Radial turbine blade

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United States of America Patent

PATENT NO 9777578
SERIAL NO

14655296

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Abstract

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An object is to provide a radial turbine blade that can reduce an impact loss of inflowing gas at a leading edge of the turbine blade and achieve a higher turbine efficiency, even in a case of a flow field corresponding to a low turbine operational velocity ratio U/C0 due to a throttling operation on a variable nozzle mechanism of a variable geometry turbocharger.

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Patent Owner(s)

Patent OwnerAddress
MITSUBISHI HEAVY INDUSTRIES LTD2-3 MARUNOUCHI 3-CHOME CHIYODA-KU TOKYO 1008332 ?1008332

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Nagae, Satomi Tokyo, JP 4 44
Tojo, Masaki Tokyo, JP 15 122
Yokoyama, Takao Tokyo, JP 61 427

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