The present invention relates to an air intake apparatus, and more particularly, it relates to an air intake apparatus including a plurality of intake ports through which air is supplied from a surge tank to cylinders
In general, a resin intake manifold (air intake apparatus) including a plurality of branch passages (intake ports) through which air is supplied from a surge tank to cylinders is known. Such an intake manifold is disclosed in Japanese Patent No. 5812696, for example.
Each of a plurality of branch passages of a resin intake manifold disclosed in Japanese Patent No. 5812696 includes funnel-shaped portions provided at its end on the surge tank side and including passage openings into which air flows from a surge tank. A plurality of passage openings are arranged along a direction in which the plurality of branch passages are aligned.
The plurality of branch passages of the resin intake manifold disclosed in Japanese Patent No. 5812696 each include a portion that curves in the direction in which the plurality of branch passages are aligned between its end on the surge tank side and its end on the cylinder side in order to avoid other installed equipment. Among the plurality of branch passages of the resin intake manifold disclosed in Japanese Patent No. 5812696, a branch passage disposed on the outermost side in the direction in which the plurality of branch passages are aligned is formed with the largest curvature. Furthermore, among the plurality of branch passages of the resin intake manifold disclosed in Japanese Patent No. 5812696, a branch passage disposed on the more inner side in the direction in which the plurality of branch passages are aligned is formed with a smaller curvature. Accordingly, the lengths of the plurality of branch passages of the resin intake manifold disclosed in Japanese Patent No. 5812696 from their ends on the surge tank side to their ends on the cylinder side are different from each other.
Patent Document 1: Japanese Patent No. 5812696
However, in the resin intake manifold disclosed in Japanese Patent No. 5812696, the lengths of the plurality of branch passages are different from each other, and thus the pulsation frequencies of the plurality of branch passages are different from each other. Thus, the resin intake manifold disclosed in Japanese Patent No. 5812696 has a problem that a pressure loss is likely to occur in the flow of air introduced into the branch passages (intake ports). Therefore, an air intake apparatus in which a pressure loss that occurs in the flow of the air introduced from the surge tank to the intake ports can be significantly reduced or prevented is desired.
The present invention has been proposed in order to solve the aforementioned problem, and an object of the present invention is to provide an air intake apparatus in which a pressure loss that occurs in the flow of air introduced from a surge tank to intake ports can be significantly reduced or prevented.
In order to attain the aforementioned object, an air intake apparatus according to an aspect of the present invention includes a surge tank including a side opening, into which air is introduced via the side opening, a plurality of intake ports through which the air is introduced from the surge tank to each of a plurality of cylinders of an engine body, and a plurality of funnel-shaped portions provided at ends of the plurality of intake ports on a side of the surge tank. The plurality of funnel-shaped portions respectively include open ends located at positions at which lengths of the plurality of intake ports from ends thereof on the side of the surge tank to ends thereof on sides of the plurality of cylinders are aligned with each other, the open ends being provided along a direction perpendicular to a direction in which respective centerlines of the plurality of intake ports extend.
In the air intake apparatus according to this aspect of the present invention, as described above, in the plurality of intake ports, the lengths from the ends on the side of the surge tank to the ends on the sides of the cylinders are aligned with each other. Accordingly, the pulsation frequencies of the plurality of intake ports can be aligned with each other. Furthermore, the open ends are provided in the direction perpendicular to the centerlines of the intake ports, and thus it is possible to facilitate air inflow from the surge tank into the intake ports along the centerlines of the intake ports. Consequently, a pressure loss that occurs in the flow of the air introduced from the surge tank into the intake ports can be significantly reduced or prevented.
In the aforementioned air intake apparatus according to this aspect, a first straight line that connects first center points as positions of the respective centerlines of the plurality of intake ports at the open ends of the plurality of funnel-shaped portions adjacent to each other is preferably inclined with respect to a direction in which the plurality of intake ports are aligned.
According to this structure, the first straight line is inclined such that one of the open ends of the adjacent funnel-shaped portions is located closer to the cylinders (on the opposite side to the surge tank) than the other of the open ends of the adjacent funnel-shaped portions. Accordingly, even when a large curve is formed in one intake port, the extension of one intake port due to the curve can be adjusted by being offset by one funnel-shaped portion disposed closer to the cylinders (on the side of the surge tank). Consequently, the lengths of the plurality of intake ports can be easily aligned with each other.
In this case, the respective centerlines of the plurality of intake ports are preferably arcuate, centered on port center points, the open ends of the plurality of funnel-shaped portions preferably include inner edges on sides of the port center points, and outer edges located further away from the port center points than the inner edges, and the open ends of the plurality of funnel-shaped portions are preferably provided in such a manner as to be twisted along the direction in which the plurality of intake ports are aligned due to a second straight line that connects second center points in the direction in which the plurality of intake ports are aligned at the inner edges of the open ends of the plurality of adjacent funnel-shaped portions and a third straight line that connects third center points in the direction in which the plurality of intake ports are aligned at the outer edges of the plurality of adjacent funnel-shaped portions.
According to this structure, the open ends of the adjacent funnel-shaped portions provided along the direction perpendicular to the centerlines of the intake ports can be continuously connected along a direction inclined with respect to the direction in which the intake ports are aligned.
In the aforementioned air intake apparatus in which surfaces defined by the second straight line and the third straight line are provided in such a manner as to be twisted along the direction in which the intake ports are aligned, the inner edges of the plurality of adjacent funnel-shaped portions are preferably connected to each other with no step therebetween, and the outer edges of the plurality of adjacent funnel-shaped portions are preferably connected to each other with no step therebetween.
According to this structure, the open ends of the adjacent funnel-shaped portions provided along the direction perpendicular to the centerlines of the intake ports can be smoothly connected along the direction inclined with respect to the direction in which the intake ports are aligned. Thus, the pressure loss that occurs in the flow of the air introduced from the surge tank into the intake ports can be further significantly reduced or prevented.
In the aforementioned air intake apparatus according to this aspect, areas of openings in respective cross sections of the plurality of intake ports preferably increase from the sides of the plurality of cylinders toward the side of the surge tank, and among the plurality of funnel-shaped portions, an area of an opening of an open end of a funnel-shaped portion located closest to the side opening of the surge tank is preferably the largest, and an area of an opening of an open end of a funnel-shaped portion located further away from the side opening preferably becomes smaller.
According to this structure, the funnel-shaped portion is disposed closest to the side opening of the surge tank such that the area of the opening of the open end of the funnel-shaped portion into which air is least likely to flow from the surge tank can be maximized. Furthermore, the funnel-shaped portion is disposed further away from the side opening of the surge tank such that the area of the opening of the open end of the funnel-shaped portion into which air is more likely to flow from the surge tank can be made smaller. Consequently, the amount of air that flows into the plurality of intake ports can be made approximately uniform.
In the aforementioned air intake apparatus according to this aspect, ends of boundary walls of the plurality of adjacent funnel-shaped portions on the side of the surge tank each preferably have an arcuate shape that protrudes toward the surge tank.
According to this structure, it is possible to facilitate air inflow into the plurality of intake ports.
In the aforementioned air intake apparatus having the first center points, the straight line that connects the first center points at respective open ends of four funnel-shaped portions in a four-cylinder engine is preferably inclined throughout at a constant angle with respect to the direction in which the plurality of intake ports are aligned.
According to this structure, a disturbance in the flow of air that flows into the plurality of intake ports can be significantly reduced or prevented. Thus, the pressure loss that occurs in the air intake apparatus can be significantly reduced or prevented.
An embodiment of the present invention is hereinafter described on the basis of the drawings.
The structure of an air intake apparatus 1 according to the embodiment of the present invention is now described with reference to
The air intake apparatus 1 is provided in an in-line four-cylinder engine 10 (an example of an engine body) for an automobile. The engine 10 includes a cylinder head 5, a cylinder block 14 below the cylinder head 5, and a head cover 15 above the cylinder head 5.
As shown in
As shown in
As shown in
The first port 31, the second port 32, and the third port 33 in the middle piece 12 and the upper piece 13 respectively include a first curved portion 31a, a second curved portion 32a, and a third curved portion 33a, each of which has a spiral portion curved in the X1 direction. The first curved portion 31a of the first port 31 is most strongly curved to the X1 side, the second curved portion 32a of the second port 32 is second most strongly curved to the X1 side, and the third curved portion 33a of the third port is least strongly curved to the X1 side. The fourth port 34 in the middle piece 12 and the upper piece 13 does not include a curved portion.
In the middle piece 12 and the upper piece 13, the length of the first port 31 in an air flow direction is longer than the length of the second port 32 in the air flow direction. In the upper piece 13, the length of the second port 32 in the air flow direction is longer than the length of the third port 33 in the air flow direction. In the upper piece 13, the length of the third port 33 in the air flow direction is longer than the length of the fourth port 34 in the air flow direction. Thus, in the middle piece 12 and the upper piece 13, the lengths of the first port 31, the second port 32, the third port 33, and the fourth port 34 in the air flow direction are different.
As shown in
As described above, in the middle piece 12 and the upper piece 13, the lengths of the first port 31, the second port 32, the third port 33, and the fourth port 34 in the air flow direction are different, and thus when the lengths of the first port 31, the second port 32, the third port 33, and the fourth port 34 in the air flow direction in the lower piece 11 are the same, the lengths of the first port 31, the second port 32, the third port 33, and the fourth port 34 in the air flow direction are different as a whole.
When the lengths of the first port 31, the second port 32, the third port 33, and the fourth port 34 in the air flow direction are different, the pulsation frequencies of the first port 31, the second port 32, the third port 33, and the fourth port 34 are different. In this case, it is difficult to increase the amount of air inflow from the first port 31, the second port 32, the third port 33, and the fourth port 34 in the plurality of cylinders 6 in the engine 10, respectively. Furthermore, a pressure loss is likely to occur in each of the first port 31, the second port 32, the third port 33, and the fourth port 34. Therefore, the plurality of funnel-shaped portions 7 according to this embodiment are arranged at positions at which the lengths of the plurality of intake ports 3 from their ends on the surge tank 2 side to their ends on the cylinder 6 side (the ends on the downstream side in the air flow direction) are aligned with each other. That is, the plurality of funnel-shaped portions 7 are arranged in such a manner that the lengths of the first port 31, the second port 32, the third port 33, and the fourth port 34 in the air flow direction are aligned with each other. The arrangement positions of the plurality of funnel-shaped portions 7 are described below.
As shown in
In the middle piece 12 and the upper piece 13, the length of the second port 32 is the second longest among the plurality of intake ports 3, and thus in the lower piece 11, the length of the second port 32 is the second shortest among the plurality of intake ports 3. Therefore, as shown in
In the middle piece 12 and the upper piece 13, the length of the third port 33 is the third longest among the plurality of intake ports 3, and thus in the lower piece 11, the length of the third port 33 is the third shortest among the plurality of intake ports 3. Therefore, as shown in
In the middle piece 12 and the upper piece 13, the length of the fourth port 34 is the shortest among the plurality of intake ports 3, and thus in the lower piece 11, the length of the fourth port 34 is the longest among the plurality of intake ports 3. Therefore, as shown in
As shown in
As shown in
The second funnel 72 includes a second open end 82 as the open end 8 formed along the direction perpendicular to the direction in which the centerline B2 of the second port 32 extends in the lower piece 11. As shown in
The third funnel 73 includes a third open end 83 as the open end 8 formed along the direction perpendicular to the direction in which the centerline B3 of the third port 33 extends in the lower piece 11. As shown in
The fourth funnel 74 includes a fourth open end 84 as the open end 8 formed along the direction perpendicular to the direction in which the centerline B4 of the fourth port 34 extends in the lower piece 11. As shown in
In the air intake apparatus 1, the areas of the openings in the cross sections of the plurality of intake ports 3 increase from the cylinder 6 side toward the surge tank 2 side. Specifically, as shown in
Thus, in the air intake apparatus 1, the area of the opening of the open end 8 of the funnel-shaped portion 7 located closest to the side opening 4 in the surge tank 2 among the plurality of funnel-shaped portions 7 is the largest, and the areas of the openings of the open ends 8 of the funnel-shaped portions 7 become smaller as the funnel-shaped portions 7 are located further away from the side opening 4. Specifically, the areas of the openings of the intake ports 3 decrease from the surge tank 2 side toward the cylinder 6 side in the air flow direction, and thus the opening of the funnel-shaped portion 7 located closer to the cylinders 6 has a smaller area.
As shown in
The second funnel 72 of the plurality of funnel-shaped portions 7 is disposed closer to the cylinders 6 than the third funnel 73 and the fourth funnel 74 in the air flow direction, and is located closer to the surge tank 2 than the first funnel 71. Therefore, the area of the second opening A2 of the second funnel 72 is the second smallest among the plurality of funnel-shaped portions 7.
The third funnel 73 of the plurality of funnel-shaped portions 7 is located closer to the cylinders 6 than the fourth funnel 74 in the air flow direction, and is located closer to the surge tank 2 than the first funnel 71 and the second funnel 72. Therefore, the area of the third opening A3 of the third funnel 73 is the third smallest among the plurality of funnel-shaped portions 7.
The fourth funnel 74 of the plurality of funnel-shaped portions 7 is located closer to the surge tank 2 than the first funnel 71, the second funnel 72, and the third funnel 73 in the air flow direction. Therefore, the area of the fourth opening A4 of the fourth funnel 74 is the largest among the plurality of funnel-shaped portions 7.
As shown in
As shown in
A line connecting the second center point U1 of the first inner edge 81a, the second center point U2 of the second inner edge 82a, the second center point U3 of the third inner edge 83a, and the second center point U4 of the fourth inner edge 84a that are adjacent to each other is a second straight line L2. As shown in
Outer edges 8b of the plurality of intake ports 3 in the lower piece 11 respectively have third center points D1, D2, D3, and D4 located in the central portions in the direction (X direction) in which the plurality of intake ports 3 are aligned. Specifically, the first outer edge 81b of the first open end 81 has the third center point D1 located in the central portion in the direction (X direction) in which the plurality of intake ports 3 are aligned. The second outer edge 82b of the second open end 82 has the third center point D2 located in the central portion in the direction (X direction) in which the plurality of intake ports 3 are aligned. The third outer edge 83b of the third open end 83 has the third center point D3 located in the central portion in the direction (X direction) in which the plurality of intake ports 3 are aligned. The fourth outer edge 84b of the fourth open end 84 has the third center point D4 located in the central portion in the direction in which the plurality of intake ports 3 are aligned.
A line connecting the third center point D1 of the first outer edge 81b, the third center point D2 of the second outer edge 82b, the third center point D3 of the third outer edge 83b, and the third center point D4 of the fourth outer edge 84b that are adjacent to each other is a third straight line L3. As shown in
Furthermore, as shown in
As shown in
Furthermore, as shown in
In the air intake apparatus 1, the open ends 8 of the funnel-shaped portions 7 are provided in such a manner as to be twisted along the direction (X direction) in which the plurality of intake ports 3 are aligned due to the second straight line L2 and the third straight line L3. Specifically, as shown in
As shown in
As shown in
The end point G1 of the first boundary wall 91 is located closer to the surge tank 2 than an end point J1 of a first side wall 94 on the first one side edge 81c side in the direction (X direction) in which the intake ports 3 are aligned. That is, the end point J1 of the first side wall 94 is located closer to the cylinders 6 in the air flow direction of the first port 31. Therefore, a negative pressure generated in the first port 31 is higher in the first funnel 71 on the end point J1 side of the first side wall 94 than on the end point G1 side of the first boundary wall 91. Thus, the air flow is stronger on the end point J1 side of the first side wall 94 than on the end point G1 side of the first boundary wall 91.
As shown in
The end point G3 of the third boundary wall 93 is located closer to the surge tank 2 than the end point G2 of the second boundary wall 92. That is, the end point G2 of the second boundary wall 92 is located closer to the cylinders 6 in the air flow direction of the third port 33. Therefore, a negative pressure generated in the third port 33 is higher in the third funnel 73 on the end point G2 side of the second boundary wall 92 than on the end point G3 side of the third boundary wall 93. Thus, the air flow is stronger on the end point G2 side of the second boundary wall 92 than on the end point G3 side of the third boundary wall 93.
An end point J2 of a second side wall 95 on the fourth other side edge 84d side in the direction (X direction) in which the intake ports 3 are aligned is located closer to the surge tank 2 than the end point G3 of the third boundary wall 93. That is, the end point G3 of the third side wall is located closer to the cylinders 6 in the air flow direction of the fourth port 34. Therefore, a negative pressure generated in the fourth port 34 is higher in the fourth funnel 74 on the end point G3 side of the third boundary wall 93 than on the end point J2 side of the second side wall 95. Thus, the air flow is stronger on the end point G3 side of the third boundary wall 93 than on the end point J2 side of the second side wall 95.
According to this embodiment, the following advantageous effects are achieved.
According to this embodiment, the funnel-shaped portions 7 include the open ends 8 arranged at the positions at which the lengths of the intake ports 3 from their ends on the surge tank 2 side to their ends on the cylinder 6 side are aligned with each other in the plurality of intake ports 3, the open ends 8 being provided along the direction perpendicular to the direction in which the centerlines B extend. Accordingly, the pulsation frequencies of the plurality of intake ports 3 can be aligned with each other. Furthermore, the open ends 8 are provided in the direction perpendicular to the centerlines B of the intake ports 3, and thus it is possible to facilitate air inflow from the surge tank 2 into the intake ports 3 along the centerlines B of the intake ports 3. Consequently, a pressure loss that occurs in the flow of the air introduced from the surge tank 2 into the intake ports 3 can be significantly reduced or prevented.
According to this embodiment, the lengths of the plurality of intake ports 3 from their ends on the surge tank 2 side to their ends on the cylinder 6 side are aligned with each other, and thus the amount of air that flows through each of the plurality of intake ports 3 can be easily distributed evenly.
According to this embodiment, the pulsation frequencies of the plurality of intake ports 3 can be aligned with each other, and thus the amount of air supplied to the plurality of cylinders 6 can be increased as compared with the case in which the pulsation frequencies of the plurality of intake ports 3 are not aligned with each other.
According to this embodiment, the first straight line L1 is inclined such that one of the open ends 8 of the adjacent funnel-shaped portions 7 is located closer to the cylinders 6 than the other of the open ends 8 of the adjacent funnel-shaped portions 7. Accordingly, even when a large curve is formed in one intake port 3, the lengths of the plurality of intake ports 3 can be adjusted by offsetting the extension of one intake port 3 due to the curve by one funnel-shaped portion 7 disposed closer to the cylinders 6. Consequently, the lengths of the plurality of intake ports 3 can be easily aligned.
According to this embodiment, at the open ends 8 of the adjacent funnel-shaped portions 7, the second straight line L2 that connects the second center points U1, U2, U3, and U4 of the inner edges 8a and the third straight line L3 that connects the third center points D1, D2, D3, and D4 of the outer edges 8b can be arranged in such a manner as to be twisted relative to each other. Accordingly, surfaces (the first opening A1, the second opening A2, the third opening A3, and the fourth opening A4) defined by the second straight line L2 and the third straight line L3 can be provided in such a manner as to be twisted along the direction in which the plurality of intake ports 3 are aligned. Consequently, the open ends 8 of the adjacent funnel-shaped portions 7 provided along the direction perpendicular to the centerlines B of the intake ports 3 can be continuously connected along a direction inclined with respect to the direction in which the intake ports 3 are aligned.
According to this embodiment, the inner edges 8a are connected to each other with no step therebetween while the outer edges 8b are connected to each other with no step therebetween, and thus the open ends 8 of the adjacent funnel-shaped portions 7 provided along the direction perpendicular to the centerlines B of the intake ports 3 can be smoothly connected along the direction inclined with respect to the direction in which the intake ports 3 are aligned. Thus, the pressure loss that occurs in the flow of the air introduced from the surge tank 2 into the intake ports 3 can be further significantly reduced or prevented.
According to this embodiment, the funnel-shaped portion 7 is disposed closest to the side opening 4 of the surge tank 2 such that the area of the opening of the open end 8 of the funnel-shaped portion 7 into which air is least likely to flow from the surge tank 2 can be maximized. Furthermore, the funnel-shaped portion 7 is disposed further away from the side opening 4 such that the area of the opening of the open end 8 of the funnel-shaped portion 7 into which air is more likely to flow from the surge tank 2 can be made smaller. Accordingly, the amount of air introduced into the plurality of intake ports 3 can be made approximately uniform.
According to this embodiment, the ends of the boundary walls 9 on the surge tank 2 side each have an arcuate shape that protrudes toward the surge tank 2, and thus it is possible to facilitate air inflow into the plurality of intake ports 3.
According to this embodiment, the entire first straight line L1 that connects the first center points T1, T2, T3, and T4 is inclined at the same angle with respect to the direction (X direction) in which the plurality of intake ports 3 are aligned, and thus a disturbance in the flow of air that flows into the plurality of intake ports 3 can be significantly reduced or prevented. Thus, the pressure loss that occurs in the air intake apparatus 1 can be significantly reduced or prevented.
An air intake apparatus 201 according to a first modified example of this embodiment is now described with reference to
As shown in
In the middle piece 212 and the upper piece 213, the length of the fourth port 234 in an air flow direction is longer than the length of the third port 233 in the air flow direction. In the upper piece 213, the length of the third port 233 in the air flow direction is longer than the length of the second port 232 in the air flow direction. In the upper piece 213, the length of the second port 232 in the air flow direction is longer than the length of the first port 231 in the air flow direction.
As shown in
In the middle piece 212 and the upper piece 213, the length of the third port 233 is the second longest among the plurality of intake ports 203, and thus in the lower piece 211, the length of the third port 233 is the second shortest among the plurality of intake ports 203. Therefore, the third funnel 273 is located closer to the cylinders 6 in the air flow direction than both the first funnel 271 and the second funnel 272. Furthermore, the third funnel 273 is located closer to the surge tank 2 in the air flow direction than the fourth funnel 274.
In the middle piece 212 and the upper piece 213, the length of the second port 232 is the third longest among the plurality of intake ports 203, and thus in the lower piece 211, the length of the second port 232 is the third shortest among the plurality of intake ports 203.
Therefore, the second funnel 272 is located closer to the cylinders 6 in the air flow direction than the first funnel 271. Furthermore, the second funnel 272 is located closer to the surge tank 2 in the air flow direction than both the third funnel 273 and the fourth funnel 274.
In the middle piece 212 and the upper piece 213, the length of the first port 231 is the shortest among the plurality of intake ports 203, and thus in the lower piece 211, the length of the first port 231 is the longest among the plurality of intake ports 203. Therefore, the first funnel 271 is located closest to the surge tank 2 in the air flow direction as compared with the second funnel 272, the third funnel 273, and the fourth funnel 274.
As shown in
An air intake apparatus 301 according to a second modified example of this embodiment is now described with reference to
As shown in
In the upper piece 313, the length of the first port 331 in an air flow direction is longer than the length of the second port 332 in the air flow direction. In the upper piece 313, the length of the fourth port 334 in the air flow direction is longer than the length of the third port 333 in the air flow direction. In addition, the length of the first port 331 in the air flow direction is the same as the length of the fourth port 334 in the air flow direction. The length of the second port 332 in the air flow direction is the same as the length of the third port 333 in the air flow direction.
As shown in
As shown in
The embodiment disclosed this time must be considered as illustrative in all points and not restrictive. The scope of the present invention is not shown by the above description of the embodiment but by the scope of claims for patent, and all modifications (modified examples) within the meaning and scope equivalent to the scope of claims for patent are further included.
For example, while the air intake apparatuses 1, 201, and 301 are each provided in an in-line four-cylinder engine for an automobile in the aforementioned embodiment, the present invention is not restricted to this. The present invention may be provided in an engine other than an in-line four-cylinder engine for an automobile.
While the open ends 8, 208, and 308 of the funnel-shaped portions 7, 207, and 307 are rectangular in the aforementioned embodiment, the present invention is not restricted to this. For example, the open ends of the funnel-shaped portions may be circular or elliptical.
While the area of the opening in the cross section of each of the intake ports 3, 203, and 303 increases from the cylinder 6 side toward the surge tank 2 side in the aforementioned embodiment, the present invention is not restricted to this. For example, the area of the opening in the cross section of each of the intake ports may be constant from the cylinder side to the surge tank side.
While each of the boundary walls 9 is formed in an arcuate shape that protrudes toward the surge tank 2 in the aforementioned embodiment, the present invention is not restricted to this. In the present invention, each of the boundary walls may not be formed in an arcuate shape. The boundary walls are preferably inclined in the flow direction of air that flows into the intake ports.
While the straight line L1 that connects the first center points T1, T2, T3, and T4 at the adjacent open ends 8, 208, and 308 is inclined at a constant angle in the aforementioned embodiment, the present invention is not restricted to this. In the present invention, the straight line that connects the first center points at the adjacent open ends may be provided in such a manner that its inclination angle is different on the way.
1, 201, 301: air intake apparatus
2: surge tank
3, 203, 303: intake port
4: side opening
5: cylinder head
6: cylinder
7, 207, 307: funnel-shaped portion
8, 208, 308: open end
8
a: inner edge
8
b: outer edge
9: boundary wall
A1: first opening
A2: second opening
A3: third opening
A4: fourth opening
B1, B2, B3, B4: centerline
C1, C2, C3, C4: port center point
D1, D2, D3, D4: third center point
L1: first straight line
L2: second straight line
L3: third straight line
T1, T2, T3, T4: first center point
U1, U2, U3, U4: second center point
Number | Date | Country | Kind |
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2017-086313 | Apr 2017 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2018/006753 | 2/23/2018 | WO | 00 |