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AI-14
AI-14R engine of a PZL-104 Wilga
Type Radial engine
National origin Soviet Union
Manufacturer Ivchenko
First run 1950

The Ivchenko AI-14 (Russian АИ-14) is a nine-cylinder, air-cooled, radial piston engine designed in the Soviet Union to power aircraft.

Contents

[edit] Variants

Its main variant is the AI-14R (АИ-14Р), which underwent state trials in December 1950 and was used in many types of light aircraft. Several thousand were built. There was also an AI-14V variant for helicopters and other applications. The AI-14R is typically used with a two-bladed propeller and is started with compressed air.

Apart from the Soviet Union, a licenced version of the AI-14R, (currently AI-14RA), has been produced by WSK-Kalisz in Poland from 1956 until 2007.

The AI-14RF was a variant uprated by Ivan Vedeneyev to 300 hp. Its further development is the Vedeneyev M14P family of engines.

Another modified version is the Czechoslovak Avia M462, which powers the Zlín Z 37 agricultural aircraft.

[edit] Applications

[edit] Specifications (Ivchenko AI-14)

General characteristics

  • Type: 9-cylinder, air-cooled, radial, engine
  • Bore: 105mm (4.13in)
  • Stroke: 130mm (5.12in)
  • Displacement: 10.13 Liters (618 cu in)
  • Dry weight: 200kg (441lb)

Components

  • Supercharger: Single stage, single speed, geared centrifugal supercharger
  • Fuel system: Carburetor
  • Cooling system: Air

Performance

  • Power output:
    • Power (take-off): 260 hp (194 kW)
    • Power (nominal): 220 hp (161 kW)
  • Compression ratio: 5.9:1

[edit] See also

[edit] References

  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 93. 
  • Kotelnikov, Vladimir (2005). Russian Piston Aero Engines. Crowood Press Ltd.. pp. 201–203. 



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