Updated: 23-Apr-2021
See AO-Aviadvigatel / PNPP / Soloviev.
They have a manufacturing plant in the city of Perm.
-It has the old design office founded by Shvetsov after WWII, where radial engines were designed and built.
-It was known as Perm Motor Group between 1934 and 1935 and there is information that it already manufactured the M-25 and various types of gearboxes.
-See also Shvetsov to learn the range of engines of this designer.
-In 1953 Soloviev came to direct it. From this new period, the TV-2M (GTV-2) turbines were designed and manufactured in Perm, as well as the GTU and GTV-5P, 4P, 6P, 12 and 16.
-PS-12 and GTE series. In 1959 the D-25 and the RD-214 rocket engine for the Kosmos rockets were made.
-In 1960 the D-20 comes out. Four years later, there is the Proton's RD-253 rocket engine.
-The D-30 turbofan is from 1965 although some were built in Rybinsk. The D-100 is also from Perm.
-The D-34F6 for the MiG-31M had a bypass with afterburner, and was made in Perm in 1979.
-The RD-275 rocket engine is from 1987. In 1992 the PS-90A was made, and later the D-200, etc.
-As stated in Aviadvigatel, the current PERM was formed in 1989 (after the division of the USSR) not as OKB but as “Joint Stock Company”.
-The PS-90 is of the 160 kN category, they have been seen in the IL-96-300, the TU-204 and as replacement on the IL-86. The upgraded version is the PS-90A.
“PS-90”
From Appendix 9: This company builds turbofans designed by Pavel Soloviev (PS).
“ PS-90-A y A1 engine”
“PS-90-A2 cutaway”
-The D-30 is similar to the PS-90.
“PS-90-A76”
From Appendix 12: It is the current Aviadvigatel, from Perm. Lately the 5th generation turbofan engine, the PD-14, has come out.
-It is an engine derived from the PD-7 (PD-18). It has about 16 proposals from the Moscow TsIAM institute.
-It was initially intended for the IL-76LL and later for the MC-21.
“El nuevo PD-14”
-They are the new generation that will replace previous engines. Another example is the PD-10V Gas Generator for the large Mi-26 helicopter that will replace the old D-136 engines.
Engines of PERM
Model: D-100
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: D-14 (y PD-7, PD-18, PD-10V)
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: D-20
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: D-200
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: D-25
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: D-30
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: D-34F6
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: GTE series
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: GTU series
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: GTV-5P, -4P, -6P, 12 y 16
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: M-25 (Shvetsov)
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: PS-12
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: PS-90A, -A1, -A2, -A76
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
Model: RD-214
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: RD-253
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: RD-275
Arquitecture:
Chambers:
Fuels:
Feed System:
Ignition:
Thrust:
Weight:
Model: TV-2M (GTV-2)
Arquitecture:
Compressor/s:
Combustion chambers:
Turbines:
Power / Thrust: / ---
Weight:
