The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 13, 2021

Filed:

Aug. 22, 2016
Applicant:

Mitsubishi Heavy Industries, Ltd., Tokyo, JP;

Inventors:

Hideaki Kaneko, Tokyo, JP;

Kenji Yamamoto, Tokyo, JP;

Takanori Karato, Tokyo, JP;

Norifumi Hirata, Kanagawa, JP;

Naoya Fujita, Kanagawa, JP;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B22D 27/04 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); C22F 1/10 (2006.01); F01D 25/00 (2006.01); C21D 9/00 (2006.01); G06F 30/17 (2020.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B22D 27/04 (2013.01); B22D 27/045 (2013.01); C21D 9/00 (2013.01); C22F 1/10 (2013.01); F01D 5/28 (2013.01); F01D 25/00 (2013.01); G06F 30/17 (2020.01); F05D 2240/301 (2013.01);
Abstract

A turbine blade designing method is for designing a turbine blade formed using a metal material in which creep including diffusion creep and dislocation creep occurs by heating. The turbine blade designing method includes: acquiring temperature distribution data relating to temperature distribution in the turbine blade to be heated; acquiring creep strength distribution data relating to distribution of the creep strength required for the turbine blade to be heated; from the correlation data, based on the temperature distribution data and the creep strength distribution data, setting the crystal grain size of a high-temperature portion that is the diffusion creep temperature range of the turbine blade to a size coarser than the reference crystal grain size, and setting the crystal grain size of a low-temperature portion that is the dislocation creep temperature range of the turbine blade to a size finer than the reference crystal grain size.


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