MULTI-CYLINDER INTERNAL COMBUSTION ENGINE
20210156333 ยท 2021-05-27
Assignee
Inventors
Cpc classification
F01N13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F1/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F1/4264
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
The disclosure provides a multi-cylinder internal combustion engine having a cylinder head that includes an exhaust port capable of cooling exhaust gas more effectively. The cylinder head includes: a first ceiling surface that closes a first cylinder having a cylinder axis separated from an exhaust opening by a first distance; a second ceiling surface that closes a second cylinder having a cylinder axis separated from the exhaust opening by a second distance shorter than the first distance; and an exhaust port that extends toward the exhaust opening from two port openings which are open to a combustion chamber for each individual cylinder. The exhaust port individually extends from each of the port openings and merges with each cylinder outside a joining surface of the cylinder head for a cylinder block in a plan view.
Claims
1. A multi-cylinder internal combustion engine (11), comprising a cylinder head (15) which comprises: a first ceiling surface (24a) that closes a first cylinder having a cylinder axis (C) separated from an exhaust opening (37) by a first distance (L1); a second ceiling surface (24b) that closes a second cylinder having a cylinder axis (C) separated from the exhaust opening (37) by a second distance (L2) shorter than the first distance (L1); and an exhaust port (32) that extends toward the exhaust opening (37) from two port openings (26) which are open to a combustion chamber (18) for each individual cylinder, wherein the exhaust port (32) individually extends from each of the port openings (26) and merges with each cylinder outside a joining surface (27) of the cylinder head (15) for a cylinder block (13) in a plan view.
2. The multi-cylinder internal combustion engine according to claim 1, wherein a wall (47) that partitions the two exhaust ports (41b) in the second cylinder extends toward an exhaust opening (37) side with respect to a virtual plane (FV) that is parallel to a virtual plane including the cylinder axis (C) of the first cylinder and the cylinder axis (C) of the second cylinder and is in contact with a tip of a wall (45) that partitions the two exhaust ports (41a) in the first cylinder.
3. The multi-cylinder internal combustion engine according to claim 1, wherein the wall (47) that partitions the two exhaust ports (41b) in the second cylinder extends to a virtual plane (SV) that is parallel to the virtual plane including the cylinder axis (C) of the first cylinder and the cylinder axis (C) of the second cylinder and is in contact with a tip of a wall (53) that partitions the exhaust port (41a) of the first cylinder and the exhaust port (41b) of the second cylinder, or extends toward the exhaust opening (37) side with respect to the virtual plane (SV).
4. The multi-cylinder internal combustion engine according to claim 2, wherein the wall (47) that partitions the two exhaust ports (41b) in the second cylinder extends to a virtual plane (SV) that is parallel to the virtual plane including the cylinder axis (C) of the first cylinder and the cylinder axis (C) of the second cylinder and is in contact with a tip of a wall (53) that partitions the exhaust port (41a) of the first cylinder and the exhaust port (41b) of the second cylinder, or extends toward the exhaust opening (37) side with respect to the virtual plane (SV).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0009]
[0010]
[0011]
[0012]
[0013]
DESCRIPTION OF THE EMBODIMENTS
[0014] In view of the above circumstances, the disclosure provides a cylinder head including an exhaust port capable of cooling the exhaust gas more effectively.
[0015] According to an embodiment, in addition to the above configuration, a wall that partitions the two exhaust ports in the second cylinder extends toward an exhaust opening side with respect to a virtual plane that is parallel to a virtual plane including the cylinder axis of the first cylinder and the cylinder axis of the second cylinder and is in contact with a tip of a wall that partitions the two exhaust ports in the first cylinder.
[0016] According to an embodiment, in addition to the above configuration, the wall that partitions the two exhaust ports in the second cylinder extends to a virtual plane that is parallel to the virtual plane including the cylinder axis of the first cylinder and the cylinder axis of the second cylinder and is in contact with a tip of a wall that partitions the exhaust port of the first cylinder and the exhaust port of the second cylinder, or extends toward the exhaust opening side with respect to the virtual plane.
[0017] According to an embodiment, two exhaust ports for each cylinder extend individually from the combustion chamber. The two exhaust ports for each cylinder merge with each cylinder outside the joining surface of the cylinder head for the cylinder block. The surface area of the exhaust port in contact with the exhaust gas increases. Since heat is transferred from the exhaust gas in the exhaust port to the metal body of the cylinder head, the exhaust gas can be effectively cooled corresponding to the increase of the surface area.
[0018] According to an embodiment, in the exhaust port, as the passage length from the port opening to the exhaust opening increases, the surface area in contact with the exhaust gas increases and the cooling effect for the exhaust gas improves. The surface area in contact with the exhaust gas decreases each time the exhaust port merges. The cooling effect is weakened. Since the passage length from the first cylinder to the exhaust opening is longer than the passage length from the second cylinder to the exhaust opening, if the wall that partitions the two exhaust ports in the second cylinder is longer than that of the first cylinder, the cooling effects of the exhaust ports in the first cylinder and the second cylinder can be balanced. The variation in exhaust temperature between the cylinders can be reduced. By converging the exhaust temperature to a specific temperature, thermal deterioration of the catalyst can be prevented. The exhaust gas can be cooled properly.
[0019] According to an embodiment, by adjusting the length of the wall that partitions the exhaust port extending from the first cylinder and the exhaust port extending from the second cylinder, the cooling effects of the exhaust ports in the first cylinder and the second cylinder can be balanced. The variation in exhaust temperature between the cylinders can be reduced. By converging the exhaust temperature to a specific temperature, thermal deterioration of the catalyst can be prevented. The exhaust gas can be cooled properly.
[0020] Hereinafter, embodiments of the disclosure will be described with reference to the accompanying drawings.
[0021]
[0022] A crankshaft 22 that is rotatably supported by a crankcase around a rotation axis Rx is connected to the piston 16. Here, four cylinder bores 12 are arranged in series in the cylinder block 13 in the axial direction of the crankshaft 22 (first cylinder bore, second cylinder bore, third cylinder bore, and fourth cylinder bore in order from one side). A connecting rod 23 connects the piston 16 and the crank pin of the crankshaft 22. The individual pistons 16 are connected to the crankshaft 22 at particular phase angles. The linear motion of the piston 16 is converted into the rotational motion of the crankshaft 22 by the action of the connecting rod 23.
[0023] As shown in
[0024] The cylinder head 15 is formed with a joining surface 27 that is liquid-tightly stacked on the cylinder block 13 around the first, second, third, and fourth ceiling surfaces 24a to 24d. On the joining surface 27, water jackets 28 connected to the water jackets (not shown) of the cylinder block 13 are opened around the first, second, third, and fourth ceiling surfaces 24a to 24d. The cylinder head 15 has a wall thickness for forming the water jackets 28 around the first, second, third, and fourth ceiling surfaces 24a to 24d. The spread of the joining surface 27 reflects the wall thickness around the first, second, third, and fourth ceiling surfaces 24a to 24d.
[0025] As shown in
[0026] The valve operating mechanism 14 causes the intake valve 34 and the exhaust valve 35 to displace in the axial direction by the action of a camshaft (not shown) that is supported by the cylinder head 15 to be rotatable around an axial center parallel to the rotation axis Rx of the crankshaft 21. A rocker arm (not shown) can be interposed between the intake valve 34 and the exhaust valve 35 and the camshaft when the intake valve 34 and the exhaust valve 35 are displaced in the axial direction.
[0027] As shown in
[0028] The exhaust port 32 includes first individual ports 41a that individually extend from the port openings 26 of the first cylinder bores toward the exhaust opening 37, second individual ports 41b that individually extend from the port openings 26 of the second cylinder bores toward the exhaust opening 37, a first confluence port 42 that is connected to the first individual ports 41a and the second individual ports 41b to merge the first individual ports 41a and the second individual ports 41b into one and gradually shrinks toward the exhaust opening 37, third individual ports 41c that individually extend from the port openings 26 of the third cylinder bores toward the exhaust opening 37, fourth individual ports 41d that individually extend from the port openings 26 of the fourth cylinder bores toward the exhaust opening 37, a second confluence port 43 that is connected to the third individual ports 41c and the fourth individual ports 41d to merge the third individual ports 41c and the fourth individual ports 41d into one and gradually shrinks toward the exhaust opening 37, and a collecting port 44 that merges the first confluence port 42 and the second confluence port 43 into one and connects them to the exhaust opening 37. The first individual ports 41a merge outside the joining surface 27 of the cylinder head 15 for the cylinder block 13 in the plan view. That is, a first wall 45 that partitions the first individual ports 41a has a mother line parallel to the cylinder axis C and extends outward from the virtual surface 46 that is in contact with the contour of the joining surface 27. The second individual ports 41b merge outside the joining surface 27 of the cylinder head 15 for the cylinder block 13 in the plan view. That is, a second wall 47 that partitions the second individual ports 41b has a mother line parallel to the cylinder axis C and extends outward from the virtual plane 48 that is in contact with the contour of the joining surface 27. Since the third cylinder bore has a cylinder axis C separated from the exhaust opening 37 by the second distance L2, similarly to the second cylinder bore, a third wall 49 that partitions the third individual ports 41c extends with the same length as the second wall 47. Here, the third individual ports 41c merge outside the joining surface 27 of the cylinder head 15 for the cylinder block 13 in the plan view. That is, the third wall 49 has a mother line parallel to the cylinder axis C and extends outward from the virtual plane 51 that is in contact with the contour of the joining surface 27. Since the fourth cylinder bore has a cylinder axis C separated from the exhaust opening 37 by the first distance L1, similarly to the first cylinder bore, a fourth wall 52 that partitions the fourth individual ports 41d extends with the same length as the first wall 45. Here, the fourth individual ports 41d merge outside the joining surface 27 of the cylinder head 15 for the cylinder block 13 in the plan view.
[0029] The second wall 47 extends toward the side of the exhaust opening 37 with respect to the virtual plane FV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the tip of the first wall 45. Similarly, the third wall 49 extends toward the side of the exhaust opening 37 with respect to the virtual plane FV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the tip of the fourth wall 52.
[0030] The second wall 47 extends to the virtual plane SV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the tip of a wall 53 that partitions the first individual ports 41a of the first cylinder bore and the second individual ports 41b of the second cylinder bore. However, the second wall 47 may extend toward the side of the exhaust opening 37 with respect to the virtual plane SV. Similarly, the third wall 49 extends to the virtual plane SV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the tip of a wall 54 that partitions the fourth individual ports 41d of the fourth cylinder bore and the third individual ports 41c of the third cylinder bore. However, the third wall 49 may extend toward the side of the exhaust opening 37 with respect to the virtual plane SV.
[0031] As shown in
[0032]
[0033] The core 56 includes a first mass portion 62 that partitions a space inside the metal body of the cylinder head 15 when forming the first confluence port 42, a second mass portion 63 that partitions a space inside the metal body of the cylinder head 15 when forming the second confluence port 43, and a third mass portion 64 that partitions a space inside the metal body of the cylinder head 15 when forming the collecting port 44. The first pipe forming portion 57 and the second pipe forming portion 58 merge with the first mass portion 62. The third pipe forming portion 59 and the fourth pipe forming portion 61 merge with the second mass portion 63. The first mass portion 62 and the second mass portion 63 merge with the third mass portion 64. An end surface 65 that is fitted to the coupling surface 36 of the cylinder head 15 is partitioned in the third mass portion 64. The end surface 65 partitions the exhaust opening 37 on the coupling surface 36 of the cylinder head 15.
[0034] The first wall 45 is established with the metal body between the first pipe forming portions 57. The second wall 47 is established with the metal body between the second pipe forming portions 58. The third wall 49 is established with the metal body between the third pipe forming portions 59. The fourth wall 52 is established with the metal body between the fourth pipe forming portions 61. The wall 53 is established with the metal body between the adjacent first pipe forming portion 57 and second pipe forming portion 58. The wall 54 is established with the metal body between the adjacent third pipe forming portion 59 and fourth pipe forming portion 61.
[0035] The confluence position 66 between the second pipe forming portions 58 is on the side of the end surface 65 with respect to the virtual plane FV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the confluence position 67 between the first pipe forming portions 57. The confluence position 68 between the third pipe forming portions 59 is on the side of the end surface 65 with respect to the virtual plane FV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the confluence position 69 between the fourth pipe forming portions 61.
[0036] The confluence position 66 between the second pipe forming portions 58 is in the virtual plane SV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the confluence position 71 between the adjacent first pipe forming portion 57 and second pipe forming portion 58. The confluence position 68 between the third pipe forming portions 59 is in the virtual plane SV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the confluence position 72 between the adjacent third pipe forming portion 59 and fourth pipe forming portion 61. However, similarly to the second wall 47 and the third wall 49 described above, the confluence positions 66 and 68 may be on the side of the end surface 65 with respect to the virtual plane SV.
[0037] In the cylinder head 15 according to the present embodiment, two individual ports 41a, 41b, 41c, 41d for each cylinder extend individually from the combustion chamber 18. The two exhaust ports 41a, 41b, 41c, 41d for each cylinder merge with each cylinder outside the joining surface 27 of the cylinder head 15 for the cylinder block 13. The surface area of the exhaust port 32 in contact with the exhaust gas increases. Since heat is transferred from the exhaust gas in the exhaust port 32 to the metal body of the cylinder head 15, the exhaust gas can be effectively cooled corresponding to the increase of the surface area.
[0038] In the exhaust port 32, as the passage length from the port opening 26 to the exhaust opening 37 increases, the surface area in contact with the exhaust gas increases and the cooling effect for the exhaust gas improves. The surface area in contact with the exhaust gas decreases each time the exhaust port 32 merges. The cooling effect is weakened. Since the passage length from the port openings 26 corresponding to the outer first cylinder bore and fourth cylinder bore among the four cylinder bores in series to the exhaust opening 37 is longer than the passage length from the port openings 26 corresponding to the inner second cylinder bore and third cylinder bore to the exhaust opening 37, if the second wall 47 and the third wall 49 that partition the individual ports 41b and 41c corresponding to the second cylinder bore and the third cylinder bore are longer than the first wall 45 and the fourth wall 52 that partition the individual ports 41a and 41d corresponding to the first cylinder bore and the fourth cylinder bore, the cooling effect can be balanced at the exhaust ports 41a and 41d corresponding to the first and fourth cylinder bores and the exhaust ports 41b and 41c corresponding to the second and third cylinder bores. The variation in exhaust temperature between the cylinders can be reduced. By converging the exhaust temperature to a specific temperature, thermal deterioration of the catalyst can be prevented. The exhaust gas can be cooled properly.
[0039] In the present embodiment, the second wall 47 and the third wall 49 that partition the individual ports 41b and 41c corresponding to the inner second cylinder bore and third cylinder bore among the four cylinder bores in series extend to the virtual plane SV that is parallel to the virtual plane including the cylinder axes C of the first, second, third, and fourth cylinder bores and is in contact with the tips of the wall 53 that partitions the adjacent first individual port 41a and second individual port 41b and the wall 54 that partitions the adjacent third individual port 41c and fourth individual port 41d. By adjusting the lengths of the walls 53 and 54 in this way, the cooling effect of the exhaust port 32 corresponding to the inner second cylinder bore and third cylinder bore among the four cylinder bores in series can be balanced with the cooling effect of the exhaust port 32 corresponding to the outer first cylinder bore and fourth cylinder bore. The variation in exhaust temperature between the cylinders can be reduced. By converging the exhaust temperature to a specific temperature, thermal deterioration of the catalyst can be prevented. The exhaust gas can be cooled properly. In order to balance the cooling effect, the second wall 47 and the third wall 49 may extend to the exhaust opening 37 with respect to the virtual plane SV.