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SWIRLER FOR A BURNER OF A GAS TURBINE ENGINE, BURNER OF A GAS TURBINE ENGINE AND GAS TURBINE ENGINE
SWIRLER FOR A BURNER OF A GAS TURBINE ENGINE, BURNER OF A GAS TURBINE ENGINE AND GAS TURBINE ENGINE
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机译:燃气轮机燃烧器的旋流器,燃气轮机燃烧器和燃气轮机的旋流器
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摘要
The present invention is related to a Swirler (50) for a burner (30) of a gas turbine engine (10), comprising a plurality of vanes (54) extending from an outer radius (64) of the swirler (50) to an inner radius (62) of the swirler (50) and a plurality of mixing channels (56) between the vanes (54) to channel air (24) from a radially outer end (58) of the mixing channel (56), located essentially at an outer radius (64) of the swirler (50), to a radially inner end (60) of the mixing channel (56), located essentially at an inner radius (62) of the swirler (50), at least one main injection means (52) for providing fuel for a main flame of the gas turbine engine (10), the main injection means (52) arranged at and/or in at least one of the mixing channels (56), and at least one pilot injection means (70) for providing fuel for a pilot flame of the gas turbine engine (10). Further, the invention is related to a burner (30) of a gas turbine engine (10) and to a gas turbine engine (10).
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