Microgas turbines are a widespread technology in cogenerative and propulsion applications. Bearings are a key factor in their design and development. The aim of the present research work is the development of the support system for a typical microturbine intended for power generation. To this goal, the present chapter defines the typical requirements of the machine and, afterward, describes the different technologies available to develop the support system of a reliable microturbine. Conventional (rolling element and oil-film) supports and cutting-edge (magnetic, aerodynamic, and aerostatic) bearings are reviewed. Particularly, their suitability to the operating conditions is compared by means of a literature review and elaboration of the r...
The problem of increase of the unit power on the shaft of an energy microturbine is of current inter...
Main energy conversion machinery used and to be used in cogeneration systems are schematically descr...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006....
Microgas turbines are a widespread technology in cogenerative and propulsion applications. Bearings ...
The design of the support system (shaft, bearings, and mechanical coupling devices) of the rotor pla...
Appraisal of the art. Technical Presentation to IFToMM Rotordynamics Conference, Seoul, Korea (Sept,...
This paper deals with the design and analysis of air bearing suitable for high speed micro gas turbi...
High-performance microturbines and turbochargers implement gas bearings in compact units of enhanced...
The design of a small turbo-generator to produce electricity in the range from a few kWs requires t...
This paper describes the development of a microgasturbine with a rotor diameter of 20 mm. The target...
Abstract: This paper describes the development of a microgasturbine with a rotor diameter of 20mm. T...
The article discusses results of the analyses of various bearing systems for the rotor of an ORC (Or...
Advances in the development of analysis and design methods for fluid-flow machines have enabled both...
Among all types of bearings, gas bearings are the most environmental friendly supports as they do no...
This paper describes the modelling of hybrid air bearings for small-scale turbomachinery. Stringent ...
The problem of increase of the unit power on the shaft of an energy microturbine is of current inter...
Main energy conversion machinery used and to be used in cogeneration systems are schematically descr...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006....
Microgas turbines are a widespread technology in cogenerative and propulsion applications. Bearings ...
The design of the support system (shaft, bearings, and mechanical coupling devices) of the rotor pla...
Appraisal of the art. Technical Presentation to IFToMM Rotordynamics Conference, Seoul, Korea (Sept,...
This paper deals with the design and analysis of air bearing suitable for high speed micro gas turbi...
High-performance microturbines and turbochargers implement gas bearings in compact units of enhanced...
The design of a small turbo-generator to produce electricity in the range from a few kWs requires t...
This paper describes the development of a microgasturbine with a rotor diameter of 20 mm. The target...
Abstract: This paper describes the development of a microgasturbine with a rotor diameter of 20mm. T...
The article discusses results of the analyses of various bearing systems for the rotor of an ORC (Or...
Advances in the development of analysis and design methods for fluid-flow machines have enabled both...
Among all types of bearings, gas bearings are the most environmental friendly supports as they do no...
This paper describes the modelling of hybrid air bearings for small-scale turbomachinery. Stringent ...
The problem of increase of the unit power on the shaft of an energy microturbine is of current inter...
Main energy conversion machinery used and to be used in cogeneration systems are schematically descr...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006....