Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 13-Jun-2022

In 1946, Russian designer Vladimir A. Dobrynin made a 2,200 CV engine known as the VD-251 that was liquid cooled and had twelve cylinders in V.

-Being in the OKB Mikulin, he participated in the M-250 design together with Skuba Chevskyi. It was a radial with 6 blocks of four cylinders, 24 in total.

Dobrynin M-250
"Dobrynin M-250"

-Dobrynin developed the M-250 engine continuing with the VD-3 from 1945 derived from the M-250.

-The VD-3TK reached 3,500 CV. It was known as the M-251TK, and had 24 cylinders with turbochargers.

-VD-4 was a logical development from the VD-3TK, with
the VD-4TK (M-253K) reaching at 4,500 CV.

-Curiously it is claimed that the M-250's specific consumption was 165 grams x CV x Hr., When by the time, even decades later the "standard" consumption was 250 gr. x CV x Hr.

-We see the installation on board an aircraft, with turbocharger and its distribution.

Dobrynin, Grupo motopropulsor M-250
"M-250 Power train"

-The Dobrynin design office passed to Koliesov in 1955. Shortly before this fact he designed the VD-7, a powerful engine of almost 25,000 lbs. of thrust.

-There were other variants (-B, -F, -M, -P and M-2). With afterburner the power went to 36,000 lbs.

-VD-5 and VD-9 are also Dobrynin engines.

DV-7 (VD-7)
"DV-7”(VD-7)

From Appendix 9: Designer V. Drobynin's Technical Office (OKB-36) was little known but inspired high-performance engines with great powers.

-The VD-3 was also the M-250. As the VD-3TK was the M-251TK (TK is for the turbocharger).

Dobrynin VD-4K (M-253K)
"VD-4K (M-253K)"

-The VD-4K is a complex and powerful engine, from 3,800 to 4,300 CV. It has six radially arranged blocks of 4 cylinders each. It is a Compound engine whose turbines, driven by the exhaust, add their power to the central shaft of the engine.

Dobrynin, Schematic diagram with turbocharger
"Schematic diagram with turbocharger"

-The turbocharger is superimposed on top behind the main engine.

-The turbines between each two cylinder blocks are the "Compounds".

-The VD-5 was mounted on the Myasischev M-4. Without more information.

-The VD-5 was a turbine, but the most common Dobrynin turbine engine was the VD-7 and its variants such as the VD-7-BA (RD-7M2). Or the VD-9 on the Tu-106.

Dobrynin VD-7B
"Dobrynin VD-7B"

Ten Dobrynin VD-7 engines on an Ekranoplane
"Ten VD-7 engines on an Ekranoplane"

-The MB-100 was a horizontal-X piston engine, built by coupling two M-103s. It was a Dobrynin design and the engine gave 2,400 CV.

Engines of DOBRYNIN

Model: M-103

Arquitecture:
Cooling:
Total Displacement:
Bore / Stroke: x
Power: @ rpm
Weight:

Other details:
Model: M-250 (VD-3)

Arquitecture: 24-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power:
Weight:

Other details:
Dobrynin M-250

"Dobrynin M-250"

Model: M-251TK (VD-3Tk)

Arquitecture: 24-cylinder
Cooling:
Total Displacement:
Bore / Stroke:
Power: 3500 CV
Weight:

Other details:

With turbocharger.

Model: M-253K (VD-4TK)

Arquitecture: 24-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 4500 CV
Weight:

Other details:

It has six radially arranged blocks of 4 cylinders each. Compound engine

Dobrynin VD-4K (M-253K)

"Dobrynin VD-4K (M-253K)"

Model: MB-100

Arquitecture: X-engine
Cooling:
Total Displacement:
Bore / Stroke:
Power: 2400 CV @ rpm
Weight:

Other details:
Model: VD-251

Arquitecture: 12-cylinder V-Engine
Cooling:
Total Displacement:
Bore / Stroke:
Power: 2200 CV
Weight:

Other details:
Model: VD-5

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:

Other details:
Model: VD-7 (Koliesov)

Arquitecture: Turbojet
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 25000 Lbf
Weight:

Other details:

With afterburner the power went to 36,000 lbs.

Dobrynin VD-7B

"Dobrynin VD-7B"

Model: VD-9

Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:

Other details:

The author of this edition of Aeroengines AtoZ, through Aeroteca, collaborated on Version 2 of this video, which is presented here.

To understand the operation of the connecting rods, the 1929 Continental R 670 single-cylinder engine was chosen.

A demonstration of Version 3, improved at the author's suggestion, is also available on YouTube at a later date. This version shows bronze valve guides, improved valve spring movement, and the split crankshaft counterweights and front bearing balls also move.

The design is from Juan Soler, Sant Cugat, Barcelona

Below we show a flash of version 3

Counting also with the coloboration of JMC of Enginys Mecanics in Mataro, Barcelona