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The JSC Klimov (or Joint Stock Company Klimov) presently manufactures internationally certified gas turbine engines, main gearboxes and accessory drive gearboxes for transport aircraft.

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JSC Klimov

Type	Joint-stock company
Industry	Aerospace
Founded	1912; 110 years ago (1912)
Headquarters	Saint Petersburg , Russia
Products	Gas turbines, Engines, Gearboxes, Auxiliary power units
Revenue	$327 million[1] (2017)
Operating income	$9.84 million[1] (2017)
Net income	$2.91 million[1] (2017)
Total assets	$482 million[1] (2017)
Total equity	$76.6 million[1] (2017)
Parent	United Engine Corporation[2]
Website	klimov.ru

Originally established as Kirill Klimov Experimental Design Bureau in Saint-Petersburg under the direction of Vladimir Yakovlevich Klimov [ru] (Влади́мир Я́ковлевич Кли́мов) (1892–1962), Klimov designed engines for Soviet aircraft based on Renault aircraft engine designs.[3]

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,[4][5] 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.[6]

Piston engines

• M-100 – Hispano-Suiza 12Ydrs built under license
• M-103 – improved M-100
• M-105 – improved M-103; later redesignated as VK-105
• 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 – prototype developed from M-105 with improved performance at lower altitudes; cancelled due to cooling problems
• VK-107
• VK-108 – prototype version of VK-107 with 1850 hp on takeoff; never entered production
• VK-109
• VK-110
• VK-150

Gas turbine engines

• 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 variants

TV7-117S Turboprop for Aircraft

• 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 [7]
• 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 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

• GTDE-117
• VK-100
• VK-150

References

External links

Wikimedia Commons has media related to Klimov aircraft engines.

• 'Full cycle engine development' at UEC Klimov
• Klimov Aircraft APU (Auxiliary power unit)- General Information (archived copy)

На других языках

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[de] Klimow (Unternehmen)

Klimow (russisch ФГУП – Завод имени В.Я. Климова / FGUP – Sawod imeni W.Ja. Klimowa) ist ein russisches Unternehmen, das vor allem Flugtriebwerke und Gasturbinen entwickelt und produziert und ist über die United Engine Corporation Teil von Rostec.[2] Es ist nach Wladimir Jakowlewitsch Klimow benannt, der ab 1935 das Konstruktionsbüro OKB-117 leitete und wesentlich an der Entwicklung des Unternehmens beteiligt war. Sitz und einziges Werk ist Sankt Petersburg.

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- [en] Klimov

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[fr] Klimov

Klimov est le nom d'un constructeur de moteurs d'avions, au cœur du complexe militaro-industriel de la Russie. Sous la direction de Vladimir Yakovlevitch Klimov (Владимир Яковлевич Климов) (1892-1962) il a conçu des moteurs pour les avions soviétiques.

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[ru] Климов (компания)

АО «ОДК-Климов» — российское предприятие, один из ведущих разработчиков газотурбинных двигателей. Занимается разработкой, серийным производством и сервисным сопровождением газотурбинных двигателей для авиационной техники. Основано в 1914 году.

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