MULTI-CYLINDER ENGINE

Abstract

A multi-cylinder engine having an engine body with a cylinder head, and mounted on a vehicle is provided. The engine includes first and second cylinder groups each provided to the engine body and comprised of first and second pluralities of cylinders, first and second exhaust passage groups each having first and second pluralities of independent exhaust passage parts provided to the cylinder head and connected to the first and second cylinder groups, respectively, and first and second collective exhaust passage parts provided to the cylinder head and collecting the first and second pluralities of independent passage parts downstream in an exhaust gas flow direction, and a cooling medium passage provided in the cylinder head, through which a cooling medium flows, and having an intermediate passage part provided between the first collective exhaust passage part and the second collective exhaust passage part.

Claims

1. A multi-cylinder engine having an engine body with a cylinder head, and mounted on a vehicle, comprising: a first cylinder group provided to the engine body and comprised of a first plurality of cylinders disposed adjacent to each other; a second cylinder group provided to the engine body, comprised of a second plurality of cylinders disposed adjacent to each other, and provided adjacent to the first cylinder group; a first exhaust passage group having a first plurality of independent exhaust passage parts provided to the cylinder head and connected to the first cylinder group, respectively, and a first collective exhaust passage part provided to the cylinder head and collecting the first plurality of independent exhaust passage parts downstream in an exhaust gas flow direction; a second exhaust passage group having a second plurality of independent exhaust passage parts provided to the cylinder head and connected to the second cylinder group, respectively, and a second collective exhaust passage part provided to the cylinder head and collecting the second plurality of independent exhaust passage parts downstream in the exhaust gas flow direction; and a cooling medium passage provided in the cylinder head, through which a cooling medium flows, and having an intermediate passage part provided between the first collective exhaust passage part and the second collective exhaust passage part.

2. The multi-cylinder engine of claim 1, wherein the cooling medium passage further includes: a first upper passage part provided to at least an upper part of the first collective exhaust passage part; and a second upper passage part provided to at least an upper part of the second collective exhaust passage part.

3. The multi-cylinder engine of claim 2, wherein the cooling medium passage further includes: a first lower passage part provided to at least a lower part of the first collective exhaust passage part; and a second lower passage part provided to at least a lower part of the second collective exhaust passage part.

4. The multi-cylinder engine of claim 1, wherein each of the first collective exhaust passage part and the second collective exhaust passage part has an opening in a side surface part of the cylinder head, wherein in a plan view of the second exhaust passage group in cylinder axis directions, the opening of the second collective exhaust passage part is offset toward the first exhaust passage group in a lineup direction of the first plurality of independent exhaust passage parts, and wherein in a plan view of the first exhaust passage group in the cylinder axis directions, the opening of the first collective exhaust passage part is disposed closer to a center in the lineup direction of the first plurality of independent exhaust passage parts, compared with the opening of the second collective exhaust passage part.

5. The multi-cylinder engine of claim 4, further comprising: a first exhaust-pipe part connected to the opening of the first collective exhaust passage part; and a second exhaust-pipe part connected to the opening of the second collective exhaust passage part.

6. The multi-cylinder engine of claim 5, further comprising: a collective exhaust-pipe part provided downstream in the exhaust gas flow direction of the first exhaust-pipe part and the second exhaust-pipe part, and collecting the first exhaust-pipe part and the second exhaust-pipe part; and a turbocharger provided downstream in the exhaust gas flow direction of the collective exhaust-pipe part.

7. The multi-cylinder engine of claim 1, wherein fuel is injected alternately over time to the first cylinder group and the second cylinder group.

8. A multi-cylinder engine having an engine body with a cylinder head, and mounted on a vehicle, comprising: a first cylinder group provided to the engine body and comprised of a first plurality of cylinders disposed adjacent to each other; a second cylinder group provided to the engine body, comprised of a second plurality of cylinders disposed adjacent to each other, and provided adjacent to the first cylinder group; a first exhaust passage group having a first plurality of independent exhaust passage parts provided to the cylinder head and connected to the first plurality of cylinders, respectively, and a first collective exhaust passage part provided to the cylinder head and collecting the first plurality of independent exhaust passage parts downstream in an exhaust gas flow direction; and a second exhaust passage group having a second plurality of independent exhaust passage parts provided to the cylinder head and connected to the second plurality of cylinders, respectively, and a second collective exhaust passage part provided to the cylinder head and collecting the second plurality of independent exhaust passage parts downstream in the exhaust gas flow direction, each of the first collective exhaust passage part and the second collective exhaust passage part having an opening in a side surface part of the cylinder head, wherein in a plan view of the second exhaust passage group in cylinder axis directions, the opening of the second collective exhaust passage part is offset toward the first exhaust passage group in a lineup direction of the first plurality of independent exhaust passage parts, and wherein in a plan view of the first exhaust passage group in the cylinder axis directions, the opening of the first collective exhaust passage part of the first exhaust passage group is disposed closer to a center in the lineup direction of the first plurality of independent exhaust passage parts, compared with the opening of the second collective exhaust passage part; and a cooling medium passage provided in the cylinder head, through which a cooling medium flows, and having an intermediate passage part provided between the first collective exhaust passage part and the second collective exhaust passage part.

9. The multi-cylinder engine of claim 8, wherein the cooling medium passage further includes: a first upper passage part provided to at least an upper part of the first collective exhaust passage part; and a second upper passage part provided to at least an upper part of the second collective exhaust passage part.

10. The multi-cylinder engine of claim 9, wherein the cooling medium passage further includes: a first lower passage part provided to at least a lower part of the first collective exhaust passage part; and a second lower passage part provided to at least a lower part of the second collective exhaust passage part.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0022] FIG. 1 is a view schematically illustrating a structure of an engine for a vehicle according to one embodiment of the present disclosure.

[0023] FIG. 2 is a side view schematically illustrating the engine.

[0024] FIG. 3 is a front view schematically illustrating the engine.

[0025] FIG. 4 is a view schematically illustrating a structure of a water jacket formed in an engine body.

[0026] FIG. 5 is a perspective view schematically illustrating a cylinder head and a turbocharger which are removed from the engine.

[0027] FIG. 6 is a cross-sectional view schematically illustrating a structure of exhaust ports and a port collected part in the cylinder head, taken along a line VI-VI in FIG. 5.

[0028] FIG. 7 is a cross-sectional view schematically illustrating a spatial relationship between the port collected part and the water jacket in the cylinder head, taken along a line VII-VII in FIG. 5.

[0029] FIG. 8 is a cross-sectional view schematically illustrating a spatial relationship between the port collected part and the water jacket in the cylinder head, taken along a line VIII-VIII in FIG. 7.

[0030] FIG. 9 is a cross-sectional view schematically illustrating a spatial relationship between the port collected part and the water jacket in the cylinder head according to one modification.

DETAILED DESCRIPTION OF THE DISCLOSURE

[0031] Hereinafter, one embodiment of the present disclosure is described, taking the accompanying drawings into consideration. Note that the form in the following description is one mode of the present disclosure, and therefore, the present disclosure is not to be limited by the following form at all except for the essential structure of the present disclosure.

[0032] Note that although detailed illustration of a vehicle is omitted in the drawings used below, a +Z side is upward in up-and-down directions of the vehicle, and a Z side is downward in the up-and-down directions of the vehicle.

Embodiment

1. Outline Structure of Multi-Cylinder Engine 2

[0033] An outline structure of a multi-cylinder engine 2 (hereinafter, simply referred to as the engine) is described using FIG. 1.

[0034] As illustrated in FIG. 1, a vehicle 1 according to this embodiment includes, in addition to the engine 2 mounted on the vehicle 1, an ECU (Engine Control Unit) 10 which executes a driving control of the engine 2.

[0035] The engine 2 includes an engine body 3, an intake system 4, an exhaust system 5, and a turbocharger 6. In this embodiment, the engine body 3 adopts a multi-cylinder diesel engine having six cylinders 3a-3f, as one example.

[0036] The intake system 4 has an intake passage 41 connected to intake ports (not illustrated) of the engine body 3. An air cleaner 42 is provided at an upstream end of the intake passage 41, and fresh air is taken into the intake passage 41 through the air cleaner 42.

[0037] The intake passage 41 is provided with a compressor 61 of the turbocharger 6, a throttle valve 43, an intercooler 44, and a surge tank 45. Air flowing through the intake passage 41 is boosted by the compressor 61 of the turbocharger 6, and is then sent to the intercooler 44 through the throttle valve 43. The intercooler 44 cools the air which is increased in temperature due to the compression by the compressor 61.

[0038] Opening and closing of the throttle valve 43 is controlled during operation of the engine 2 so that the throttle valve 43 fundamentally maintains being in or near a fully-open state. The throttle valve 43 is closed only when it is necessary, e.g., when the engine 2 is stopped.

[0039] The surge tank 45 is provided immediately in front of a connection of the intake system 4 with the intake ports (not illustrated) of the engine body 3 to equalize an inflow air amount to the cylinders 3a-3f.

[0040] The exhaust system 5 has an exhaust passage 51 which is connected at one end to the part where a turbine 62 of the turbocharger 6 is provided. The exhaust passage 51 is provided with a DOC (Diesel Oxidation Catalyst) 52, a DPF (Diesel Particulate Filter) 53, an exhaust shutter valve 54, and a silencer 55.

[0041] The DOC 52 detoxicates CO and HC in exhaust gas discharged from the engine body 3 by oxidizing, and the DPF 53 captures particulates, such as soot, contained in the exhaust gas. The exhaust shutter valve 54 is provided between the DPF 53 and the silencer 55 in the exhaust passage, which is a valve to control a flow rate of the exhaust gas discharged outside through the silencer 55.

[0042] The turbocharger 6 includes, in addition to the compressor 61 and the turbine 62, a casing passage part 63 (i.e., a first exhaust-pipe part), a casing passage part 64 (i.e., a second exhaust-pipe part), and a casing collected part 65 (i.e., a collective exhaust-pipe part). The casing passage part 63 is connected to a first cylinder group 3A comprised of the cylinders 3a-3c, and the casing passage part 64 is connected to a second cylinder group 3B comprised of the cylinders 3d-3f. The casing collected part 65 is a pipe part at which the casing passage part 63 and the casing passage part 64 are collected, and is connected to the part where the turbine 62 is provided.

[0043] The engine 2 further includes an HP-EGR (High Pressure-Exhaust Gas Recirculation) device 7, an LP-EGR (Low Pressure-Exhaust Gas Recirculation) device 8, and a blowby gas device 9. The HP-EGR device 7 has an HP-EGR passage (EGR passage) 71. The HP-EGR passage 71 is provided so as to connect the intake passages 41 to the cylinder head of the engine body 3. Note that the connected part of the HP-EGR passage 71 to the intake passage 41 is located between the surge tank 45 and the intercooler 44. An EGR valve 72 is provided to the HP-EGR passage 71. The EGR valve 72 adjusts the flow rate of the exhaust gas recirculated to the intake passage 41.

[0044] The LP-EGR device 8 has an LP-EGR passage 81. The LP-EGR passage 81 is provided so as to connect the exhaust passage 51 to the intake passage 41. The connected part of the LP-EGR passage 81 to the exhaust passage 51 is located between the DPF 53 and the exhaust shutter valve 54. The connected part of the LP-EGR passage 81 to the intake passage 41 is located between the air cleaner 42 and the compressor 61 of the turbocharger 6.

[0045] An EGR cooler 82 and an EGR valve 83 are provided to the LP-EGR passage 81. The EGR valve 83 adjusts the flow rate of the exhaust gas recirculated to the intake passage 41, similar to the EGR valve 72 in the HP-EGR device 7. The EGR cooler 82 is provided in order to cool the exhaust gas to be recirculated to the intake passage 41.

[0046] The blowby gas device 9 has a blowby gas passage 91. The blowby gas passage 91 is provided so as to connect a head cover of the engine body 3 to the intake passage 41. The blowby gas passage 91 returns the blowby gas generated inside the engine body 3 to the intake passage 41.

[0047] The ECU 10 executes, for example, a control of fuel-injection timing in the engine body 3, and an opening-and-closing control of the various valves 43, 54, 72, and 83.

2. Outside Structure of Engine 2

[0048] The outside structure of the engine 2 is described using FIGS. 2 and 3. FIG. 2 is a side view schematically illustrating the engine 2, and FIG. 3 is a front view schematically illustrating the engine 2.

[0049] As illustrated in FIGS. 2 and 3, the LP-EGR passage 81 and the EGR cooler 82 of the LP-EGR device 8, the DOC 52 and the DPF 53 of the exhaust system 5, and the turbocharger 6 are disposed along a side surface part on the Y side of the engine body 3 of the engine 2. The LP-EGR passage 81 is provided so as to connect an upstream part of the compressor 61 (see FIG. 1) of the turbocharger 6 disposed on the +Z side to a downstream part of the DPF 53 disposed on the Z side. The EGR cooler 82 is disposed substantially in the Z-directions.

[0050] As illustrated in FIG. 2, the exhaust system 5 is curved in a substantially U-shape between the DOC 52 and the DPF 53. The exhaust passage 51 is bent at a part downstream of the DPF 53 (downstream in the exhaust gas flow direction) to the Z side (toward an oil pan 33 of the engine body 3) and to the Y side (toward a viewer of FIG. 2).

[0051] As illustrated in FIG. 3, the DOC 52 of the exhaust system 5 is disposed on the Y side of and close to a cylinder-head 31 and a head cover 34 of the engine body 3. The DPF 53 is disposed on the Y side of and close to a cylinder block 32 of the engine body 3.

[0052] As illustrated in FIG. 2, a cover 101 and a cover 102 are disposed on the X side of the turbocharger 6. These covers 101 and 102 are insulated.

[0053] In this embodiment, a variable displacement turbocharger is adopted as the turbocharger 6. Thus, the turbocharger has a VGT (variable geometry turbine) actuator which varies the displacement (detailed illustration is omitted). The cover 101 is provided in order to protect the VGT actuator from heat radiated from the engine body 3 and the DPF 53 which are located nearby.

[0054] Similarly, the cover 102 is provided in order to protect the EGR valve 83 (illustration is omitted in FIGS. 2 and 3) of the LP-EGR device 8 from the heat radiated from the engine body 3 and the DPF 53 which are located nearby. Note that the covers 101 and 102 may be separately or integrally formed.

3. Water Jackets 11, 12, 15, and 16 of Engine Body 3

[0055] Outline structure of water jackets 11, 12, 15, and 16 of the engine body 3 is described using FIG. 4, which is a view schematically illustrating the water jackets 11, 12, 15, and 16 of the engine body 3.

[0056] As illustrated in FIG. 4, a water pump 18 which pumps a coolant (i.e., a cooling medium) WF is attached to the engine body 3. In FIG. 4, although the water pump 18 is illustrated as attached to the cylinder block 32, the water pump 18 may be disposed at any other locations.

[0057] In the cylinder block 32, the intake-side water jacket 11 is formed along the intake side (IN side) of the cylinders 3a-3f and the exhaust-side water jacket 12 is formed along the exhaust side (EX side) of the cylinders 3a-3f. The coolant WF is supplied from the water pump 18 to each end part of the intake-side water jacket 11 and the exhaust-side water jacket 12 on the cylinder 3a side.

[0058] Moreover, an outlet part 13 is formed at an end of the cylinder block 32 on the cylinder 3f side, and the intake-side water jacket 11 and the exhaust-side water jacket 12 join to each other at the outlet part 13.

[0059] The outlet part 13 of the cylinder block 32 is connected to an inlet part 14 of the cylinder head 31. The inlet part 14 of the cylinder head 31 is formed at an end on the cylinder 3f side. The inlet part 14 is connected to the intake-side water jacket 15 formed along the intake side (IN side) of the cylinders 3a-3f in the cylinder head 31, and the exhaust-side water jacket 16 formed along the exhaust side (EX side) of the cylinders 3a-3f.

[0060] An outlet part 17 is formed at an end of the cylinder head 31 on the cylinder 3a side, and the intake-side water jacket 15 and the exhaust-side water jacket 16 join to each other at the outlet part 17. The outlet part 17 is connected to the water pump 18.

[0061] As illustrated in FIG. 4, the coolant WF pumped from the water pump 18 passes through the intake-side water jacket 11 and the exhaust-side water jacket 12 of the cylinder block 32, and flows into the outlet part 13. Then, the coolant WF which flowed in the water jackets 11 and 12 of the cylinder block 32 is sent to the inlet part 14 of the cylinder head 31, passes through the intake-side water jacket 15 and the exhaust-side water jacket 16, and is sent to the outlet part 17. The coolant WF sent to the outlet part 17 is returned to the water pump 18 via a radiator (not illustrated).

4. Spatial Relation between Cylinder Head 31 and Turbocharger 6

[0062] A spatial relation between the cylinder head 31 and the turbocharger 6 is described using FIG. 5. FIG. 5 is a perspective view schematically illustrating the cylinder head 31 and the turbocharger 6 which are removed from the engine 2.

[0063] As illustrated in FIG. 5, the cylinder head 31 has a substantially rectangular parallelepiped shape elongated in the X-directions. The +Z side of the cylinder head 31 is opened (i.e. an upper opening 31a), and is closed by the head cover 34 (see FIG. 3) attached thereto.

[0064] The turbocharger 6 is disposed along a side surface part 31b of the cylinder head 31 on the Y side. The casing passage parts 63 and 64 (in FIG. 5, only the casing passage part 63 is illustrated for convenience of illustration) of the turbocharger 6 are connected to openings of the exhaust ports formed in the side surface part 31b of the cylinder head 31. This will be described later.

[0065] The casing collected part 65 following the casing passage parts 63 and 64 is bent to the +Z side at the Y side of the casing passage parts 63 and 64. The casing collected part 65 is connected to the turbine 62.

[0066] Note that an exhaust gas temperature sensor 103 which detects the temperature of the exhaust gas is attached to the casing passage part 63.

5. Structures of Exhaust Ports 31c-31h and 31j-31o, and Port Collected Parts 31i and 31p of Cylinder Head 31

[0067] Structures of exhaust ports 31c-31h and 31j-31o and port collected parts 31i and 31p in the cylinder head 31 are described using FIG. 6. FIG. 6 is a schematic cross-sectional view taken along a line VI-VI in FIG. 5.

[0068] As illustrated in FIG. 6, in the engine body 3 according to this embodiment, from the +X side, a first cylinder 3a, a second cylinder 3b, a third cylinder 3c, a fourth cylinder 3d, a fifth cylinder 3e, and a sixth cylinder 3f are disposed in this order. Note that in FIG. 6, reference characters 3a-3f are assigned in order to indicate the locations corresponding to the cylinders 3a-3f in the cylinder head 31.

[0069] In this embodiment, a group comprised of the first cylinder 3a to the third cylinder 3c is referred to as the first cylinder group 3A, and a group comprised of the fourth cylinder 3d to the sixth cylinder 3f is referred to as the second cylinder group 3B. In the engine 2 according to this embodiment, the driving control is carried out so that fuel is not injected successively to the first cylinder 3a to the third cylinder 3c belonging to the first cylinder group 3A, and similarly, the fuel is not injected successively to the fourth cylinder 3d to the sixth cylinder 3f belonging to the second cylinder group 3B. For example, in the engine 2, the fuel is injected in the order of the first cylinder 3a=>the fifth cylinder 3e=>the third cylinder 3c=>the sixth cylinder 3f=>the second cylinder 3b=>the fourth cylinder 3d.

[0070] The first cylinder 3a is connected to the exhaust port 31c (independent exhaust passage part) and the exhaust port 31d (independent exhaust passage part). Similarly, the second cylinder 3b is connected to the exhaust port 31e (independent exhaust passage part) and the exhaust port 31f (independent exhaust passage part), and the third cylinder 3c is connected to the exhaust port 31g (independent exhaust passage part) and the exhaust port 31h (independent exhaust passage part).

[0071] The exhaust ports 31c-31h are collected at a port collected part 31i provided on the Y side of the cylinder head 31. In this embodiment, the exhaust ports 31c-31h and the port collected part 31i are collectively referred to as a first exhaust port group 31A (i.e., first exhaust passage group). That is, in this embodiment, the exhaust passages provided corresponding to the first cylinder group 3A are referred to as the first exhaust port group 31A.

[0072] The casing passage part 63 of the turbocharger 6 is connected to the port collected part 31i of the first exhaust port group 31A. Specifically, the casing passage part 63 is connected to an opening 31u of the port collected part 31i on the exhaust gas downstream side.

[0073] The fourth cylinder 3d is connected to an exhaust port 31j (independent exhaust passage part) and an exhaust port 31k (independent exhaust passage part), and the fifth cylinder 3e is connected to an exhaust port 31l (independent exhaust passage part) and an exhaust port 31m (independent exhaust passage part), and the sixth cylinder 3f is connected to an exhaust port 31n (independent exhaust passage part) and an exhaust port 31o (independent exhaust passage part).

[0074] The exhaust ports 31j-31o are collected at a port collected part 31p provided on the Y side of the cylinder head 31. In this embodiment, similarly to the above, the exhaust ports 31j-31o and the port collected part 31p are collectively referred to as a second exhaust port group 31B (i.e., second exhaust passage group).

[0075] The casing passage part 64 of the turbocharger 6 is connected to the port collected part 31p of the second exhaust port group 31B. Specifically, the casing passage part 64 is connected to an opening 31v of the port collected part 31p on the exhaust gas downstream side.

[0076] In the first exhaust port group 31A, in the X-directions, the opening 31u of the port collected part 31i is disposed substantially at the center in a range from a part where the exhaust port 31c is connected to the first cylinder 3a to a part where the exhaust port 31h is connected to the third cylinder 3c. In other words, as for the opening 31u of the port collected part 31i, the port collected part 31i is disposed on the Y side of a part where the exhaust port 31f is connected to the second cylinder 3b. That is, in the first exhaust port group 31A, the exhaust ports 31c-31h have the same length (substantially the same length).

[0077] On the other hand, in the second exhaust port group 31B, in the X-directions, the opening 31v of the port collected part 31p is disposed so as to be offset to the +X side (toward the first exhaust port group 31A) from the center of a range from the part where the exhaust port 31j is connected to the fourth cylinder 3d to a part where the exhaust port 31o is connected to the sixth cylinder 3f. More specifically, the opening 31v of the port collected part 31p is disposed on the +X side from the part where the exhaust port 31j is connected to the fourth cylinder 3d.

[0078] As illustrated in FIG. 6, the casing passage part 64 is formed so as to extend substantially linearly between the part connected to the port collected part 31p to the part connected to the casing collected part 65. That is, a central path (i.e., center axis) Ax.sub.64 of the casing passage part 64 is formed substantially linearly between the opening 31v of the port collected part 31p and the casing collected part 65.

[0079] On the other hand, the casing passage part 63 has a portion bent toward the X side between the part connected to the port collected part 31i and the part connected to the casing collected part 65. That is, a central path Ax.sub.63 of the casing passage part 63 is formed so as to be bent between the opening 31u of the port collected part 31i and the casing collected part 65.

[0080] As illustrated in FIG. 6, in the cylinder head 31 of the engine body 3, the HP-EGR passage 71 is selectively connected only to the exhaust port 31c. At least a part of the HP-EGR passage 71 is formed in the cylinder head 31.

[0081] The HP-EGR passage 71 extends to the +X side from the part connected to the exhaust port 31c, and is bent to the +Y side at a tip end portion thereof. The HP-EGR passage 71 is connected to a part on the +Y side of a junction part with the exhaust port 31d of the exhaust port 31c (on the upstream in the exhaust gas flow direction).

6. Relation between Port Collected Parts 31i and 31p and Exhaust-side Water Jacket 16 in Cylinder Head 31

[0082] A relation between the port collected parts 31i and 31p and the exhaust-side water jacket 16 in the cylinder head 31 is described using FIGS. 7 and 8. FIG. 7 is a schematic cross-sectional view taken along a line VII-VII in FIG. 5, and FIG. 8 is a schematic cross-sectional view taken along a line VIII-VIII in FIG. 7.

[0083] As illustrated in FIG. 7, in a plan view of the cylinder head 31 in the Z-directions (cylinder axis directions), the port collected part 31i of the first exhaust port group 31A and the port collected part 31p of the second exhaust port group 31B are disposed so as to be separated from each other. An intermediate passage part 16a of the exhaust-side water jacket 16 is formed in an area between the port collected part 31i and the port collecting part 31p.

[0084] The coolant WF flows in the exhaust-side water jacket 16 via the intermediate passage part 16a.

[0085] As illustrated in FIG. 7, the intermediate passage part 16a of the exhaust-side water jacket 16 is formed close to and along a side wall part of the port collected part 31i on the X side, and formed close to and along a side wall part of the port collected part 31p on the +X side.

[0086] As illustrated in FIG. 8, the exhaust-side water jacket 16 of the cylinder head 31 includes an upper passage part 16b (i.e., a first upper passage part) formed on the +Z side (upward in the up-and-down directions) of the port collected part 31i, and an upper passage part 16c (i.e., a second upper passage part) formed on the +Z side (upward in the up-and-down directions) of the port collected part 31p.

[0087] The upper passage parts 16b and 16c are communicated with the intermediate passage part 16a so that the coolant WF flows therethrough.

7. Effects

[0088] According to the engine 2 of this embodiment, as described using FIGS. 7 and 8, in the cylinder head 31 of the engine body 3, the intermediate passage part 16a of the exhaust-side water jacket 16 is formed at least between the port collected part 31i of the first exhaust port group 31A and the port collected part 31p of the second exhaust port group 31B. Thus, in the engine 2 according to this embodiment, the heat generated from the port collected part 31i of the first exhaust port group in the cylinder head 31 and the heat generated from the port collected part 31p of the second exhaust port group 31B are absorbed by the intermediate passage part 16a of the exhaust-side water jacket 16.

[0089] Therefore, the engine 2 according to this embodiment is provided in the cylinder head 31 with the two exhaust port groups 31A and 31B having the port collected parts 31i and 31p, respectively, and reduces the thermal load in the area between the port collected part 31i and the port collected part 31p in the cylinder head 31.

[0090] Moreover, in the engine 2 according to this embodiment, as described using FIG. 8, since the exhaust-side water jacket 16 has the upper passage parts 16b and 16c, the heat transmitted to the +Z side from the port collected part 31i of the first exhaust port group 31A and the heat transmitted to the +Z side from the port collected part 31p of the second exhaust port group 31B are absorbed by the upper passage parts 16b and 16c. Therefore, the engine 2 according to this embodiment may reduce the thermal load at +Z side parts of the areas in the cylinder head 31 where the port collected parts 31i and 31p are disposed.

[0091] Moreover, in the engine 2 according to this embodiment, as described using FIG. 6, the location in the X-directions of the opening 31u of the port collected part 31i in the first exhaust port group 31A, and the location in the X-directions of the opening 31v of the port collected part 31p in the second exhaust port group 31B differ from each other, and the area where the intermediate passage part 16a is formed is secured between the port collected part 31i and the port collected part 31p. Therefore, it is advantageous to reduce the thermal load in the area between the port collected part 31i and the port collected part 31p in the cylinder head 31.

[0092] Moreover, in the engine 2 according to this embodiment, as described using FIGS. 5 and 6, since the structure is adopted in which the casing passage part 63 is connected to the opening 31u of the port collected part 31i, and the casing passage part 64 is connected to the opening 31v of the port collected part 31p, it is possible to reduce the exhaust resistance of exhaust gas discharged from the openings 31u and 31v.

[0093] Moreover, in the engine 2 according to this embodiment, as described using FIG. 1, since the turbine 62 of the turbocharger 6 is provided to the casing collected part 65 connected to the casing passage part 63 and the casing passage part 64, downstream in the exhaust gas flow direction, it can collect kinetic energy of the exhaust gas to improve the efficiency.

[0094] Moreover, in the engine 2 according to this embodiment, since the ECU 10 performs the fuel injection alternately over time to the cylinders 3a-3c belonging to the first cylinder group 3A and the cylinders 3d-3f belonging to the second cylinder group 3B, it can reduce the exhaust interference to achieve a higher exhaust efficiency.

[0095] As described above, the engine 2 according to this embodiment is provided in the cylinder head 31 with the two exhaust port groups 31A and 31B having the port collected parts 31i and 31p, respectively, and reduces the thermal load in the area between the port collected part 31i and the port collected part 31p in the cylinder head 31.

Modification

[0096] A structure of a multi-cylinder engine according to one modification is described using FIG. 9. FIG. 9 is a view corresponding to FIG. 8 used for the description of the previous embodiment, where a spatial relationship between a port collected part 131i and a port collected part 131p of a cylinder head 131, and an exhaust-side water jacket 116 is schematically illustrated in cross section.

[0097] Note that in the multi-cylinder engine according to this modification, since it has the same structure as the previous embodiment except for parts particularly described below, and therefore, the repeating description will be omitted.

[0098] As illustrated in FIG. 9, the cylinder head 131 according to this modification is also provided with the port collected part 131i of a first exhaust port group, the port collected part 131p of a second exhaust port group, which are separated from each other in the X-directions. Each of the port collected parts 131i and 131p extends in a direction perpendicular to the drawing sheet.

[0099] The cylinder head 131 is also provided with an exhaust-side water jacket 116 having an intermediate passage part 116a which is formed in an area between the port collected part 131i and the port collected part 131p in the X-directions. Moreover, the exhaust-side water jacket 116 has an upper passage part 116b formed in an area on the +Z side of the port collected part 131i, and an upper passage part 116c formed in an area on the +Z side of the port collected part 131p.

[0100] Further, in the cylinder head 131 of the multi-cylinder engine according to this modification, the exhaust-side water jacket 116 has a lower passage part 116d formed in an area on the Z side of the port collected part 131i, and a lower passage part 116e formed in an area on the Z side of the port collected part 131p.

[0101] In the exhaust-side water jacket 116, the upper passage parts 116b and 116c and the lower passage parts 116d and 116e are formed continuous to the intermediate passage part 116a. Thus, the coolant WF which flows in the exhaust-side water jacket 116 also flows through the upper passage parts 116b and 116c and the lower passage parts 116d and 116e.

[0102] The multi-cylinder engine according to this modification has the following effects because it is provided in the cylinder head 131 of the engine body with the exhaust-side water jacket 116 having the above structure, in addition to the effects of the multi-cylinder engine 2 according to the previous embodiment.

[0103] In the multi-cylinder engine according to this modification, since the exhaust-side water jacket 116 has the lower passage parts 116d and 116e in addition to the intermediate passage part 116a and the upper passage parts 116b and 116c, heat transmitted to the Z side from the port collected part 131i of the first exhaust port group and heat transmitted to the Z side from the port collected part 131p of the second exhaust port group are absorbed by the lower passage parts 116d and 116e. Therefore, the multi-cylinder engine according to this modification also reduces the thermal load at the Z side parts of the respective areas in the cylinder head 131 where the port collected part 131i and the port collected part 131p are provided.

Other Modifications

[0104] Although in the above embodiment and modification, the coolant is used as one example of the cooling medium, the present disclosure is not limited to the coolant. For example, the cylinder head and the cylinder block may also be cooled using a gas or a gas-liquid mixture.

[0105] Although in the above embodiment and modification, the intermediate passage parts 16a and 116a formed respectively between the port collected parts 31i and 131i and the port collected parts 31p and 131p are described, in the present disclosure, the passage parts of the water jacket may be provided so that the passage parts are located adjacent to other parts of the first exhaust port group 31A and the second exhaust port group 31B.

[0106] Although in the above embodiment and modification, the intermediate passage parts 16a and 116a are formed as parts of the exhaust-side water jackets 16 and 116, the present disclosure is not limited to this structure. For example, another water jacket which is separately formed from the exhaust-side water jacket may be provided in the cylinder head, and it may cool exhaust gas which passes through the port collected part.

[0107] Although in the above embodiment and modification the HP-EGR passage 71 is branched from the exhaust port 31c inside the cylinder heads 31 and 131, the present disclosure is not limited to this structure. For example, the EGR passage may also be branched from the exhaust-pipe part (corresponding to the casing passage part 63 in the above embodiment) connected to the side surface part of the cylinder head.

[0108] Although in the above embodiment and modification, the structure in which the two exhaust ports are connected to one cylinder is adopted, the present disclosure is not limited to this structure. For example, other structures in which one exhaust port is connected to one cylinder, and three or more exhaust ports are connected to one cylinder, may also be adopted.

[0109] Although in the above embodiment and modification, the engine 2 is provided with a single turbocharger 6 as one example, the present disclosure is not limited to this structure. For example, a naturally aspirated engine without the turbocharger may also be adopted, or an engine with two or more turbochargers may also be adopted, or an engine with an electric supercharger, a mechanical supercharger, etc. may also be adopted.

[0110] Although in the above embodiment and modification, the 6-cylinder diesel engine is adopted as one example of the engine body 3, the present disclosure is not limited to this structure. For example, the number of cylinders may be four or five, or may be seven or more. Moreover, the engine may be a gasoline engine, or may be a V-type, W-type, or horizontally opposed engine, without being limited to the in-series engine.

[0111] It should be understood that the embodiments herein are illustrative and not restrictive, since the scope of the invention is defined by the appended claims rather than by the description preceding them, and all changes that fall within metes and bounds of the claims, or equivalence of such metes and bounds thereof, are therefore intended to be embraced by the claims.

DESCRIPTION OF REFERENCE CHARACTERS

[0112] 2 Multi-Cylinder Engine

[0113] 3 Engine Body

[0114] 3A First Cylinder Group

[0115] 3B Second Cylinder Group

[0116] 3a-3f Cylinder

[0117] 4 Intake System

[0118] 5 Exhaust System

[0119] 6 Turbocharger

[0120] 16, 116 Exhaust-Side Water Jacket (Cooling Medium Passage)

[0121] 16a, 116a Intermediate Passage Part

[0122] 16b, 116b Upper Passage Part (First Upper Passage Part)

[0123] 16c, 116c Upper Passage Part (Second Upper Passage Part)

[0124] 31, 131 Cylinder Head

[0125] 31A First Exhaust Port Group (First Exhaust Passage Group)

[0126] 31B Second Exhaust Port Group (Second Exhaust Passage Group)

[0127] 31c-31h, 31j-31o Exhaust Port (Independent Exhaust Passage Part)

[0128] 31i, 31p, 131i, 131p Port Collected Part (Collective Exhaust Passage Part)

[0129] 41 Exhaust Passage

[0130] 63 Casing Passage Part (First Exhaust-pipe Part)

[0131] 64 Casing Passage Part (Second Exhaust-pipe Part)

[0132] 65 Casing Collected Part (Collective Exhaust-pipe Part)

[0133] 116d Lower Passage Part (First Lower Passage Part)

[0134] 116e Lower Passage Part (Second Lower Passage Part)