Oil cooled internal combustion engine

• US 4,440,118 A
• Filed: 04/07/1981
• Issued: 04/03/1984
• Est. Priority Date: 05/13/1980
• Status: Expired due to Term

• Current Assignee: Cummins Incorporated
• Original Assignee: Cummins Incorporated
• Inventors: Stang, John H., Cusick, Steven M.
• Primary Examiner(s): Feinberg, Craig R.
• Assistant Examiner(s): Wolfe, W. R.
• Application Number:
  US06/251,932
• Time in Patent Office: 1,092 Days
• Field of Search: 123/41.42, 123/41.79, 123/41.72, 123/41.81, 123/41.83, 123/41.84, 123/193 C, 123/668, 123/669
• US Class Current: 123/41.84
• CPC Class Codes: F01P 2003/006 the liquid being oil
• CPC Class Codes: F01P 3/02 Arrangements for cooling cylinders or cylinder heads
• CPC Class Codes: F02B 2275/14 Direct injection into combustion chamber
• CPC Class Codes: F02B 2275/34 Lateral camshaft position
• CPC Class Codes: F02B 3/06 with compression ignition compression ignition engines using air or gas for blowing fuel into compressed air in cylinder F02B13/02
• CPC Class Codes: F02F 1/16 Cylinder liners of wet type
• CPC Class Codes: F02F 1/163 the liner being midsupported
• CPC Class Codes: F02F 2007/0063 Head bolts; Arrangements of cylinder head bolts

Abstract

An oil cooled system for an internal combustion engine (2 and 2'"'"') includes a cylinder liner (22 and 22'"'"') shaped to form an annular oil flow passage (36 and 36'"'"') by an inner flow control surface (52 and 52'"'"') and outer flow control surface (56 and 56'"'"') through which engine lubrication oil flows in a very thin film under laminar flow conditions to produce a very large convective heat transfer coefficient of 300-400 BTU'"'"'s per hour-feet squared-degree Fahrenheit. To insure laminar flow conditions, the radial thickness of the annular flow passage (36 and 36'"'"') is held to less than 0.016 inches and is preferably in the range of 0.008 to 0.010 inches. The disclosed liner (22 and 22'"'"') is very accurately positioned within a cylinder bore (8) of the engine block (4) by liner stop means (68 and 68'"'"') for retaining the liner in a fixed axial position within the cylinder bore ( 8) and by inner and outer radial locating means (106, 106'"'"', 101 and 101'"'"') positioned, respectively, inwardly and outwardly of the inner flow control surface (52 and 52'"'"'). Annular oil supply passage (30 and 30'"'"') and oil collecting passages (66 and 66'"'"') are also formed to supply and collect, respectively, the cooling oil to cause the oil to flow within the flow passage (36 and 36'"'"') inwardly from the outermost portion of the liner (22) toward the crankshaft (6) for no more than about 40 percent of the total axial length of the liner (22). In one embodiment (FIGS. 1 and 2), the liner stop means (68) is adjacent the inner locating means (106). In a second embodiment, the liner stop means (68'"'"') is positioned adjacent the outer locating means (101'"'"').

Claims

1. An oil cooled cylinder liner for use in an internal combustion engine containing a cylinder bore extending inwardly from a surface for engaging an engine head toward a crankshaft to which is connected a piston for reciprocating travel within the cylinder bore and having a radially oriented liner support surface positioned inwardly from the head engaging surface and further having a lubrication oil circuit including an oil inlet for supplying oil to an exterior surface of the cylinder liner at a point axially adjacent the head engaging surface and still further having a cylindrical outside flow control surface formed on the interior of the cylinder bore having a fixed radius starting adjacent the oil inlet and extending inwardly, said cylinder liner comprising:

(a) a generally hollow cylindrical body having an interior cylindrical surface for guiding the piston during reciprocating movement and having an exterior surface one portion of which includes an oil flow passage forming means for cooperating with the outside flow control surface when the cylinder liner is mounted within the cylinder bore for forming a circumferential flow passage through which a very thin film of lubrication oil of uniform radial thickness may pass under laminar flow conditions having no circumferential component and having a linear component in a direction parallel to the central axis of said hollow cylindrical body and extending inwardly from the oil inlet when the liner is mounted within the cylinder bore, said oil flow passage forming means including an inside flow control surface having a fixed radius along its entire length which is 0.006 to 0.016 inches less than the radius of the outside flow control surface; and

(b) liner positioning means for positioning said inside flow control surface concentrically within the outside flow control surface when said hollow cylindrical body is positioned within the cylinder bore to form the oil flow passage between said inside flow control surface and the outside flow control surface with a constant radial dimension between 0.006 and 0.016 inches throughout the axial and circumferential extent of the oil flow passage, said liner positioning means including;

(1) outer locating means adjacent the outer end of said hollow cylindrical body for forming a precise radial fit with the outermost portion of the cylinder bore, said outer locating means including a radial flange positioned outwardly from said inside flow control surface,

(2) inner locating means positioned inwardly from said inside flow control surface for forming a precise radial fit with a corresponding portion of the cylinder bore when the cylinder liner is mounted within the cylinder bore, and

(3) stop means for holding said cylindrical body in a generally fixed axial position, said stop means including a radially oriented stop surface positioned outwardly from said inside flow control surface to engage the liner support surface.

2. A liner as defined in claim 1, wherein said radially oriented stop surface forms a fluid tight seal with the liner support surface when the liner is mounted within the cylinder bore.

3. In combination with the liner as claimed in claim 1, further including pump means for supplying oil to said lubrication circuit in a manner to cause oil to flow through said circumferential flow passage at a linear velocity from 5.3 to 6.6 feet per second with a total pressure drop of 17 to 33 pounds per square inch.

4. A liner as defined in claim 1, wherein said inside flow control surface extends over an axial distance which is equal to but no greater than the axial distance over which laminar flow of oil is required to achieve adequate cooling of said cylindrical body, and inside flow control surface extending over no more than approximately 40 percent of the axial length of said cylindrical body.

5. A liner as defined in claim 4, wherein said cylindrical body contains a circumferential groove located in the exterior surface of said cylindrical body inwardly from said radial flange for distributing oil from the oil inlet around the entire outer perimeter of said inside flow control surface.

6. In combination with the liner as claimed in claim 1, further including oil collecting means connected with the lubrication oil circuit for collecting oil which has passed through said circumferential flow passage, said oil collection means communicates with said circumferential flow passage through an annular opening formed at the inner end of said circumferential flow passage, said annular opening being spaced axially from the oil inlet by a distance which causes said lubrication oil to flow under laminar flow conditions over said inside flow control surface for no more than approximately 40 percent of the total axial length of said cylindrical body.

7. The combination as defined in claim 6, wherein said oil collecting means includes an annular oil collecting channel positioned between said inside flow control surface and said inner locking means, said annular oil collecting channel being formed as an undercut in the cylinder bore.