Hirth HM 504

{{Short description|1930s German aircraft engine}}

{{Infobox Aircraft Begin

|name = Hirth HM 504

|image = File:Hirth HM 504 Aircraft engine at Flugausstellung Hermeskeil, pic1.jpg

|caption = Hirth HM 504 on display at the Flugausstellung Hermeskeil

}}{{Infobox Aircraft Engine

|type=Inline piston engine

|manufacturer= Hirth-Motoren GmbH, Stuttgart-Zuffenhausen

|national origin= Germany

|first run=

|major applications=Bücker Bü 131

|number built =

|program cost =

|unit cost =

|developed from =

|developed into = Hitachi Hatsukaze

|variants with their own articles =

}}

The Hirth HM 504 is a four-cylinder air-cooled inverted inline engine. The HM 504 was a popular engine for light aircraft of the 1930s-1940s, and it was used to power a number of Germany's trainer aircraft of World War II. The engine featured a cast magnesium alloy crankcase made of Elektron{{cite book |last=Gunston |first=Bill |title=World Encyclopaedia of Aero Engines |year=1989 |publisher=Patrick Stephens Limited |location=Cambridge, England |isbn=978-1-85260-163-8 |edition=2nd |page=77}}{{cite journal |title=Werkstoff-Volumenanteile der 'AR' 79 |trans-title=Materials proportions by volume of the AR 79 (advertising back matter)  |journal=Flugsport |place=Frankfurt/Main |volume=31 |issue=8 |date=12 April 1939 |lang=de |page=229 [pdf 32] |url=https://archive.org/details/leseprobe-flugsport-1939/page/n31/mode/1up}} The Hitachi Hatsukaze Model 11 was a Japanese licensed version.

Applications

Specifications (HM 504 A-2)

{{pistonspecs

|

|ref=Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944,{{cite book |last=Schneider |first=Helmut (Dipl.Ing.) |title=Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 |date=1944 |publisher=Herm. Beyer Verlag |location=Leipzig |isbn=381120484X |edition=Facsimile reprint 1986 |language=German |page=396}} Der Flugmotor. Bauteile und Baumuster{{cite book |last1=Katz |first1=Hans (Dr.Ing) |title=Der Flugmotor. Bauteile und Baumuster. Luftfahrt Lehrbücherei Band 7 |date=1940 |publisher=de Gruyter |location=Berlin}}

|type=4-cylinder air-cooled inverted inline

|bore={{cvt|105|mm|2}}

|stroke={{cvt|115|mm|2}}

|displacement={{cvt|3.980|L|cuin|2}}

|length={{cvt|945|mm|1}}

|diameter=

|width= {{cvt|520|mm|1}}

|height={{cvt|780|mm|1}}

|weight={{cvt|107|kg|0}} dry, unequipped

::::{{cvt|124|kg|0}} wet, equipped

|valvetrain=1 inlet and 1 exhaust under-valve per cylinder driven by pushrods and rockers

|supercharger=

|turbocharger=

|fuelsystem=

|fueltype=80 Octane

|oilsystem=dry sump, pressure feed with scavenge

|coolingsystem=air-cooled

|power=

:*{{cvt|105|PS|hp kW|0}} at 2,530 rpm (5 minutes) at sea level

:*{{cvt|95|PS|hp kW|0}} at 2,450 rpm (30 minutes) at sea level

:*{{cvt|85|PS|hp kW|0}} at 2,360 rpm (max. continuous / cruise) at sea level

|specpower={{cvt|26.35|PS/L|hp/cuin kW/L|2}}

|compression=6.2:1

|fuelcon=

|specfuelcon={{cvt|0.228|kg/PSh|lb/hph kg/kWh|3}} at max continuous

|oilcon={{cvt|0.002|-|0.003|kg/PSh|lb/hph kg/kWh|3}} at max continuous

|power/weight={{cvt|0.98|PS/kg|hp/lb kW/kg}}

  • B.M.E.P.: {{cvt|9.37|atm|bar psi}}

}}

See also

References

{{Commons category}}

{{reflist}}