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. 14, 2021

Filed:

Dec. 08, 2017
Applicant:

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

Inventors:

Takaaki Hase, Aichi, JP;

Daigo Fujimura, Tokyo, JP;

Tadayuki Hanada, Aichi, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 9/02 (2006.01); F02C 7/00 (2006.01); F01D 9/04 (2006.01); F02C 3/073 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); F01D 9/023 (2013.01); F01D 9/04 (2013.01); F02C 3/073 (2013.01); F02C 7/00 (2013.01); F05D 2240/12 (2013.01); F05D 2250/311 (2013.01); F05D 2250/314 (2013.01);
Abstract

Provided is a transition duct that forms an annular gas flow channel through which a main flow gas flows from a high-pressure turbine to a low-pressure turbine, wherein the gas flow channel has an inner peripheral flow channel surface and an outer peripheral flow channel surface, the inner peripheral flow channel surface and the outer peripheral flow channel surface extend radially outward while angles of inclination relative to an axial direction of a rotating shaft change from the high-pressure turbine (first turbine) toward the low-pressure turbine (second turbine), and an inner peripheral maximum inclined part is provided in a range Athat extends in the axial direction from a position of alignment with an outer peripheral maximum inclined part to a position advanced toward the low-pressure turbine by a length no more than 20% of the duct length.


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