28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS2012-P4.15

THE EXPERIENCE OF HIGH PRESSURE RATIO SINGLE STAGE HPT DESIGNING
V. D. Venediktov, V. G Krupa, S. V. Rudenko, A. D. Nepomnyashchiy, V. K. Sichev*, A. A. Shvirev*
CIAM, Moscow, Russia; *"Aviadvigatel", Russia
Keywords: experimental module, high-pressure turbine, intermediate duct

Some results of calculated and experimental investigations of the high loading single-stage cooled high-pressure turbine (HPT) for a turbofan engine of the civil aviation are shown in this paper.

view full paper

28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS2012-P4.15

THE EXPERIENCE OF HIGH PRESSURE RATIO SINGLE STAGE HPT DESIGNING

V. D. Venediktov, V. G Krupa, S. V. Rudenko, A. D. Nepomnyashchiy, V. K. Sichev, A. A. Shvirev
CIAM, Moscow, Russia; *"Aviadvigatel", Russia

Keywords: experimental module, high-pressure turbine, intermediate duct

Some results of calculated and experimental investigations of the high loading single-stage cooled high-pressure turbine (HPT) for a turbofan engine of the civil aviation are shown in this paper.

view full paper

28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia Paper ICAS2012-P4.15

THE EXPERIENCE OF HIGH PRESSURE RATIO SINGLE STAGE HPT DESIGNING

V. D. Venediktov, V. G Krupa, S. V. Rudenko, A. D. Nepomnyashchiy, V. K. Sichev*, A. A. Shvirev* CIAM, Moscow, Russia; *"Aviadvigatel", Russia

Keywords: experimental module, high-pressure turbine, intermediate duct Some results of calculated and experimental investigations of the high loading single-stage cooled high-pressure turbine (HPT) for a turbofan engine of the civil aviation are shown in this paper.

view full paper

28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS2012-P4.15

V. D. Venediktov, V. G Krupa, S. V. Rudenko, A. D. Nepomnyashchiy, V. K. Sichev, A. A. Shvirev
CIAM, Moscow, Russia; *"Aviadvigatel", Russia

Keywords: experimental module, high-pressure turbine, intermediate duct

Some results of calculated and experimental investigations of the high loading single-stage cooled high-pressure turbine (HPT) for a turbofan engine of the civil aviation are shown in this paper.