Rotor for a turbine or a compressor or a turbine/compressor geometry
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United States of America Patent
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Oct 31, 2017
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N/A
app pub date -
Jan 15, 2015
filing date -
Jan 16, 2014
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Abstract
A rotor for at least one of a turbine and a compressor of a supercharging device may include a shaft defining an axis of rotation and at least one impeller. The at least one impeller may have a thread which is arranged coaxially to the axis of rotation. The shaft may include a complementary thread which is arranged coaxially to the axis of rotation. The shaft and the at least one impeller may be secured together via the respective threads. The shaft and the at least one impeller may be fixed with respect to one another via at least one of a soldered connection, a welded connection, an adhesive bond, a clamped connection and a crystallization connection.
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