O conceito de um motor rotativo de palhetas é apresentado e o modelo que opera similar aos motores recíprocos dois tempos é analisado. Este motor é formado por estator cilíndrico, rotor descentralizado, palhetas radiais e tampas laterais, similar aos compressores de palhetas radiais. Parâmetros geométricos estão definidos para que o motor possua características similares a dois motores recíprocos comerciais igualmente modelados. Suas geometrias estão detalhadas, assim como a modelagem termodinâmica e suas hipóteses, as quais devido ao caráter comparativo do trabalho não têm grande influência no alcance dos objetivos. Em relação aos motores recíprocos, o novo conceito prospecta algumas vantagens: maior compacidade; menor nível de vibrações; maior facilidade de alteração da razão de compressão; possibilidade de produção e montagem em módulos; e devido a todas estas, as maiores possibilidades para o projeto, fabricação, montagem e operação dos motores. Para melhor entendimento de algumas tendências relativas a estas vantagens, a sensibilidade dos parâmetros geométricos é estudada, com variações nos diâmetros do estator e do rotor, na espessura do rotor e das palhetas, na excentricidade entre rotor e estator, e no número de palhetas do conceito. Este estudo demonstra características únicas do motor rotativo de palhetas, dentre elas, a variação da espessura do rotor se destaca por proporcionar a alteração do tamanho do motor sem modificar os demais aspectos. A excentricidade entre o rotor e estator demonstra grande potencial na capacidade de alterar a razão de compressão do equipamento, inclusive podendo ser modificada após a construção do motor ou até mesmo durante sua operação. Também se destaca o número de palhetas, o qual tem influência direta sobre a curva de torque do ciclo e a efetividade do posicionamento das janelas de admissão e exaustão. Com isto, é concluída a caracterização da geometria e do funcionamento do motor rotativo de palhetas, obtendo uma boa base para as próximas etapas de seu desenvolvimento. / The concept of a rotary vane engine is presented and the model that operates similar to twostroke reciprocating engines is analyzed. This engine is formed by a cylindrical stator, decentralized rotor, radial vanes and side housing plates, similar to the radial vane compressors. Geometrical parameters are defined so that the motor has similar characteristics to two commercial reciprocating engines also modeled. Their geometries are detailed, as well as the thermodynamic model and its assumptions, which due to the comparative nature of the work do not have significant influence in achieving the objectives. With respect to reciprocating engines, the new concept is prospecting some advantages: higher compactness; lowest level of vibration; ease of adjustment of compression ratio; possibility of manufacture and assembly in modules; and due to all these, the numerous possibilities to the design, manufacture, assembly and operation of the engines. For a better understanding of some these advantages trends, the sensitivity of geometric parameters are studied, with variations in the diameters of the stator and rotor, in the thickness of the rotor and the vanes, in the eccentricity between rotor and stator, and in the number of vanes of the concept. This study demonstrates unique rotary vane engine characteristics, among them, the range of rotor thickness stands out for providing a change in engine size without changing other aspects. The eccentricity between the rotor and stator shows great potential for the ability to change the compression ratio of the equipment and can be modified even after the construction or even during operation of the engine. It also highlights the number of vanes, which has a direct influence on the torque curve of the cycle and the effectiveness of the positioning of inlet and exhaust ports. Therewith, the characterization of rotary vane engine geometry and operational design is complete, obtaining a good basis for its next development stages.

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No description available.

O conceito de um motor rotativo de palhetas é apresentado e o modelo que opera similar aos motores recíprocos dois tempos é analisado. Este motor é formado por estator cilíndrico, rotor descentralizado, palhetas radiais e tampas laterais, similar aos compressores de palhetas radiais. Parâmetros geométricos estão definidos para que o motor possua características similares a dois motores recíprocos comerciais igualmente modelados. Suas geometrias estão detalhadas, assim como a modelagem termodinâmica e suas hipóteses, as quais devido ao caráter comparativo do trabalho não têm grande influência no alcance dos objetivos. Em relação aos motores recíprocos, o novo conceito prospecta algumas vantagens: maior compacidade; menor nível de vibrações; maior facilidade de alteração da razão de compressão; possibilidade de produção e montagem em módulos; e devido a todas estas, as maiores possibilidades para o projeto, fabricação, montagem e operação dos motores. Para melhor entendimento de algumas tendências relativas a estas vantagens, a sensibilidade dos parâmetros geométricos é estudada, com variações nos diâmetros do estator e do rotor, na espessura do rotor e das palhetas, na excentricidade entre rotor e estator, e no número de palhetas do conceito. Este estudo demonstra características únicas do motor rotativo de palhetas, dentre elas, a variação da espessura do rotor se destaca por proporcionar a alteração do tamanho do motor sem modificar os demais aspectos. A excentricidade entre o rotor e estator demonstra grande potencial na capacidade de alterar a razão de compressão do equipamento, inclusive podendo ser modificada após a construção do motor ou até mesmo durante sua operação. Também se destaca o número de palhetas, o qual tem influência direta sobre a curva de torque do ciclo e a efetividade do posicionamento das janelas de admissão e exaustão. Com isto, é concluída a caracterização da geometria e do funcionamento do motor rotativo de palhetas, obtendo uma boa base para as próximas etapas de seu desenvolvimento. / The concept of a rotary vane engine is presented and the model that operates similar to twostroke reciprocating engines is analyzed. This engine is formed by a cylindrical stator, decentralized rotor, radial vanes and side housing plates, similar to the radial vane compressors. Geometrical parameters are defined so that the motor has similar characteristics to two commercial reciprocating engines also modeled. Their geometries are detailed, as well as the thermodynamic model and its assumptions, which due to the comparative nature of the work do not have significant influence in achieving the objectives. With respect to reciprocating engines, the new concept is prospecting some advantages: higher compactness; lowest level of vibration; ease of adjustment of compression ratio; possibility of manufacture and assembly in modules; and due to all these, the numerous possibilities to the design, manufacture, assembly and operation of the engines. For a better understanding of some these advantages trends, the sensitivity of geometric parameters are studied, with variations in the diameters of the stator and rotor, in the thickness of the rotor and the vanes, in the eccentricity between rotor and stator, and in the number of vanes of the concept. This study demonstrates unique rotary vane engine characteristics, among them, the range of rotor thickness stands out for providing a change in engine size without changing other aspects. The eccentricity between the rotor and stator shows great potential for the ability to change the compression ratio of the equipment and can be modified even after the construction or even during operation of the engine. It also highlights the number of vanes, which has a direct influence on the torque curve of the cycle and the effectiveness of the positioning of inlet and exhaust ports. Therewith, the characterization of rotary vane engine geometry and operational design is complete, obtaining a good basis for its next development stages.

O conceito de um motor rotativo de palhetas é apresentado e o modelo que opera similar aos motores recíprocos dois tempos é analisado. Este motor é formado por estator cilíndrico, rotor descentralizado, palhetas radiais e tampas laterais, similar aos compressores de palhetas radiais. Parâmetros geométricos estão definidos para que o motor possua características similares a dois motores recíprocos comerciais igualmente modelados. Suas geometrias estão detalhadas, assim como a modelagem termodinâmica e suas hipóteses, as quais devido ao caráter comparativo do trabalho não têm grande influência no alcance dos objetivos. Em relação aos motores recíprocos, o novo conceito prospecta algumas vantagens: maior compacidade; menor nível de vibrações; maior facilidade de alteração da razão de compressão; possibilidade de produção e montagem em módulos; e devido a todas estas, as maiores possibilidades para o projeto, fabricação, montagem e operação dos motores. Para melhor entendimento de algumas tendências relativas a estas vantagens, a sensibilidade dos parâmetros geométricos é estudada, com variações nos diâmetros do estator e do rotor, na espessura do rotor e das palhetas, na excentricidade entre rotor e estator, e no número de palhetas do conceito. Este estudo demonstra características únicas do motor rotativo de palhetas, dentre elas, a variação da espessura do rotor se destaca por proporcionar a alteração do tamanho do motor sem modificar os demais aspectos. A excentricidade entre o rotor e estator demonstra grande potencial na capacidade de alterar a razão de compressão do equipamento, inclusive podendo ser modificada após a construção do motor ou até mesmo durante sua operação. Também se destaca o número de palhetas, o qual tem influência direta sobre a curva de torque do ciclo e a efetividade do posicionamento das janelas de admissão e exaustão. Com isto, é concluída a caracterização da geometria e do funcionamento do motor rotativo de palhetas, obtendo uma boa base para as próximas etapas de seu desenvolvimento. / The concept of a rotary vane engine is presented and the model that operates similar to twostroke reciprocating engines is analyzed. This engine is formed by a cylindrical stator, decentralized rotor, radial vanes and side housing plates, similar to the radial vane compressors. Geometrical parameters are defined so that the motor has similar characteristics to two commercial reciprocating engines also modeled. Their geometries are detailed, as well as the thermodynamic model and its assumptions, which due to the comparative nature of the work do not have significant influence in achieving the objectives. With respect to reciprocating engines, the new concept is prospecting some advantages: higher compactness; lowest level of vibration; ease of adjustment of compression ratio; possibility of manufacture and assembly in modules; and due to all these, the numerous possibilities to the design, manufacture, assembly and operation of the engines. For a better understanding of some these advantages trends, the sensitivity of geometric parameters are studied, with variations in the diameters of the stator and rotor, in the thickness of the rotor and the vanes, in the eccentricity between rotor and stator, and in the number of vanes of the concept. This study demonstrates unique rotary vane engine characteristics, among them, the range of rotor thickness stands out for providing a change in engine size without changing other aspects. The eccentricity between the rotor and stator shows great potential for the ability to change the compression ratio of the equipment and can be modified even after the construction or even during operation of the engine. It also highlights the number of vanes, which has a direct influence on the torque curve of the cycle and the effectiveness of the positioning of inlet and exhaust ports. Therewith, the characterization of rotary vane engine geometry and operational design is complete, obtaining a good basis for its next development stages.

Due to its complex and multidisciplinary nature, the conceptual design phase of helicopters becomes critical in meeting customer satisfaction. Statistical (probabilistic) design methods can be employed to understand the design better and target a design with lower variability. In this thesis, a conceptual design and helicopter sizing methodology is developed and shown on a helicopter design for Turkey.

Doctor of Philosophy / Department of Electrical and Computer Engineering / James E. DeVault / Prakash Krishnaswami / Most state-of-the-art systems are multidisciplinary in nature and encompass a wide range of components from domains such as electronics, mechanics, hydraulics, etc. Design considerations and design parameters of the system can come from any or a combination of these domains. The traditional optimization approach for multidisciplinary systems utilizes sequential optimization, wherein each subsystem is optimized in isolation in a predetermined order, assuming that the designs of the other subsystems remain fixed. This often leads to system designs that are suboptimal. In recent years emphasis has been placed on development of an integrated scheme for analysis and design of multidisciplinary systems. An important aspect is the software architecture required to support such a scheme. This dissertation presents MIXEDMODELS (Multidisciplinary Integrated eXtensible Engine for Driving Metamodeling, Optimization and DEsign of Large-scale Systems) - a unified analysis and design tool for multidisciplinary systems that is based on a procedural, symbolic-numeric architecture. This architecture offers great modeling flexibility at the component level, allowing any engineer to add components in his/her domain of expertise to the platform in a modular fashion. The symbolic engine in the MIXEDMODELS platform synthesizes the system governing equations as a unified set of nonlinear differential-algebraic equations (DAEs). These equations are differentiated with respect to design variables to obtain an additional set of DAEs that describe the sensitivity coefficients of the system state variables. This combined set of DAEs is solved numerically to obtain the solution for the state variables and the state sensitivity coefficients of the system. Finally, knowing the system performance functions, their design sensitivity coefficients can be calculated by using the values of the state variables and state sensitivity coefficients obtained from the DAEs. For ease in error control and software implementation, sensitivity analysis formulation described in this work uses direct differentiation approach as opposed to the adjoint variable approach. The MIXEDMODELS capabilities are demonstrated through several numerical examples and the results indicate that the MIXEDMODELS formulation and architecture is effective in terms of accuracy, modeling convenience, computational efficiency, and the ability to simulate the behavior of a general class of multidisciplinary systems.

Cette thèse présente des travaux effectués dans le cadre de l'optimisation de forme de pièces mécaniques, sous critère dynamique, par approche isogéométrique. Pour réaliser une telle optimisation nous mettons en place dans un premier temps les éléments coque au travers des formulations Kirchhoff-Love puis Reissner-Minlin. Nous présentons une méthode permettant d'atteindre les vecteurs normaux aux fibres dans ces formulations au travers de l'utilisation d'une grille mixte de fonctions de base interpolantes, traditionnellement utilisées en éléments finis, et de fonction non interpolantes issues de la description isogéométrique des coques. Par la suite, nous détaillons une méthode pour le couplage de patch puis nous mettons en place la méthode de synthèse modale classique dans le cadre de structures en dynamique décrites par des éléments isogéometriques. Ce travail établit une base pour l'optimisation de forme sous critères dynamique de telles structures. Enfin, nous développons une méthode d'optimisation de forme basée sur le calcul du gradient de la fonction objectif envisagée. La sensibilité de conception est extraite de l'analyse de sensibilité au niveau même du maillage du modèle, qui est obtenue par l'analyse discrète de sensibilité. Des exemples d'application permettent de montrer la pertinence et l'exactitude des approches proposées. / Isogeometric method is a promising method in bridging the gap between the computer aided design and computer aided analysis. No information is lost when transferring the design model to the analysis model. It is a great advantage over the traditional finite element method, where the analysis model is only an approximation of the design model. It is advantageous for structural optimization, the optimal structure obtained will be a design model. In this thesis, the research is focused on the fast three dimensional free shape optimization with isogeometric shell elements. The related research, the development of isogeometric shell elements, the patch coupling in isogeometric analysis, the modal synthesis with isogeometric elements are also studied. We proposed a series of mixed grid Reissner-Minlin shell formulations. It adopts both the interpolatory basis functions, which are from the traditional FEM, and the non-interpolatory basis functions, which are from IGA, to approximate the unknown elds. It gives a natural way to define the fiber vectors in IGA Reissner-Mindlin shell formulations, where the non-interpolatory nature of IGA basis functions causes complexity. It is also advantageous for applying the rotational boundary conditions. A modified reduce quadrature scheme was also proposed to improve the quadrature eficiency, at the same time, relieve the locking in the shell formulations. We gave a method for patch coupling in isogeometric analysis. It is used to connect the adjacent patches. The classical modal synthesis method, the fixed interface Craig-Bampton method, is also used as well as the isogeometric Kirchhoff-Love shell elements. The key problem is also the connection between adjacent patches. The modal synthesis method can largely reduce the time costs in analysis concerning structural dynamics. This part of work lays a foundation for the fast shape optimization of built-up structures, where the design variables are only relevant to certain substructures. We developed a fast shape optimization framework for three dimensional thin wall structure design. The thin wall structure is modelled with isogeometric Kirchhoff-Love shell elements. The analytical sensitivity analysis is the key focus, since the gradient base optimization is normally more fast. There are two models in most optimization problem, the design model and the analysis model. The design variables are defined in the design model, however the analytical sensitivity is normally obtained from the analysis model. Although it is possible to use the same model in analysis and design under isogeomeric framework, it might give either a highly distorted optimum structure or a unreliable structural response. We developed a sensitivity mapping scheme to resolve this problem. The design sensitivity is extracted from the analysis model mesh level sensitivity, which is obtained by the discrete analytical sensitivity analysis. It provides exibility for the design variable definition. The correctness of structure response is also ensured. The modal synthesis method is also used to further improve the optimization eficiency for the built-up structure optimization concerning structural dynamics criteria.