Ivchenko AI-14

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

Variants

Its main variant is the AI-14R (АІ-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.

The Zhuzhou HS-6' was the designation for AI-14 Licence production in China.

Applications

Aero L-60 Brigadýr (L-60S variant)
Antonov An-14 - AI-14RF
ICA IS-23 - AI-14RF
Kamov Ka-15 - AI-14V
Kamov Ka-18 - AI-14VF
Kamov Ka-26
Nanchang CJ-6
PZL-101 Gawron
PZL-104 Wilga
Sever-2 (aerosled based on GAZ-M20 Pobeda passenger car)
Yakovlev Yak-12
Yakovlev Yak-18 (Yak-18A variant)

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

References

Wikimedia Commons has media related to Ivchenko AI-14.

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

v t e Ivchenko-Progress aircraft engines

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