Aircraft Configuration

Pusher - Puller

 Maximum Altitude

30,000 ft

Dry Weight (Except Accessories)

19 kg (±1)

Aircraft Configuration

Pusher - Puller

Engine Control

Electronic Engine Control Unit

Fuel Consumption

Cruise SFC < 400g/kWh

Electrical Power Generation 

1100 W Continous Electrical Power

 

 

 

 

 

 

 

TEI-PG50

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