Search for dissertations about: "Aircraft electric power"
Showing result 1 - 5 of 6 swedish dissertations containing the words Aircraft electric power.
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1. On magnetic amplifiers in aircraft applications
Abstract : In the process of designing an electric power supply system for an aircraft, parameters like low weight and low losses are important. Reliability, robustness and low cost are other important factors. READ MORE
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2. Conceptual Design of Propulsion Systems for Boundary Layer Ingestion
Abstract : To reduce the climate impact of aviation new aircraft and engine concepts as well as improved design methods are needed. In this thesis, two fronts are explored. The first concerns improved methods for the conceptual design of the engine. READ MORE
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3. Evaluation of Aircraft Actuator Technologies
Abstract : The flight control actuation system is one of the most critical systems in an aircraft. A failure of this system cannot occur, since it would have catastrophic consequences. READ MORE
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4. Analysis of Electro-Meachanical Actuator Systems in More Electric Aircraft Applications
Abstract : Conventional hydraulic actuators in aircraft are demanding regarding maintenance which implies high operation costs. In recent years the focus therefore has been set on electro-hydrostatic and electro-mechanical actuators. READ MORE
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5. Dimensioning Tools of MEA Actuator Systems, Including Modeling, Analysis and Technology Comparison
Abstract : Aircraft design is an example of complex engineering where dimensioning tools can be valuable for the designers and decision makers in the early stage of the development process. These tools can be in form of a database over key numbers for different components or technologies. One of the critical parts of an aircraft is the actuator system. READ MORE