Rahul Sharma (Editor)

Progress D 27

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Progress D-27 httpsuploadwikimediaorgwikipediacommonsthu

The Progress D-27 is a three-shaft propfan engine developed by Ivchenko Progress. It is not clear whether the D-27 engine's core is related to or derived from the D-36 turbofan which is a three-shaft turbofan. The D-27 engine was developed specifically to power more efficient passenger aircraft such as the abandoned Yak-46 project and it was chosen to power the An-70 military transport aircraft. The D-27 is expected to be a base platform for future engine derivatives.

Contents

Design and development

The engine was developed by the Ivchenko-Progress Design Bureau for commercial and military transport aircraft. It was designed to meet the expected growth in demand for aeronautical products which include the development of a number of new aero engines of civil and military application.

D-27 is regarded as a pacesetter and perhaps a first in the world for production turbopropfan engines. It is rated at a maximum power of 14000shp. Currently, the D-27 is undergoing official flight testing as installed in medium-range military airlifter, the An-70.

In developing the D-27 engine, Ivchenko-Progress also came up with a proposal for several derivatives based on the core of the D-27 engine. For instance the following derivatives have been proposed for different purposes and at different times:

  • AI-127 - a turboshaft derivative with a rated power of 14500 hp proposed for the Mil Mi-26 helicopter.
  • AI-727 - a family of ultra-high bypass geared turbofan engines with a thrust of between 9000kgf and 11000 kgf.
  • (These are proposed drive low-noise wide-span fans via a reduction gear)

    The D-27’s three-shaft gas turbine engine is made up of an axial low-pressure compressor, a mixed-flow high-pressure compressor, an annular combustion chamber, a single-stage high-pressure turbine, and a single-stage low-pressure turbine. The SV-27 contra-rotating propfan, provided by SPE Aerosila, is driven by a four-stage turbine via a shaft connected to a planetary reduction gear housing a thrust meter and mechanism to prevent rotor acceleration.

    Currently, there are no mass-produced aircraft that are powered by the D-27.

    Applications

  • Antonov An-70
  • Beriev A-42PE
  • Antonov An-180
  • Yakovlev Yak-44 (not built)
  • Specifications (D-27)

    Data from forecastinternational.com

    General characteristics

  • Type: Three-shaft propfan engine
  • Length: 4.2 m (165.3 in)
  • Width: 1.2 m (49.5 in)
  • Height: 1.3 m (53.9 in)
  • Propeller diameter: 4.5 m (177.1 in)
  • Diameter:
  • Dry weight: 1,650 kilograms (3,638 lb)
  • Components

  • Compressor: Low-pressure five-stage, axial flow and high-pressure 2 axial and single centrifugal stages
  • Combustors: Annular combustion chamber
  • Turbine: Single-stage high-pressure, single-stage low-pressure
  • Performance

  • Maximum power output: 14,000 horsepower (10,440 kW)
  • Power-to-weight ratio: 6.33 kW/kg (3.85 hp/lb)
  • References

    Progress D-27 Wikipedia