Invention Grant
- Patent Title: Thermal barrier coating, turbine member, gas turbine, and method for producing thermal barrier coating
-
Application No.: US16979971Application Date: 2019-02-06
-
Publication No.: US11946147B2Publication Date: 2024-04-02
- Inventor: Taiji Torigoe , Yoshifumi Okajima , Daisuke Kudo , Masahiko Mega , Shuji Tanigawa
- Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Applicant Address: JP Tokyo
- Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Current Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Current Assignee Address: JP Tokyo
- Agency: Wenderoth, Lind & Ponack, L.L.P.
- Priority: JP 18057716 2018.03.26
- International Application: PCT/JP2019/004158 2019.02.06
- International Announcement: WO2019/187663A 2019.10.03
- Date entered country: 2020-09-11
- Main IPC: F01D5/28
- IPC: F01D5/28 ; B32B15/04 ; C23C4/02 ; C23C4/04 ; C23C4/134 ; C23C28/00 ; F01D1/00 ; F01D25/00 ; F02C7/00

Abstract:
A thermal barrier coating includes a bond coat layer deposited on a substrate, and a ceramic layer deposited on the bond coat layer. The ceramic layer includes a first layer having a porosity of 10% or more and 15% or less, and a second layer having a porosity of 0.5% or more and 9.0% or less and deposited on the first layer.
Public/Granted literature
- US20210054492A1 THERMAL BARRIER COATING, TURBINE MEMBER, GAS TURBINE, AND METHOD FOR PRODUCING THERMAL BARRIER COATING Public/Granted day:2021-02-25
Information query