PROJECTS
Compressor Design
The purpose of this project was to design a compressor based on a set of design requirements, including the inlet turbine temperature, net shaft power, and shaft RPM. The primary objective of the study was to develop a compressor design that achieves a minimum isentropic efficiency of 89%.
Spring Pallet Loader
The purpose of this project was to design a spring pallet loader based on a set of design requirements.
Mortise Lock
The purpose of this project was to design a Mortise Lock based on existing designs available on the market and manufacture using CNC, 3D printers and common machining tools.
Repowering of existing coal-fired plant
The purpose of this project was to design a system with combined cycle to replace an existing plant coal-fired plant.
Automotive Engine Design
The purpose of this project was to reverse engineer an automotive segment/class and design an improved engine based on a specific market/class/platform comparison.
Reverse Engineering of Table Lamp
The purpose of this project was to reverse engineer a product with complex curves, which would require the use of advanced SolidWorks features.
Electric Transmission Tower
The purpose of this project is to design electric transmission towers, 3D print the model, perform ANSYS fluid simulation and wind tunnel testing.
FEM Study - Extension of a Circular Bar
The purpose of this project is to conduct FEA on a circular bar with filleted shoulders using the SolidWorks Simulation tool.
Portable Wireless Charging Stand
This project aims to design a portable wireless charging stand capable of carrying the loads from a typical phone and tablet.
Soap Dispenser
The purpose of this project was to reverse engineer a soap dispenser and add improvements to the design.
DC Motor
The purpose of this project was to design and build a rudimentary dc motor.
Aileron
The purpose of this project was to fabricate an aileron of an aircraft based on design schematic.
Aircraft Stressed Skin Structure
The purpose of this project was to fabricate a section of an aircraft stress skin structure based on a design schematic.