Invention Grant
- Patent Title: Gas turbine rotor, gas turbine, and gas turbine equipment
-
Application No.: US15768709Application Date: 2016-10-21
-
Publication No.: US10738618B2Publication Date: 2020-08-11
- Inventor: Shinya Hashimoto , Keita Takamura
- Applicant: Mitsubishi Hitachi Power Systems, Ltd.
- Applicant Address: JP Kanagawa
- Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee Address: JP Kanagawa
- Agency: Wenderoth, Lind & Ponack, L.L.P.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@9f34cc4
- International Application: PCT/JP2016/081299 WO 20161021
- International Announcement: WO2017/069249 WO 20170427
- Main IPC: F01D5/08
- IPC: F01D5/08 ; F02C7/18 ; F02C3/073 ; F04D29/053 ; F04D29/58 ; F02C6/08 ; F04D29/32

Abstract:
A ventilation flow path, a cooling air flow path, a mixing space, and a mixed air flow path are formed in a gas turbine rotor. The ventilation flow path guides compressed air farther on an axially upstream side than an air discharge port of a compressor to an interior of a compressor rotor as compressor extracted air. The cooling air flow path guides cooling air to a part farther on an axially downstream side than the air discharge port. The compressor extracted air and the cooling air are mixed in the mixing space. The mixed air flow path guides mixed air containing the compressor extracted air and the cooling air into a turbine rotor.
Public/Granted literature
- US20190063224A1 GAS TURBINE ROTOR, GAS TURBINE, AND GAS TURBINE EQUIPMENT Public/Granted day:2019-02-28
Information query