Jump to content

ULPower UL520i

From Alfawiki
Adapted from the English Wikipedia article ULPower UL520i, available under CC BY-SA 4.0Updated 29 November 2025
ULPower Aero Engines
IndustryAerospace
Headquarters
Geluveld
,
Belgium
ProductsAircraft engines

Template:Infobox aero engine

The ULPower UL520i is an aircraft engine originating from Belgium, engineered and manufactured by ULPower Aero Engines based in Geluveld. This engine is primarily intended for installation in homebuilt aircraft.

Design and development

This powerplant features a six-cylinder, four-stroke, horizontally opposed configuration with an air-cooled system. It has a displacement of 5,254 cc (320.6 cu in) and operates on gasoline with direct-drive. Dual electronic ignition is incorporated, enabling it to deliver between 180 to 200 hp (134 to 149 kW) at 3300 rpm.

Variants

UL520i
Standard version equipped with fuel injection and an 8:1 compression ratio, capable of producing 180 hp (134 kW) at 3300 rpm.
UL520iS
Enhanced model featuring fuel injection and an increased compression ratio of 8.7:1, generating 200 hp (149 kW) at 3300 rpm.
UL520iST
A turbo-normalized variant currently in development, utilizing fuel injection and designed to output 220 hp (164 kW) at 2700 rpm at sea level.
UL520iSA
This version of the UL520iS incorporates an inverted oil system while maintaining a power output of 200 hp (149 kW) at 3300 rpm.
UL520iHPS
A forthcoming model still under development.
UL520iSRR
Features reversed rotation, fuel injection, and an 8.7:1 compression ratio, delivering 200 hp (149 kW) at 3300 rpm.

Applications

Specifications (UL520i)

Template:Pistonspecs

See also

Template:Aircontent

References

External links

Template:ULPower Aero Engines