One of the best ways to learn is by doing, and thats what I've done here. The goal of this project is to learn more about compressors, and ultimatly find a compressor design that best suits my future ambitions of building a small turbojet engine. This project serves as a helpful tool for gaining insight into complexities of integrated systems, while also being usefull in the long term.
The compressor shaft is driven by a 750 watt BLDC motor, which is reduced to spin the shaft up to 10,000 rpm. The front of the wind tunnel is designed to be removable with two screws, providing access to the compressor blades. I designed the blades to be forward-mounted so they can be easily swapped out for testing. The motor and electronics are enclosed in a housing to prevent debree entering, and to protect the operator from any catastrophic failures.
There are a multitude of sensors to collect preformance data. RPM is measured with an optocoupler that reads an encoder mounted to the motor shaft. The RPM provides closed loop feedback for speed control. The speed is adjustable in increments of 100rpm, while actual rpm prints to the serial port. Current is measured with a hall-effect module - this measures the current into the motor driver. The output power of the motor is estimated using manufacturer-supplied data on motor efficency. Both total pressure and static pressure are measured using seperate pressure probes. The probes are placed about halfway into the tunnel to measure close to the average.
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