公开(公告)号：US11913383B2

公开(公告)日：2024-02-27

申请号：US17615895

申请日：2020-06-12

申请人： Mitsubishi Power, Ltd.

发明人： Yoshifumi Okajima ,  Masahiko Mega ,  Taiji Torigoe ,  Atsushi Moriwaki ,  Hiroshi Makigano ,  Koichi Tanimoto

IPC分类号： F02C7/24 ,  C23C4/073 ,  C23C4/134 ,  G01N25/18 ,  F01D5/28 ,  F01D17/08 ,  F01D21/00

CPC分类号： F02C7/24 ,  C23C4/073 ,  C23C4/134 ,  F01D5/288 ,  F01D17/085 ,  F01D21/003 ,  G01N25/18 ,  F05D2220/32 ,  F05D2230/312 ,  F05D2230/90 ,  F05D2260/231 ,  F05D2270/80 ,  F05D2300/2118 ,  F05D2300/514 ,  F05D2300/611

摘要： The present invention provides a thermal barrier coated component, monitoring or evaluation of the soundness of which is able to be adequately carried out on the basis of the thermal boundary conditions that are detected by a sensor. A thermal barrier coated component according to the present invention comprises: a base material; a first bond coat layer that is a metal bonding layer formed on the base material; a sensor unit that comprises a sensor and a conductive wire, which are formed on the first bond coat layer; a second bond coat layer that is formed on the first bond coat layer so as to cover at least the sensor unit, while having a surface roughness higher than that of the first bond coat layer; and a top coat layer that is formed on the second bond coat layer.

公开(公告)号：US11834962B2

公开(公告)日：2023-12-05

申请号：US17439273

申请日：2020-04-08

申请人： Mitsubishi Power, Ltd.

发明人： Satoshi Hada ,  Yoshifumi Okajima ,  Kunihiko Waki

IPC分类号： F01D5/18 ,  F01D9/02 ,  F01D9/04 ,  F02C7/18

CPC分类号： F01D5/187 ,  F01D9/023 ,  F01D9/041 ,  F02C7/18 ,  F05D2220/32 ,  F05D2240/81 ,  F05D2260/201 ,  F05D2260/202

摘要： A turbine stator vane includes; an airfoil portion; a shroud disposed on at least one of the side of a tip end portion or the side of a root end portion of the airfoil portion; and a protruding portion protruding toward the opposite side to the airfoil portion across a gas path surface in a radial direction. The shroud includes: a circumferential-direction passage disposed at the side of a trailing edge and extending in a circumferential direction; and a plurality of trailing edge end portion passages arranged in the circumferential direction at the side of the trailing edge, each trailing edge end portion passage having a first end portion connected to the circumferential-direction passage and a second end portion having an opening on a trailing edge end surface of the shroud. The circumferential-direction passage includes, in a cross-sectional view as seen in the circumferential direction, an oblique passage having a third end portion to protrude closer to the gas path surface toward the side of a leading edge, and a fourth end portion formed at the side of the trailing edge with respect to the third end portion, the oblique passage having an opening portion disposed on a trailing-edge side end surface of the protruding portion and closed by a lid portion, and a position, in an axial direction, of the first end portion where each trailing edge end portion passage connects to the circumferential-direction passage is positioned at the side of the leading edge with respect to a position of the trailing-edge side end surface of the protruding portion at a position where the protruding portion connects to the shroud.

公开(公告)号：US11946389B2

公开(公告)日：2024-04-02

申请号：US17431827

申请日：2020-02-18

申请人： Mitsubishi Power Ltd.

发明人： Yoshifumi Okajima ,  Masahiko Mega ,  Taiji Torigoe

IPC分类号： F01D5/28

CPC分类号： F01D5/288 ,  F05D2230/90 ,  F05D2300/611

摘要： A turbine rotor blade includes a blade body and a tip shroud on a tip of the blade body. The tip shroud has a contact block configured to face a tip shroud of an adjacent turbine rotor blade, and the contact block includes a base material, an oxidation resistant coating on the surface of the base material, and a hard wear resistant coating on the surface of the oxidation resistant coating.