Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 15-Sep-2020

Known as the builder of the Ivchenko (sometimes Ivtchenko) radial piston engines from the great designer Aleksandr Georiyevich Ivchenko.

-His piston engines were well known and manufactured in many of the industrialized countries under Soviet influence.

-After the division of the USSR in 1989 it was renamed "Ivchenko Progress ZMKB" and finally only "Progress".

-ZMKB are the initials of “Zaporozhye Machine-Building Design Bureau” (Progress State Enterprise).

-The activity of Ivchenko began in 1916 and after the chaos of the revolution they began to build engines such as the M-11 and M-22 (Bristol Jupiter), M-85, M-86 and M-87.

-At that time, the Head of the Design Office (OKB) in Zaporozhye was A.S. Nazarov

-Later Tumanskii and Umin passed, until Ivchenko entered in 1945.

Ivchenko AI-14
“AI-14”

-He used the initials AI of A. Ivchenko and the AI-14 and AI-26 piston engines came out. They are still in production today.

-For example the AI-14 of 9 radial cylinders, with powers between 225 and 300 CV. The AI-26 with 9 cylinders too, but with nominal 575 CV, varying according to the series (the AI-26B 575 CV on the MIL-M-1, the same power as the AI-26W and AI-26GR).

AI-14, side view
“AI-14, side view”

-An AI-4V with 55 CV at 4,500 rpm, with 4 opposite horizontal cylinders, is known. This engine was built from 1948 to 1955.

-Another one was the AI-V. This was an AI-7 ramjet propulsion system at the tips of the rotor blades of an experimental helicopter.

-The AI-9 is a small turbine - auxiliary? - that we see in the photograph below.

Ivchenko AI-9
“Ivchenko AI-9”

-By 1953 he got to know the Kuznetsov TV-2 engine and developed it to the TV-2T turboprop and the TV-2K turboshaft.

-The former, in turn, continued to be developed to the TV-20 (AI-20).

Ivchenko AI-20, right side
“Ivchenko AI-20, right side”

AI-20, left side
“AI-20, left side”

-Since 1958 when it entered production, several series have been made, such as the A and the K with 4,000 shp, the M with 4192 shp, the DK with 4190 shp, the D and DM with 5180 shp and then the DME and DMU for land vehicles.

Ivchenko AI-20D
“AI-20D”

-The AI-20 turboprop is an engine with a large 10-stage axial compressor with 4 single-shaft discharge valves (by-pass for start-up, etc.), and with a large gearbox. It has a three-stage turbine and an annular combustion chamber with 10 injectors. These engines have been mounted on AN-10 and Il-18 aircraft.

Ivchenko AI-20, secciónIvchenko AI-20, cross-section
“AI-20, cross-section”

Ivchenko AI-20M
“Ivchenko AI-20M”

We obtained a cutaway drawing of the Type-K engine (possibly from the AI-20K), a successful turboprop engine in countries of Russia's orbit.

Ivchenko, tipo K
“Ivtchenko, tipo K”

-More than 15,000 AI-20 engines have been manufactured. The engines designed by the MKB (OKB) “Progress” are manufactured by Kazan Motorbuilding Plant and by Motor Sich.

-The AI-21 was used on the Yak-38.

-The AI-22 is a turbofan of 3,850 Kgf of thrust that was used on the Tu-324 and Yak-48 aircraft. It is a small fan type turbine for business or regional aircraft. It uses the core of the Lotarev DV-2.

Ivchenko AI-22
“AI-22”

-It is of recent design -relatively- with the following maximum power performance: 8,532 lbf of thrust in one of his latest evolutions.

Ivchenko AI-222
“Ivchenko AI-222”

-The current AI-222 too, is being developed (like the previous one) jointly by Ukrainian and Russian aviation engine construction companies, such as A.G. Ivchenko, ZMKB Progress, FSUE-MMPP, Salyut and Motor-Sich. With the participation of Baranov, among others.

Ivchenko AI-222-25
“AI-222-25”

-The AI-222-25 gives from 2,800 to 3,000 Kgf of thrust varying according to the -B, -F, -FK, or -28F version.

Ivchenko AI-222 variants
“AI-222 variants”

-The AI-24 is a propeller turbine designed in 1960, in fact it is a power-reduced AI-20 to equip the An-24. In its different versions the delivered power varies around 2,500 shp.

Ivchenko AI-24
“Ivchenko AI-24”

-The AI-25 is the turbofan for the small well-known Yak-25 trijet and the Czechoslovak L-39 trainer.

Ivchenko AI-25
“AI-25”

-The AI-25 gives the order of 3,300 lbf of thrust, and the -25TL version can reach 3,790 lbf.

IvchenkoAI-25, cutaway
“AI-25, cutaway”

-In the illustration above we can see this engine's cutaway with a 3-stage fan. The design is of the basic AI-25 engine from 1965.

-Today with just one fan you get the same results. It continues with a very generous bypass duct.

-The AI-30. Under this designation the TV3-117 was prepared for several airplanes. It delivered 2,800 shp. At this time it has not entered production.

Ivchenko AI-450
“AI-450”

-The AI-450 is a newly designed 550 shp turboshaft for light helicopters. This project by L. Martynenko was started in 1998, and is built together with Motor-Sich.

-A turboprop version of the AI-450CV is underway through Motor-Sich director, V. Boguslayev. It has a free turbine, a centrifugal compressor and inverted annular chamber.

Ivchenko D-18
“D-18”

Ivchenko D-18
“D-18”

-The D-18 engine was projected in 1977, and has a long historical journey on airline aircraft.

-It is still being built today, in the versions -T, -T1 and TR / TM. They have a single fan with two shafts. These engines have a reverse system for the fan as we can see in the illustration.

-It gives 51,600 lbf. thrust in the D-18-T version and increases to 57,320 in the -T1, to 55,777 lbf. in the -TM, to reach 60,627 lbf in the -TR version.

Ivchenko D-27, PropFan
“D-27, PropFan”

-The D-27 is a contra-rotating turboprop of multi-bladed propellers from Ivchenko-Progress-ZMKB.

-In fact it is an impressive looking propfan. See D-27 and D-127 that will be handled later in this chapter.

Ivchenko D-36
“D-36”

-The D-36 is a turbofan, projected in 1977 with 6,500 Kgf of thrust.

-It is the base for the D-136 turboshaft family, the D-236 propfan, the D-336 industrial engine and the D-436 turbofans.

Ivchenko D-136
“D-136”

-The turboshafts are used on helicopters such as the Mi-26 with 11,000 CV on the shaft approximately.

Ivchenko D-136
“D-136”

The D-236 contrafan had the same power and flew for the first time in 1987. Below we see it installed on a Yak-42.

Ivchenko
“D-236”

-The contrafan that drives the above mentioned D-27 turboprop, although it seems derived from the D-236, it is larger because it delivers 14,000 shp.

Ivchenko D-27 cross-sectionD-627
“D-27 cross-section”

-The spectacular propellers are of Aerosila's Stupino brand. This is model SV-36 with 8 front blades and 6 rear ones.

Ivchenko D-27
“D-27”

-For the D-27, the Stupino SV-27 model propellers are contra-rotating as we have seen above. The front propeller has eight blades, while the rear one only has six. All blades are made of composite.

-The D-127 is the turboshaft version for helicopters in a modernization and performance-increase plan, with 14,350 CV to the shaft, they can lift heavy weights, as on the Mi-26M.

-They have a modular design and are equipped with a FADEC control system.

Ivchenko D-127
“D-127”

-The D-627 is a high-bypass turbofan, with reverse thrust. It is based on the D-27 and delivers 26,000 lbf of thrust. Possibly for the Yak-46.

-From aviation engines, the Ivchenko Office has developed industrial engines.

Ivchenko industrial engine
“Ivchenko industrial engine”

-Industrial turbine with shaft power output for driving large generators, pumps, etc.

Another Ivchenko industrial engine
“Another Ivchenko industrial engine”

From Appendix 6: The AI-22 is a 3,820 Kgf turbofan designed and evolved by Ivchenko Progress and built by Motor Sich, both in Zaporozhye.

Ivchenko AI-22
“Ivchenko AI-22”

-The AI-25 have evolved from the basic engine to the AI-25W and the AI-25T, -TL, -TL2 and -TLK.

Ivchenko AI-25
“Ivchenko AI-25”

Ivchenko AI-25TL
“Ivchenko AI-25TL”

-The Ivchenko AI-25 is not a large engine because the maximum diameter is 510 mm. Therefore it is an engine for training aircraft such as the L-39.

Real look of the Ivchenko AI-25TL
“Real look of the Ivchenko AI-25TL”

-We have got a better view of Ivchenko's APU engine, the AI-9, used as starter for the TW3-117 on the Mi-14 and Mi-24 helicopters. And for the TW2-117 on the Mi-8.

Ivchenko AI-9
“The AI-9”

-The AI-9V version is a gas generator. The AI-9B gives 16 Kilowatts of electrical power output.

-The AI-26 engine does not appear in the main text. Now we have pictures of the AI-26V, that was installed on the Mi-1 helicopter. These two photographs have been taken at the Stolnok AirMuseum.

Ivchenko AI-26V
“AI-26V” (AEHS)

Another view of thel AI-26V
“Another view of the same engine” (AEHS)

-As we can see, it has a generous fan, necessary while the helicopter is in hover, so it does not advance and requires forced cooling air.

-It is visible that a rotating shaft for the main rotor sticks out from the gearbox.

-And from the Budapest Museum of Technology another very colorful photograph of the AI-20M, a large turboprop of 4,250 shp that was (and is) installed on the IL-18.

Ivchenko AI-20M
“AI-20M” (photo AEHS)

From Appendix 9: There are more AI-450 versions. Precisely at the German Aero-13 Show, the DA-50 aircraft was shown with two propulsion systems, one with the Austro AE-440 V8 piston engine, and the other with an Ivchenko AI-450-S conversion.

AI-450-MC turboshaft
“AI-450-MC turboshaft”

-Both AI-450-S and S-2 versions are aimed at propeller planes. This in addition to the -TP.

AI-450-S turboprop
“AI-450-S turboprop”

Installed on Diamond D-50, with 5-blade propeller
“Installed on Diamond D-50, with 5-blade propeller”

Ivchenko AI-450-BP and -BP-2 turbofans
“AI-450-BP and -BP-2 turbofans”

-All AI-450 engines have the same "Core" with the same centrifugal compressor and the same combustor.

Engines of IVCHENKO

Model: AI-10

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

Other details:
Model: AI-14

Arquitecture: 9-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 300 CV
Weight:

Other details:
Ivchenco AI-14

"Ivchenco AI-14"

Model: AI-20, -A, -K, -M, -DK, -D, DM, -DME, DMU

Arquitecture: Turboprop
Compressor/s: 10-stage axial compressor
Combustion chambers: Annular combustion chamber with 10 injectors
Turbines: 3-stage turbine
Power / Thrust:
Weight:

Other details:

Thrust for the different versions:
A and K: 4000 CV,
M: 4192 CV
DK: 4190 CV
D and DM: 5180 CV

Ivchenko AI-20, left side view

"Ivchenko AI-20, left side view"

Model: AI-21

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

Other details:
Model: AI-22

Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 3850 Kgf
Weight:

Other details:
Ivchenco AI-22

"Ivchenco AI-22"

Model: AI-222, l25

Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 3000 Kgf
Weight:

Other details:
Ivchenko AI-222-25

"Ivchenko AI-222-25"

Model: AI-24

Arquitecture: Turboprop
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: 2500SHP / ---
Weight:

Other details:
Ivchenko AI-24

"Ivchenko AI-24"

Model: AI-25, TL, TLSh

Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 3300 Lbf
Weight:

Other details:

The -25TL version can reach 3,790 lbf.

Ivchenko AI-25TL real look

"Ivchenko AI-25TL real look"

Model: AI-26

Arquitecture: 9-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 575 CV
Weight:

Other details:
Ivchenko AI-26V, fig.2

"Ivchenko AI-26V, fig.2"

Model: AI-30 (TV3-117, -VMA,)

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

Other details:
Model: AI-4, -4V

Arquitecture: 4-cylinder Horizontally opposed
Cooling:
Total Displacement:
Bore / Stroke:
Power: 55 HP @ 4500 rpm
Weight:

Other details:
Model: AI-450, M,

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

Other details:
Ivchenco AI-450MC turboshaft

"Ivchenco AI-450MC turboshaft"

Model: AI-450-BP, BP-2 (turbofan)

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

Other details:
Ivchenko turbofan AI-450-BP and -BP-2

"Ivchenko turbofan AI-450-BP and -BP-2"

Model: AI-450-S (turboprop)

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

Other details:
Ivchenco AI-450S turboprop

"Ivchenco AI-450S turboprop"

Model: AI-5

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

Other details:
Model: AI-7

Arquitecture: Ramjet
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:

Other details:
Model: AI-8

Model: AI-9, 9V, -3B

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

Other details:
Ivchenko AI-9, fig. 2

"Ivchenko AI-9, fig. 2"

Model: D-127

Arquitecture: Turboshaft
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: 14350SHP /
Weight:

Other details:
Ivchenco D-127, sección

"Ivchenco D-127, sección"

Model: D-136

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

Other details:
Ivchenco D-136

"Ivchenco D-136"

Model: D-18, -T, -TM, -TR

Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 51600 Lbf
Weight:

Other details:

D-18-T: 51600 lbf
D-18-T1: 57320 lbf
D-18-TM: 57777 lbf
D-18-TR: 60627 lbf

Ivchenco D-18

"Ivchenco D-18"

Model: D-236

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

Other details:
Ivchenco D-236

"Ivchenco D-236"

Model: D-27

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

Other details:
Ivchenco D-27

"Ivchenco D-27"

Model: D-36-1, 1A, 2A, 3A, 4A

Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 6500 Kgf
Weight:

Other details:
Ivchenco D-36

"Ivchenco D-36"

Model: D-627

Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 26000 Lbf
Weight:

Other details:
Model: D.436, T1, T2, T3, TP, -148

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

Other details:
Model: TV-2T, -2K

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