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US Patent 12000304 Turbine blade and gas turbine

Patent 12000304 was granted and assigned to Mitsubishi Heavy Industries on June, 2024 by the United States Patent and Trademark Office.

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Is a
Patent
Patent
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Patent attributes

Patent Applicant
Mitsubishi Heavy Industries
Mitsubishi Heavy Industries
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Current Assignee
Mitsubishi Heavy Industries
Mitsubishi Heavy Industries
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
120003040
Patent Inventor Names
Yasuo Miyahisa0
Yusuke Izumi0
Shunsuke Torii0
Date of Patent
June 4, 2024
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Patent Application Number
181377630
Date Filed
April 21, 2023
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Patent Citations
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US Patent 8231350 Turbine rotor blade
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US Patent 7572102 Large tapered air cooled turbine blade
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US Patent 7645122 Turbine rotor blade with a nested parallel serpentine flow cooling circuit
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US Patent 7988417 Air cooled turbine blade
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US Patent 8628298 Turbine rotor blade with serpentine cooling
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Patent Primary Examiner
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John M Zaleskas
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CPC Code
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F05D 2250/185
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F05D 2260/22141
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F01D 5/187
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F05D 2240/127
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F05D 2260/2212
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Patent abstract

A turbine blade includes: a blade body; and a plurality of cooling passages each extending inside the blade body along a blade height direction and are connected to each other via return portions disposed at an end portion in the blade height direction to form a serpentine passage. The cooling passages include: an upstream passage disposed on an upstream side in a flow of a cooling fluid among the plurality of cooling passages; a downstream passage disposed on a downstream side in the flow of the cooling fluid among the plurality of cooling passages; and at least one intermediate passage disposed between the upstream passage and the downstream passage among the plurality of cooling passages. The upstream passage is disposed closest to a leading edge in a chord direction of the blade body among the plurality of cooling passages formed inside the blade body and extending along the height direction.

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