History.

 

Sh-82, Sh-82V aircraft motors are produced by the Omsk Engine-Building Enterprise named after P.I.Baranov, developed by Perm Design Bureau (EDB-19). On the Omsk Engine-Building  Enterprise named after P.I.Baranov the brunch of Experimental-Design Bureau-19 (EDB-19) was established for improvement of Sh-82 and Sh-82V motors. Valentin Andreyevich Glushenkov became the head of the brunch. The collective of branch performed a technical control of serial production of Sh-82 and Sh-82V motors at the Omsk Engine-Building Enterprise named after P.I.Baranov, improving their reliability and service life.

 

1956 year

On the basis of Experimental-Design Bureau-19 by the Order of the Ministry of Aircraft Industry No. 544 dd. 15.10.56 the State Union Experimental-Design Bureau-29 (EDB-29) was established. It continued the development of ASh-82T and Sh-82V piston engines and the development of small-size gas turbine engines. Two ASh-82T engines were installed on the IL14 airplane, and the ASh-82V engine was installed on the Mi-4 helicopter. Both aircrafts were one of the best in their class. During a serial production of the engines their warranty service life was increased up to 1500 hours for Ash-82T and 1200 hours for Ash-82V by the efforts of the EDB personnel.

The first joint development with the Central Institute of Aircraft Engine Production (CIAEP) was the 300-hp GTD-1 gas turbine engine. This work has allowed to the Omsk Engine Design Bureau (OEDB) specialists to receive necessary experience in gas turbine engine production.

1958 year

The first 100-hour lengthy tests of the GTD-1 engine are successfully conducted. The GTD-1 was supposed to be used as power unit.

1960 year

The first test of the GTD-3. A first flight of the KA-25 helicopter of marine basing with the GTD-3. Development of engine and reduction gearbox began in the OEDB since November 1957. Original developments, unknown in a domestic air engine building, such as axial-centrifugal compressor, are introduced into an engine design. After realization of the first flight tests there was found out necessity of engine boosting up to power of 900 hp. A success became the development in 1964 of the GTD-3F power plant for the Ka-25 deck helicopter, consisting of two 900-hp GTD-3M and the RV-3M power reduction gearbox of main rotors. These engines were produced serially more than 20 years on Omsk Engine Production Association named after P.I. Baranov.

Operations of helicopters in marine conditions have indicated the increased corrosion of compressor blades. By efforts of the EDB specialists the given problem has been decided by introduction of blades manufactured of titanium alloy. In 1973 series production of the 1100-hp GTD-3M engines is started. The warranty service life of engines is developed up to 500 h. Serially the engine was manufactured till 1985. The Ka-25 antisubmarine helicopters had been equipped the Moscow antisubmarine cruiser.

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1963 year

Tests of the Object 167һ tank with the GTD-3TU engine.

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1967 year

Production Association named after P.I. Baranov has started series production of the GTD-5M engine. On the basis of experience received by the GTD-1 development, the OEDB specialists have started development of the GTD-5 (GTD-40) new gas turbine engine of the small power made under the single-shaft scheme and intended for the drive of the 20-kW S-20 radio-frequency generator on a 2P24 product. In the following for the 40-kW S-40 generator drive on the Cube 2P25 product the development of the GTD-5M engine realized. Activities on operational development of the engine proceeded till 80th years. In 1980 to the engine the warranty service life of 2250 h has been established and the specified life - 3250 h. Series production of engines proceeded till 1991.

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1968 year

Under the Ministry offer the OEDB design department has started development of the TVD-10M engine for SKAT marine motorboats. In the beginning of 1970 the preliminary design of the TVD-10M engine has been developed. The engine of next generation in the same power category became the 940-hp TVD-10 turboprop engine developed in 1970 for the Be-30 airplane for local airlines.

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Laid at development of the TVD-10 engine the high technological level of design solutions made it possible to produce a number of its modifications: VD-10 - for air cushion vehicles; TVD-10B - for the An-28 airplane operated on local airlines; TVD-20 - for the An-3 single-engined agricultural aircraft, and also modification of this engine for the n-38 airplane. The VSU-10 auxiliary power plant - for IL-86 and IL-96-300 airbuses.

1971 year

In 1971 the State Commission has signed Act about successful realization of lengthy tests of the TVD-10M engine. The series manufacturing and overhaul of the TVD-10M engines was made by the OEDB. Engines of our manufacture were successfully maintained a long time on cross-country boats of the Navy.

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1974 year

Under joint Decision of Ministry of Aviation Industry (MAI) - Ministry of Civil Aviation (MCA) modernization of the An-2 series airplane in the An-3 has been made by replacement of the ASh-62IR reciprocating engine on the TVD-20 turboprop engine. In 1975 under the Contract with Aeronautical Scientific and Technical Complex named after O.K. Antonov, activities on development of the TVD-10B engine for the n-28 airplane for local airlines are started.

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1976 year

The OEDB was entrusted with the development of an auxiliary power plant for the IL-86 airbus.

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Design departments per 1977-1978 release design documentation on the VSU-10 engine.

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The auxiliary power plant is a derivative of the TVD-20 engine. There are manufactured units and mounted test rigs for tests of air by-pass mechanism and end seals. Manufacturing of prime equipment and experimental units of the engine is started. In December, 1980 the VSU-10 engine underwent state official tests, but in 1981 there were still conducted capacious verifying and lengthy tests on four rigs in the OEDB and OEPA named after P.I. Baranov in maintenance of State official tests of the engine. By results of the large done work in January, 1982 the Act by results of the State 300-hour rig tests of the VSU-10 auxiliary gas-turbine engine intended for an engine start-up and a supply of airborne systems by the electric power and compressed air on the IL-86 airplane has been authorized.

1979 year

The An-28 airplane with the TVD-10B engines took part in Paris Air Show.

1992 year

In the OEDB the overhaul of the TVD-10B engines is made and proceeds on the present time.

1994 year

Works on the TVD-10B engine application on the Gratch single-engined airplane developed by "MiG" are carried out. For this time the OEDB has produced and put to the Customer six engines.

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1997-1998 years

The OEDB specialists have executed great volume of works on re-equipment of the n-2 first airplane in n-3.

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The OEDB has transmitted to the Production association "Polyot" a power plant of the n-3 airplane for use of units of this installation (engine mount, aircraft air intake, oil system, etc.) to the equipment of the first airplane. The action mockup of the TVD-20 engine is put for fulfilment of adjustment and test of systems on operating engine.

There are developed the TVD-20 engine modifications for application::

- TVD-20-01 - An-3T transport airplane;

- TVD-20-01B - n-3 airplane in agricultural version;

- TVD-20-03B - n-38-200 cargo-passenger carrying airplane.

The Type certificate S 177-D with Additions S 177-D/D-01; /D-02; /D-03; /D-04; /D-05 is made out for above-stated engine modifications. Works on development of the TVD-20-01B engine modifications connected to the installation of the BUK-203 electronic unit on the n-3 airplane are carried out. The design department executes great volume of works on issue and transfer on the Omsk Engine Production Association named after P.I. Baranov of the repair documentation on the TVD-20 engine.

One of the OEDB achievements is development of the TV-O-100 turboshaft engine for the Ka-126 helicopter and the unified pendant vehicle of refueling for air fuel trailers.

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The OEDB has worked on developing of the VGTD-43 auxiliary gas-turbine engine of a new generation with parameters at a level of the best foreign analogs.

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The VGTD-43 is intended for installation on the Tu-204-type medium-haul airplanes.

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The design bureau personnel has a experience in designing of ground gas-turbine units, turbine starters and air turbines.

The OEDB specialists are engaged also in developing of instruments, installations, devices for improving of production and experimental bases, various test rigs and integrated systems, in particular, induction brakes with consumed power up to 1000 hp.

At present the OEDB is a leading authority on development of small-size turbine engines. The designing, laboratory, production and test bases of the OEDB provide for the required technical level of the products at all stages from project work till certification, manufacturing and repair.