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.
Patent No.:
Date of Patent:
Jun. 17, 2025
Filed:
Oct. 15, 2021
Mitsubishi Heavy Industries, Ltd., Tokyo, JP;
MITSUBISHI HEAVY INDUSTRIES, LTD., Tokyo, JP;
Abstract
A turbine stationary blade is a turbine stationary blade that includes: a blade body; and a shroud formed in an end portion of the blade body in a blade height direction. The shroud includes: a bottom plate in contact with a combustion gas flow passage; a peripheral wall formed in the blade height direction and along a peripheral edge of the bottom plate; a recess forming a space surrounded by the peripheral wall and the bottom plate; a plurality of partition ribs connecting the blade body and the peripheral wall, dividing the recess into a plurality of spaces, and forming a plurality of cavities; and an impingement plate dividing the space into an outer cavity formed on an outer side in the blade height direction and an inner cavity formed on an inner side of the outer cavity, and having a plurality of through holes via which the outer cavity and the inner cavity communicate with each other. The peripheral wall includes: a leading edge end portion extending to a leading edge side of the blade body; a suction side end portion extending from a leading edge to a trailing edge on a suction side of the blade body, and internally including a suction side passage; a pressure side end portion extending from a leading edge to a trailing edge on a pressure side of the blade body, and internally including a pressure side passage; and a trailing edge end portion extending to a trailing edge side of the blade body. The plurality of cavities are formed from the inner cavity, and include: a first cavity disposed on a leading edge pressure side so as to surround a circumference of the blade body between the blade body and the peripheral wall, connected to the cooling hole formed in the bottom plate, and connected to the pressure side passage; and a second cavity disposed adjacent to an axially downstream side of the first cavity, disposed on a most axially upstream side of the pressure side among the partition ribs, disposed via a first partition rib connecting the pressure side end portion and the pressure surface of the blade body, and having a plurality of cooling holes in the bottom plate. An opening density of the through holes of the impingement plate in the second cavity is lower than the opening density of the through holes of the impingement plate in the first cavity.