{{Short description|Belgian aircraft engine manufacturer}} {{Promotional|date=September 2025}}

{{Infobox company |name = ULPower Aero Engines |logo = 160px|center| ULPower Company Logo |type = NV |foundation = 2006 |location = Ypres, Belgium |industry = Aircraft Engine Manufacturer |products = Aircraft Engines |revenue = |operating_income = |net_income = |num_employees = |parent = |subsid = |homepage = http://www.ulpower.com |footnotes = }}

'''ULPower Aero Engines''' is a Belgian company which manufactures engines designed for use in light aircraft and rotorcraft.

==History== thumb|UL350iS thumb|UL520iS installation In 2001, the founding partners of ULPower were asked to fix an issue with a Jabiru engine fitted into a helicopter. By examining the setup they decided to build a new engine from scratch instead, because the particular Jabiru engine simply was too small for the application. The new engine should have the following aims and objectives: FADEC, simple, robust, easy to maintain, low parts count, high power to weight ratio and low cost of ownership.<ref>{{cite web |title=ULPower history |url=http://ulpower.news/where-did-ulpower-come-from |website=Where did ULPower come from |date=2 December 2017 |access-date=1 March 2019}}</ref> The founding partners had years of experience in the professional automotive rally industry. This included engine design, development and production for the Dakar Rally and a proprietary ECU<ref name="ULP_EAA_2010">{{cite news |last1=Kern |first1=Tim |title=The ULPower Family of Engines |agency=Sport Aviation |issue=July 2010 |publisher=Experimental Aircraft Association |date=1 July 2010}}</ref> Based on the years of engine experience from Rally, the prototype helicopter engine and the proprietary ECU, they decided to form a company producing aero engines. A couple of more objectives were added: The engine should be direct drive, air cooled and be able to run on both AVGAS and MOGAS with ethanol.<ref name="ULP_EAA_2010" />

Three of the four founding partners are Nicolas Josson of ROPA.BE and Lionel and Pascal D’Hondt who owns DR Tuning in Belgium. ROPA.BE is a metal turning and milling company making engine parts, while DR Tuning works in the motor racing arena.<ref name="Kitplane_2010">{{cite news |last1=Ellis |first1=Steve |title=ULPower's new four ushers in small-scale FADEC. |issue=June 2010 |publisher=Kitplanes |date=1 June 2010}}</ref>

After a few years of development and testing of several prototypes the first UL260i 72&nbsp;kW (97&nbsp;hp) engine was installed in an aircraft (a Lambert Mission 106). First flight tests were performed in December 2005. After proving{{citation needed|date=May 2016}} the engine reliability on the ground and in the air, the project was merged into an official company structure. ULPower Aero Engines was officially formed in March 2006 to concentrate on the further design and manufacture of engines where light weight, power and reliability are important to the client. Series production commenced by the end of that year.{{Citation needed|date=March 2019}}

Over the first years, the UL260i has equipped several popular light aircraft, e.g. Fly Synthesis Storch, Zenair Zodiac CH601, Just Escapade, Dyn'Aéro MCR01, Hannuman X-Air. In 2017 Sonex Aircraft introduced their "B" models with slightly larger fuselage giving room for more engine options.<ref name="bigger_and_better">{{cite news |last1=Esau |first1=Megan |title=Bigger and Better |agency=Sport Aviation |issue=May 2017 |publisher=Experimental Aircraft Association |date=1 May 2017}}</ref> Along that introduction the 4 cylinder ULPower engines became a standard factory supported alternative.<ref name="bigger_and_better" />

In 2009, ULPower launched new engine types: the UL260iS 80&nbsp;kW (107&nbsp;hp) and the UL350i/iS 93&nbsp;kW (125&nbsp;hp) where the stroke was increased from 74&nbsp;mm to 100&nbsp;mm. About the same time the Twister Aerobatics Team, flying the Silence Twister, was looking for a more powerful engine that also could run inverted, as a replacement for the original 80&nbsp;hp Jabiru 2200.<ref name="Twister" /> They already knew about the UL260i/iS and in cooperation the UL260iSA was developed. It has 80&nbsp;kW (107&nbsp;hp) and a fully inverted oil system.<ref name="Twister">{{cite web |title=The Silence SA1100 Twister |url=http://www.twister-aerobatics.co.uk/the-silence-sa1100-twister/ |website=Twister Aerobatics Team |access-date=2 March 2019}}</ref>

For the French market specifically, two adapted versions were available: the UL260iF 74&nbsp;kW (100&nbsp;hp) based on the UL260iS and the UL350iF 90&nbsp;kW (120&nbsp;hp) based on the UL350iS, specifically for gyrocopter application.{{Citation needed|date=March 2019}} The UL350iF is no longer available.

The product line was expanded again in 2013, with a line of 6-cylinder engines in both 3900 cc and 5200 cc variants, each with an option for higher or lower compression requiring different minimum fuel grades. The 6 cylinder engines can power larger experimental and kit-planes (non-certified planes) that are typically powered by Lycoming and Lycoming clones in the O320-O360 range.<ref name="new_old_aero_engine">{{cite news |last1=Ellis |first1=Steve |title=The New Old Aero Engine |issue=January 2016 |publisher=Kitplanes |date=1 January 2016}}</ref>

The ULPower engines are modular. They all have the same bore of 105.6&nbsp;mm. The stroke is either 74 or 100&nbsp;mm, which makes the 260 and 350 series of engines. Adding one extra set of cylinders makes the 390/520 family.<ref name="new_old_aero_engine" />

== Engines == ULPower produces a range of direct drive air-cooled horizontally-opposed engines with multiport fuel-injection and FADEC. All engines can run on avgas (100LL or UL91). All engines can run on automotive gasoline with up to 15% ethanol and with octane ratings as specified.

{| border="1" class="wikitable" |+ 4-cylinder engines ! Model ! Power ! Displacement ! Ready to fly weight ! Minimum octane ! Notes |- ! UL260i | {{convert|97|hp|kW|0|abbr=on}} || 2592 cc || {{convert|72.9|kg|lb|0|abbr=on}} || 95RON 87MON (91AKI) || |- ! UL260iS | {{convert|107|hp|kW|0|abbr=on}} || 2592 cc || {{convert|72.9|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || |- ! UL260iF | {{convert|100|hp|kW|0|abbr=on}} || 2592 cc || {{convert|72.9|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Built for French UL regulations |- ! UL260iSA | {{convert|107|hp|kW|0|abbr=on}} || 2592 cc || {{convert|75.4|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Aerobatic |- ! UL260iSK | {{convert|107|hp|kW|0|abbr=on}} || 2592 cc || {{convert|72.9|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Unknown at this time |- ! UL350i | {{convert|118|hp|kW|0|abbr=on}} || 3503 cc || {{convert|78.4|kg|lb|0|abbr=on}} || 95RON 87MON (91AKI) || |- ! UL350iS | {{convert|130|hp|kW|0|abbr=on}} || 3503 cc || {{convert|78.4|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || |- ! UL350iSA | {{convert|130|hp|kW|0|abbr=on}} || 3503 cc || {{convert|78.9|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Aerobatic |- ! UL350iHPS | {{convert|150|hp|kW|0|abbr=on}} || 3503 cc || {{convert|82.4|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Helicopter |}

{| border="1" class="wikitable" |+ 6-cylinder engines ! Model ! Power ! Displacement ! Ready to fly weight ! Minimum octane ! Notes |- ! UL390i | {{convert|140|hp|kW|0|abbr=on}} || 3888 cc || {{convert|100|kg|lb|0|abbr=on}} || 95RON 87MON (91AKI) || |- ! UL390iS | {{convert|160|hp|kW|0|abbr=on}} || 3888 cc || {{convert|100|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || |- ! UL390iSA | {{convert|160|hp|kW|0|abbr=on}} || 3888 cc || {{convert|103.8|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Aerobatic |- ! UL520i | {{convert|180|hp|kW|0|abbr=on}} || 5254 cc || {{convert|108|kg|lb|0|abbr=on}} || 95RON 87MON (91AKI) || |- ! UL520iS | {{convert|200|hp|kW|0|abbr=on}} || 5254 cc || {{convert|108|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || |- ! UL520T | {{convert|220|hp|kW|0|abbr=on}} || 5254 cc || {{convert|122|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Turbocharged |- ! UL520iSRR | {{convert|200|hp|kW|0|abbr=on}} || 5254 cc || {{convert|108|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Reverse Rotation |- ! UL520iSA | {{convert|200|hp|kW|0|abbr=on}} || 5254 cc || {{convert|108|kg|lb|0|abbr=on}} || 98RON 90MON (94AKI) || Aerobatic |}

== References == <references /> *{{cite journal |last=Norton |first=Thomas F. |date=June 2007 |title=The promise of things to come... Engine makers report progress and innovation |journal=The Southern Aviator |url=http://www.southern-aviator.com/ |access-date= 2008-02-03}}

== External links == {{Commons category|ULPower aircraft engines}} *[http://www.ulpower.com/ ULPower Company]

{{ULPower Aero Engines}}

Category:ULPower aircraft engines Category:Aircraft engine manufacturers of Belgium Category:Belgian companies established in 2006 Category:Belgian brands Category:Manufacturing companies established in 2006