Klimov
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UEC-Klimov (Script error: No such module "Lang".) 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 Template:Ill (Влади́мир Я́ковлевич Кли́мов) (1892–1962), Klimov designed engines for Soviet aircraft based on Renault aircraft engine designs.[1] It may have used the designation Aircraft Repair Factory (aviazavod, ARZ) 117 during the Soviet period.Script error: No such module "Unsubst".
History
The Klimov OKB was formed in the early 1930s to produce and improve upon the liquid-cooled Hispano-Suiza 12Y V-12 piston engine for which the USSR had acquired a license. At that time Klimov also manufactured motorcycles.
In 1946 the British government allowed Rolls-Royce to sell a number of Nene and Derwent V turbojet engines to the Soviet Union. Klimov OKB was given the task of "metrifying" the British designs, without the knowledge or permission of the West, as the VK-1 and RD-500.
Klimov United Engine Company is now located in Saint Petersburg.
It used the nationalised buildings originally erected by 1914 in the city's present-day Vyborgsky District for the joint stock Russian Renault automotive works,[2][3] adding new workshop and administrative premises on the land in Bolshoy Sampsoniyevskiy Prospect avenue near the present Kantemirovskaya Street. By 2020 the premises have been vacated for redevelopment for a housing project.[4]
Piston engines
- M-100 – Hispano-Suiza 12Ydrs built under license
- M-103 – improved M-100
- M-105 – improved M-103; redesignated as VK-105 in 1943
- M-110
- M-120 – prototype inline 18-cylinder with three M-103A blocks in an inverted Y configuration; cancelled due to engine malfunction
- During World War II, designations were changed from M (motor) to VK (the lead designer's initials)
- VK-106 (M-106 before March 1944) – prototype developed from M-105 with improved performance at lower altitudes; cancelled due to cooling problems
- VK-107 (M-107 before March 1944) - development of M-105 and VK-106 with four valves per cylinder and more power
- VK-108 – prototype version of VK-107 with 1850 hp on takeoff; never entered production
- VK-109 - 1945-1946 development of the VK-108 with water injection, intended for the Myasishchev VB-109
- VK-110 - based on VK-109, 2100 hp; only a project
- VK-150 - inline 24-cylinder concept, 3700 hp
Gas turbine engines
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- RD-10 (along AI Ivchenko Progress (Motor Sich), KMPO & SNTK Kuznetsov (OAO Motorostroitel), elsewhere)
- RD-33 and variants, derivatives: RD-5000B for UCAV UAV like MiG Skat
- RD-93MA is a derivative of the RD-33 and is specifically designed for single engine light fighter jets. It uses the BARK-93MA automatic control system
- Klimov VK-10M 22 to 24,200 lbf (97.87 - 107.647 kN)
- RD-35, agreement with Slovakian PSLM ZVL
- RD-45
- GTD-350
- RD-500, copy of the Rolls-Royce Derwent V
- TV2-117 (built by Isotov from 1959–1964)
- TV3-117 variants
- TV3-117VM VMA for Mil and Kamov helicopters
- TV3-117VMA-SBM1 Turboprop for the An-140, MiG-110, Be-32K
- ТV7-117 TV7-117ST-01 TV7-117ST-02 Gas turbines
- TV7-117S Turboprop for Aircraft
- TV7-117K naval variant
- Klimov TV and VK derived Turboprop and Turbofan engines powerplants
- Klimov TV17-117 new perspective engine, follow up of the TV family
- VK-1
- VK-3 turbojet [5]
- VK- (and TV-) turbojets turbofan, gas turbines, turboprop turboshafts
- VK-13 turbojet turbofan
- TR3-117 turbojet for UAV Tu-143
- VK-800, VK800V also at Motor Sich
- VK-1500 variant or derivative of TV3-117 engine
- VK-2500 VK-2500PS-03 enhancement of TV3-117
- VK-650V 400 5 - 750 hp turboshaft for Ka-226 . VK-1600V project for Ka-62
- PDV-4000 4 5000 hp (3 3.8 MW) turboshaft, turboprop
- VK-3000 (VK300V also at OMKB OMO Baranov), VK3500 (TVa-3000) also at Motor Sich, VK-5000 and/or VK-6000 perspective
- GTU-18P GTU-14F GTU-24R GTU-28N Gas Turbines
- MBT and vehicles, wagon locomotives GTs
- GTD-1000T, GTD-1250
- GTD-1400, GTD-1500
Auxiliary power unit
References
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- ↑ History of UEC Klimov at klimov.ru Accessed 10 January 2018
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- ↑ web.archive.org/web/20160304142121if_/http://www.missiles.ru/_foto/Klimov_muz/IMG_7412.jpg Template:Webarchive
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External links
- 'Full cycle engine development' at UEC Klimov
- Klimov Aircraft APU (Auxiliary power unit)- General Information (archived copy)
Template:United Engine Corporation Template:Klimov aeroengines