Invention Grant
- Patent Title: Sequential liner for a gas turbine combustor
-
Application No.: US15050161Application Date: 2016-02-22
-
Publication No.: US10253985B2Publication Date: 2019-04-09
- Inventor: Michael Thomas Maurer , Jeffrey De Jonge , Felix Baumgartner , Patrik Meng
- Applicant: General Electric Technology GmbH
- Applicant Address: CH Baden
- Assignee: ANSALDO ENERGIA SWITZERLAND AG
- Current Assignee: ANSALDO ENERGIA SWITZERLAND AG
- Current Assignee Address: CH Baden
- Agency: Buchanan Ingersoll & Rooney PC
- Priority: EP15157730 20150305
- Main IPC: F23R3/04
- IPC: F23R3/04 ; F01P7/02 ; F23R3/00

Abstract:
The invention concerns a sequential liner for a gas turbine combustor, having a sequential liner outer wall spaced apart from a sequential liner inner wall to define a sequential liner cooling channel between the sequential liner outer wall and the sequential liner inner wall. The sequential liner outer wall includes a first face, a first adjacent face and a second adjacent face, the first and second adjacent faces each being adjacent to the first face, the first face of the sequential liner outer wall having a first convective cooling hole adjacent to the first adjacent face and a second convective cooling hole adjacent to the second adjacent face, each convective cooling hole being arranged to direct a convective cooling flow into the sequential liner cooling channel adjacent to each adjacent face. The invention also concerns a method of cooling using the sequential liner and a method of retrofitting a gas turbine.
Public/Granted literature
- US20160258625A1 SEQUENTIAL LINER FOR A GAS TURBINE COMBUSTOR Public/Granted day:2016-09-08
Information query