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Before and After Photo Gallery, Dr. Kimball Crofts - Case #106 croftsmd.com | 1993-5-3-106-113 - Saudi Dental Journal sdsjournal.org | Oral EDTA Reference #106 gordonresearch.com |
The Klimov VK-106 was an experimental liquid-cooled V12 piston aircraft engine intended for Soviet aircraft during World War II.[1]
[edit] DevelopmentWith 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
Components
Performance
[edit] See alsoRelated development Comparable engines Related lists [edit] References[edit] Notes[edit] Bibliography
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