Turbine rotor and turbocharger having the turbine rotor

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9874100
APP PUB NO 20160003059A1
SERIAL NO

14766356

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A turbine rotor comprising: a turbine wheel 5 obtainable by precision casting of titanium aluminide, including a hub 50 extending along a rotational center of the turbine wheel, and a plurality of impellers 40 arranged along a circumferential direction around an outer circumference of the hub, and having a web-like scallop 30 formed by making a cutout between adjacent impellers among the plurality of the impellers; and a rotor shaft 7 extending along the rotational center line C-C of the turbine wheel on a back side of the hub of the turbine wheel; wherein the turbine wheel has a balance cut portion 11 arranged along the circumferential direction of the rotational turbine wheel on the back side of the hub of the turbine wheel, wherein an area of the balance correcting part arranged in the circumferential direction is placed so that a balance cut minimum diameter BCmin is larger than a maximum diameter of the rotor shaft on the wheel mounting side, and that a balance cut maximum diameter BCmax is smaller than a scallop diameter S of the turbine wheel, and that a thickness t from the back side of the turbine wheel to a surface of the hub satisfies 1.75t≧w, where w is a width in a radial direction of the area arranged in the circumferential direction (i.e. balance cut).

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Patent Owner(s)

Patent OwnerAddress
MITSUBISHI HEAVY INDUSTRIES LTD2-3 MARUNOUCHI 3-CHOME CHIYODA-KU TOKYO 100-8332

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Arai, Takashi Tokyo, JP 236 2194
Nakagawa, Hiroshi Tokyo, JP 252 3848
Otsubo, Hitomi Tokyo, JP 4 11
Yamaguchi, Hideki Tokyo, JP 112 2316
Yoshida, Masakazu Tokyo, JP 68 911

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