Geometric regeneration and mechanical analysis of a gas turbine blade type Frame 9001 GE

Simulation and visualization of the mechanical components have become a predominant phase during the design and the production stages. Several means are used to improve the design and to reduce study time. | Geometric regeneration and mechanical analysis of a gas turbine blade type Frame 9001 GE Engineering Solid Mechanics 2018 105-112 Contents lists available at GrowingScience Engineering Solid Mechanics homepage esm Geometric regeneration and mechanical analysis of a gas turbine blade type Frame 9001 GE Salah Amrounea Barhm Mohamadb Mustafa Moussaouic and Hafida Saaidia a Université Mohamed Boudiaf 166 ICHBELIA M sila 28000 Algérie b Petroleum Technology Department Koya Technical Institute EPU KRG Iraq c Université Ziane Achour 3117 Djelfa 17000 Algérie A R T I C L EI N F O ABSTRACT Article history Simulation and visualization of the mechanical components have become a predominant phase Received 22 September 2017 during the design and the production stages. Several means are used to improve the design and Accepted 10 January 2018 to reduce study time. Today the powerful hardware and the software available on the market Available online have contributed greatly on the improvement of design visualization and manufacturing 18 March 2018 Keywords process of complex parts turbine blade . In this context our study is a contribution to the Geometric regeneration establishment of a methodology to a CAD modelling and finite element analysis which allows Gas turbine blade us to identify the mechanical behavior of a gas turbine blade. The profile of the blade turbine Structural analyses model is obtained after regeneration using the CATIA V5R20 software from the retro-design Energy elastic technique using a FARO-type scanner. The turbine blade is analyzed under a static mechanical behavior. It has been observed that the maximum stresses and deformations are located in the vicinity of the root and the upper surface along the turbine blade. On the other hand the elastic energy is located at a distance from the root of the turbine blade. 2018 Growing Science Ltd. All rights reserved. 1. Introduction The turbine blades are the individual components

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