Invention Grant
- Patent Title: Gas turbine engine combustor with tailored temperature profile
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Application No.: US13725137Application Date: 2012-12-21
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Publication No.: US10260748B2Publication Date: 2019-04-16
- Inventor: Timothy S. Snyder , Randal G. McKinney , James B. Hoke
- 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: O'Shea Getz P.C.
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/12 ; F02C7/236 ; F23R3/28 ; F23R3/26 ; F23R3/06
Abstract:
A method of tailoring a combustor flow for a gas turbine engine includes controlling an airflow into a swirler to be generally uniform and controlling an airflow into a quench zone to provide a desired pattern factor.
Public/Granted literature
- US20140338351A1 GAS TURBINE ENGINE COMBUSTOR WITH TAILORED TEMPERATURE PROFILE Public/Granted day:2014-11-20
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