Pistons

Abstract: Pistons are described having polar profiles or axial profiles or both polar and axial profiles machined to asymmetric curvatures about the plane which includes both the piston axis and the minor axis over at least a part of the skirt length. By machining pistons to asymmetric profiles the bedding areas, for example, of the thrust and counter-thrust faces of the piston skirt may be more nearly optimised. This has been found to have a beneficial effect with regard to piston noise, scuffing and wear, for example, in some applications.

Description: The present invention relates to pistons and particularly to pistons for internal combustion engines. Broadly speaking a piston may be categorised into two regions; the crown and piston ring belt forming one region and the skirt including the gudgeon pin bosses forming the second region. When being machined to final shape the crown and ring belt region is usually machined to a circular polar profile. There are, however, exceptions; specific designs of some engines having deviations from this generalisation. The skirt region, however, is generally neither circular in polar profile nor linear in axial profile. The skirt region is often machined on a cam tuming machine to an oval polar profile. One example of such an oval polar profile is an ellipse where the minor diameter is parallel to the gudgeon pin axis and the major diameter lies in a direction at right-angles to the gudgeon pin axis. The ovality of a piston may be defined as the difference between the dimension of the major diameter and that of the minor diameter. The resulting figure of ovality, however, only gives the maximum deviation from a true circular polar profile and gives no indication of the shape of the curve between the major and minor diameters. Any given ovality figure could in theory be applied to an infinite number of different curves. The reasons for machining piston skirts to shapes other than circular in polar profile include some based on thermal considerations and others based on dynamic considerations relating to the environment in which the piston operates. Since for practical reasons pistons may only be economically produced by machining at ambient temperatures the form to which it is machined is an attempt to compensate for the thermal distortion which occurs during heat-up to and dynamic operation at the normal running temperature of the piston. Such distortion may be anything but uniform and will be greatly influenced by the temperature variations which occur within the piston itself. Temperatures will be higher nearer to the crown and lower at the lower skirt portions. Furthermore, the changes of section thickness in the skirt region will also influence the manner and degree of the distortion and will vary from the thin sections of the skirt per se to the thicker, stiffer regions around the pin boss and ring belt. The dynamic considerations to be made stem from the stress/strain effects during operation of the engine. The forces acting on the piston are generally at a maximum during the power stroke of the engine during combustion of the fuel. The forces due to combustion are borne mainly on one side of the piston known as the thrust face of the piston. The forces generated in the remainder of the cycle are much lower and are borne both by the thrust face and the other side of the piston which is known as the counter-thrust face. These forces are not necessarily, however, spread evenly between the thrust and counter-thrust faces of the piston. The curvature to which the piston is machined generally attempts to produce in the running engine a "bedding" or contact area between the piston and its associated cylinder wall which lies within an arc subtending between approximately 40° and 80° on the thrust and counter-thrust faces of the piston. Heretofore piston skirts have been machined symmetrically about the plane which includes both the piston and the minor axis. The curvature of the piston skirt has generally been calculated to produce the desired bedding area to accomodate the combustion generated forces on the thrust face of the piston. It has now been discovered that significant improvements in, for example, noise reduction, stability and scuffing between a piston and its associated cylinder wall may be obtained by machining non-symmetrically about the plane which includes both the piston axis and the minor axis. D E-A-3 022 858 describes a form of asymmetry wherein the piston is machined having a polar profile which includes «shoulders» the intention of which are to trap oil to give a cushioning effect. This is not possible, however, since any oil trapped between the shoulders will be expelled at the open upper and lower skirt extremities and possibly lead to seizure initiated at the shoulders. JP-A-51 42 251 discloses polar asymmetry of a piston skirt in the plane including the gudgeon pin axis and at right angles to the piston axis, and such that the bedding area region of the thrust face extending about the major axis has a curvature of greater convexity than the curvature of the bedding area region of the counter thrust face. JP-U-57 139 649 discloses a piston with an external shape defined first by offsetting the gudgeon pin axis from the normal centre axis for a rectilinear piston. The external shape is then completed by inclining the centre axis relative to the conventional centre axis. If noise reduction in the piston operation is sought, the gudgeon pin is offset towards the thrust face, and the top part of the inclined centre axis is directed generally towards the counter thrust face, and the bottom part is directed generally towards the thrust face. Thus, the external shape of the piston is of symmetrical barrelling about the inclined centre axis, and has asymmetric curvature of the external surface in the plane normal to the gudgeon pin axis and including the conventional centre axis for a rectilinear piston. The extent of this axial asymmetry increases on either side of the point of intersection of the inclined centre axis and the conventional centre axis. The extent of the axial asymmetry increases on either side of the point of intersection of the axes, and is proportional to the displacement from this point of intersection along the inclined centre axis. There is a greater convexity at the top portion of the piston skirt on the counter thrust face compared with the thrust face. According to the present invention there is provided a piston having a crown and piston belt region and a skirt region which includes a thrust face and a counter thrust face wherein at least a part of the skirt region has first asymmetry either side of a first axial plane including the gudgeon pin axis and the piston axis, the first asymmetry comprising curves of smoothly changing form, the thrust face and counter thrust face each having a bedding area region with an associated cylinder wall, and in a polar plane at at least one axial level of the skirt region the bedding area region of the thrust face extending about the major axis has a curvature of greater convexity than the curvature of the bedding area region of the counter thrust face, and the contact area regions of the thrust face and the counter thrust face lie opposite each other in the same polar plane at the ends of the major axis, characterised in that at least one axially extending portion of the piston skirt region has second asymmetry either side of the first axial plane, this second asymmetry comprising curves of smoothly changing form in a second axial plane including the piston axis and the major axis, and has on one side of the first axial plane a curvature of greater convexity than the curvature on the other side of the first axial plane, there being a further axially extending portion of the piston skirt region in which the second asymmetry is not present. The plane which includes both the piston axis and the minor axis may also include the gudgeon pin axis. The degree of first asymmetry to which the piston skirts are machined may also vary along the axial length of the piston skirt. Furthermore, in addition to the polar profile of the piston skirt being asymmetric the axial length of the piston skirt portion is formed to a convex curvature. Such axial curvature is both symmetrical about the axial plane which includes both the piston axis and the minor axis and is asymmetrical, i.e. the curvature either side of the first axial plane may be different at any given polar plane. Pistons according to the invention may be conveniently visualised as having ovoid-shaped polar profiles. The concept of an ovoid-shaped piston is of course greatly exaggerated but nevertheless the general idea of the piston polar profile having a relatively high convexity (or low radius of curvature) on one working face and a relatively low convexity (or high radius of curvature) on the other working face is applicable. Pistons according to the invention may be constructed wherein the piston thrust side has the higher convexity and the counter-thrust side has the lower convexity profile, for better performance in respect of noise or scuffing, for example. Furthermore it is also envisaged that the pistons may have skirts wherein the relative orientation of the ovoid shape with respect to thrust and counter-thrust side changes within a single piston. For example, at the lower end of the skirt the polar profile may have the lower convexity on the thrust side whilst at the top of the skirt near to the ring belt the higher convexity profile may be on the thrust side with the curvature gradually changing over along the skirt length. With respect to the axial profile in, for example, the piston skirt near to the piston ring belt region the convexity may, for example, generally be lower on the thrust side than on the counter-thrust side. The physical manifestation of this is that the radial dimension which is measured normal to the plane which includes both the piston axis and the gudgeon pin axis to the outer skirt wall in the relevant polar plane is greater on the thrust side than on the non-thrust side. In some engine designs, however, superior performance may be obtained with these parameters reversed. Preferably pistons according to the invention may have the intervening skirt portions between the working faces relieved in some manner such as, for example, by machining or utilising piston castings having cast-in skirt relief. Generally speaking the polar profile of the intervening skirt between the working faces is immaterial provided that contact with the cylinder bore does not occur in places where contact is undesirable. In order that the invention may be more fully understood examples of pistons will now be given by way of illustration only with reference to the accompanying drawings, of which: Figure 1 shows an elevation of a schematic piston indicating the various regions; Figure 2 shows a diagrammatic comparison, greatly exaggerated, of a polar profile through a prior art piston and one polar profile through a piston according to the present invention; Figure 3 shows a diagrammatic comparison, greatly exaggerated, between a prior art piston axial profile and alternative axial profiles of a piston according to the present invention. Referring now to the figures and where in Figure 1 a piston is indicated generally at 10. The piston comprises a crown and ring belt region 11 and a skirt region 12 also including the gudgeon pin boss region 13. For the purposes of illustration the skirt 12 may be sub-divided into three levels; Level 1 lying just below the ring belt 11, Level 3 lying near the lower end of the skirt and Level 2 lying between Levels 1 and 3 approximately coplanar with the gudgeon pin axis for convenience and for no other specific reason. The thrust face is denoted by T and the counter-thrust face by T¹. Figure 2 shows a greatly exaggerated representation of a skirt profile through one polar plane. Profile 20 is typical of a conventional prior art piston, the oval shape 20 being symmetrical about both the major axis TT¹ and the minor axis PP¹. Profile 21 shows one plane through a piston according to the invention. As may be seen the curvature of the thrust face T is of high convexity and that of the counter-thrust face T¹ is of lower convexity. Figure 3 shows a greatly exaggerated representation of the axial skirt profile. The profile shown by the lines 30 represents a conventional symmetrical piston having what is known as a "barrelled" profile. The degree of barrelling varies from piston to piston and will depend upon the specific design thereof for the engine application. A piston according to the invention may have an axial profile shown by the dashed lines 31 or with a profile indicated by dashed lines 32 between Levels 1 and 2. The effect of this would be to offset the polar profile 21 of Figure 2, for example, either slightly to the thrust or non-thrust side depending upon the specific piston. Such asymmetries may also be included at the lower skirt regions around Level 3 and further schematic examples of such asymmetries are given by dashed lines 33 and 34. Asymmetry may also be incorporated if appropriate at any axial level including Level 2. During operation of the piston in the engine the stresses imposed by combustion are much higher on the thrust face T. Therefore, the convexity is higher so that the piston skirt may deform against its associated cylinder wall to provide an optimum bedding or contact area. The stresses on the counter-thrust face T¹ are much lower and, therefore, if the convexity of face T were applied to face T¹ the bedding or contact area between skirt and wall would be much less leading, in some engines, to piston instability. A low convexity profile is, therefore, adopted on face T¹ to increase bedding area and promote piston stability and hence increase performance and reduce noise. The dotted portions of the curve 21 represent portions of the piston skirt which are relieved or removed either by machining or by having cast-in relieved panels for example. The bedding area is approximately represented by the solid portions of the curve 21 and lies, in a real piston, approximately within arcs subtending between 20° and 40° either side of the major axis TT¹ measured from the piston axis 22. The types of curve shown in Figure 2 may be denoted by 'A' for the curvature of a typical symmetrical type oval piston, 'B' for the relatively higher relatively convexity portion of curve 21 and 'C' for the lower convexity portion of curve 21. The complete symmetrical profile 20 may be regarded as a reference profile applicable to a typical conventional piston. The actual shape of the curve 'A' may be combined in one polar plane with a shape of type B or C to form a piston according to the present invention. For the purpose of clarification it should be noted that the curved shapes A, B and C only denote relative curvatures and not absolute curvatures. Thus a conventional piston may, for example, comprise curves of type B in the same polar planes on both thrust and counter-thrust faces along the axial length of the skirt. Depending upon the requirements of a particular piston the various types of curvature typified in Figure 2 may be incorporated into the skirt in any desired combination as indicated in the table below. The principles disclosed in the present invention may be applied to almost any piston design to optimise the bedding areas on the piston working face.

Claims: A piston having a crown and piston belt region (11) and a skirt region (12) which includes a thrust face and a counter thrust face wherein at least a part of the skirt region has first asymmetry either side of a first axial plane including the gudgeon pin axis (PP′) and the piston axis (22), the first asymmetry comprising curves of smoothly changing form, the thrust face and counter thrust face each having a bedding area region with an associated cylinder wall, and in a polar plane at at least one axial level of the skirt region (12) the bedding area region of the thrust face extending about the major axis (TT′) has a curvature of greater convexity than the curvature of the bedding area region of the counter thrust face, and the contact area regions of the thrust face and the counter thrust face lie opposite each other in the same polar plane at the ends of the major axis (TT′), characterised in that at least one axially extending portion of the piston skirt region (12) has second asymmetry either side of the first axial plane, this second asymmetry comprising curves of smoothly changing form in a second axial plane including the piston axis (22) and the major axis (TT′), and has on one side of the first axial plane a curvature of greater convexity than the curvature on the other side of the first axial plane, there being a further axially extending portion of the piston skirt region in which the second asymmetry is not present. A piston according to claim 1 characterised by the portion (31) of the piston skirt region (12) adjacent to the crown and ring belt region (11) having second asymmetry in the second axial plane with a curvature of greater convexity on the thrust side than on the counter thrust side of the first axial plane.

Inventors: BRUNI LUDOVICO, BRUNI, LUDOVICO
Applicants: AE PLC
Application year: 1986
Main classification: F02F3
IPC codes: F16G1, F02F3