Recirculation fan turbocharger assembly and fuel cell system
US-2024183308-A1 · Jun 6, 2024 · US
US2016160756A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016160756-A1 |
| Application number | US-201414904716-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 17, 2014 |
| Priority date | Jul 24, 2013 |
| Publication date | Jun 9, 2016 |
| Grant date | — |
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A turbocharger ( 1 ) with an axial flow turbine ( 2 ) includes a compressor stage ( 4 ) using active casing treatment ( 50 ) for choke flow improvement. With switchable slots ( 52, 54 ), one of the slots ( 52 ) may be between the compressors full and splitter blades ( 27, 23 ) and one of the slots ( 54 ) can be located downstream of the compressors splitter blades ( 23 ) to maximize choke flow capacity. In turbochargers with a wastegate assembly, an actuator ( 32 ) may control both a wastegate control valve ( 30 ) and an active casing treatment slot selection valve ( 56 ).
Opening claim text (preview).
What is claimed is: 1 . A turbocharger ( 1 ) comprising a turbine stage ( 2 ) and a compressor stage ( 4 ), the turbine stage ( 2 ) including a turbine wheel ( 16 ) selected from the group consisting of an axial flow turbine wheel and a mixed-flow turbine wheel, the compressor stage ( 4 ) including a compressor housing ( 20 ), and a compressor wheel ( 28 ) disposed in the compressor housing ( 20 ) and connected to the turbine wheel ( 16 ) via a shaft ( 18 ), wherein the compressor housing ( 20 ) includes active casing treatment ( 50 ) that is configured to control air flow to the compressor wheel ( 28 ). 2 . The turbocharger ( 1 ) of claim 1 , wherein a ratio of the size of the compressor wheel ( 28 ) to the size of the turbine wheel ( 16 ) is in a range of 0.95:1.00 to 1.05:1.00. 3 . The turbocharger ( 1 ) of claim 1 , wherein a ratio of the size of the compressor wheel ( 28 ) to the size of the turbine wheel ( 16 ) is 1.00:1.00. 4 . The turbocharger ( 1 ) of claim 1 , wherein a Blade Speed Ratio of the turbocharger ( 1 ), defined as U/Co, is in a range of 0.75 to 0.90. 5 . The turbocharger ( 1 ) of claim 1 wherein active casing treatment ( 50 ) comprises a slot ( 52 , 54 ) formed in the compressor inlet wall, the slot ( 52 , 54 ) opening facing the compressor wheel ( 28 ) and configured to selectively circulate air relative to the compressor wheel ( 28 ). 6 . The turbocharger ( 1 ) of claim 1 wherein active casing treatment ( 50 ) comprises a first slot ( 52 ) formed in the compressor inlet ( 22 ) wall, the first slot ( 52 ) opening facing the compressor wheel ( 28 ) at a first location, a second slot ( 54 ) formed in the compressor inlet ( 22 ) wall, the second slot ( 54 ) opening facing the compressor wheel ( 28 ) at a second location, a slot selection valve ( 56 ) configured to control gas flow to the first slot ( 52 ) and the second slot ( 54 ), and to permit selection between using the first slot ( 52 ) and using the second slot ( 54 ). 7 . The turbocharger ( 1 ) of claim 6 wherein the second location comprises a location downstream of a leading edge ( 21 ) of splitter blades ( 23 ) of the compressor wheel ( 28 ). 8 . The turbocharger ( 1 ) of claim 6 wherein the first location comprises a location between a leading edge ( 25 ) of full blades ( 27 ) of the compressor wheel ( 28 ) and a leading edge ( 21 ) of splitter blades ( 23 ) of the compressor wheel ( 28 ). 9 . The turbocharger ( 1 ) of claim 6 , wherein the turbine stage ( 2 ) comprises a wastegate valve ( 30 ) and the turbocharger ( 1 ) includes a single actuator ( 32 ) configured to control both the position of the wastegate valve ( 30 ) and the slot selection valve ( 56 ). 10 . The turbocharger ( 1 ) of claim 1 , wherein the turbine wheel ( 16 ) is an axial flow turbine wheel.
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