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Lotarev DV-2

Turbofan aircraft engine


Summary

Turbofan aircraft engine

FieldValue
nameDV-2
imageLotarev DV-2 Kosice.jpg
captionDV-2 turbofan engine
engine_typeTurbofan
national_originSoviet Union/Czechoslovakia
manufacturerIvchenko-Progress/PSLM
first_run1987
major_applications
number_built124
developed_fromIvchenko AI-25

RD-35 by Klimov

The Lotarev DV-2 (or PSLM DV-2, DV: Dnepr-Váh, )MOT Site:

Design and development

Developed from the Ivchenko AI-25 turbofan engine, ZVL was also responsible for pre-production and serial engine production.

The DV-2 is a two-spool modular aviation turbofan engine with a single-stage overhung fan, two-stage LP compressor, seven-stage HP compressor, single-stage HP turbine, and two-stage LP turbine, and an annular combustion system. Maximum power at T-O is 21.58 kN with a specific fuel consumption of 60 kg/(kN h) (0.593 (lb/lbf h)), at Maximum Rating, Sea Level Static, ISA.

One of the most unusual features of this military engine is the single stage fan; most trainer and combat engines have multi-staged fans, single stage fans normally being the preserve of civil and military transport turbofans. Ivchenko Lotarev chose a very low specific thrust (net thrust/airflow) cycle for the DV-2, so a single stage fan is sufficient to develop the desired fan pressure ratio. Even so, the pressure ratio produced is somewhat higher than that normally developed by a single stage fan. Owing to the low specific thrust, the bypass ratio for the engine is higher than normal for a military turbofan.

This engine was required to power new versions of the L-39 trainer, L-39MS and L-59. Other turbofan engine models in the DV-2 family include the DV-2A, DV‑2A.2 and DV-2S.

The DV-2S was renamed "RD-35" by the Klimov under license agreement with the PSLM in 1993.

Applications

  • L-59 Super Albatros (L-39MS Albatros)
  • Hongdu L-15
  • Ilyushin Il-108

Specifications (DV-2S)

  • Width: 0.82 m (32.2 in)
  • Height: 1.04 m (40.9 in)
  • Bypass ratio: 1.4 |power/weight= |thrust/weight= 5.69

References

References

  1. [http://www.janes.com/articles/Janes-Aero-Engines/PSLM-DV-2-Slovakia.html PSLM-DV-2] at janes.com
  2. [http://www.janes.com/articles/Janes-Aero-Engines/PSLM--Povazske-Strojarne-Letecke-Motory-a-s-Slovakia.html PSLM Aero-engines manufacturer]
  3. [http://www.forecastinternational.com/archive/at/ea0448.doc Russia, Central/Eastern Europe and China Turbofan and Turbojet Engines]{{dead link. (January 2018)
  4. [http://www.pslm.sk/index_engl.html DV-2S by PSLM] {{webarchive. link. (2010-01-10)
Wikipedia Source

This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.

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