Klimov GTD-350

GTD-350
TypeTurboshaft
ManufacturerKlimov
First run1963
Major applicationsMil Mi-2
Number built> 11,000
Compressor of GTD-350 engine

The Klimov GTD-350 (initially Isotov GTD-350) is a Soviet gas-turbine turboshaft engine intended for helicopter use. Designed in the early 1960s by the Isotov Design Bureau the engine was later produced by Klimov and PZL, production ending in the late 1990s.

The GTD-350 powers the Mil Mi-2, the first Soviet gas-turbine powered helicopter, and has accumulated over 20 million hours in service.

Applications

Specifications (GTD-350)

Data from Klimov, World Encyclopaedia of Aero Engines, Aircraft engines of the World 1970

General characteristics

Components

Performance

Take-off: 300 kW (400 shp) at 45,000 rpm (gas generator)
Normal: 240 kW (320 shp) at 40,000 rpm (gas generator)

See also

Comparable engines

Related lists

References

  1. 1 2 3 "GTD-350". klimov.ru. moscow. 2013. Archived from the original on 7 March 2013. Retrieved 23 March 2019.
  2. ↑ Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 81. ISBN 978-1-85260-163-8.
  3. ↑ Wilkinson, Paul H. (1970). Aircraft engines of the World 1970 (21st ed.). Washington D.C.: Paul H. Wilkinson. p. 215.