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Desarrollo de un motor Wankel para su integración en turbinas de aviación con el programa de ordenador Pacelab
| Content Provider | Semantic Scholar |
|---|---|
| Author | Sánchez, Iñigo |
| Copyright Year | 2017 |
| Abstract | In order to increase the efficiency of future aviation turbines in the aeronautical sector, new processes to improve the thermodynamic cycle are being investigated. These include technologies such as intercooling, heat recovery and increasing the effective average pressure. The technical implementation of these technologies poses a challenge in the thermodynamic, aerodynamic and mechanical design of the engines. For this, the Aircraft Propulsion Institute (ILA) of the University of Stuttgart, along with two companies in the sector, Rolls Royce and MTU have created a strategic innovation plan, together with seven other universities in Germany. This part of the project consists of a study that analyses the use of a Wankel engine as a high-pressure compressor, combustion chamber and high-pressure turbine. The objective of this work is to create a model that allows to make a preliminary study of the performance of a turbofan with this configuration and to study its viability. For this, a computer program called Pacelab is used, which allows creating a 3D model of the hypothetical rotary engine necessary for specific turbine operating conditions. Validations are carried out with other rotary engines already in existence, such as the Mazda Renesis 13B. This software allows knowing the dimensions, the weight and the basic performance of the rotary engine, characteristics necessary to see the viability of the project and determine future investigations. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://uvadoc.uva.es/bitstream/10324/27355/1/TFG-I-779.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
