Investigation of the requirements for the selection of materials for high pressure Turbine blades of conventional turbojet engines
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The material selection method is critically evaluated to enable high pressure (HP) turbine blades to deal with in-service damaging phenomena such as creep, low cycle fatigue and high cycle fatigue, oxidation and corrosion. The material selection method is analyzed in order to improve the service life of the aero engine. To increase the turbine inlet temperature, HP turbine blades need improved creep and fatigue resistance. more quality. By the typical working condition of HP turbine blade, using CES Edu Pack (CES) material selection software was used to select suitable materials for HP turbine blade material. Nickel based alloys are selected for HP turbine blades, such as Nickel-Cr-Co-Mo superalloy.
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2015 ◽
Vol 39
(11)
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pp. 1145-1151
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2007 ◽
Vol 29
(1)
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pp. 69-80
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2021 ◽
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