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VK-106
Type V12 inline engine
Manufacturer Klimov
First run 1943
Number built Prototypes only
Developed from Klimov M-105

The Klimov VK-106 was an experimental liquid-cooled V12 piston aircraft engine intended for Soviet aircraft during World War II.[1]

Contents

[edit] Development

With the VK-105PF2 exhausting the potential of the M-105, Klimov designed a new VK-106 engine in 1943. Since air combat on the Eastern Front took place primarily at medium altitudes (under 4,000 m {13,000 ft}), the new engine was built specifically for peak performance at those altitudes with a reduced compression ratio and a single-speed supercharger. Although reliable and easily installed in M-105-powered aircraft, VK-106 did not enter production because it differed from M-105 enough to require new tooling, and Soviet engine factories at the time lacked the capacity to produce another design. Like M-105P, VK-106P could house an autocannon in the "vee" between the cylinder banks.

[edit] Specifications (VK-106-1sk)

Data from Kotelnikov[2]

General characteristics

  • Type: 12-cylinder supercharged liquid-cooled piston aircraft engine
  • Bore: 148mm (5.83 in)
  • Stroke: 170mm (6.69 in)
  • Displacement: 35.08 liters (2,140 in³)
  • Dry weight: 600 kg (1,320 lb)

Components

Performance

[edit] See also

Related development

Comparable engines

Related lists

[edit] References

[edit] Notes

  1. ^ Gunston 1989, p. 90.
  2. ^ Kotelnikov 2005, p. 142.

[edit] Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Kotelnikov, Vladimir. Russian Piston Aero Engines. Marlborough, Wiltshire. The Crowood Press Ltd. 2005. ISBN 1 86126 702 9.



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