Micro Turbine Technology, Bv

Eclipse Combustion, Inc.

Winnox Combustion Systems, B.v.

Gustaaf Jan Witteveen

Arij Iza??k Van Berkel

Robert Johan Maria Bastiaans

Willibald Mattheus Petrus Ahout

When the compressor is a multistage compressor, each compression space includes an inlet arranged in the vicinity of the center axis and an outlet arranged in the vicinity of the outer circumference of the turbine wheel, and there is a connecting conduit between the outlet of a first compressor stage and the inlet of a second compressor stage. The connecting conduit is delimited by a first wall of the space of the first compressor stage and a second wall of the space of the second compressor stage. Each wall can be a friction disk.

Micro reaction turbine with integrated combustion chamber and rotor

A mixing device and a combustor provided with such a device. The mixing device includes tangentially oblique passages for combustion air. Fuel gas is admitted into the passages with a light fuel preferably at the outer side of the passages. Further, the mixing device contains a tapered down portion ending in a sharp edge after which a considerably broader combustion chamber is present.

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Molenhoek, Netherlands

Gustaaf Jan Witteveen