3D Printing of Nickel Based Super Alloy for Aero-Engine Applications / (Record no. 614898)

000 -LEADER
fixed length control field 03450nam a22001577a 4500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 670
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Absar, Muhammad
245 ## - TITLE STATEMENT
Title 3D Printing of Nickel Based Super Alloy for Aero-Engine Applications /
Statement of responsibility, etc. Muhammad Absar
264 ## - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Place of production, publication, distribution, manufacture Islamabad :
Name of producer, publisher, distributor, manufacturer SMME- NUST;
Date of production, publication, distribution, manufacture, or copyright notice 2025.
300 ## - PHYSICAL DESCRIPTION
Extent 118p.
Other physical details Soft Copy
Dimensions 30cm
500 ## - GENERAL NOTE
General note From the past few years, Additive Manufacturing (AM) or 3D printing has<br/>achieved a significant role among the latest emerging technologies of the<br/>fourth industrial revolution. 3D printing strategy allows us to build<br/>components of various materials without any geometrical constraint. This<br/>feature is unique in the field of industrial production, and it has transformed<br/>the traditional manufacturing concept of mechanical design permitting<br/>lightweight components and improving stiffness. Moreover, another<br/>advantage of additive manufacturing is decreased production waste and<br/>energy consumption. The Nickel based Super Alloy powder has its wide<br/>applicability in the defense industry and mainly Aero-Engine components.<br/>This can also be used for biomedical, power generation and automotive<br/>applications. Nickel and its alloys are useful due to their properties at elevated<br/>temperatures. The aim of this research was to develop the build parameters of<br/>Nickel based powder and successfully print functional parts using Selective<br/>Laser Melting (SLM) process. The properties desired for the functional part<br/>have been verified through mechanical testing. The print worthiness of this<br/>powder along with desired results achieved through this research has led to<br/>qualified printing of metal parts for high temperature applications. In the<br/>presented thesis, the objective was to conduct a series of experiments to<br/>develop parameters for printing Nickel based superalloy K465 powder for<br/>aero-engine applications. The properties that were evaluated against the<br/>printing parameters include Actual Density measurement, Microstructure and<br/>Tensile values. The best samples were optically viewed to look for<br/>microstructure. Alongside metallography, UTS samples were printed to carry<br/>xv<br/>out mechanical testing of the best samples. The experiment yielding finest<br/>results was chosen for functional part printing. Though additive<br/>manufacturing of nickel-based superalloys presents significant technological<br/>advancement, their unique material behavior and properties also present<br/>several common challenges like fusion of layers, microstructure control,<br/>residual stress and cracking during 3D printing that require careful<br/>consideration and process optimization. The K465 superalloy powder is also<br/>prone to cracking which was faced during this research. Though higher preheat temperatures were provided to mitigate this issue, cracking couldn’t be<br/>avoided due to available SLM limitation. To avoid this challenge, the further<br/>optimization of developed K465 parameters can be carried out through EBM<br/>process and even through more R&D and advanced strategies at SLM<br/>machine discussed in this thesis. These studies will be crucial for optimizing<br/>K465 additive manufacturing processes and ensuring the production of crackfree, high-integrity components for the most demanding applications.
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element MS Design and Manufacturing Engineering
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Supervisor : Dr. Muhammad Rizwan ul Haq
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="http://10.250.8.41:8080/xmlui/handle/123456789/55031">http://10.250.8.41:8080/xmlui/handle/123456789/55031</a>
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme
Koha item type Thesis
Holdings
Withdrawn status Permanent Location Current Location Shelving location Date acquired Full call number Barcode Koha item type
  School of Mechanical & Manufacturing Engineering (SMME) School of Mechanical & Manufacturing Engineering (SMME) E-Books 09/26/2025 670 SMME-TH-1175 Thesis
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