Invention Grant
US08671692B2 Annular gas turbine combustor including converging and diverging segments
有权
环形燃气轮机燃烧器,包括会聚和发散段
- Patent Title: Annular gas turbine combustor including converging and diverging segments
- Patent Title (中): 环形燃气轮机燃烧器,包括会聚和发散段
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Application No.: US13251586Application Date: 2011-10-03
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Publication No.: US08671692B2Publication Date: 2014-03-18
- Inventor: Steven W. Burd , William Sowa , Albert K. Cheung , Stephen Karl Kramer , Reid Dyer Curtis Smith , James Hoke
- Applicant: Steven W. Burd , William Sowa , Albert K. Cheung , Stephen Karl Kramer , Reid Dyer Curtis Smith , James Hoke
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F02G3/00

Abstract:
A combustor assembly includes a convergent segment followed by a divergent segment to advantageously improve combustion. The combustor assembly includes a first segment beginning at a forward end that transitions to a second segment past a transition segment in a direction along a combustor axis toward an aft end. The reduction in cross-sectional area within the first segment provides desirable fuel and air mixing properties. The convergent first segment in combination with the divergent second segment decreases residence time of fuel-air mixture within the combustor chamber that decreases production of undesirable emissions from the combustor assembly.
Public/Granted literature
- US20120017599A1 ANNULAR GAS TURBINE COMBUSTOR Public/Granted day:2012-01-26
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