Invention Grant
- Patent Title: Combustor hole arrangement for gas turbine engine
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Application No.: US14826463Application Date: 2015-08-14
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Publication No.: US10514169B2Publication Date: 2019-12-24
- Inventor: Albert K. Cheung , Christos Adamopoulos
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/00 ; F23R3/50
Abstract:
A combustor liner for a gas turbine is provided. The combustor liner comprises a wall and a plurality of airflow injection holes in the wall arranged in a circumferentially-extending row, the plurality of airflow injection holes including a plurality of circular first airflow injection holes and at least one non-circular second airflow injection hole.
Public/Granted literature
- US10670267B2 Combustor hole arrangement for gas turbine engine Public/Granted day:2020-06-02
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