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:
May. 03, 2005

Filed:

Jul. 10, 2002
Applicants:

Friedrich Soechting, Miami, FL (US);

Satoshi Hada, Takasago, JP;

Masamitsu Kuwabara, Takasago, JP;

Junichiro Masada, Takasago, JP;

Yasuoki Tomita, Takasago, JP;

Inventors:

Friedrich Soechting, Miami, FL (US);

Satoshi Hada, Takasago, JP;

Masamitsu Kuwabara, Takasago, JP;

Junichiro Masada, Takasago, JP;

Yasuoki Tomita, Takasago, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D011/00 ;
U.S. Cl.
CPC ...
Abstract

A stationary blade of a gas turbine, which can reduce thermal stress produced at a portion in the vicinity of a rear edge of an inner shroud of the stationary blade. The stationary blade is positioned adjacent to at least one of moving-blade disks in an axial direction of the gas turbine. A concave portion is provided in the inner shroud in a manner such that the concave portion is formed in the vicinity of a rear edge of the inner shroud and on an inner-peripheral face of the inner shroud, where cooling air passes along the inner-peripheral face which faces a rotation shaft of the moving-blade disks; and a protruding portion which protrudes towards the rotation shaft is formed at the rear edge of the inner shroud.


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