Invention Grant
- Patent Title: Gas turbine combustor with variable airflow
- Patent Title (中): 具有可变气流的燃气轮机燃烧器
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Application No.: US12696311Application Date: 2010-01-29
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Publication No.: US08966877B2Publication Date: 2015-03-03
- Inventor: Randal G. McKinney
- Applicant: Randal G. McKinney
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Miller, Matthias & Hull LLP
- Main IPC: F02C7/057
- IPC: F02C7/057 ; F23R3/06 ; F23R3/10

Abstract:
An annular combustor and a method for operating a gas turbine engine over a power demand range facilitate combustion in a lean direct ignition (LDI) mode over an extended range of operating fuel air ratios. The flow primary combustion air admitted into the primary combustion zone is varied in response to power demand from a maximum air flow rate of high power demand to a minimum flow air rate of low power demand, while the flow of dilution air into a quench zone downstream of the primary combustion zone is increased from a minimum air flow rate at high power demand to a maximum air flow rate at low power demand.
Public/Granted literature
- US20110185736A1 GAS TURBINE COMBUSTOR WITH VARIABLE AIRFLOW Public/Granted day:2011-08-04
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