Invention Grant
- Patent Title: Turbine rotor blade assembly
-
Application No.: US16082874Application Date: 2017-03-06
-
Publication No.: US10781700B2Publication Date: 2020-09-22
- Inventor: Nobuyori Yagi , Naoyuki Nagai , Shin Yanagisawa , Yuki Nakamura
- Applicant: MITSUBISHI HEAVY INDUSTRIES COMPRESSOR CORPORATION
- Applicant Address: JP Tokyo
- Assignee: MITSUBISHI HEAVY INDUSTRIES COMPRESSOR CORPORATION
- Current Assignee: MITSUBISHI HEAVY INDUSTRIES COMPRESSOR CORPORATION
- Current Assignee Address: JP Tokyo
- Agency: Osha Liang LLP
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@532105b6
- International Application: PCT/JP2017/008847 WO 20170306
- International Announcement: WO2017/154852 WO 20170914
- Main IPC: F01D5/22
- IPC: F01D5/22 ; F01D5/16 ; F01D5/20 ; F01D5/30

Abstract:
In a turbine rotor blade assembly 1 of the present invention, each turbine rotor blade 10 includes a platform 11 having a blade root 12 fixed to a turbine disk 30, a profile 13 rising from the platform 11, and a shroud 14 provided at a top end of the profile 13. The shroud 14 of the present invention includes a first contact end part 15 that comes into contact with an adjacent shroud adjacent to one end side in a circumferential direction, a second contact end part 16 that comes into contact with an another adjacent shroud adjacent to the other end side in the circumferential direction, and a main body part disposed between the first and second contact end parts 15 and 16. One or both of the first and second contact end parts 15 and 16 are lower in rigidity than the main body part.
Public/Granted literature
- US20190078447A1 TURBINE ROTOR BLADE ASSEMBLY Public/Granted day:2019-03-14
Information query