Valve assembly and exhaust gas system
US-9657652-B2 · May 23, 2017 · US
US9784221B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9784221-B2 |
| Application number | US-201514827368-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 17, 2015 |
| Priority date | Feb 22, 2013 |
| Publication date | Oct 10, 2017 |
| Grant date | Oct 10, 2017 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
In an exhaust gas flow control system for an internal combustion engine, with a first exhaust gas duct and a second exhaust gas duct, through both of which exhaust gas from the internal combustion engine can flow to a turbine of an exhaust gas turbocharger with an exhaust gas recirculation line branching off the first exhaust gas duct, a shut-off element is provided which is adjustable between a closed position in which exhaust gas is prevented from flowing into the exhaust gas recirculation line and directing it via a communication passage into the second exhaust gas duct, and at least a first open position in which exhaust gas is directed out of the first exhaust gas duct into the exhaust gas recirculation line while blocking the communication passage between the first and second exhaust gas ducts and a second open position wherein both the first and the second exhaust gas ducts as well as the communication passage between the two ducts is open but the recirculation line is closed.
Opening claim text (preview).
What is claimed is: 1. An exhaust gas flow control system ( 10 ) for an internal combustion engine, comprising: a first exhaust gas duct ( 14 ), which is associated with a first inlet duct ( 16 ) of a turbine of an exhaust gas turbocharger and through which exhaust gas from the internal combustion engine can flow, a second exhaust gas duct ( 16 ), which is at least partially fluidically separated from the first exhaust gas duct ( 14 ) and through which exhaust gas from the internal combustion engine can flow and which is associated with a second inlet duct of the turbine, an exhaust gas return line ( 22 ) which branches off from the first exhaust gas duct ( 14 ), and a shut-off valve ( 26 ) which is adjustable between at least one closed position ( 1 ), which prevents exhaust gas from flowing out of the first exhaust gas duct ( 14 ) into the exhaust gas return line ( 22 ), and a first open position ( 2 ), which allows exhaust gas to flow out of the first exhaust gas duct ( 14 ) into the exhaust gas return line ( 22 ), a fluidic connecting passage ( 30 ) provided between the exhaust gas ducts ( 14 , 16 ), via which exhaust gas can be diverted out of the first exhaust gas duct ( 14 ) and can be delivered to the second exhaust gas duct ( 16 ) when the shut-off valve ( 26 ) is in the first closed position ( 1 ) and the shut-off element ( 26 ) in the first open position ( 2 ) blocking the first exhaust gas duct ( 14 ) at least downstream of the fluidic connection ( 30 ) and opening the gas exhaust gas return line ( 22 ), the shut-off element ( 26 ) being movable to a second closed position ( 4 ), in which the return line ( 22 ) is blocked so that the exhaust gas from the first exhaust gas duct ( 14 ) is prevented from flowing into the exhaust gas return line ( 22 ) and the connecting passage ( 30 ) between the exhaust gas ducts ( 14 , 16 ) and the first exhaust gas duct ( 14 ) is opened so as to divert exhaust gas from the first exhaust gas duct ( 14 ) into the second exhaust das duct ( 16 ). 2. The exhaust gas flow control system ( 10 ) according to claim 1 , wherein the first exhaust gas duct ( 14 ) is fluidically shut off by the shut-off valve ( 26 ) in its first open position ( 2 ) downstream of a branch point ( 24 ) so that all the exhaust gas from the first exhaust gas duct ( 14 ) is diverted into the exhaust gas return line ( 22 ). 3. The exhaust gas flow control system ( 10 ) according to claim 1 , wherein the shut-off valve ( 26 ) is adjustable into an intermediate open position ( 3 ), in which the exhaust gas return line ( 22 ) and also the first exhaust gas duct ( 14 ) as well as the connecting passage ( 30 ) are open. 4. The exhaust gas flow control system ( 10 ) according to claim 1 , wherein second exhaust gas duct ( 16 ) has a larger cross-section through which exhaust gas flows than the first exhaust gas duct ( 14 ). 5. The exhaust gas flow control system ( 10 ) according to claim 1 , wherein the cross-sections of the exhaust gas ducts ( 14 , 16 ) are the same size.
Arrangements of bypass valves or actuators therefor · CPC title
Mechanical Engineering · mapped topic
Exhaust brakes · CPC title
by varying cross-section of exhaust passages or air passages {, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits} (F02B37/24 takes precedence) · CPC title
Cross-Sectional Technologies · mapped topic
Related publications grouped by family.
Answers are generated from the same data shown on this page.