Search results
Results from the WOW.Com Content Network
UEC-Aviadvigatel JSC (Russian: АО "ОДК-Авиадвигатель", lit. Aeroengine) is a Russian developer and builder of aircraft engines, most notably jet engines for commercial aircraft. Based at the Perm Engine Plant, its products power the Ilyushin Il-76MF, Ilyushin Il-96, Tupolev Tu-204, and Tupolev Tu-214.
Pages in category "Soviet and Russian aircraft engines" The following 8 pages are in this category, out of 8 total. This list may not reflect recent changes. C.
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.
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 ...
TV7-117S 2800 hp; TV7-117SM/ST (the S stands for the Russian word for aircraft, the M for airliner, as opposed to military cargo aircraft, which are designated ST, with the T being for transport) is the turboprop variant for fixed wing aircraft, that was introduced by Klimov in 2002, featuring a Full Authority Digital Electric Control system based on the BARK-12 or BARK-57 electronic engine ...
It has produced turbojet and turboprop engines for military and civil use, including Blackjack and Backfire bombers and Tu-154 transports. The NK-12M engine produced by Frunze is the most powerful turboprop in the world. Samara Frunze also produced engines for the Salyut spacecraft and for the Mir space station. [3]
Baseline model developed in 1976 to power the MiG-29. Development work started in 1968 at the Klimov Design Bureau, led by Sergey Isotov. The first few engines for the 9.01 MiG-29 prototype were equipped with a longer nozzle, without the double wall design, which is featured on the current RD-33 [3] [4] and RD-33MK models.
A new engine, this time a low-bypass turbofan, was needed to power the new interceptor. The Mikoyan-Gurevich (MiG) design bureau contracted OKB-19 design bureau (now part of Aviadvigatel) to build such an engine, for the aircraft that would become known as the MiG-31. The Soloviev design bureau came up with the D-30F6 turbofan.