GB2125515A - Piston ring lubrication in internal combustion engines - Google Patents

Piston ring lubrication in internal combustion engines Download PDF

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Publication number
GB2125515A
GB2125515A GB08320671A GB8320671A GB2125515A GB 2125515 A GB2125515 A GB 2125515A GB 08320671 A GB08320671 A GB 08320671A GB 8320671 A GB8320671 A GB 8320671A GB 2125515 A GB2125515 A GB 2125515A
Authority
GB
United Kingdom
Prior art keywords
piston ring
recess
running surface
ducts
groove
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB08320671A
Other versions
GB2125515B (en
GB8320671D0 (en
Inventor
Goosen Joop Hellingman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sulzer AG
Original Assignee
Sulzer AG
Gebrueder Sulzer AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sulzer AG, Gebrueder Sulzer AG filed Critical Sulzer AG
Publication of GB8320671D0 publication Critical patent/GB8320671D0/en
Publication of GB2125515A publication Critical patent/GB2125515A/en
Application granted granted Critical
Publication of GB2125515B publication Critical patent/GB2125515B/en
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J9/00Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
    • F16J9/12Details
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

An internal combustion engine having a piston ring (28) and a cylinder running surface formed with lubrication openings (20). The running surface (34) of the piston ring (28) is formed with at least one recess (43) extending in the axial direction of the piston ring (28) as far as its end face on the cylinder head side, the recess having on the crankshaft side a boundary edge extending in the running surface (34) at an inclination to the peripheral direction. <IMAGE>

Description

SPECIFICATION Internal combustion engines This invention relates to an internal combustion engine having a piston ring and a cylinder running surface formed with lubrication openings.
Engines of the aforementioned kind have a disadvantage in that oil is inadequately distributed in the peripheral direction, since the piston ring, when it travels over the lubrication openings, has a wiping action, as a result of which the edge of the piston ring on the cylinder head side drives the oil from the lubrication opening in a bead or drop in the axial direction of the cylinder. The result is an excessive concentration of oil in the immediate neighbourhood of the lubrication opening, whereas the oil film is inadequate in the regions between lubrication openings. This causes excessively rapid wear of the cylinder liner in the region between lubrication openings, and a corresponding deterioration in running properties and an increase in the consumption of lubricant by the engine.
It is known from Swiss Patent Specification CH-A-6 1 6 989 for the lubrication openings to be in the form of inclined lubrication grooves in the cylinder wall, but this construction is relatively expensive to manufacture.
An object of the invention is to design an internal combustion engine of the initially mentioned kind which is relatively cheap to manufacture but ensures good distribution of oil in the peripheral direction and thus improves the running properties and reduces the consumption of lubricant.
According to the present invention, an inter nal combustion engine has a cylinder with a running surface formed with lubrication openings, and a piston reciprocatable in the piston and having a piston ring the running surface of which is formed with at least one recess extending in the axial direction of the piston ring as far as its end face adjacent the cylinder head and having on the crankshaft side a boundary edge extending in the running surface at an inclination to the peripheral direction. As a result, when the piston ring travels over the lubrication openings, it scrapes the lubricating oil and spreads it out peripherally over the entire cylinder running surface. The lubrication openings can be ordinary capillary bores, without the need to form expensive lubrication grooves in the contact surface.
In a specially advantageous embodiment, the recess has a concave surface, thus increasing the oil-storing action of the recess.
In a preferred form, the running surface of the piston ring is formed with a groove extending transversely of the piston ring axis, the groove communicating with the side of the piston ring adjacent the cylinder head via at least two ducts extending in a direction having at least a component transversely to the peripheral direction, the recess extending between those openings of two successive ducts which are adjacent the cylinder head.
This further increases the oil-storing action of the groove in the piston ring.
Preferably, the groove and/or the ducts are inclined to the peripheral direction and that boundary wall of the recess which is adjacent the crankshaft is inclined to the peripheral direction in the same sense as the groove and/or ducts. This additionally increases the scraping and oil-distributing action of the recess.
The invention may be carried into practice in various ways but one engine embodying the invention will now be described by way of example with reference to the accompanying drawings, in which: Figure 1 is a longitudinal section through the cylinder of an internal combustion engine with a piston fitted with piston rings; Figure 2 is an enlarged view of part of one of the piston rings in Fig. 1, shown from the front in the ring plane; Figure 3 is a plan view corresponding to Fig. 2; Figure 4 shows part of another piston ring, in a view corresponding to Fig. 2; Figure 5 is a plan view corresponding to Fig. 4; Figure 6 shows part of a gas-tight piston ring in a view corresponding to Fig. 2; Figure 7 is a section along line VII-VII in Fig. 4; and Figure 8 is a section along line VIII-VIII in Fig. 6 A cylinder liner (Fig. 1) of a two-stroke diesel engine, e.g. for ships, is formed with inlet ports 1 2 and exhaust ports 1 4 and has an inner wall 1 6 formed with lubrication bores 20 supplied with lubricating oil. A piston 22 reciprocates in the liner 10 and has a top part 24 in which both conventional piston rings 25 and piston rings 26, 28, 30 formed with recesses or peripheral grooves and ducts are guided in grooves. The top part 24 merges into a bottom part 32 having a substantially cylindrical outer surface, the outer diameter of which is less than the outer diameter of part 24. The piston 22 is secured to a piston-rod (not shown), the other end of which is pivoted to a cross-head (not shown).
The piston ring 26 (Figs. 2, 3) has a running surface 34 which engages against the wall 1 6 of the liner 10 and has, as latch, a slit 38 to provide resilience to enable the running surface 34 to be pressed against the wall 16.
The running surface of the piston ring 26 has at least one recess 40 extending axially as far as the ring end face 39 adjacent the cylinder head and having on the side adjacent the crankshaft a boundary edge 42 extending in the running surface 34 at an inclination to the peripheral direction. Each recess 40 has a plane inclined surface 36 which, as shown in Fig. 7, extends towards the upper end face 39 at an angle a which is advantageously more than about 10 but less than 90 .
Piston ring 28 (Figs. 4, 5) is formed with a peripheral groove 37 and ducts 41, which latter extend perpendicularly to the peripheral direction and between which the recesses 43 extend. The groove 37 has a semi-circular cross-section.
The gas-tight piston ring 30 (Figs. 6, 8) has a latch 44 in the form of interlocking tabs or fingers 46, 48 at its ends, as described, for example, in Swiss Patent Specification CH-A482 954. In this case a helical groove 50 ends before the latch 44 and ducts 52 which extend at an inclination to the top end face open into the groove 50. As in the previous example, recesses 54 extend between ducts 52. In the present case, the boundary edge 55 on the crankshaft side is inclined to the peripheral direction in the same sense as and at approximately the same angle of inclination as the groove 50 but could be closer to the inclination of the ducts 52. As Fig. 8 shows, in this case the recess 54 has a concave surface 53 whereas the groove 50 has a triangular cross-section which also enables the wear and rotational position of the piston ring to be determined.
When the engine described is in operation and the gas pressure drives the piston 22 from its bottom dead-centre position towards the cylinder head, a film of lubricating oil which is stored in the recess 54 is scraped over the surface of the cylinder wall 1 6 and spread out by the oblique boundary edge 55 as shown in Fig. 6, the diagrammatically indicated lubrication bore 20 coinciding with the groove 50 in the position shown. Gas flows in the direction of arrows 56 through the ducts 52 and the groove 50, and then flows past the bores 20 and accelerates the peripheral distribution of lubricating oil. The ducts 52 also co-operate with the groove 50 to equalise the pressure.
Of course, each of recesses 40, 43, 54 may alternatively be formed so as to extend as a single recess substantially around the entire periphery of the piston ring.

Claims (4)

1. An internal combustion engine having a cylinder with a running surface formed with lubrication openings, and a piston reciprocatable in the piston and having a piston ring the running surface of which is formed with at least one recess extending in the axial direction of the piston ring as far as its end face adjacent the cylinder head and having on the crankshaft side a boundary edge extending in the running surface at an inclination to the peripheral direction.
2. An engine as claimed in Claim 1 in which the recess has a concave surface.
3. An engine as claimed in Claim 1 or Claim 2 in which the running surface of the piston ring is formed with a groove extending transversely of the piston-ring axis, the groove communicating with the side of the piston ring adjacent the cylinder head via at least two ducts extending in a direction having at least a component transverse to the peripheral direction, and the recess extending between those openings of two successive ducts which are adjacent the cylinder head.
4. An engine as claimed in Claim 3 in which the groove and/or the ducts are inclined to the peripheral direction and that boundary wall of the recess which is adjacent the crankshaft is inclined to the peripheral direction in the same sense as the groove and/or ducts.
4. An engine as claimed in Claim 3 in which the groove and/or the ducts are inclined to the peripheral direction and that boundary wall of the recess which is adjacent the crankshaft is inclined to the peripheral direction in the same sense as the groove and/or ducts.
5. An internal combustion engine substantially as described herein with reference to Fig. 1 and having a piston ring substantially as described herein with reference to Figs. 2 and 3 or a piston ring substantially as described herein with reference to Figs. 4 and 5 or a piston ring substantially as described herein with reference to Figs. 6, 7 and 8 of the accompanying drawings.
CLAIMS (13 Oct 1983)
1. An internal combustion engine having a cylinder with a running surface formed with lubrication openings, and a piston reciprocatable in the cylinder and having a piston ring the running surface of which is formed with at least one recess extending in the axial direction of the piston ring as far as its end face adjacent the cylinder head, (the recess being open here along its full length), and having on the crankshaft side a boundary edge extending in the running surface at an inclination to the peripheral direction.
2. An engine as claimed in Claim 1 in which the recess has a concave surface.
3. An engine as claimed in Claim 1 or Claim 2 in which the running surface of the piston ring is formed with a groove extending transversely of the piston ring axis, the groove communicating with the side of the piston ring adjacent the cylinder head via at least two ducts extending in a direction having at least a component transverse to the peripheral direction, and the recess extending between those openings of two successive ducts which are adjacent the cylinder head.
GB08320671A 1982-08-16 1983-08-01 Piston ring lubrication in internal combustion engines Expired GB2125515B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH4884/82A CH657667A5 (en) 1982-08-16 1982-08-16 PISTON INTERNAL COMBUSTION ENGINE WITH A PISTON RING AND A CYLINDER TUBE HAVING LUBRICATION OPENINGS.

Publications (3)

Publication Number Publication Date
GB8320671D0 GB8320671D0 (en) 1983-09-01
GB2125515A true GB2125515A (en) 1984-03-07
GB2125515B GB2125515B (en) 1986-01-22

Family

ID=4284217

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08320671A Expired GB2125515B (en) 1982-08-16 1983-08-01 Piston ring lubrication in internal combustion engines

Country Status (7)

Country Link
JP (1) JPS5949355A (en)
CH (1) CH657667A5 (en)
DE (1) DE3231336C2 (en)
DK (1) DK154905C (en)
GB (1) GB2125515B (en)
IT (1) IT1164379B (en)
SU (1) SU1304753A3 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5088745A (en) * 1989-11-09 1992-02-18 Hallite Seals International Limited Seals and seal assemblies

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02118282U (en) * 1989-03-06 1990-09-21
DE19942242A1 (en) * 1999-09-04 2001-03-15 Man B & W Diesel As Kopenhagen Reciprocating machine
DE19942241C2 (en) * 1999-09-04 2003-12-24 Man B & W Diesel As Kopenhagen reciprocating engine
JP2007309376A (en) * 2006-05-17 2007-11-29 Toyota Motor Corp Piston ring
DE102015116838B3 (en) * 2015-10-05 2017-02-02 Federal-Mogul Burscheid Gmbh piston ring

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB411426A (en) * 1932-09-30 1934-05-30 Anglo Persian Oil Company Ltd Improvements relating to pistons
GB586577A (en) * 1944-01-28 1947-03-24 Constantino Penco Improvements in or relating to internal combustion engines
GB1029899A (en) * 1964-08-29 1966-05-18 Burmeister & Wains Mot Mask Improvements in and relating to a lubrication arrangement for pistons, such as pistons for internal combustion engines
GB1504478A (en) * 1975-08-26 1978-03-22 Sulzer Ag Piston rings for internal combustion engines
GB2108237A (en) * 1981-10-23 1983-05-11 Sulzer Ag Internal combustion engine having a split piston ring

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE515025A (en) *
AT281504B (en) * 1967-11-10 1970-05-25 Bayerische Motoren Werke Ag Pistons with piston rings for internal combustion engines
CH616989A5 (en) * 1976-11-18 1980-04-30 Sulzer Ag Piston internal combustion engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB411426A (en) * 1932-09-30 1934-05-30 Anglo Persian Oil Company Ltd Improvements relating to pistons
GB586577A (en) * 1944-01-28 1947-03-24 Constantino Penco Improvements in or relating to internal combustion engines
GB1029899A (en) * 1964-08-29 1966-05-18 Burmeister & Wains Mot Mask Improvements in and relating to a lubrication arrangement for pistons, such as pistons for internal combustion engines
GB1504478A (en) * 1975-08-26 1978-03-22 Sulzer Ag Piston rings for internal combustion engines
GB2108237A (en) * 1981-10-23 1983-05-11 Sulzer Ag Internal combustion engine having a split piston ring

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5088745A (en) * 1989-11-09 1992-02-18 Hallite Seals International Limited Seals and seal assemblies

Also Published As

Publication number Publication date
IT8322440A0 (en) 1983-08-05
JPS6410653B2 (en) 1989-02-22
GB2125515B (en) 1986-01-22
JPS5949355A (en) 1984-03-21
GB8320671D0 (en) 1983-09-01
IT1164379B (en) 1987-04-08
DE3231336C2 (en) 1984-05-24
DE3231336A1 (en) 1984-02-16
DK276883D0 (en) 1983-06-16
CH657667A5 (en) 1986-09-15
DK276883A (en) 1984-02-17
DK154905C (en) 1989-05-29
SU1304753A3 (en) 1987-04-15
IT8322440A1 (en) 1985-02-05
DK154905B (en) 1989-01-02

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930801