UGC Approved Journal no 63975(19)

ISSN: 2349-5162 | ESTD Year : 2014
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Published in:

Volume 8 Issue 3
March-2021
eISSN: 2349-5162

UGC and ISSN approved 7.95 impact factor UGC Approved Journal no 63975

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Published Paper ID:
JETIR2103232


Registration ID:
306974

Page Number

1876-1880

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Title

THERMAL AND STRUCTURAL ANALYSIS FOR TURBINE ENGINE BLADES AT MAXIMUM TEMPERATURE

Abstract

Additive manufacturing is the process of making objects from 3D model data by joining materials layer by layer, as opposed to subtractive manufacturing methodologies, such as traditional machining. It processes can reduce waste, speed up production, and enable designs that might not be feasible with conventional production processes. The novel shapes and unusual material properties the technology makes possible, such as propeller, turbine blades optimized for strength at one end and flexibility at the other could change the way airplanes are designed. Additive Manufacturing offers the freedom to design very complex components, which makes it an extraordinary tool to meet your most challenging requirements. More recently, AM is being used to fabricate end-use products in aircraft, dental restorations, medical implants, automobiles, and even fashion products. Additive manufactured parts are used in the aerospace industry for functional parts including engine turbine blades, fuel systems and guide vanes. The topological optimization of parts can improve functionality and reduce weight. Lighter parts can contribute to lighter aircraft and reduce fuel consumption. This project explores the effective use of additive manufacturing complex designs, for this jet engine turbine blade is modeled in software and then manufactured using 3D printer to get cost effective and light weight parts.

Key Words

Additive manufacturing, Aircraft technology, Jet engine, Turbine blade, 3D printing.

Cite This Article

"THERMAL AND STRUCTURAL ANALYSIS FOR TURBINE ENGINE BLADES AT MAXIMUM TEMPERATURE ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.8, Issue 3, page no.1876-1880, March-2021, Available :http://www.jetir.org/papers/JETIR2103232.pdf

ISSN


2349-5162 | Impact Factor 7.95 Calculate by Google Scholar

An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 7.95 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator

Cite This Article

"THERMAL AND STRUCTURAL ANALYSIS FOR TURBINE ENGINE BLADES AT MAXIMUM TEMPERATURE ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.8, Issue 3, page no. pp1876-1880, March-2021, Available at : http://www.jetir.org/papers/JETIR2103232.pdf

Publication Details

Published Paper ID: JETIR2103232
Registration ID: 306974
Published In: Volume 8 | Issue 3 | Year March-2021
DOI (Digital Object Identifier):
Page No: 1876-1880
Country: -, -, - .
Area: Engineering
ISSN Number: 2349-5162
Publisher: IJ Publication


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