Abstract—A single-crystal silicon micromachined air turbine supported on gas-lubricated bearings has been operated in a controlled and sustained manner at rotational speeds greater than 1 million revolutions per minute, with mechanical power levels approaching 5 W. The device is formed from a fusion bonded stack of five silicon wafers individually patterned on both sides using deep reactive ion etching (DRIE). It consists of a single stage radial inflow turbine on a 4.2-mm diameter rotor that is supported on externally pressurized hydrostatic journal and thrust bearings. This paper presents the design, fabrication, and testing of the first microfabricated rotors to operate at circumferential tip speeds up to 300 m/s, on the order of convent...
This dissertation presents the development of an integrated electromagnetic micro-turbo-generator su...
International audienceThis paper presents the experimental demonstration and characterization of a M...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.In...
As part of progress in developing a micro gas turbine engine, this paper presents the design, fabric...
As part of progress in developing a micro gas turbine engine, this paper presents the design, fabric...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1999.Include...
Micromachines rotating at high speeds require low drag bearings with adequate load capacity and stab...
We report here new and further developments into the MicroBearing device for the MIT Microengine Pro...
Design considerations for lubrication in high speed rotating MEMS devices are discussed, using the M...
Abstract: This paper presents the design, fabrication, and testing of a fully-integrated permanent-m...
MIT is developing micro-electro-mechanical systems (MEMS)-based gas turbine engines, turbogenerators...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004....
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006....
This paper presents the design, fabrication, and testing of an integrated microturbogenerator utiliz...
This paper introduces and experimentally demonstrates the design concept of multistage microturbomac...
This dissertation presents the development of an integrated electromagnetic micro-turbo-generator su...
International audienceThis paper presents the experimental demonstration and characterization of a M...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.In...
As part of progress in developing a micro gas turbine engine, this paper presents the design, fabric...
As part of progress in developing a micro gas turbine engine, this paper presents the design, fabric...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1999.Include...
Micromachines rotating at high speeds require low drag bearings with adequate load capacity and stab...
We report here new and further developments into the MicroBearing device for the MIT Microengine Pro...
Design considerations for lubrication in high speed rotating MEMS devices are discussed, using the M...
Abstract: This paper presents the design, fabrication, and testing of a fully-integrated permanent-m...
MIT is developing micro-electro-mechanical systems (MEMS)-based gas turbine engines, turbogenerators...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004....
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006....
This paper presents the design, fabrication, and testing of an integrated microturbogenerator utiliz...
This paper introduces and experimentally demonstrates the design concept of multistage microturbomac...
This dissertation presents the development of an integrated electromagnetic micro-turbo-generator su...
International audienceThis paper presents the experimental demonstration and characterization of a M...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.In...