“Hirth HM 60”的意思、由来-开放百科全书

词条

Hirth HM 60

释义

Variants
Applications
Specifications (HM 60R2)
See also
References
Notes Bibliography
External links

name = HM 60

image = Hirth HM 60.JPG

caption =

}}{{Infobox Aircraft Engine

type=Inline piston engine

manufacturer=Hirth

national origin=

1923}}

major applications=Klemm Kl 25

number built =

program cost =

unit cost =

developed from =

developed into =

variants with their own articles =
}}

The Hirth HM 60 was a four-cylinder inverted air-cooled inline aircraft engine designed in 1923 and first sold in 1924. The engine was of very high quality, and its sales success contributed to Hirth's rapid pre-war expansion. It was a popular engine for light aircraft delivering 80 hp (60 kW) at 2,300 rpm. Later Hirth engines built upon the HM 60's success and provided greater power with many of the same design features.^[1]

Variants

HM60

HM60R

HM60R2

Applications

Fieseler Fi 5
Göppingen Gö 9
Horten H.V
Klemm Kl 25
Klemm Kl 35
Klemm Kl 107
Shackleton-Murray SM.1
WNF Wn 16

Specifications (HM 60R2)

{{pistonspecs
|
|type=4-cylinder air-cooled inverted inline engine.
|bore=102 mm (4 in)
|stroke=110 mm (4.33 in)
|displacement=3.6 L (220 cu in)
|length=856 mm (33.7 in)
|diameter=
|width=391 mm (15.4 in)
|height=688 mm (27.1 in)
|weight=97 kg (214 lb)
|valvetrain=1 inlet and 1 exhaust valve per cylinder.
|supercharger=
|turbocharger=
|fuelsystem=Carburetor
|fueltype=74 octane
|oilsystem=
|coolingsystem=Air-cooled
|power=80 hp (60 kW) at 2,400 rpm
|compression=5.8:1
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=507 W/kg (0.3 hp/lb) at cruise speed
}}

References

Notes

1. ^Gunston 1989, p.77.

Bibliography

Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. {{ISBN|1-85260-163-9}}

External links

Oldengine.org

2 : Hirth aircraft engines|Aircraft piston engines 1920–1929

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