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Proceedings Papers

Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A019, June 7–11, 2021
Paper No: GT2021-58823
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-58823 MECHANISM ANALYSIS OF THE INFLUENCE OF BLADE THICKNESS DEVIATION ON THE PERFORMANCE OF AXIAL FLOW COMPRESSOR Tianyuan Ji1, Wuli Chu1, Zhengtao Guo1, Jibo...
Proceedings Papers

Proc. ASME. GT2021, Volume 8: Oil and Gas Applications; Steam Turbine, V008T22A005, June 7–11, 2021
Paper No: GT2021-58632
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-58632 RECONSTRUCTION OF A STEAM TURBINE BLADE USING PIECEWISE BERNSTEIN POLYNOMIALS AND TRANSFINITE INTERPOLATION Luis David Pérez Sergio Ricardo Galván Francisco...
Proceedings Papers

Proc. ASME. GT2020, Volume 10B: Structures and Dynamics, V10BT26A001, September 21–25, 2020
Paper No: GT2020-14002
...MODELING OF RESIDUAL STRESSES AFTER SHOT PEENING AND THE EFFECT OF ACCOUNTING THEIR INFLUENCE ON THE STRESS STATE OF TURBINE BLADE FIR TREE ROOTS Boris Vasilyev1,2, Nikita Zhukov 2, Igor Kiselev2, Alexander Selivanov1 1 Central Institute of Aviation Motors, Moscow, Russia 2 Bauman Moscow State...
Proceedings Papers

Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T01A034, September 21–25, 2020
Paper No: GT2020-16039
...CREATION OF MODELS OF FAN BLADES ACCORDING TO AIRFOIL MEASUREMENTS Alexandr N. Arkhipov, Yury A. Ravikovich, Dmitry P. Kholobtsev Moscow Aviation Institute (National Research University), Moscow, Russian Federation ABSTRACT One of the main parts of the engine for the regional aircraft, affecting...
Proceedings Papers

Proc. ASME. GT2020, Volume 10B: Structures and Dynamics, V10BT27A016, September 21–25, 2020
Paper No: GT2020-14866
...DETERMINING THE OPTIMAL CRYSTALLOGRAPHIC ORIENTATION IN A SINGLE CRYSTAL TURBINE BLADE TO INCREASE ITS STRENGTH RELIABILITY Boris Vasilyev1,3, Alexander Selivanov1,3, Artem Semenov1, Andrei Bortnikov1, Valentina Limonova2 1Central Institute of Aviation Motors, Moscow, Russia 2JSC UEC-Aviadvigatel...
Proceedings Papers

Proc. ASME. GT2008, Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Manufacturing, Materials and Metallurgy; Microturbines and Small Turbomachinery, 495-500, June 9–13, 2008
Paper No: GT2008-51097
... 04 08 2009 Gas turbine blades are operating under very demanding conditions. In modern industrial gas turbines, the rotating blades and the guide vanes of the first stages are hollow to allow internal cooling. This means that there is a possibility of having crack initiation...
Proceedings Papers

Proc. ASME. GT2007, Volume 5: Turbo Expo 2007, 155-159, May 14–17, 2007
Paper No: GT2007-28208
.... In particular, the following technologies used by Siemens will be addressed: • Weld restoration; • Braze restoration processes; • Coating; • Re-opening of cooling holes. blade vane repair welding brazing coating G Solidifie compon technolo while m cost.. This developm repair technolo Key...
Proceedings Papers

Proc. ASME. GT2005, Volume 2: Turbo Expo 2005, 857-863, June 6–9, 2005
Paper No: GT2005-68787
... selection, metallurgical and mechanical tests, a full-scale production test and an engine test in the 15MW gas turbine, will be described here. Single crystal Blade Creep Fatigue Engine test Proceedings of GT2005 ASME Turbo Expo 2005: Power for Land, Sea and Air June 6-9, 2005, Reno-Tahoe...