Apparatus for diagnosing EGR valve and method thereof
US-11035312-B2 · Jun 15, 2021 · US
US11629612B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11629612-B2 |
| Application number | US-202117237121-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 22, 2021 |
| Priority date | Apr 24, 2020 |
| Publication date | Apr 18, 2023 |
| Grant date | Apr 18, 2023 |
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A system for feeding operating gas to a drive (1) of a motor vehicle, including an atmosphere-side suction inlet (2a) for air under atmospheric pressure, and a feed line (2) for the operating gas to the drive (1) under an operating pressure, the operating gas which is conducted to the drive comprising at least part of the air which is sucked in, at least part of the operating gas being conducted through a turbomachine (3) upstream of the drive (1) in a first operating type, the turbomachine (3) comprising an electric generator (4), and the turbomachine (3) being operated in a second operating type as a compressor for the operating gas, an actuable valve arrangement (5) being provided, at least part of the air which is sucked in being conducted in a turbine direction (T) through the turbomachine (3) in a first position of the valve arrangement (5), and at least part of the air which is sucked in being conducted in a reversed compressor direction (V) through the turbomachine (3) in a second position of the valve arrangement (5).
Opening claim text (preview).
What is claimed: 1. A system for feeding operating gas to a drive ( 1 ) of a motor vehicle, comprising: an atmosphere-side suction inlet ( 2 a ) for air under atmospheric pressure; and a feed line ( 2 ) for the operating gas to the drive ( 1 ) under an operating pressure, the operating gas which is conducted to the drive comprising at least part of the air which is sucked in, at least part of the operating gas being conducted through a turbomachine ( 3 ) upstream of the drive ( 1 ) in a first operating type; the turbomachine ( 3 ) comprising an electric generator ( 4 ), and the turbomachine ( 3 ) being operated in a second operating type as a compressor for the operating gas, wherein an actuable valve arrangement ( 5 ) is provided, at least part of the air which is sucked in being conducted in a turbine direction (T) through the turbomachine ( 3 ) in a first position of the actuable valve arrangement ( 5 ), and at least part of the air which is sucked in being conducted in a reversed compressor direction (V) through the turbomachine ( 3 ) in a second position of the actuable valve arrangement ( 5 ) and wherein the actuable valve arrangement ( 5 ) comprises a multiway valve, and wherein the turbomachine ( 3 ) comprises a turbine of radial design, and wherein the operating pressure in at least one regular operating state is smaller by a differential pressure than the atmospheric pressure, and wherein the drive ( 1 ) is configured as an internal combustion engine, and wherein no further compressor is provided in addition to the turbomachine ( 3 ) for feeding the operating gas to the engine. 2. The system as claimed in claim 1 , wherein the rotational direction of the electric generator ( 4 ) runs in an opposed manner in the first and second operating types. 3. The system as claimed in claim 1 , wherein the generator ( 4 ) is switched as an electric motor ( 4 ) of the turbomachine ( 3 ) by means of control electronics ( 8 ) in the second operating type. 4. The system as claimed in claim 1 , wherein the turbomachine ( 3 ) comprises precisely one turbomachine wheel ( 6 ), the wheel ( 6 ) acting as a turbine or as a compressor for the operating gas depending on the operating type. 5. The system as claimed in claim 1 , wherein the turbomachine ( 3 ) comprises a turbine wheel which is driven by way of exhaust gas of the internal combustion engine ( 1 ). 6. The system as claimed in claim 1 , wherein the operating pressure in a part load range of the drive ( 1 ) is smaller by the differential pressure than the atmospheric pressure. 7. The system as claimed in claim 1 , wherein the turbomachine ( 3 ) has stationary guide vanes. 8. The system as claimed in claim 1 , wherein the turbomachine ( 3 ) comprises adjustable guide vanes ( 12 ).
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differential pressure · CPC title
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