Invention Grant
- Patent Title: Cooling method and structure of vane of gas turbine
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Application No.: US17692572Application Date: 2022-03-11
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Publication No.: US11982206B2Publication Date: 2024-05-14
- Inventor: Satoshi Mizukami , David Allen Flodman , Satoshi Hada
- 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: WHDA, LLP
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D9/04

Abstract:
A method of cooling a vane of a turbine is provided. The turbine includes an airfoil, an outer shroud disposed at an outer radial end of the airfoil and an inner shroud, the airfoil including a plurality of air channels extending along the radial direction of the turbine, the air channels comprising a first air channel and a second air channel. A cooling air is caused to flow inside the first air channel to cool the first air channel, then cool one of the outer shroud and the inner shroud. A cooling air is caused to flow inside the second air channel to cool the second air channel, then cool the other one of the outer shroud and the inner shroud.
Public/Granted literature
- US20230287796A1 COOLING METHOD AND STRUCTURE OF VANE OF GAS TURBINE Public/Granted day:2023-09-14
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