Method for venting a fuel supply line, and internal combustion engine
US-2015377199-A1 · Dec 31, 2015 · US
US9951737B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9951737-B2 |
| Application number | US-201214002873-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 2, 2012 |
| Priority date | Mar 4, 2011 |
| Publication date | Apr 24, 2018 |
| Grant date | Apr 24, 2018 |
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An internal combustion engine ( 1 ) has a plurality of combustion cylinders at each of which a fuel injection device ( 120 ) is provided. Every combustion cylinder is provided with its own pilot unit ( 10 c - 10 f ) with a fuel accumulator which is integrated therein and which is connected by one of a plurality of first fuel lines ( 110 ) to the fuel injection device associated with the respective combustion cylinder for supplying fuel to the latter. A fuel pump which can be connected to a fuel source for supplying a predetermined fuel pressure is integrated in at least one of the pilot units ( 10 d ). The fuel accumulator of every pilot unit is so adapted that it ensures that fuel delivered by the fuel pump is supplied to the respective associated fuel injection device in a pressure-stable manner.
Opening claim text (preview).
The invention claimed is: 1. An internal combustion engine ( 1 , 1 a ) comprising: a plurality of combustion cylinders each of which having an associated fuel injection device ( 120 ), each of the plurality of combustion cylinders being provided with its own pilot unit ( 10 , 10 a - 10 g ) having a fuel accumulator ( 20 ) integrated therein, each fuel accumulator ( 20 ) being connected by one of a plurality of first fuel lines ( 110 ) to the fuel injection device ( 120 ) associated with the respective combustion cylinder for supplying fuel to the respective combustion cylinder; and a fuel pump ( 50 ) configured to be connectable to a fuel source for supplying a predetermined fuel pressure, the fuel pump ( 50 ) being integrated in each instance of the plurality of the pilot units ( 10 , 10 a - 10 g ), wherein the fuel accumulator ( 20 ) of each pilot unit ( 10 , 10 a - 10 g ) is configured to ensure that fuel delivered by the fuel pump ( 50 ) is supplied to the respective associated fuel injection device ( 120 ) in a pressure-stable manner, and wherein the respective fuel accumulators ( 20 ) of the pilot units ( 10 , 10 a - 10 g ) are connected to one another via a plurality of second fuel lines ( 100 ). 2. The internal combustion engine ( 1 , 1 a ) according to claim 1 , further comprising a quantity limiting valve ( 30 ) for limiting a quantity of fuel to be supplied per time unit to an associated fuel injection device ( 120 ), the quantity limiting valve ( 30 ) being integrated in at least one of the pilot units ( 10 , 10 a - 10 g ). 3. The internal combustion engine ( 1 , 1 a ) according to claim 1 , further comprising a quantity limiting valve ( 30 ) for limiting a quantity of fuel to be supplied per time unit to an associated fuel injection device ( 120 ), the quantity limiting valve ( 30 ) being integrated in at least one pilot unit ( 10 d ) that has an integrated fuel pump ( 50 ). 4. The internal combustion engine ( 1 , 1 a ) according to claim 1 , further comprising a pressure limiting valve ( 60 ) for limiting the fuel pressure, the pressure limiting valve ( 60 ) being integrated in at least one of the pilot units ( 10 b , 10 c ). 5. The internal combustion engine ( 1 , 1 a ) according to claim 1 , further comprising a quantity limiting valve ( 30 ) for limiting a quantity of fuel to be supplied per time unit to an associated fuel injection device ( 120 ) and a pressure limiting valve ( 60 ) for limiting the fuel pressure, wherein the quantity limiting valve ( 30 ) and the pressure limiting valve ( 60 ) are integrated in at least one of the pilot units ( 10 b ). 6. The internal combustion engine ( 1 , 1 a ) according to claim 1 , wherein at least some of the combustion cylinders are arranged in a row relative to one another, and the internal combustion engine ( 1 , 1 a ) further comprises a purge valve ( 70 ) integrated in the pilot unit ( 10 f ) of a combustion cylinder forming an end of the row of combustion cylinders. 7. The internal combustion engine ( 1 , 1 a ) according to claim 6 , further comprising a pressure limiting valve ( 60 ) for limiting the fuel pressure, the pressure limiting valve being integrated in the pilot unit ( 10 f ) with the purge valve ( 70 ) integrated therein. 8. The internal combustion engine ( 1 , 1 a ) according to claim 1 , further comprising at least one pressure measuring location ( 80 ), for connecting at least one fuel pressure sensor for measuring the fuel pressure in the fuel accumulator ( 20 ) of the respective pilot unit ( 10 g ), the at least one pressure measuring location being integrated in at least one of the pilot units ( 10 g ). 9. The internal combustion engine ( 1 , 1 a ) according to claim 1 , wherein the first fuel lines ( 110 ) are all constructed so as to be identical to one another, and wherein the second fuel lines ( 100 ) are all constructed so as to be identical to one another.
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for damping fuel pressure fluctuations · CPC title
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Conduits between injection pumps and injectors {, e.g. conduits between pump and common-rail or conduits between common-rail and injectors} · CPC title
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