X
TEI'Yİ SOSYAL MEDYADA<BR>TAKİP EDİN
ARAMAK İSTEDİĞİNİZ<BR>KELİMEYİ YAZINIZ
LÜTFEN WEB SİTESİNİN<BR>DİLİNİ SEÇİNİZ
TR
EN
DIESEL ENGINE MODIFICATION PROJECT

This project is intended for modification of the commercial diesel engine planned for use in the Unmanned Aerial Vehicles (UAVs), so as to meet the needs of UAVs. The power supply and electricity generation of the engine at high altitude conditions are increased through the modifications, making it ready for use in UAVs.

 

Technical specifications of the Modificated Engine:

Maximum Continuous Power
:
155 hp
 
Weight
:
165 kg 
 
Fuel Consumption
:
<215 gr/kWh 
 
Electricity Power Generation Capacity
:
9 kW (2 x 4.5kW)
 
Critical Altitude
:
11.500 ft  
 
Maximum Altitude
:
30.000 ft
 
Propeller Rotation Control
:
Variable pitch , Single lever control, hydromechanics
 
Gear Case
:
Impreller configuration
 
Engine Control
:
Redundant electronic engine control system (FADEC)
 
Engine Control Software
:
 DO178-C DAL-C compatible
 
EGÜS Control Software
:
 DO178-C DAL-C compatible
 
Fuel
:
JP8, Jet A1, Diesel
 
Aircraft Interface
:
Mechanical, Electronic and Signal inrerface compatible with MALE Class UAV