Shvetsov ASh-62

{{short description|Soviet radial piston aircraft engine}}

{{Infobox Aircraft Begin

|name= ASh-62

|image = File:Neunzylinder-Sternmotor Schwezow ASch-62.jpg

|caption =

}}

{{Infobox Aircraft Engine

|type= Radial engine

|national origin =

|manufacturer= Shvetsov

|first run=1937

|major applications= Antonov An-2, Polikarpov I-153, Polikarpov I-16, Lisunov Li-2

|number built = 40,361

|program cost =

|unit cost =

|developed from = Shvetsov M-25

|developed into = Shvetsov ASh-82

|variants with their own articles =

}}

The Shvetsov ASh-62 (Russian: АШ-62, designated M-62 before 1941) is a nine-cylinder, air-cooled, radial aircraft engine produced in the Soviet Union. A version of this engine is produced in Poland as the ASz-62 and the People's Republic of China as the HS-5.

Design and development

The ASh-62 was a development of the Wright R-1820 Cyclone that had been built in Russia under licence as the Shvetsov M-25, the main improvements including a two-speed supercharger and a more efficient induction system. Power was increased from the Cyclone's 775 hp to 1,000 hp. First run in 1937, licensed versions are still in production by WSK "PZL-Kalisz" in Poland (as of 2017).Gruszczyński, Jerzy. W pierwszej lidze dostawców, "Lotnictwo Aviation International" Nr. 9/2017, p. 34-37 (in Polish) The Ash-62 was also produced in China. It is estimated that 40,361 were produced in the USSR.

Polish-built ASz-62IR engines (Polish transcription of Russian name), by WSK "PZL-Kalisz" in Kalisz, are compatible with FAR-33 requirements. Further developments in Poland are the K9-AA, K9-BA and K9-BB engines, with take-off power of 1178 hp (860 kW), indicated power 698 kW. From 2015 the ASz-62IR-16E was produced with electronic fuel injection, offering greater power and the possibility of running on commercial automotive fuel.

The M-63 was an improved version of the M-62 with the power output increased to 821 kW (1,100 hp) at 2,300 rpm for takeoff and 671 kW (900 hp) at 2,200 rpm at {{convert|4500|m|ft|abbr=on}} due to a higher compression ratio of 7.2:1 and a higher redline.

Applications

Specifications (M-62)

File:Shvetsov.jpg

{{pistonspecs

|

|ref=Liss.Liss 1966, p. 9

|type=Nine-cylinder single-row supercharged air-cooled radial engine

|bore={{cvt|155.5|mm|2}}

|stroke={{cvt|174.5|mm|2}}

|displacement={{cvt|29.876|L|cuin}}

|length={{cvt|1213|mm|2}}

|diameter={{cvt|1378|mm|2}}

|width=

|height=

|weight={{cvt|560|kg}}

|valvetrain=Overhead valves

|supercharger=Two-speed centrifugal type supercharger

|turbocharger=

|fuelsystem=Carburetor

|fueltype=92 RON, 87 (R+M)/2 (AKI) octane rating gasoline

|oilsystem=

|coolingsystem=Air-cooled

|power=

  • 746 kW (1,000 hp) at 2,200 rpm for takeoff
  • 634 kW (850 hp) at 2,100 rpm at 4,200 m (13,780 ft)

|specpower=25.03 kW/L (0.55 hp/in3)

|compression=6.4:1

|fuelcon=

|specfuelcon=469 g/(kW•h) (0.77 lb/(hp•h))

|oilcon=

|power/weight=1.3 kW/kg (.81 hp/lb)

}}

See also

{{aircontent

|see also=

|related=

|similar engines=

|lists=

}}

References

=Notes=

{{reflist}}

=Bibliography=

{{refbegin}}

  • {{cite book |last= Gunston |first= Bill |title=World Encyclopedia of Aero Engines |year=1986 |publisher=Patrick Stephens |location= Wellingborough |pages=154 }}
  • [http://www.ctrl-c.liu.se/misc/RAM/eng_ash-62.html Russian Aviation Museum]
  • [https://web.archive.org/web/20060925012426/http://www.aeronautics.ru/archive/reference/Piston_Engines/Poland.htm Venik's Aviation]
  • {{cite book |last=Kotelnikov |first=Vladimir |title=Russian Piston Aero Engines|year=2005 |publisher=Crowood Press Ltd.|pages=119–122}}
  • {{cite book|last=Liss|first=Witold|title=The Polikarpov I-16 (Aircraft in Profile Number 122)|publisher=Profile Publications Ltd|year=1966}}

{{refend}}