Jet for orifice damping
The present invention provides a jet for providing orifice damping in the fuel delivery system of a compression-ignition combustion engine, wherein the jet ( 100 ) is formed by means of a deep draw process and comprises a hollow cylindrical body ( 102 ) having first and second ends ( 104, 106 ), the first end ( 104 ) being open to enable unrestricted flow of fuel therethrough, in use, the second end ( 106 ) comprising an orifice ( 110 ) therein having a smaller cross-sectional area than the opening in the first end ( 104 ), to restrict the flow of fuel therethrough and dampen pressure waves in the fuel, in use, the second end ( 106 ) being shaped so as to provide resistance to pressure changes occurring in the fuel delivery system, in use.
1 . A jet for providing orifice damping in the fuel delivery system of a compression-ignition combustion engine, wherein the jet ( 100 ) is formed by means of a deep draw process and comprises;
a hollow cylindrical body ( 102 ) having first and second ends ( 104 , 106 ),
the first end ( 104 ) being open to enable unrestricted flow of fuel therethrough, in use,
the second end ( 106 ) comprising an orifice ( 110 ) therein having a smaller cross-sectional area than the opening in the first end ( 104 ), to restrict the flow of fuel therethrough and dampen pressure waves in the fuel, in use, the second end ( 106 ) being shaped so as to provide resistance to pressure changes occurring in the fuel delivery system, in use.
2 . A jet according to claim 1 , wherein the second end ( 106 ) comprises a part-spherical region ( 108 ; 150 ) extending inwardly from a wall of the cylindrical body ( 102 ).
3 . A jet according to claim 2 , wherein said part-spherical region ( 108 ) projects outwardly from the cylindrical body ( 102 ).
4 . A jet according to claim 2 , wherein said part-spherical region ( 150 ) projects into the cylindrical body ( 102 ).
5 . A jet according to any one of claims 2 , 3 or 4 , wherein said part-spherical region ( 108 ) terminates in a flat region ( 109 ).
6 . A jet according to claim 5 , wherein said orifice ( 110 ) is formed within the flat region ( 109 ) and is co-axial with the primary axis of the cylindrical body ( 102 ).
7 . A jet according to any one of claims 2 , 3 or 4 , comprising a pair of orifices ( 110 a , 110 b ) in the part-spherical region ( 108 ), said pair of orifices ( 110 a , 110 b ) being disposed at spaced apart locations equidistant from, and on opposite sides of the primary axis of the cylindrical body ( 102 ).
8 . A jet according to claim 1 , wherein the second end ( 106 ) comprises a flat region ( 130 ; 142 ; 160 ; 182 ) extending inwardly from and substantially perpendicularly to the wall of the cylindrical body ( 102 ).
9 . A jet according to claim 8 , wherein said orifice ( 110 ) is formed in the flat region ( 140 ; 160 ) co-axial with the primary axis of the cylindrical body ( 102 ).
10 . A jet according to claim 8 or 9 , wherein said flat region ( 142 ) comprises a concentric rib ( 140 ).
11 . A jet according to claim 8 , wherein said flat region ( 182 ) comprises a cruciform rib ( 180 ).
12 . A jet according to claim 8 or 11 , comprising a pair of orifices ( 110 a , 110 b ) in the flat region ( 160 ), said pair of orifices ( 110 a , 110 b ) being disposed at spaced apart locations equidistant from, and on opposite sides of the primary axis of the cylindrical body ( 102 ).
13 . A jet according to claim 8 , wherein the second end ( 106 ) comprises a part-spherical region ( 132 ) which projects from the flat region ( 130 ) and terminates in a second flat region ( 134 ), said orifice ( 110 ) being formed in the second flat region ( 134 ).
14 . A jet according to claim 13 , wherein the part-spherical region projects outward from the cylindrical body ( 102 ).
15 . A jet according to claim 13 , wherein the part-spherical region projects into the cylindrical body ( 102 ).
16 . A fuel delivery system for a compression-ignition combustion engine, the system comprising a jet ( 100 ) according to any preceding claim;
a high pressure pump ( 3 ) for pressurising fuel in the delivery system; and
a rail cavity ( 8 ) for receiving pressurised fuel from the high pressure pump ( 3 ) via an inlet pipe ( 4 ), the rail cavity ( 8 ) having at least one outlet pipe ( 5 ) for conveying fuel to at least one respective fuel injector ( 6 ).
17 . A system according to claim 16 , wherein said jet ( 100 ) is disposed in said outlet pipe ( 5 ) or said inlet pipe ( 4 ).
18 . A system according to claim 16 , wherein said jet ( 100 ) is disposed between said pump ( 3 ) and said rail cavity ( 8 ).
19 . A system according to claim 16 , wherein said jet ( 100 ) is formed integrally with any one of said high pressure pump ( 3 ), said rail cavity ( 8 ), said inlet pipe ( 4 ) or said outlet pipe ( 5 ).
20 . A method of manufacturing a jet for providing orifice damping in the fuel delivery system of a compression-ignition combustion engine, the method comprising;
forming a hollow cylindrical body ( 102 ) by means of a deep draw process,
the cylindrical body ( 102 ) comprising first and second ends ( 104 , 106 ),
the first end ( 104 ) being open to enable unrestricted flow of fuel therethrough, in use,
the second end ( 106 ) comprising an orifice ( 110 ) therein having a smaller cross-sectional area than the opening in the first end ( 104 ), to restrict the flow of fuel therethrough and dampen pressure waves in the fuel, in use, the second end ( 106 ) being shaped so as to provide resistance to pressure changes occurring in the fuel delivery system, in use.