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:
Oct. 20, 2020

Filed:

Jul. 27, 2016
Applicant:

Honda Motor Co., Ltd., Tokyo, JP;

Inventors:

Yasuharu Kamoi, Wako, JP;

Koji Murata, Wako, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/10 (2006.01); F23R 3/50 (2006.01); F23R 3/60 (2006.01); F23R 3/28 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F23R 3/10 (2013.01); F23R 3/286 (2013.01); F23R 3/50 (2013.01); F23R 3/60 (2013.01); F23R 2900/03042 (2013.01);
Abstract

Formed in a wall part of a dome part of an annular combustor encircling an axis of a gas turbine engine are multiple fuel supply holes spaced at predetermined intervals in circumferential direction around the axis and many cooling holes extending through the wall part in direction inclined to a normal thereof. When two adjacent fuel supply holes are defined as first and second fuel supply holes, a virtual boundary line contacting an outer semi-circular portion, far from the axis, of the first fuel supply hole and an inner semi-circular portion, close to the axis, of the second fuel supply hole is set. The first cooling holes in region radially outward, relative to the axis, of the line are inclined toward the second fuel supply hole, and the second cooling holes in region radially inward, relative to the axis, of the line are inclined toward the first fuel supply hole.


Find Patent Forward Citations

Kamoi, Yasuharu. (2020). Structure for cooling gas turbine engine (U.S. Patent No. 10808929). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10808929

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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