A miniature gas turbine is under development with the aim of generating electrical energy from fuel. This system consists of a compressor, combustion chamber, turbine and generator. The turbine is a single-stage axial impulse turbine (Laval turbine) with a rotor diameter of 10 mm, made of stainless steel using die-sinking electro-discharge machining. It has been tested with compressed air to speeds up to 160 000 rpm and generates a maximum mechanical power of 28 W with an efficiency of 18.4%. When coupled to a small generator, it generates 16 W of electrical power, which corresponds to an efficiency for the total system of 10.5%. The power density is mainly limited by the maximal speed of the ball bearings. The main losses are the blade pro...
A single-stage axial microturbine has been developed with a rotor diameter of 10 mm. This turbine is...
In the operation of a mini-jet engine, the turbine plays a critical role of driving the compressor. ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004....
A miniature gas turbine is under development with the aim of generating electrical energy from fuel....
Summary: A miniature gas turbine is under development with the aim to generate electrical energy fro...
A new small gas turbine technology is being developed which promises to bring the economic,environme...
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...
A single-stage axial microturbine has been developed with a rotor diameter of 10 mm. This turbine is...
The advancement in the design and prototype testing of an ultra-micro gas turbine set for portable e...
A new small gas turbine technology is being developed which promises to bring the economic, environm...
Micro turbines are becoming widely used for combined power generation and heat applications. Their s...
A new small gas turbine technology is being developed which promises to bring the economic, environm...
The current means of energy distribution relies heavily upon a single power generation station, whos...
A compact, high power-density turbo-generator system was conceived, designed and experimentally test...
A single-stage axial microturbine has been developed with a rotor diameter of 10 mm. This turbine is...
In the operation of a mini-jet engine, the turbine plays a critical role of driving the compressor. ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004....
A miniature gas turbine is under development with the aim of generating electrical energy from fuel....
Summary: A miniature gas turbine is under development with the aim to generate electrical energy fro...
A new small gas turbine technology is being developed which promises to bring the economic,environme...
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...
A single-stage axial microturbine has been developed with a rotor diameter of 10 mm. This turbine is...
The advancement in the design and prototype testing of an ultra-micro gas turbine set for portable e...
A new small gas turbine technology is being developed which promises to bring the economic, environm...
Micro turbines are becoming widely used for combined power generation and heat applications. Their s...
A new small gas turbine technology is being developed which promises to bring the economic, environm...
The current means of energy distribution relies heavily upon a single power generation station, whos...
A compact, high power-density turbo-generator system was conceived, designed and experimentally test...
A single-stage axial microturbine has been developed with a rotor diameter of 10 mm. This turbine is...
In the operation of a mini-jet engine, the turbine plays a critical role of driving the compressor. ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004....