Dynamic Response Assessment and Design Optimization of Aircraft Tyre Pressure Monitoring Unit (Tpmu)

Aviation industry demands higher efficiency and reliability of a gas turbine engine and it must provide predictable thrust performance over the tyre operating envelope of the engine, covering altitudes ranging from below sea level to tens of thousands of feet above. These altitude changes, along with differing flight speeds from takeoff to supersonic velocities, result in large variations in engine inlet temperature, inlet pressure, and exhaust pressure. Large variations in engine operating conditions, coupled with the need for precise thrust control and highly reliable operation, create a significant challenge for the design of engine control systems, especially given the complexity of the engine itself. Controlling such complex machinery requires a thorough understanding of the performance of the engine system as a whole. This current research covers the design of aircraft tyre pressure monitoring unit. It focuses on four areas of interest: 1) Modeling of aircraft tyre pressure monitoring unit. 2) Aircraft tyre pressure monitoring unit dynamic response. 3) Design assessment using Steinberg relation.