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:
Nov. 14, 2023

Filed:

Oct. 11, 2021
Applicant:

Ihi Corporation, Tokyo, JP;

Inventors:

Kensuke Shiomi, Tokyo, JP;

Kosuke Iwamoto, Tokyo, JP;

Teruyoshi Otoyo, Tokyo, JP;

Takashi Mori, Tokyo, JP;

Takaomi Inada, Tokyo, JP;

Assignee:

IHI CORPORATION, Tokyo, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 15/14 (2006.01); F01D 5/26 (2006.01); F01D 5/30 (2006.01); G01M 7/02 (2006.01);
U.S. Cl.
CPC ...
G01M 15/14 (2013.01); F01D 5/26 (2013.01); F01D 5/30 (2013.01); G01M 7/027 (2013.01);
Abstract

Provided is a jig for a vibration test of a rotor blade, for use in the vibration test for evaluating high cycle fatigue characteristics of the rotor blade for an aircraft engine, and the jig is provided with a jig body holding a dovetail portion of a fan blade and fixed onto an excitation table of a shaker, and a hydraulic jack that applies a load in a blade span direction to the fan blade to fix the fan blade to the jig body. Consequently, in the vibration test for evaluating the high cycle fatigue characteristics of the rotor blade, a test simulating an actual operation state can be carried out, the rotor blade can be efficiently excited to reach a large deformation region, and high cycle fatigue failure can occur without any increase in test cost.


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