Invention Grant
- Patent Title: Combustion turbine vane cooling system
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Application No.: US16741609Application Date: 2020-01-13
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Publication No.: US11225873B2Publication Date: 2022-01-18
- Inventor: Eric Koenig , Brett Barker
- Applicant: Rolls-Royce Corporation
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Crowell & Moring LLP
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
A system includes an air foil positionable in a combustion flow path of a combustion turbine. A shank may be integrally formed with the air foil, and the platform may be integrally formed with the shank. The platform includes linear fluid passageways, access ducts penetrating a wedge face surface of the platform, and outlet apertures formed in a radially outward surface of the platform. The outlet apertures are in fluid communication with respective linear fluid passageways such that fluid flowing through the respective linear fluid passageways is discharged from the outlet apertures into the combustion flow path. The platform also includes plugs is disposed in respective access ducts to form a fluid tight seal and be positioned in at least one of the respective linear fluid passageways. Fluid flowing through the respective linear fluid passageways flows away from a respective plug for discharge from a respective outlet aperture.
Public/Granted literature
- US20210215051A1 COMBUSTION TURBINE VANE COOLING SYSTEM Public/Granted day:2021-07-15
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