Invention Grant
- Patent Title: Burner for a gas turbine engine
- Patent Title (中): 燃气轮机的燃烧器
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Application No.: US12768078Application Date: 2010-04-27
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Publication No.: US08739545B2Publication Date: 2014-06-03
- Inventor: Andrew Cant , Paul Headland , Daniel Leggett
- Applicant: Andrew Cant , Paul Headland , Daniel Leggett
- Applicant Address: DE München
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE München
- Priority: EP09159093 20090429
- Main IPC: F02C7/22
- IPC: F02C7/22

Abstract:
A burner for a gas turbine engine is provided. The burner includes a radial swirler for creating a swirling fuel/air mix, a combustion chamber where combustion of the swirling fuel/air mix occurs, and a pre-chamber located between the radial swirler and the combustion chamber. The radial swirler includes a plurality of vanes arranged in a circle, generally radially inwardly extending flow slots are defined between adjacent vanes in the circle, each flow slot includes a radially outer inlet end, a radially inner outlet end, first and second generally radially inwardly extending sides provided by adjacent vanes, and a base and top. A flow slot includes a first gas fuel injection hole in its base and a flow slot includes a second gas fuel injection hole in its first side wherein the amounts of gas fuel injected via the first and second gas fuel injection holes are independently variable.
Public/Granted literature
- US20100275602A1 BURNER FOR A GAS TURBINE ENGINE Public/Granted day:2010-11-04
Information query
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