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词条 Continental IO-346
释义

  1. Design and development

  2. Variants

  3. Applications

  4. Specifications (IO-346)

  5. See also

  6. References

name=IO-346image=caption=

}}{{Infobox Aircraft Engine

type=Piston aero-enginenational origin= United Statesmanufacturer=Teledyne Continental Motorsfirst run=1962produced= 1965-1969major applications=Beechcraft Musketeerdeveloped into = Continental IO-520
}}

The Continental IO-346 engine is a fuel-injected four-cylinder aircraft engine that was developed especially for the Beechcraft Musketeer Custom III by Continental Motors. It was produced for that aircraft between 1965 and 1969.[1]

Design and development

There is no carbureted version of the engine, which would have been designated O-346 and therefore the base model is the IO-346.[1][2]

The IO-346 was designed to run on 91-98 avgas. The engine has a dry weight of 269¾ lb or 297 lb including the generator and starter. The ignition system consists of dual magnetos, one Scintilla S4RN-201 and one S4RN-205 or, alternatively, two Slick Electro 449 magnetos.[1][2]

Variants

IO-346-A

Base model, certified 27 July 1962[2]

IO-346-B

Identical to IO-346-A except it incorporates provisions for a hydraulic propeller control. Certified 23 June 1964.[2]

Applications

  • Beechcraft Musketeer[1]
  • Gadfly E.S 102[1]
  • Piel Emeraude[1]
  • Stampe SV-4D[1]

Specifications (IO-346)

Reference: Engines for Homebuilt Aircraft & Ultralights[1]{{pistonspecs
|
|type=4-cylinder air-cooled horizontally opposed aircraft piston engine
|bore=5.25 in (133 mm)
|stroke=4.00 in (102 mm)
|displacement=346 in³ (5.68 L)
|length=30 in (762 mm)
|diameter=
|width=33.38 in (848 mm)
|height=22.4 in (569 mm)
|weight=297 lb dry, with starter and generator (135 kg)
|valvetrain=One intake and one exhaust valve per cylinder
|supercharger=
|turbocharger=
|fuelsystem=CMC fuel injection
|fueltype=91/98 octane avgas
|oilsystem=
|coolingsystem=Air-cooled
|power=165 hp (121 kW) at 2,700 rpm
|specpower=0.47 hp/in³ (21.2 kW/L)
|compression=7.5:1
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=0.56 hp/lb (0.90 kW/kg)
}}

See also

  • List of aircraft engines

References

1. ^Christy, Joe: Engines for Homebuilt Aircraft & Ultralights, pages 63. TAB Books, 1983. {{ISBN|0-8306-2347-7}}
2. ^{{cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/764ef6a32608a1cc8525670e0046d972/$FILE/E3ce.pdf|format=PDF|title = TYPE CERTIFICATE DATA SHEET NO. E3CE|accessdate = 2008-12-14|last = Federal Aviation Administration|authorlink = |date=November 1973}}
{{Continental aeroengines}}

3 : Aircraft piston engines 1960–1969|Boxer engines|Continental aircraft engines

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