Progress D-27

D-27
Progress propfan on the Antonov An-70
Type Propfan
National origin Ukraine
Manufacturer Ivchenko-Progress
First run 1992
Major applications Antonov An-70
Beriev A-42PE
Antonov An-180
Number built 16[1]
Developed from Lotarev D-36

The Progress D-27 is a three-shaft propfan engine derived from the D-36 turbofan.

Contents

Design and development

The engine was developed by the Ivchenko-Progress Design Bureau for commercial and military transport aircraft.

The D-27’s two-shaft gas generator 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 is no mass-produced aircraft that is powered by the D-27.

Applications

Specifications (D-27)

Data from forecastinternational.com[1][2]

General characteristics

Components

Performance

See also

Comparable engines
Related lists

References

External links