Invention Grant
- Patent Title: Cooling insert for a turbomachine
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Application No.: US17007076Application Date: 2020-08-31
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Publication No.: US11460191B2Publication Date: 2022-10-04
- Inventor: Jonathan Dwight Berry , Michael John Hughes
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, P.A.
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/26

Abstract:
Integrated combustor nozzles and turbomachines are provided. An integrated combustor nozzle includes a cooling insert having a flange. The cooling insert further includes a first wall and a second wall that each define respective passages therein. The first wall and the second wall each extend from an open end defined within the flange to a closed end. The first wall and the second wall each include an impingement side spaced apart from a solid side. Each impingement side defines a plurality of impingement apertures configured to direct coolant from the respective passage towards a side wall of the combustion liner. The cooling inserts further includes a collection passageway that is defined between the solid sides of the first wall and the second wall.
Public/Granted literature
- US20220065454A1 COOLING INSERT FOR A TURBOMACHINE Public/Granted day:2022-03-03
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