Lobe mixer for jet engine
AssigneeIshikwawjima-Harima Heavy Industries, Co. Ltd.
InventorTsutomu Oishi
Life of this patent
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Abstract
A lobe mixer (22) used in jet engines, is provided with diameter expansion portions (22a) in which the diameters gradually increase in the downstream direction, in which adjacent diameter expansion portions have different diameters from each other, and which guide the core gasses that flow along the inner sides of the adjacent diameter expansion portions, peripherally outwards at different angles. Thus, the gasses are mixed without the thrust of the jet engine being reduced, and the noise of the jet is reduced.
Claims2
A lobe mixer for jet engines, that mixes core gasses passing through a compressor, a combustor and a turbine and bypass gasses bypassing the compressor, the combustor, and the turbine,
- the lobe mixer comprising diameter expansion portions in which the diameters gradually increase in the downstream direction and the diameter expansion portions have different angles of slope in adjacent diameter expansion between each other.
A lobe mixer for jet engines, that mixes mixed gasses comprising core gasses passing through a compressor, a combustor and a turbine, and bypass gasses bypassing the compressor, the combustor, and the turbine, with air drawn into an exhaust nozzle from atmosphere,
- the lobe mixer comprising diameter expansion portions in which the diameters gradually increase in the downstream direction and the diameter expansion portions have different angles of slope in adjacent diameter expansion between each other.
Dependencies are inferred from the claim text.