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Lotarev DV-2
Turbofan aircraft engine
Turbofan aircraft engine
| Field | Value |
|---|---|
| name | DV-2 |
| image | Lotarev DV-2 Kosice.jpg |
| caption | DV-2 turbofan engine |
| engine_type | Turbofan |
| national_origin | Soviet Union/Czechoslovakia |
| manufacturer | Ivchenko-Progress/PSLM |
| first_run | 1987 |
| major_applications | |
| number_built | 124 |
| developed_from | Ivchenko AI-25 |
RD-35 by Klimov
The Lotarev DV-2 (or PSLM DV-2, DV: Dnepr-Váh, )MOT Site:
- Letecká Atlantída (03/2013)
- Letecká Atlantída II (04/2013)
- Letecká Atlantída IV (06/2013)
- Letecká Atlantída V (07-08/2013) is a two-spool turbofan engine manufactured in Považská Bystrica, Slovakia by Považské Strojárne Letecké Motory (PS Aircraft Engines/Motors) (PSLM) (former ZVL Závody na Výrobu Ložísk "Bearings Production/Manufacturing Plant") and designed in partnership with Ivchenko Lotarev Design Bureau.
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
- [http://www.janes.com/articles/Janes-Aero-Engines/PSLM-DV-2-Slovakia.html PSLM-DV-2] at janes.com
- [http://www.janes.com/articles/Janes-Aero-Engines/PSLM--Povazske-Strojarne-Letecke-Motory-a-s-Slovakia.html PSLM Aero-engines manufacturer]
- [http://www.forecastinternational.com/archive/at/ea0448.doc Russia, Central/Eastern Europe and China Turbofan and Turbojet Engines]{{dead link. (January 2018)
- [http://www.pslm.sk/index_engl.html DV-2S by PSLM] {{webarchive. link. (2010-01-10)
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