Uncooled oilless internal combustion engine having uniform gas squeeze film lubrication

Abstract: An apparatus is described for providing a gas phase film lubrication between a reciprocal piston and a cylinder of an uncooled oilless internal combustion engine, said piston being effective to drive a rotary crankshaft in response to an expanding gas charge, comprising: (a) means connecting said crankshaft to said piston for transferring reciprocal thrust into rotary thrust, said means aligning said piston concentrically within said cylinder wall to limit the imposition of side loads on said piston; and (b) interfacing walls on said piston and cylinder, which walls (i) are sized to provide a predetermined annular gap therebetween at ambient conditions that has a radial dimension in the range of .001 ± .0005 inches, (ii) consist of matched materials that prevent closure of said gap due to thermal expansion under the maximum temperature differential to be experienced between said piston and cylinder wall, and (iii) are preshaped to anticipate any thermal growth of said interfacing walls for maintaining the annular gap substantially constant at elevated temperatures.

Description: This invention relates to the art of engine lubrication and, more particularly, to oilless lubrication for the piston/cylinder chamber of an uncooled engine. A low heat rejection engine, particularly for a diesel engine, has the potential to provide significant improvement in fuel economy. Heat rejection can be reduced by eliminating liquid cooling normally incorporated in the block of a diesel engine and replacing all or a portion of the combustion chamber components with materials that can operate at uncooled combustion temperatures, such as ceramics. This is sometimes referred to as an adiabatic diesel engine. The temperature gradient in such low heat rejection engine will range up to 1600°F (871°C). At such temperatures, conventional oil, used as a piston lubricant, will pyrolyze. Therefore, some means must be provided to create an antifriction relationship between the cylinder wall and piston which is devoid of fossil lubricants. One approach, suggested in 1983 by S. Timoney and G. Flynn in an article entitled "A Low Friction, Unlubricated Silicon Carbide Diesel Engine", SAE Paper #830313, was to install a close-fitting SiC piston in a SiC cylinder, the piston having no ring grooves. Blowing of gases past the pistons could not be detected. The authors concluded that the piston must be riding on a gas film due to the reduction in friction horsepower. However, much of their test work was carried out without the engine firing, so a pressurised gas film was not the total reason for non-scuffing but was also due to the low interfacial friction of SiC on SiC. The structure of the Timoney and Flynn piston and cylinder had made no accommodation for thermal growth and assumed uniform dimensions; oil lubrication was fed to the piston pin area which assured little dimensional change and, in fact, contributed to oil lubrication notwithstanding the authors' label of an unlubricated engine. This reference merely defined the problem without providing a specific solution as how to provide a reliable gas phase lubrication while encountering thermal growth, wide variations in the fit, and without oil lubrication. This reference did suggest that if clearances could somehow be controlled, a gas film would function to lubricate the sliding piston in such cylinder. GB 2 189 005 describes an engine including a ceramic piston with piston rings at its upper and lower ends reciprocating in a ceramic cylinder. Air is supplied by a passage to the annular cavity bounded on the inside by the piston, on the outside by the cylinder and at its top and bottom by the piston rings to provide a supporting gas film for the piston motion as the air leaks pasts the upper and lower piston rings. The present invention differs fundamentally from this prior art proposal in that it does not use piston rings and relies on air being entrained by viscous drag into the gap between the piston and the cylinder rather than being pumped into it through a special supply passage. Furthermore, GB-A-1 096 655 discloses an engine corresponding to the preamble of claim 1. According to the invention, there is provided an uncooled oilless internal combustion engine having uniform gas squeeze film lubrication between a reciprocal piston devoid of piston rings and a cylinder, said piston being effective to drive a rotary crankshaft in response to an expanding gas charge, characterised in that said engine comprises; (a) a pin and connecting rod linkage connecting said crankshaft to said piston and aligning said piston concentrically within said cylinder wall to limit the imposition of side loads on said piston; and (b) interfacing walls on said piston and cylinder which walls (i) are sized to provide a predetermined annular gap therebetween at ambient conditions that has a radial dimension in the range of .0025 ± .00125 cms (.001 ± .0005 inches). (ii) consist of matched materials that prevent closure of said gap due to thermal expansion under the maximum temperature differential to be experienced between said piston and cylinder wall, the material for the wall of said piston being silicon nitride and the material for the wall of the cylinder being selected from the group consisting of silicon nitride, silicon carbide and partially stabilised zirconia, and (iii) are preshaped to anticipate any thermal growth of said interfacing walls for maintaining the annular gap substantially constant at elevated temperatures, the piston being preshaped to have a chamber along the upper crown and said cylinder wall being preshaped to have a radial taper with the smallest dimension of said taper being at the top end of said cylinder wall. Preferably, to assure concentricity to limit side loading of the piston, the pin and connecting rod linkage are arranged with the axis of the crankshaft lying in a common plane with the axes of the piston and cylinder wall, all within a tolerance of .001cm (.0004 inches). Advantageously, the driving connection between the crankshaft and piston has the axes parallel within a tolerance of .0025cm (.001 inches) at bearings comprising; crankshaft to main bearing, crank arm to connecting rod, connecting rod to piston pin, and has the axes all perpendicular to each other within a tolerance of .001cm (.0004 inches) for the piston pin, connecting rod bearing to pin bearing, and piston travel. Advantageously, the bearings may consist of ceramic bearing elements, particularly the roller elements. The annular gap may preferably be dimensioned to limit blow-by of the gas flow charge volume to less than 2% of the flow at engine operating speeds above 1500 rpm. The invention will now be described further, by way of example, with reference to the drawings, in which : Figure 1 is a partially sectional and partially schematic view of a four-stroke uncooled oilless engine within which the invention herein is incorporated; Figure 2 is an enlarged schematic view of a piston and cylinder assembly, broken away to illustrate more clearly the gas squeeze film concept; Figure 3 is a diagram depicting side loading of the piston as a function of crank angle, with positioning of the piston and crank connection being shown in different quadrants of the crank angle; Figures 4-7 are graphical illustrations of gas blow-by and piston offset as a function of crank angle, for different gaps, engine speeds and alignments; Figures 8-10 are graphical illustrations of gas pressure and side load as a function of crank angle, for different gaps, engine speeds and alignments; Figure 11 is a schematic illustration of a preshaped piston and cylinder wall shown both in the ambient condition (cold) and in the hot (high speed) condition, and also in both the top dead centre and bottom dead centre position of the piston. Figure 12 is a thermal gradient map superimposed on each of the piston and cylinder wall and piston pin; Figure 13 is a graphical illustration of gaseous blow-by as a function of engine speed; and Figure 14 is a graphical illustration of gas blow-by as a function of the coefficient of thermal expansion for different materials at different gap clearances. An uncooled oilless four-stroke engine 10 is shown in Figure 1. Such engine has solid structural ceramic components (head 11, cylinder walls 12, piston 13 and valves 14) in the vicinity of the combustion chamber 15; metal components are eliminated in the high temperature areas of the engine. Uncooled is used herein to mean an engine that is devoid of conventional cooling such as from a water jacket or fins for air cooling. The resulting higher operating temperatures can be projected to provide at least a 9% improvement in the indicated specific fuel consumption relative to a water cooled, base line, engine at part load operating conditions (i.e., 1200 rpm at 38 psi BMEP). Since conventional oil lubrication cannot be used at the higher operating temperatures because such oils will pyrolyse, gas phase lubrication is used herein. Oil is also eliminated in the crankcase; without crankcase oil, a sealing system to separate the oil from the hot upper cylinder area, where coking can occur, is not required. Oilless ceramic roller bearings 17 and 16, for the crankshaft and connecting rod respectively, eliminate this need for oil in the crankcase. With ceramic roller bearings for the valve train finger followers and camshaft (19 and 18), as well as suitable dry lubrication, the engine is further simplified by eliminating the need for oil, the oil pump, oil filter and oil gallery drilling. However, oilless is used herein to mean devoid of conventional piston rings between the piston and cylinder wall that are designed to ride on a liquid phase film. Sintered silicon nitride was used as the material for the structural cylinder wall and piston. Sintered silicon nitride has a coefficient of thermal expansion of about 3.6 x 10⁶/°C, a modulus of rupture of about 85 ksi which is stable up through the temperature range of 871°C (1600°F) and has a thermal conductivity which is about 50% of the value of cast iron. Referring to Figure 2, gas phase lubrication between the piston 13 and the cylinder wall 12 is dependent on maintaining a tight clearance or annular gap 20 effective in triggering viscous drag 22 to hold a gas phase squeeze film 21 therebetween. Unfortunately, it is very difficult to achieve and maintain a tight and uniform annular gap 20 throughout all aspects of engine operation. The gas film 21, at low pressure gradients (when pressure 23 feeding the gas film is low during exhaust and intake strokes of a four cycle engine) will be essentially trapped between the piston 13 and the cylinder wall 12 and will ride with the piston provided the gap 20 is sufficiently narrow. The gas film at high pressure gradients (when pressure 23 feeding the gas film is high during expansion and compression strokes) will cause blow-by through the gap 20 but will be throttled due to viscous drag of the stationary cylinder wall. Such viscosity will increase with an increase in temperature of the gas at higher engine speeds. Side loading 24 of the piston (a radially directed component of a reaction force 25 from the connecting rod 26 to the piston pin 27 and thence to the piston 13) will distort concentricity of the piston within the cylinder wall and cause the gap 20 at one side of the piston to begin to close and allow contact between the piston and cylinder wall without gas phase lubrication. When the term "closure of gap" is used, one side of the annulus will move to touch the cylinder wall; it does not necessarily mean the entire annular gap is fully closed. It is important to this invention to recognise that side loading forces 24 will reach a level of less than 483 kPa (70 psi) in an engine having a peak gas pressure of 11040 kPa (1600 psi). It should also be noted that when higher peak pressures exist due to change in engine design, the squeeze film pressure will correspondingly increase and prevent piston from touching the cylinder wall at side loading up to 552kPa (80psi). The concentricity to limit side loading can be brought about by assuring alignment of the driving connection of the piston to the crankshaft 28 or crank arm 34 (which includes a piston pin 27 and a connecting rod 26). Referring again to Figure 1, this includes maintaining; (a) the axis 28 of the crankshaft in a common plane with the axes 37 of the piston 13 and cylinder wall 12 all within a tolerance of .001cm (.0004 inches); (b) parallelism within a tolerance of .0025cm (.001 inches) between the axes 28, 29 and 9 of the following respective bearings: the bearing 30 for the crankshaft 31 to the main bearing cap 32, the bearing 17 for the crank arm 34 to the connecting rod 26, and the bearing 16 for the connecting rod 26 to the piston pin 27; (c) perpendicularity within a tolerance of ±.001cm (±.0004 inches) of the axis 9 of bearing 16, axis (also 9) of the piston pin 27, and central axis 37 of the cylinder wall; and (d) maintaining the several axes 28, 9 and 37 within a common plane (seen as axis 37 in Figure 1). If this is done, the piston side loading will be limited so that concentricity of the piston during the four-stroke operation will be assured and the gas squeeze film will not be penetrated by the piston. Turning to Figure 3, operation of a gas squeeze lubricated piston was calculated by a model. The calculation was for a speed of 4200 rpm and a peak cylinder pressure 11040kPa (1600psi). The figure shows the location of the piston, depicted as a solid line 35, within the total available hot diametrical clearance 36 between the piston and cylinder wall for 720° of engine operation. Throughout the operation. it was found that the calculated gas squeeze film was adequate to prevent the piston from contacting the cylinder wall provided the clearance was .0025 ± .00125cm (.001 ± .0005 inches). The minimum clearance occurred at the bottom dead centre of the expansion stroke. Actual tests of this gas phase squeeze film lubrication system was carried out in engines to determine effective side loading due to nonalignment (offset), as shown in Figure 4-10. Figures 4 and 5 show how the fluid film blow-axes are all aligned within the criteria set forth above, Figure 4 being at 700 rpm and Figure 5 being at 4200 rpm. The plot labelled "O" is for the degree of offset (which correlates with the degree of misalignment) and plot labelled "B" is for the blow-by in percentage fraction of mass which is trapped. Figure 8 shows the amount of side loading and pressure that is experienced for the conditions of Figure 4 and, correspondingly, Figure 9 shows the amount the side loading pressure that is experienced with the conditions of Figure 5. Note that side loading does not exceed 318kg (600 pounds) at 700 rpm and does not exceed 204kg (450 pounds) at 4200 rpm. The units for side loading can be converted from pounds to psi by dividing the pounds force by the area of the piston side wall. Even when the gap is increased to .04mm, as shown in Figures 6 and 7, the piston offset will be great enough to close the gap at 700 rpm. Correspondingly, the aberrations of the side load will increase due to inertia at the higher speeds in Figure 10. It should be noted that if the gap is selected small enough as prescribed herein, the side loading will not become more severe at higher engine speeds because the gas phase film cannot be squeezed out of the gap due to its incompressible nature at such velocities and the lesser ability of the piston to travel fast enough from side to side at such higher speeds. The gap dimension was theoretically calculated and empirical tests were made to corroborate that viscosity of the gas phase increases from room temperature to higher operating temperatures. Gaps in the range of .0025 - .00375 cm (.001 - .0015 inches) would function to provide a squeeze gas film lubrication between the piston and cylinder wall so that the blow-by would not exceed 2% of the gas flow charge to the combustion chamber at higher speeds (above 1500 rpm). This invention broadly contemplates providing gas phase lubrication with a blow-by of up to 5% (on average of all speeds) of the engine mass f low charge. Normal blow-by of a conventional piston ring engine in use today has an average blow-by of about 2%. This higher toleration of blow-by in this engine is justified because the total engine energy savings from this lubrication system is much greater than the energy lost due to an increase of blow-by up to 5%. However, several factors intervene to disrupt the effectiveness of the gap 20 during operation of the piston in the engine, even though concentricity of the piston is substantially maintained within the cylinder wall. First, the inherent differential thermal expansion of the material selected for either the piston and the cylinder wall will change the gap due to experiencing the maximum temperature differential between the piston and cylinder. For example, looking at Figure 12 wherein a thermal mapping of the piston 13, cylinder wall 12 and piston pin 27 is displayed, the maximum temperature differential occurs at the upper edge 38 of the piston crown and upper edge 39 of the cylinder wall. This differential to be experienced here between the piston and cylinder wall is 1250 - 950°F = 300°F (149°C). It is possible that this differential can be as little as 149°C in some engine designs. The materials of the piston and cylinder wall must be matched so that the gap is not closed as a result of experiencing such maximum temperature differential. The piston will get hotter at its piston crown than the opposite facing cylinder wall; accordingly, the piston crown will expand or mushroom outwardly. The cylinder wall, even if made of the same material as the piston, will not move outwardly to the same degree, not only because it is cooler, but because hollow cylindrical structures place restraints on the expansion characteristic. Looking at Figure 14, it is apparent that the material with the lower coefficient of thermal expansion is more suitable to preventing a closure of the gap (indicated by elimination of blow-by) as the gap is narrowed. For purposes of this invention, it is best to utilise a material having a coefficient of thermal expansion which is less than 6 x 10⁶/°C, and preferably less than 4 x 10⁶/°C. With this in mind, the material selected for the piston should preferably be silicon nitride or silicon nitride coated with cordierite (magnesium aluminium silicate or MAS) . The cylinder wall should preferably be selected from the group consisting of silicon carbide, silicon nitride, and partially stable zirconia PSZ). Secondly, the viscosity of the combustion gas charge increases as the engine goes to higher engine speeds (see Figure 13). The third effect that must be considered is that even though the material selection is made to achieve good matching so that the gap does not close off, even under the maximum temperature differential experience, the gap may not remain uniform and may result in a closing effect. The gap should be maintained substantially uniform throughout the operation of the engine and the thermal gradients to be experienced. To this end, it is important that the interfacing surfaces of the piston and cylinder wall be preshaped to anticipate any thermal growth of such interfacing walls. As shown in Figure 11, the piston crown 40 is preshaped by chamfering at its upper region (from 41 to 42) to compensate for the extreme mushrooming effect or thermal growth that will take place along the upper annular shoulder of the crown 40. The cylinder wall, experiencing thermal expansion to a lesser degree, is preshaped by tapering the wall to have its narrowest taper at the top 43. Thus, the piston 12, in the cold condition or ambient, makes the narrowest throat or gap dimension 44 of about .0025 cm (.001 inch) in the top dead centre position, and the gap increases to .0075 cm (.003 inches) in the bottom dead centre position (see solid line for piston and cylinder wall representation). This gap distance remains roughly 0.00375 cm (.0015 inches) even in the hot clearance condition at high speed engine conditions because the preshaping of the piston crown and the matching of the materials (Si₃N₄ for the piston and Si₃N₄ for the cylinder wall) causes the piston to have a contour as shown in broken outline in the top dead centre position which is spaced a distance of .00375cm (.0015 inches) from the cylinder wall in its changed expanded condition. Even in the bottom dead centre position, the spacing remains at about .00375cm (.0015 inches) from the cylinder wall. By selection of materials to have a low coefficient of thermal expansion, sizing of the gap to provide a predetermined gap at ambient conditions of .0025 ± .00125 cm (.001 ± .0005 inches) and by preshaping the interfacing walls to anticipate thermal growth, an improved gas phase squeeze film lubrication system can be provided.

Claims: An uncooled oilless internal combustion engine having uniform gas squeeze film lubrication between a reciprocal piston (13) devoid of piston rings and a cylinder (12), said piston (13) being effective to drive a rotary crankshaft (31) in response to an expanding gas charge, characterised in that said engine comprises: (a) a pin and connecting rod linkage (26,27) connecting said crankshaft (31) to said piston (13) and aligning said piston concentrically within said cylinder wall to limit the imposition of side loads on said piston (13); and (b) interfacing walls on said piston and cylinder (13,12), which walls (i) are sized to provide a predetermined annular gap (20) therebetween at ambient conditions that has a radial dimension in the range of .0025 ± .00125cm (.001 ± .0005 inches) in the top dead center position. (ii) consist of matched materials that prevent closure of said gap due to thermal expansion under the maximum temperature differential to be experienced between said piston and cylinder wall, the material for the wall of said piston being silicon nitride and the material for the wall of the cylinder being selected from the group consisting of silicon nitride, silicon carbide and partially stabilised zirconia, and (iii) are preshaped to anticipate any thermal growth of said interfacing walls for maintaining the annular gap substantially constant at elevated temperatures, the piston (13) being preshaped to have a chamfer along the upper crown (41,42) and said cylinder wall (12) being preshaped to have a radial taper with the smallest dimension of said taper being at the top end (43) of said cylinder wall. An apparatus as claimed in claim 1, in which said pin and connecting rod linkage is arranged with the axis of said crankshaft lying in a common plane with the axes of said piston and cylinder wall, all within a tolerance of .001cm (.0004 inches). An apparatus as claimed in claim 1, in which said means (a) comprises a pin and connecting rod with antifriction bearings between said pin to connecting rod, connecting rod to crank arm, and crankshaft to main bearing, the axes of said bearings being maintained in parallelism within a plus or minus tolerance of .0025cm (.001 inches). An apparatus as claimed in claim 3, in which said means (a) further comprises perpendicularity between the axes of said bearings for said piston pin to connecting rod, the piston pin axis itself, and the axis of said cylinder wall, all within a tolerance of .001cm (.0004 inches). An apparatus as claimed in claim 3, in which said means (a) further comprises maintenance of the axis of said bearing for said crankshaft to bearing caps, the axis of the bearing for said piston pin to the connecting rod, and the axis for said cylinder wall all within a common plane in a tolerance of .001cm (.004 inches). An apparatus as claimed in claim 3, in which said antifriction bearing connection comprises ceramic roller elements. An apparatus as claimed in any preceding claim, in which said elevated temperature of (b) (iii) is in the range of 800-1200°C.

Inventors: HAVSTAD PETER H, RAO VEMULAPALLI DURGA NAGESWAR, WADE WALLACE R, HAVSTAD, PETER H., RAO, VEMULAPALLI DURGA NAGESWAR, WADE, WALLACE R.
Applicants: FORD FRANCE, FORD MOTOR CO, FORD WERKE AG, FORD FRANCE SOCIETE ANONYME, FORD MOTOR COMPANY LIMITED, FORD-WERKE AKTIENGESELLSCHAFT
Application year: 1989
Main classification: F01M9
IPC codes: F02B41, F02F7, F01M9