Methods and apparatus for mitigating fuel in oil
US-2024409080-A1 · Dec 12, 2024 · US
US10100756B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10100756-B2 |
| Application number | US-201515120857-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 19, 2015 |
| Priority date | Feb 27, 2014 |
| Publication date | Oct 16, 2018 |
| Grant date | Oct 16, 2018 |
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A method for determining atmospheric pressure AMP during operation in a partial load state of a turbocharged engine ( 1 ) including an air intake line ( 2 ) incorporating a butterfly valve ( 16 ), and an exhaust line ( 3 ) including a bypass duct ( 20 ) incorporating an exhaust gas discharge valve ( 21 ), the method includes measuring the air pressure PUT upstream of the butterfly valve ( 16 ), and for a given speed of N rpm of the engine ( 1 ), when the boost pressure PUT corresponds substantially to the natural boost pressure, determining the atmospheric pressure AMP=AMP(0)+PUT−PUT(0), wherein AMP(0) is the atmospheric pressure previously measured, and PUT(0) is boost pressure naturally obtained for the speed N rpm of the engine ( 1 ) for the atmospheric pressure AMP(0).
Opening claim text (preview).
The invention claimed is: 1. A method for determining atmospheric pressure (AMP) during operation, in a partial load state, of a turbocharged engine ( 1 ) equipped with an air intake line ( 2 ) containing an intake pipe (A) that incorporates a compressor ( 12 ) and a butterfly valve ( 16 ), and an exhaust line ( 3 ) that includes, in parallel, a main exhaust pipe (E) incorporating a turbine ( 19 ) and a bypass duct ( 20 ) incorporating an exhaust gas discharge valve ( 21 ), the method comprising: in a state of a maximum opening of the discharge valve ( 21 ) and a partial opening of the butterfly valve ( 16 ), measuring, by way of a pressure sensor ( 25 ) provided in the intake pipe (A) upstream of the butterfly valve ( 16 ), a boost pressure (PUT) of air in the intake pipe (A) upstream of the butterfly valve ( 16 ); for a given speed (N) of the engine ( 1 ), when the boost pressure (PUT) corresponds substantially to a natural boost pressure, determining the atmospheric pressure (AMP) from the following equation: AMP=AMP(0)+ PUT−PUT (0); and using said determined atmospheric pressure (AMP) for operation of the engine, wherein: AMP(0) is a previously measured reference atmospheric pressure, and PUT(0) is a boost pressure naturally obtained for the speed (N) of the engine ( 1 ) for the atmospheric pressure AMP(0). 2. The method as claimed in claim 1 , further comprising: measuring, by way of a second pressure sensor ( 26 ) located downstream of the butterfly valve ( 16 ), a manifold pressure (MAP) of air downstream of the butterfly valve ( 16 ), and wherein the atmospheric pressure (AMP) is determined when the a MAP/PUT ratio of the measured values of the manifold pressure (MAP) and boost pressure (PUT) is greater than 0.80. 3. The method as claimed in claim 1 , wherein, in a start-up phase of the engine ( 1 ), the boost pressure (PUT) is measured and a value of said measured boost pressure is allocated to the reference atmospheric pressure (AMP (0)). 4. The method as claimed in claim 2 , wherein, in a start-up phase of the engine ( 1 ), the boost pressure (PUT) is measured and a value of said measured boost pressure is allocated to the reference atmospheric pressure (AMP (0)).
Arrangements of bypass valves or actuators therefor · CPC title
air passages · CPC title
for temperature or pressure · CPC title
for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12) · CPC title
Engine speed · CPC title
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