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词条 Zenoah G-50
释义

  1. Development

  2. Variants

  3. Applications

  4. Specifications (G-50C)

  5. References

name=Zenoah G-50 image= caption=

}}{{Infobox Aircraft Engine

type=Twin cylinder two-stroke aircraft enginemanufacturer=Zenoahnational origin=Japanfirst run=major applications=produced=number built=program cost=unit cost=US$2990 (2006 price, complete, used)developed from=variants with their own articles=
}}

The Zenoah G-50 is a twin-cylinder, horizontally opposed, two stroke, carburetted aircraft engine, designed for use on ultralight aircraft.[1][2]

Development

The Zenoah G-50 is equipped with single capacitor discharge ignition and dual Mikuni slide-type carburetors. It is equipped with a recoil starter system or optionally electric start and a 2.1 or 2.6:1 belt reduction drive.[1][2][3]

The engine runs on a mixture of unleaded auto fuel and oil.[1][2]

Producing {{convert|45|hp|kW|0|abbr=on}} at 5800 rpm, the G-50 competed in the early 1980s ultralight powerplant market against the similar Rotax 447. Production of the engine was completed in the late 1980s and today only used engines and parts are available.[1][2]

Variants

G50C

Twin-cylinder, horizontally opposed, two stroke, dual-carburetor, fan cooled aircraft engine.[2][3]

G50D

Twin-cylinder, horizontally opposed, two stroke, dual-carburetor, free air cooled aircraft engine.[2][3]

G50DFW

Twin-cylinder, horizontally opposed, two stroke, dual-carburetor, free air cooled aircraft engine, configured for firewall mounting, recoil starting not available.[2][3]

Applications

  • AmeriPlanes Mitchell Wing T-10
  • Eagles Wing Scout
  • Goodwin Buckshot
  • TEAM 1200Z Z-MAX
  • TEAM 1300Z Z-MAX
  • NWT Spruce Coupe
  • Tennessee Propellers Scout

Specifications (G-50C)

{{pistonspecs|
|ref=Cliche & Tennessee Propellers[1][2]
|type=Two cylinder, two-stroke aircraft engine
|bore={{convert|72|mm|in|1|abbr=on}}
|stroke={{convert|59.5|mm|in|1|abbr=on}}
|displacement=484 cc (29.54 cu in)
|length={{convert|14.96|in|mm|1|abbr=on}}
|diameter=
|width={{convert|23.39|in|mm|1|abbr=on}}
|height={{convert|15.00|in|mm|1|abbr=on}}
|weight={{convert|90|lb|kg|1|abbr=on}} equipped with reduction drive, electric start and muffler
|valvetrain=piston ported
|supercharger=
|turbocharger=
|fuelsystem=
|fueltype=unleaded auto fuel
|oilsystem=pre-mixed
|coolingsystem=free air
|power={{convert|45|hp|kW|0|abbr=on}} at 5800 rpm
|specpower=
|compression=6.5:1
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=
|designer=
|reduction_gear=2.1 or 2.6:1 belt system
|general_other=
|components_other=
|performance_other=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

1. ^Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page G-8 Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}
2. ^{{cite web|url = http://www.tn-prop.com/Engines.html |title = Zenoah Engines |accessdate = 2009-12-24|last = Tennessee Propellers |authorlink = |year = n.d.}}
3. ^{{cite web|url = http://www.tn-prop.com/g50.htm |title = Zenoah Engine Retail Pricing |accessdate = 2009-12-24|last = Tennessee Propellers |authorlink = |year = 2006}}
{{Zenoah aircraft engines}}

2 : Air-cooled aircraft piston engines|Two-stroke aircraft piston engines

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