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.
“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”
-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”
-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”
“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.
“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.
“AI-20, cross-section”
“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.
“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.
“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”
-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.
“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.
“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”
-The AI-25 is the turbofan for the small well-known Yak-25 trijet and the Czechoslovak L-39 trainer.
“AI-25”
-The AI-25 gives the order of 3,300 lbf of thrust, and the -25TL version can reach 3,790 lbf.
“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.
“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.
“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.
“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.
“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.
“D-136”
-The turboshafts are used on helicopters such as the Mi-26 with 11,000 CV on the shaft approximately.
“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.
“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.
D-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.
“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.
“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”
-Industrial turbine with shaft power output for driving large generators, pumps, etc.
“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”
-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-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”
-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.
“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.
“AI-26V” (AEHS)
“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.
“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”
-Both AI-450-S and S-2 versions are aimed at propeller planes. This in addition to the -TP.
“AI-450-S turboprop”
“Installed on Diamond D-50, with 5-blade propeller”
“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:
Model: AI-14
Arquitecture: 9-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 300 CV
Weight:
"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:
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"
Model: AI-21
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: AI-22
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 3850 Kgf
Weight:
"Ivchenco AI-22"
Model: AI-222, l25
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 3000 Kgf
Weight:
"Ivchenko AI-222-25"
Model: AI-24
Arquitecture: Turboprop
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: 2500SHP / ---
Weight:
"Ivchenko AI-24"
Model: AI-25, TL, TLSh
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 3300 Lbf
Weight:
The -25TL version can reach 3,790 lbf.
"Ivchenko AI-25TL real look"
Model: AI-26
Arquitecture: 9-cylinder Radial
Cooling:
Total Displacement:
Bore / Stroke:
Power: 575 CV
Weight:
"Ivchenko AI-26V, fig.2"
Model: AI-30 (TV3-117, -VMA,)
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: AI-4, -4V
Arquitecture: 4-cylinder Horizontally opposed
Cooling:
Total Displacement:
Bore / Stroke:
Power: 55 HP @ 4500 rpm
Weight:
Model: AI-450, M,
Arquitecture: Turboshaft
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"Ivchenco AI-450MC turboshaft"
Model: AI-450-BP, BP-2 (turbofan)
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"Ivchenko turbofan AI-450-BP and -BP-2"
Model: AI-450-S (turboprop)
Arquitecture: Turboprop
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"Ivchenco AI-450S turboprop"
Model: AI-5
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: AI-7
Arquitecture: Ramjet
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: AI-8
Model: AI-9, 9V, -3B
Arquitecture: Gas turbine
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"Ivchenko AI-9, fig. 2"
Model: D-127
Arquitecture: Turboshaft
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: 14350SHP /
Weight:
"Ivchenco D-127, sección"
Model: D-136
Arquitecture: Turboshaft
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"Ivchenco D-136"
Model: D-18, -T, -TM, -TR
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 51600 Lbf
Weight:
D-18-T: 51600 lbf
D-18-T1: 57320 lbf
D-18-TM: 57777 lbf
D-18-TR: 60627 lbf
"Ivchenco D-18"
Model: D-236
Arquitecture: PropFan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"Ivchenco D-236"
Model: D-27
Arquitecture: Turboprop
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
"Ivchenco D-27"
Model: D-36-1, 1A, 2A, 3A, 4A
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 6500 Kgf
Weight:
"Ivchenco D-36"
Model: D-627
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: --- / 26000 Lbf
Weight:
Model: D.436, T1, T2, T3, TP, -148
Arquitecture: Turbofan
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust:
Weight:
Model: TV-2T, -2K
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight: