An alternative coating material for gas turbine blade for aerospace applications

Yajnesh M. Poojari; Koustubh S. Annigeri; Nilesh Bandekar; Kiran U. Annigeri; Vinayak Badiger; Arun Patil; Santosh Billur; Basavaraj B. Kotturshettar

doi:10.1088/1742-6596/1706/1/012183

An alternative coating material for gas turbine blade for aerospace applications

Yajnesh M. Poojari
, Koustubh S. Annigeri
, Nilesh Bandekar
, Kiran U. Annigeri
, Vinayak Badiger
, Arun Patil^*
, Santosh Billur
, Basavaraj B. Kotturshettar

^*Corresponding author for this work

Department of Mechanical and Industrial Engineering, Manipal Institute of Technology, Bengaluru

Research output: Contribution to journal › Conference article › peer-review

9 Citations (Scopus)

Abstract

Gas turbine needs to withstand high temperature, stresses and fatigue loads they are exposed to, while still being affordable and maintaining a long-life span. This paper presents an alternative material for Thermal Barrier Coating (TBC) of the gas turbine blade. The paper also summarizes the basic properties of nickel superalloys that are used as a base material for the blades. The simulation study is conducted on the CAD model with and without coating in ANSYS.

Original language	English
Article number	012183
Journal	Journal of Physics: Conference Series
Volume	1706
Issue number	1
DOIs	https://doi.org/10.1088/1742-6596/1706/1/012183
Publication status	Published - 22-12-2020
Event	1st International Conference on Advances in Physical Sciences and Materials 2020, ICAPSM 2020 - Coimbatore, Virtual, India Duration: 13-08-2020 → 14-08-2020

All Science Journal Classification (ASJC) codes

General Physics and Astronomy

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10.1088/1742-6596/1706/1/012183

Cite this

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title = "An alternative coating material for gas turbine blade for aerospace applications",

abstract = "Gas turbine needs to withstand high temperature, stresses and fatigue loads they are exposed to, while still being affordable and maintaining a long-life span. This paper presents an alternative material for Thermal Barrier Coating (TBC) of the gas turbine blade. The paper also summarizes the basic properties of nickel superalloys that are used as a base material for the blades. The simulation study is conducted on the CAD model with and without coating in ANSYS.",

author = "Poojari, \{Yajnesh M.\} and Annigeri, \{Koustubh S.\} and Nilesh Bandekar and Annigeri, \{Kiran U.\} and Vinayak Badiger and Arun Patil and Santosh Billur and Kotturshettar, \{Basavaraj B.\}",

note = "Publisher Copyright: {\textcopyright} Published under licence by IOP Publishing Ltd.; 1st International Conference on Advances in Physical Sciences and Materials 2020, ICAPSM 2020 ; Conference date: 13-08-2020 Through 14-08-2020",

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AU - Poojari, Yajnesh M.

AU - Annigeri, Koustubh S.

AU - Bandekar, Nilesh

AU - Annigeri, Kiran U.

AU - Badiger, Vinayak

AU - Patil, Arun

AU - Billur, Santosh

AU - Kotturshettar, Basavaraj B.

PY - 2020/12/22

Y1 - 2020/12/22

N2 - Gas turbine needs to withstand high temperature, stresses and fatigue loads they are exposed to, while still being affordable and maintaining a long-life span. This paper presents an alternative material for Thermal Barrier Coating (TBC) of the gas turbine blade. The paper also summarizes the basic properties of nickel superalloys that are used as a base material for the blades. The simulation study is conducted on the CAD model with and without coating in ANSYS.

AB - Gas turbine needs to withstand high temperature, stresses and fatigue loads they are exposed to, while still being affordable and maintaining a long-life span. This paper presents an alternative material for Thermal Barrier Coating (TBC) of the gas turbine blade. The paper also summarizes the basic properties of nickel superalloys that are used as a base material for the blades. The simulation study is conducted on the CAD model with and without coating in ANSYS.

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U2 - 10.1088/1742-6596/1706/1/012183

DO - 10.1088/1742-6596/1706/1/012183

M3 - Conference article

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SN - 1742-6588

VL - 1706

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

IS - 1

M1 - 012183

T2 - 1st International Conference on Advances in Physical Sciences and Materials 2020, ICAPSM 2020

Y2 - 13 August 2020 through 14 August 2020

ER -

An alternative coating material for gas turbine blade for aerospace applications

Abstract

All Science Journal Classification (ASJC) codes

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