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:
Sep. 07, 2021

Filed:

Dec. 26, 2018
Applicant:

Mitsubishi Heavy Industries Aero Engines, Ltd., Komaki, JP;

Inventors:

Daigo Fujimura, Tokyo, JP;

Hiroshi Watanabe, Tokyo, JP;

Tadayuki Hanada, Komaki, JP;

Takaaki Hase, Komaki, JP;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); B64D 27/10 (2006.01); F01D 5/02 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); B64D 27/10 (2013.01); F01D 5/02 (2013.01); F01D 9/02 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2240/24 (2013.01);
Abstract

A gas turbine for an aircraft includes: blades each including a blade body extending outward from a rotor rotating about an axis in a radial direction of the rotor and a fin protruding from an outer peripheral surface of a blade shroud formed on a distal end of the blade body; a casing installed to form gaps between the casing and the fins; and vanes each including a vane shroud formed such that at least a leading end portion of the vane shroud formed upstream in an axial direction is located outside with respect to an extended line of an inner peripheral surface of the casing in the radial direction.


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