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  2. Soloviev D-30 - Wikipedia

    en.wikipedia.org/wiki/Soloviev_D-30

    The D-30 engine has a two-stage compression spool, a cannular combustion chamber and a 4-stage turbine, and was the first Soviet-built engine to use cooled turbine blades. The turbine was manufactured using the newest heat-resistant material of the time, along with an exhaust nozzle with a lobe mixer.

  3. Mikulin M-17 - Wikipedia

    en.wikipedia.org/wiki/Mikulin_M-17

    The M-17 was the most powerful engine available to the Soviet aircraft industry and it was in high demand, so much that Factory No. 24 in Moscow also began to build the M-17. 165 engines were produced in 1930 at Rybinsk and Factory No. 24 had managed to build its first three engines by June 1930.

  4. Klimov M-105 - Wikipedia

    en.wikipedia.org/wiki/Klimov_M-105

    The M-105 was the first Klimov V-12 engine design to use reverse-flow cylinder heads, forcing the induction system to be placed on the outside of the cylinder banks, with the exhaust system also exiting from the outboard side, with twin sets of "siamesed" exhaust ports adjacent to each other. About 129,000 M-105 and its variants were built.

  5. Klimov - Wikipedia

    en.wikipedia.org/wiki/Klimov

    UEC-Klimov (ОДК-Климов) is a Russian manufacturer of gas turbine engines, main gearboxes and accessory drive gearboxes for transport aircraft.. Originally established as Kirill Klimov Experimental Design Bureau in Saint-Petersburg under the direction of Vladimir Yakovlevich Klimov [] (Влади́мир Я́ковлевич Кли́мов) (1892–1962), Klimov designed engines for ...

  6. Mikulin AM-34 - Wikipedia

    en.wikipedia.org/wiki/Mikulin_AM-34

    Despite these failures it began production in 1932 at Factory No. 24 in Moscow, and 64 engines had been delivered by the end of the year. 790 were built the following year, and it was exhibited in Paris as an achievement of the Soviet aviation industry. The M-34 was redesignated with Alexsander Mikulin's initials as the AM-34 on 9 August 1936 ...

  7. Vedeneyev M14P - Wikipedia

    en.wikipedia.org/wiki/Vedeneyev_M14P

    The Vedeneyev M14P is a Russian nine-cylinder, four-stroke, air-cooled, petrol-powered radial engine. Producing 360 hp (268 kW), its design dates from the 1940s (Kotelnikov 2005), and is itself a development of the Ivchenko AI-14 engine. The engine has been used extensively by the Yakovlev and Sukhoi Design Bureaus.

  8. Ivchenko AI-24 - Wikipedia

    en.wikipedia.org/wiki/Ivchenko_AI-24

    The first airplane powered by two Ivchenko AI-24 turboprops was the An-24. They drove four-bladed AV-72T constant-speed reversible propellers. [5] Early production aircraft had AI-24 engines providing 1,790 kW (2,400 shp) takeoff power each, while later production airplanes were equipped with the newer AI-24A engines.

  9. Shvetsov ASh-82 - Wikipedia

    en.wikipedia.org/wiki/Shvetsov_ASh-82

    Most of the flaws were fixed in the mid-fifties, but the production was cancelled: in those days, the priority for the Soviet Air Force were the turboprop and jet engines. [5] Dongan HS-7 A Chinese license built copy of the ASh-82FN, and the chosen engine for powering modern 21st century reproductions of the Focke-Wulf Fw 190A. [6] [7] Dongan HS-8