Piston and an internal combustion engine system
A piston for an internal combustion engine operable on a gaseous fuel is provided. The piston has a piston top end comprising a piston bowl for receiving at least one gaseous fuel jet from a fuel injector of the ICE, said piston bowl having a bottom section and a circumferential side section extending in an axial direction between the bottom section and a piston top end surface, wherein said bottom section comprises a protrusion segment configured to guide said at least one gaseous fuel jet. The protrusion segment further extends between spaced apart regions of the circumferential side section.
1. A piston for an internal combustion engine (ICE), operable on a gaseous fuel, said piston having a piston top end comprising a piston bowl for receiving at least one gaseous fuel jet from a fuel injector of the ICE, said piston bowl having a bottom section and a circumferential side section extending in an axial direction between the bottom section and a piston top end surface, wherein said bottom section comprises a protrusion segment configured to guide said at least one gaseous fuel jet,
wherein said protrusion segment further extends between spaced apart regions of the circumferential side section, and
wherein the extension of the protrusion segment in the axial direction does not exceed the piston top end upper surface of the piston, as defined by the circumferential side section.
2. The piston according to claim 1 , wherein said protrusion segment is a straight protrusion segment.
3. The piston according to claim 1 , wherein said protrusion segment is a diameter protrusion segment extending through a centre of the piston bowl.
4. The piston according to claim 1 , wherein said protrusion segment is a chord protrusion segment being arranged offset the centre of the piston bowl.
5. The ICE system according to claim 1 , wherein said controllable fuel injector is controllable by the controller to inject gaseous fuel into the combustion chamber with a velocity of up to about 1600 m/s.
6. An internal combustion engine (ICE), system comprising:
an internal combustion engine for combustion of gaseous fuel and having a combustion chamber at least partially delimited by a cylinder;
a piston having a piston top end comprising a piston bowl for receiving at least one gaseous fuel jet from a fuel injector of the ICE, said piston bowl having a bottom section and a circumferential side section extending in an axial direction between the bottom section and a piston top end surface, wherein said bottom section comprises a protrusion segment configured to guide said at least one gaseous fuel jet,
wherein said protrusion segment further extends between spaced apart regions of the circumferential side section, and
wherein the extension of the protrusion segment in the axial direction does not exceed the piston top end upper surface of the piston, as defined by the circumferential side section, wherein said piston is moveable within said cylinder between a bottom dead centre (BDC) and a top dead centre (TDC), said piston bowl being intended to form part of the combustion chamber;
a controllable fuel injector arranged to inject gaseous fuel into the combustion chamber and towards the piston bowl; and
a controller configured to control the controllable fuel injector to inject at least one gaseous fuel jet towards the bottom section of the piston bowl during a fuel injection period occurring prior to an ignition event of the gaseous fuel.
7. The ICE system according to claim 6 , wherein said controller is configured to control the controllable fuel injector to inject at least one gaseous fuel jet towards the bottom section of the piston bowl during the fuel injection period when said reciprocating piston moves from BDC to TDC during a compression stroke.
8. The ICE system according to claim 7 , wherein said controller is configured to control the controllable fuel injector to inject at least one gaseous fuel jet during the compression stroke when the reciprocating piston travels from BDC to a piston position corresponding to 90 crank angle degrees (CAD), before the TDC.
9. The ICE system according to claim 6 , wherein said controllable fuel injection period is initiated by the controllable fuel injector when the piston is at any one of a position being a piston position before BDC during an intake stroke, a piston position at the BDC and a piston position after the BDC during the compression stroke.
10. The ICE system according to claim 6 , wherein said controllable fuel injector is configured to inject at least one gaseous fuel jet towards said protrusion segment, whereby said protrusion segment is configured to guide said at least one gaseous fuel outwardly and towards said circumferential side section.
11. The ICE system according to claim 6 , wherein said controllable fuel injector is configured to inject at least one gaseous fuel jet towards said circumferential side section, whereby said circumferential side section is configured to guide at least one gaseous fuel jet inwardly and towards said protrusion segment.
12. The ICE system according to claim 6 , wherein the controller is configured to control the controllable fuel injector in response to a control signal.
13. The ICE system according to claim 6 , wherein said internal combustion engine further comprises an ignition source comprising a spark plug for igniting the gaseous fuel.
14. The ICE system according to claim 6 , wherein said fuel injection period is terminated by the controllable fuel injector prior to ignition of the fuel by the ignition source.
15. The ICE system according to claim 6 , wherein said controllable fuel injector is controllable by the controller to inject the at least one gaseous fuel jet in form of an under-expanded jet.
16. The ICE system according to claim 7 , wherein said controllable fuel injector is controllable by the controller to inject a number of gaseous fuel jets during said compression stroke.
17. The ICE system according to claim 6 , wherein the controllable fuel injector comprises a nozzle device configured to form the at least one gaseous fuel jet from a gaseous fuel delivered to the fuel injector from a fluid conduit.
18. The ICE system according to claim 17 , wherein the nozzle device comprises a cap device arranged at an end of the nozzle device, said cap device having at least one orifice for directing the at least one gaseous fuel jet towards the piston bowl.
19. The ICE system according to claim 6 , wherein said internal combustion engine is a low pressure direct injection fuel gas ICE.
20. The ICE system according to claim 19 , wherein said controllable fuel injector is controllable by the controller to inject gaseous fuel into the combustion chamber with a low injection pressure of not more than about 60 bar.
21. The ICE system according to claim 6 , wherein the fuel is hydrogen.
22. A vehicle comprising a piston having a piston top end comprising a piston bowl for receiving at least one gaseous fuel jet from a fuel injector of the ICE, said piston bowl having a bottom section and a circumferential side section extending in an axial direction between the bottom section and a piston top end surface, wherein said bottom section comprises a protrusion segment configured to guide said at least one gaseous fuel jet,
wherein said protrusion segment further extends between spaced apart regions of the circumferential side section, and
wherein the extension of the protrusion segment in the axial direction does not exceed the piston top end upper surface of the piston, as defined by the circumferential side section.