Hexadyne P60

{{Short description|American aircraft engine}}

{{Use mdy dates|date=January 2022}}

{{Use American English|date=January 2022}}

{{Infobox aircraft begin

| name=Hexadyne P60

| image=

| caption=

}}{{Infobox Aircraft Engine

|type=Aircraft engine

|manufacturer=Hexatron Engineering Co., Inc.

|designer=

|national origin=United States

|first run=

|major applications=

|produced=

|number built=

|developed from=

|variants with their own articles=

}}

The Hexadyne P60 is an American aircraft engine, designed and produced by Hexatron Engineering of Salt Lake City, Utah for use in ultralight and homebuilt aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 238-241. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Design and development

The engine is a twin cylinder four-stroke, horizontally-opposed, {{convert|800|cc|cuin|1|abbr=on}}, air-cooled, gasoline engine design, with a mechanical gearbox spur gear reduction drive with a reduction ratio of 2.5:1. It employs electronic ignition and produces {{convert|60|hp|kW|0|abbr=on}} continuous at 5750 rpm. The engine management system is a six-sensor computer and the engine is optimized to drive a {{convert|68|to|70|in|cm|0|abbr=on}} propeller.{{cite web|url=http://hexatronengineering.com/prod02.htm|title=Hexatron Product 2|work=hexatronengineering.com|accessdate=14 July 2015}}

The engine was initially displayed at AirVenture, Oshkosh, Wisconsin in 2001.

Applications

  • Blue Yonder Merlin{{cite web|url=http://hexatronengineering.com/fire_wall_mounting_photos.htm|title=Hexadyne P60 Fire Wall Mounting|work=Hexatron Engineering|accessdate=15 July 2015|url-status=dead|archiveurl=https://web.archive.org/web/20150705025558/http://www.hexatronengineering.com/fire_wall_mounting_photos.htm|archivedate=5 July 2015}}

Specifications (Hexadyne P60)

{{pistonspecs|

|ref=World Directory of Leisure Aviation 2011-12 and manufacturer

|type=Twin cylinder, four-stroke aircraft engine

|bore={{convert|92|mm|in|1|abbr=on}}

|stroke=

|displacement={{convert|800|cc|cuin|1|abbr=on}}

|length={{convert|596|mm|in|1|abbr=on}}

|diameter=

|width={{convert|406|mm|in|1|abbr=on}}

|height={{convert|450|mm|in|1|abbr=on}}

|weight={{convert|45|kg|lb|1|abbr=on}}

|valvetrain=

|supercharger=

|turbocharger=

|fuelsystem=fuel injection

|fueltype=gasoline

|oilsystem=

|coolingsystem=air

|power={{convert|60|hp|kW|0|abbr=on}} at 5750 rpm

|specpower=

|compression=9.0:1

|fuelcon={{convert|3|u.s.gal}} per hour

|specfuelcon=

|oilcon=

|power/weight=

|designer=

|reduction_gear=mechanical gearbox spur gear reduction drive, reduction ratio of 2.5:1

|general_other=

|components_other=

|performance_other=

}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists= *List of aircraft engines

}}

References

{{Reflist}}