Invention Grant
- Patent Title: Rotor disk assembly for gas turbine
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Application No.: US16148068Application Date: 2018-10-01
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Publication No.: US11280207B2Publication Date: 2022-03-22
- Inventor: Victor Shemyatovskiy , Ja Won Seo , Young Seok Heo
- Applicant: DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD.
- Applicant Address: KR Changwon-si
- Assignee: DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD.
- Current Assignee: DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD.
- Current Assignee Address: KR Changwon-si
- Agency: Harvest IP Law, LLP
- Priority: KR10-2017-0133238 20171013
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F04D29/32 ; F01D5/06 ; F01D5/02 ; F01D5/22

Abstract:
A rotor disk assembly for a gas turbine maintains a sealing capability even though adjacent labyrinth arms are dislocated from each other due to torsion or similar relative movement by thermal expansion or by rotation of the rotor disks of the gas turbine. The rotor disk assembly includes a plurality of rotor disks axially assembled to each other, the plurality of rotor disks including adjacent rotor disks coupled to each other by Hirth parts. Each rotor disk includes two labyrinth arms that extend axially and bilaterally and are located on the rotor disk more radially outward than the Hirth parts, and a first labyrinth arm of the two labyrinth arms having an end surface in which a receiving groove for receiving a seal ring is formed.
Public/Granted literature
- US20190112938A1 ROTOR DISK ASSEMBLY FOR GAS TURBINE Public/Granted day:2019-04-18
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