Omsk Engine Design Bureau

Omsk Engine Design Bureau is a Russian aerospace-engine design organization associated with the development of engines and auxiliary power systems for military and civilian applications. Its institutional history began in Moscow during the Soviet period. In 1941, during the Second World War, the bureau was evacuated from Moscow and relocated to a site described in reference material as a farm-machinery facility. The wartime move formed part of the broader Soviet relocation of industrial and engineering capabilities away from threatened western areas. After the war, the organization returned to Moscow and became independent on 5 July 1947. At that point it received the designation OKB-20. The bureau subsequently expanded its technical responsibilities and in 1963 absorbed OKB-29. In 1966 it was renamed Mashinostroitel'noe KB, commonly abbreviated MKB. Since 1994, the organization has been known as Omskoe mashinostroitel'noe KB, or OMKB, the name reflected in the English rendering Omsk Engine Design Bureau. The bureau's work has covered several propulsion categories, including turboshafts, turbojets, turboprops, turbofans, gas turbines and auxiliary power units. Reference material associates the organization with the Glushenkov name because many engines are identified with V. A. Glushenkov, a designer who became prominent at the bureau from 1963. The portfolio also includes reduction gearboxes, gears and other engine-related systems. Listed engine families and projects include the 36MT, also designated TRDD-50, the R95, the 37 series of small turbofans for missile and unmanned-aircraft applications, the TRDD-50B or 37-04, and the TVD-10 and TVD-20 turboprops. Other associated or supported designs include the AL-21F-3T, GTD-20/20S, various TV3-117 derivatives, and APU families such as the GTD-5 and GTD-5M. The bureau's history is connected to the wider Soviet and post-Soviet aerospace-engineering network. During the Soviet era, some engineers from OMKB and the OMO Baranov Polyot organization moved to Zaporozhye-based Ivchenko-Progress, later associated with Motor Sich, where related helicopter-engine, turboprop, turbojet, turbofan and gas-turbine production was developed. The reference account also describes how Soviet industrial decentralization and design-allocation decisions influenced the relative emphasis placed on larger aircraft engines rather than smaller turbojets, turbofans, turboprops and helicopter turboshafts. OMKB is therefore best understood as a specialist engineering institution rather than a consumer-facing brand. Its significance lies in design capability, engine families, derivative development and the continuity of Soviet-era aerospace expertise into the Russian period. Publicly available reference material does not establish a current corporate owner, a separate commercial website, financial results, listing status or a definitive present-day executive roster.

The organization that became Omsk Engine Design Bureau originated as a Soviet aircraft-engine design bureau based in Moscow. Its early institutional history was shaped by the Second World War. In 1941, the bureau was evacuated from Moscow and transferred to a facility characterized in reference material as a site of farm machinery. This relocation reflected the Soviet wartime practice of moving strategic industrial and engineering operations away from the front and into safer interior regions. Following the war, the bureau returned to Moscow. On 5 July 1947 it became an independent organization and was designated OKB-20. The OKB designation identified it as a Soviet experimental design bureau, while its subsequent name changes reflected changes in institutional structure and technical responsibilities. In 1963 it absorbed OKB-29, bringing additional engineering capability into the organization. Three years later, in 1966, it was renamed Mashinostroitel'noe KB, generally abbreviated MKB. The bureau's technical identity became associated with a number of designers and chief designers over time. Many of its engines are known by the Glushenkov name, referring to V. A. Glushenkov, who was a designer at the bureau from 1963. The naming practice illustrates how Soviet engine programs were often linked to the leading engineer or design collective rather than marketed under a single consumer-style brand. The organization worked across a broad propulsion field. Its reported activities included turboshafts, turbojets, turboprops, turbofans, gas turbines and auxiliary power units. It also designed or supported reducers, gears and other transmission-related components. The cited portfolio includes the 36MT, also known as TRDD-50, the R95, the 37-series turbofan family, the TRDD-50B or 37-04, and the TVD-10 and TVD-20 turboprops. Reference material also associates the bureau with the AL-21F-3T, the GTD-20/20S, TV3-117-related engines and several APU designs, including GTD-5 and GTD-5M. OMKB's history cannot be separated from the wider Soviet aerospace-engineering system. During the Soviet period, engineers from OMKB and the OMO Baranov Polyot organization moved to Zaporozhye, where Ivchenko-Progress developed manufacturing and design activity later linked with Motor Sich. The transferred expertise covered helicopter turboshafts, turboprops, turbojets, turbofans and gas turbines. The reference account further describes the influence of Soviet industrial decentralization, design assignments and production priorities on the development of different engine sizes and categories. In 1994 the bureau adopted the name Omskoe mashinostroitel'noe KB, abbreviated OMKB. The English name Omsk Engine Design Bureau is used to identify the organization in English-language reference material. It remains a specialist aerospace-engineering entity associated with engine design and related propulsion systems. Public references supplied for this dossier do not provide enough information to establish its current ownership, legal structure, leadership, finances, listing status or a verified official website.

• 1994

  Adopted the OMKB name

  [1]Omsk Engine Design Bureauen.wikipedia.org

  The bureau became known as Omskoe mashinostroitel'noe KB, or OMKB.

• 1966

  Renamed Mashinostroitel'noe KB

  [1]Omsk Engine Design Bureauen.wikipedia.org

  The organization adopted the name Mashinostroitel'noe KB, commonly shortened to MKB.

• 1963

  Absorption of OKB-29

  [1]Omsk Engine Design Bureauen.wikipedia.org

  The bureau absorbed OKB-29, broadening the institutional base of its engine-design activities.

• 1947

  Independence and OKB-20 designation

  [1]Omsk Engine Design Bureauen.wikipedia.org

  After returning to Moscow, the bureau became independent on 5 July 1947 and was renamed OKB-20.

• 1941

  Wartime evacuation

  [1]Omsk Engine Design Bureauen.wikipedia.org

  The bureau was evacuated from Moscow during the Second World War and relocated to a facility described as a farm-machinery site.

Specialist aerospace propulsion design bureau serving military and civilian engine programs, with capabilities spanning engine families, gas turbines, auxiliary power units and related transmission systems.

• Small turbofan engine

  36MT / TRDD-50

  The 36MT, also designated TRDD-50, is listed among the bureau's small turbofan-related engine programs. The reference material associates this family with propulsion applications in the military aerospace field.

• Turbojet engine

  R95

  The R95 is identified in the bureau's reported product and design portfolio as a turbojet engine. Publicly supplied material does not provide sufficient detail on variants, production quantities or current operational status.

• Turbofan engine

  37 series

  The 37 series is described as a turbofan family intended for missile and unmanned or remotely piloted aircraft applications. The available reference does not establish a complete variant list or detailed service history.

• Turbofan engine

  TRDD-50B / 37-04

  The TRDD-50B, also designated 37-04, is listed as a related turbofan design. The supplied material specifically connects it with the Kh-59MK2 missile program.

• Turboprop engine

  TVD-10 and TVD-20

  The TVD-10 and TVD-20 are turboprop engines included in the bureau's historical portfolio. The available sources do not provide detailed specifications, production dates or current support arrangements.

• Turbojet engine

  AL-21F-3T

  The AL-21F-3T appears in reference material among engines associated with the bureau's technical capabilities and portfolio. No further authoritative product-level information is supplied.

• Auxiliary power systems

  Auxiliary power units

  OMKB has been associated with multiple auxiliary power unit designs, including the GTD-5 and GTD-5M. These systems form part of the bureau's broader aerospace support and propulsion-engineering activities.

1. 1Omsk Engine Design Bureauen.wikipedia.org