INTERNAL COMBUSTION ENGINE WITH DUAL-CHANNEL CYLINDER LINER COOLING
20210254578 · 2021-08-19
Assignee
Inventors
- Allen Yao Chen (Dunlap, IL, US)
- Aaron Gary Heintz (Washington, IL, US)
- Jason Lee Van Farowe (Brimfield, IL, US)
- Thomas L. Atwell (Peoria, IL, US)
- David L. Lueders (Henry, IL, US)
- John W. Milem (Brimfield, IL, US)
- Suresh Babu Chennagowni (Peoria, IL, US)
- Khairul Hassan (Peoria, IL, US)
Cpc classification
F02F1/004
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F1/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01P5/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F7/007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02F1/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01P5/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A cylinder liner is provided that includes a cylinder bore capable of housing a piston, a top end having an annular flange, a first cylindrical section, a second cylindrical section, and an annular ridge that separates the first cylindrical section and the second cylindrical section. When employed in an a liner bore of an engine bock, the cylinder liner provides for two channels that allow for coolant to be supplied to the cylinder liner.
Claims
1. An internal combustion engine comprising: a cylinder head; a piston; and an engine block having a liner bore and a cylinder liner countersunk into the liner bore, wherein a first annular coolant channel having a channel top end and a channel bottom end is formed between the liner bore and the cylinder liner, the cylinder liner comprising a cylinder bore housing the piston, the piston slideably received within the cylinder bore for reciprocating between a top dead center position and a bottom dead center position, and a top end having an annular flange, wherein the channel top end is closer to the top end of the cylinder liner than the piston when at a top dead center position.
2. The internal combustion engine of claim 1, wherein the channel top end is above the top dead center position of the piston.
3. The internal combustion engine of claim 1, wherein the cylinder liner and the liner bore form a second annular coolant channel below the first annular coolant channel.
4. The internal combustion engine of claim 3, wherein the engine block includes a coolant passage that is configured to accept coolant from the cylinder head and feed the coolant into the first annular coolant channel and the second annular coolant channel.
5. The internal combustion engine of claim 1, wherein the liner bore includes a recessed area with an upward facing shoulder and the annular flange of the cylinder liner forms an interface with the upward facing shoulder.
6. The internal combustion engine of claim 5, wherein the interface between the annular flange and the upward facing shoulder is a sealing interface capable of retaining coolant in the first annular coolant channel.
7. The internal combustion engine of claim 6, wherein there is no secondary seal between the cylinder liner and liner bore above the channel top end.
8. The internal combustion engine of claim 1, wherein the annular flange of the cylinder liner is at least partially positioned lower than the surface of an engine block deck.
9. The internal combustion engine of claim 1, wherein the liner bore includes a liner bore ridge and the annular ridge of the cylinder liner forms an interface with the liner bore ridge.
10. The internal combustion engine of claim 9, wherein the cylinder liner countersunk into the liner bore forms a second annular channel and the first annular channel and the second annular channel are separated by the interface between the liner bore ridge and the annular ridge of the cylinder liner.
11. The internal combustion engine of claim 9, wherein the top dead center of the piston is closer to the top end of the cylinder liner than the annular ridge of the cylinder liner.
12. The internal combustion engine of claim 11, wherein the top dead center of the piston is above the annular ridge of the cylinder liner.
13. A cylinder liner, comprising: a cylinder bore capable of housing a piston; a top end having an annular flange; a first cylindrical section acting as a first coolant groove; a second cylindrical section acting as a second coolant groove; and an annular ridge that separates the first cylindrical section and the second cylindrical section.
14. The cylinder liner of claim 1, wherein each of the first cylindrical section and the second cylindrical section of the cylinder liner have a smooth surface.
15. The cylinder liner of claim 1, wherein the annular flange is configured to form a sealing interface with a portion of an engine block.
16. A cooling system for an internal combustion engine, comprising: a water pump; an oil cooler in fluid communication with the water pump; and an engine block and cylinder head assembly, comprising: a cylinder head; a piston; and an engine block having a liner bore and a cylinder liner countersunk into the liner bore, wherein a first annular channel having an annular channel top end and an annular channel bottom end is formed between the liner bore and the cylinder liner, wherein the cylinder liner comprises: a cylinder bore housing the piston, the piston is capable of a piston stroke that includes a top dead center; a top end having an annular flange; a first cylindrical section; a second cylindrical section; and an annular ridge that separates the first cylindrical section and the second cylindrical section, wherein the annular channel top end is closer to the top end of the cylinder liner than a top dead center position of the piston.
17. A cooling system of claim 16, wherein each of the first cylindrical section and the second cylindrical section of the cylinder liner have a smooth surface.
18. The cooling system of claim 16, wherein the cylinder liner forms a second annular channel below the first annular channel.
19. The cooling system of claim 16, wherein the liner bore includes a liner bore ridge and the annular ridge of the cylinder liner forms an interface with the liner bore ridge.
20. The cooling system of claim 19, wherein the top dead center position of the piston is closer to the top end of the cylinder liner than the annular ridge of the cylinder liner.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0009] Further features and advantages of the invention will become apparent from the description of embodiments using the accompanying drawings. In the drawings:
[0010]
[0011]
[0012]
[0013]
[0014]
[0015]
DETAILED DESCRIPTION
[0016] Referring to the drawings,
[0017]
[0018] Returning to
[0019] When housed in the liner bore 214, the cylinder liner 100, in conjunction with the liner bore 214, forms a first annular coolant channel 250 and a second annular channel 252 below the first annular coolant channel 250 that allow for the passage of a coolant to cool the cylinder liner 100. The coolant is pumped within the internal combustion engine 10 through coolant passages and each of the first annular coolant channel 250 and a second annular coolant channel 252 may be fed from one or more coolant passages 254 (out of plane and shown in relief). The one or more coolant passages 254 may be configured to received coolant from the cylinder head 300. For example, the one or more coolant passages 254 may receive coolant from the cylinder head water jacket (not shown). Suitable coolants include, but are not limited to, water, glycol, or a mixture thereof.
[0020]
[0021] The cylinder liner 100 also includes an annular ridge 112 protruding radially outward from the cylindrical body of the cylinder liner 100. The annular ridge 112 may also be referred to as the pilot diameter. The annular ridge 112 separates the cylindrical body of cylinder liner 100 to form a first cylindrical section 114 and a second cylindrical section 116. The first cylindrical section 114 spans the length of the cylinder liner 100 between the annular flange 108 and the annular ridge 112. When the cylinder liner 100 is housed in the liner bore 214 of the engine block 200, the first annular coolant channel 250 is formed to allow the passage of a coolant around the cylinder liner 100 at the first cylindrical section 114. The first cylindrical section 114 has a smooth surface. The smooth surface of the first cylindrical section 114 may transition to each of the annular flange 108 and annular ridge 112 via a radiused corner.
[0022] Similar to the first cylindrical section 114, when the cylinder liner 100 is housed in the liner bore 214 of the engine block 200, a second annular coolant channel 252 is formed to allow the passage of a coolant around the cylinder liner 100 at the second cylindrical section 116. The second cylindrical section 116 has a smooth surface. The smooth surface of the second cylindrical section 116 may taper to meet the annular ridge 112. The cylinder liner 100 may be made from any suitable material or materials, such as for example, from an alloyed gray iron, aluminum, or steel (e.g., stainless steel).
[0023]
[0024] The annular flange 108 of the cylinder liner 100 includes a lower face 110. When the cylinder liner 100 is inserted into the liner bore 214, the lower face 110 of the cylinder liner 100 engages the a radially-extending, upward facing shoulder 206 of the engine block 200. Further, the annular ridge 112 of the cylinder liner 100 engages the liner bore ridge 218. The first annular coolant channel 250 is formed between the first cylindrical section 114 of the cylinder liner 100 and the cylinder bore groove 208. In certain embodiments, the first cylindrical section 114 and the cylinder bore groove 208 do not come into contact with each other within the first annular coolant channel 250. The radially-extending, upward facing shoulder 206 and the lower face 110 engage to form an interface that defines the top of the top of the first annular coolant channel 250. The lower face 110 of the cylinder liner 100 and the radially-extending, upward facing shoulder 206 of the engine block 200 are machined to form smooth surfaces. Accordingly, when coolant flows through the first annular coolant channel 250, coolant is retained within the first annular coolant channel 250 without the need for a secondary seal (e.g., sealing is provided only by the interfaces between the cylinder liner and the cylinder bore). This provides the ability for the first annular coolant channel 250 to be situated closer to the top end 102.
[0025] The second annular coolant channel 252 is formed between the second cylindrical section 116 of the cylinder liner 100 and the inner surface of the liner bore 210. When the cylinder liner 100 is inserted into the liner bore 214, an interface is formed between the liner bore ridge 218 and the annular ridge 112 of the cylinder liner 100. The interface between the liner bore ridge 218 and the annular ridge 112 forms a seal and separates the first annular coolant channel 250 and second annular coolant channel 252. While liner bore ridge 218 and the annular ridge 112 forms a seal, in certain conditions, for example during use in extremely cold temperatures, the seal may allow some cross talk of coolant between the first annular coolant channel 250 and the second annular coolant channel 252. In certain embodiments, an incomplete seal may be desired if cross talk of coolant between channels 250 and 252 is desired to prevent stagnation. The second annular coolant channel 252 may terminate at the bottom with an external seal (not shown).
[0026]
[0027]
INDUSTRIAL APPLICABILITY
[0028] The disclosed cylinder liner or cylinder liner and engine block assembly may be used in any application where it is desired to increase the reliability and operating life of the associated engine. In the disclosed embodiment, the cylinder liner includes a first coolant channel and a second coolant channel. Due to the location of the first channel being in particularly close proximity to the top of the cylinder, the coolant can achieve better access to locations on the cylinder liner that are exposed to higher levels of heat from combustion. The second channel may provide cooling to the remaining portions of the cylinder liner. Accordingly, the disclosed cylinder liner allows for the management and removal of heat generated during combustion without the need for sacrificing the durability of the cylinder liner.
[0029] It will be appreciated that the foregoing description provides examples of the disclosed system and technique. However, it is contemplated that other implementations of the disclosure may differ in detail from the foregoing examples. All references to the disclosure or examples thereof, are intended to reference the particular examples being discussed at that point and are not intended to imply any limitation as to the scope of the disclosure more generally. All language of distinction and disparagement with respect to certain features is intended to indicate a lack of preference for those features, but not to exclude such from the scope of the disclosure entirely unless otherwise indicated.
TABLE-US-00001 ELEMENT LIST Element Number Element Name 10 internal combustion engine 50 cooling system 52 water pump 54 oil cooler 56 cylinder block and head 58 thermostat housing 60 radiator 62 bypass circuit 64 cooler 100 cylinder liner 102 top end 104 bottom end 106 cylinder bore 108 annular flange 110 lower face 112 annular ridge 114 first cylindrical section 116 second cylindrical section 120 interior surface 122 exterior surface 200 engine block 204 recessed area 206 upward facing shoulder 208 liner bore groove 210 liner bore 212 piston 214 liner bore 216 combustion chamber 218 liner bore ridge 220 engine block deck 250 first annular coolant channel 252 second annular coolant channel 254 coolant passages 256 outlet 300 cylinder head 302 at least one valve 350 top dead center 352 top of the first channel 354 bottom of the first channel 356 top of the second channel 358 bottom dead center 360 piston stroke 362 first channel height 364 second channel height 366 distance to the first channel