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Combustion chamber for gas turbine engine has first and second turbulators for staged mixing of charge to combustion chamber
Combustion chamber for gas turbine engine has first and second turbulators for staged mixing of charge to combustion chamber
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机译:用于燃气涡轮发动机的燃烧室具有第一和第二湍流器,用于向燃烧室的装料阶段性混合
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摘要
The combustion chamber with staged premixing (120) mixes a forced air feed (150) from a compressor (110) and a fuel feed (170) from a supply (160). The intake has a first turbulator (180) for mixing the air and fuel feeds in a first charge flow (190). There is a second flow source (200) to produce a flow downstream of the first turbulator. There is a second turbulator (220) for mixing the first fuel-air flow and the second flow. Claims include a method of mixing the flows.
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