Soloviev D-30
The Soloviev D -30 is a Russian twin-shaft turbofan engine, which was designed by Pavel Soloviev at Awiadwigatel in Perm in the 60s.
It was at that time one of the most advanced engines in 1967 first made in a Tupolev Tu-134 Aeroflot commercially in service and further developed in different versions.
Versions
D -30
The original version of the D -30 from 1964 with 6,800 kp thrust for the short-range airliner Tupolev Tu-134 was in 1974 for follow-on versions Tu- 134A and 134B to D- 30 Series 2 (1970 ) and D -30 Series 3 (1980 ) equipped with a thrust reverser. The fan diameter was 1.050 mm, the mass of 1550-1810 kg.
D -30 -KP
The D- 30KP 1974 with 12,000 kp thrust drives the cargo plane Ilyushin Il -76. An improved version of the engine features a new and larger fan, which increases both the thrust and fuel consumption and noise emission cuts. The name for this version is D - 30KP3 Burlak; it may also older engines to be converted.
D -30 -KU
The D- 30KU Series 1 with 11,000 kp thrust from 1975 is the most produced jet engine of the Soviet Union. It is used in long-haul transport aircraft IL- 62M. These engines were more economical and had a better reverse thrust, because the fan diameter has been increased to 1,455 mm. The mass thus increased to 2985 kg.
D- 30KU -154
With the D- 30KU -154 (1986 ) with 10,500 kp thrust the Tupolev Tu- 154M was able to meet the ICAO Chapter 3 noise conditions. Due to the noise damping, the mass grew to 3126 kg.
D- 30F6
This version with afterburner is used in supersonic Mikoyan-Gurevich MiG -31 and developed a thrust of 93.2 kN and 152.1 kN with afterburner without.