GB2105439A

GB2105439A - Pistons for internal combustion engines

Info

Publication number: GB2105439A
Application number: GB08221993A
Authority: GB
Inventors: Ludovico Bruni
Original assignee: AE PLC
Current assignee: AE PLC
Priority date: 1981-07-31
Filing date: 1982-07-30
Publication date: 1983-03-23
Also published as: DE3273182D1; ES8402048A1; BR8204455A; EP0071361B1; DK341182A; CH650319A5; GB2105439B; US4674399A; CA1211010A; SE453849B; NL8202966A; MX154283A; ES514560A0; AU8665782A; DK157461C; FR2510661B1; LU84299A1; DE3228616A1; SE8204488L; AU557207B2

Description

1

SPECIFICATION

Pistons for internal combustion engines The invention relates to pistons for internal combustion engines.

A conventional piston for an internal combustion engine comprises a crown, a gudgeon pin bore and a skirt extending all round the piston. The skirt performs no gas sealing function; this is provided by piston rings carried on the piston.

Rather, the skirt transmits lateral thrust on the piston produced by a connecting rod during reciprocation to an associated cylinder or liner.

Although the weight of such pistons has, in recent years, been reduced by use of aluminium or aluminium alloys, such pistons are still compartively heavy and the area of skirt in contact with the cylinder or liner provides a considerable frictional force which must be overcome by the engine, so reducing its power. There have been various proposals for reducing the area of the skirt, 85 but, in general, they have not achieved commercial success because of problems of lubrication and skirt rigidity.

According to first aspect of the invention, there is provided a piston for an internal combustion engine comprising a crown, a gudgeon pin bore, and, on both sides of the plane including the gudgeon pin axis and the piston axis, at least two bearing surfaces, one bearing surface or group of bearing surfaces being towards the crown end of the piston and being spaced by an axially and circumferentially extending gap from the remaining surface or surfaces in an axial direction, the bearing surfaces being disposed about a plane including the piston axis and normal to the gudgeon pin bore axis, and extending only partially around the piston.

According to a second aspect of the invention, there is provided a piston for an internal combustion engine comprising a crown, a ring band and, on both sides of a plane including the gudgeon pin bore axis and the piston axis, two bearing surfaces or groups of bearing surfaces extending only partially around the piston on either side of a plane including the piston axis and normal to the gudgeon pin bore axis, one bearing surface or group of bearing surfaces being supported by the ring band and the other bearing surface or group of bearing surfaces being spaced from the ring band and being carried on a strut or struts.

The following is a more detailed description of two embodiments of the invention, by way of example, reference being made to the accompanying drawings in which:- Figure 1 is a side elevation of a first form of piston, Figure 2 is a section on the line 11-11 of Figure 1, Figure 3 is a side elevation of an alternative embodiment of the first form of invention, Figure 4 is a schematic view from beneath of the piston of Figures 1 and 2.

Figure 5 is a schematic view from beneath of the piston of Figure 3, GB 2 105 439 A 1 Figure 6 is a section on the lines V]-V1 of Figure 1 or Figure 3, Figure 7 is a side elevation of a second form of piston, Figure 8 is a section on line W-VII of Figure 7, and Figure 9 is a section on the line VIII-Vill of Figure 7, Figures 1 OA and 1 OB are alternative sections on the line X-X of Figure 7.

Referring first to Figures 1, 2 and 4, the first piston 1 comprises a crown 2 surrounded by a ring band 3 for receiving the piston rings (not shown).

A single gudgeon pin boss 6 is provided which defines a gudgeon pin bore (see Fig. 2) extending through the piston.

On both sides of a plane containing the gudgeon pin bore axis and the piston axis, the piston is provided with two bearing surfaces 4, 5, spaced by an axially and circumferentially extending gap. The crown-end bearing surface 4 depends from the ring band (see Fig. 2) while the remaining, lower, bearing surface 5 is connected to the gudgeon pin boss 6 by a pair of struts 7 (which may be formed as described below with reference to Figs. 1 OA and 1 OB). The lower bearing surface 5 is thus cantilevered by the struts 7 from the gudgeon pin boss 6 and is otherwise unsupported. The bearing surfaces 4, 5 are symmetrically disposed about a plane including the piston axis and normal to the gudgeon pin axis (i.e. the plane of the section of Fig. 2), and extend only partially around the circumference of the piston. For example, they may extend up to 451 on either side of this plane. 100 In a modified arrangement (not shown) the struts 7 may carry the bearing surface 5 in addition to to the bearing surface 4. The bearing surfaces 4, 5 are generally the shape of segments of a cylinder with the lower edge of the crown-end bearing surface 4 and the two circumferentially extending edges of the lower bearing surface 5 lying in respective planes normal to the piston axis. These edges are provided with chamfers 8.

A preferred shape of the lower bearing surface and the associated chamfers 8 is shown in Figure 6 in a very exagerated manner. The surface 9 is curved i-n planes including the piston axis with a maximum radial depth (x in Fig. 6) of, for example, 0.02 mm. The chamfers 8 are planar in planes including the piston axis, the length of the chamfers being 1 mm with the chamfers being inclined at an angle of 151 to the vertical or the length of the chamfers being 1 mm with a radial depth (y in Fig. 6) of 0.04mm. The chamfers 8 may, however, be curved and it will be appreciated that they, and the surface, may have any suitable shape. It will also be appreciated that the chamfer 8 on the lower edge of the crown-end bearing surface 4 may be of similar dimensions to the preferred shape described above.

In use, the lateral thrust loads on the piston are transmitted to the associated cylinder or liner 20 (Fig. 6) by the bearing surfaces 4, 5. The presence 2 GB 2 105 439 A 2 of the chamfers 8 ensures a supply of lubricant over the bearing surfaces 4, 5 during reciprocation by forming a passage of decreasing dimensions leading to the associated surface. This forces lubricant under pressure over the surfaces and thus ensurs full hydrodynamic lubrication. In the lower bearing surface 5, where this is curved as shown in Figure 6, this curvature also assists in ensuring adequate lubrication. The reduced size of the bearing surfaces 4, 5 and the windows thereby 75 defined in the skirt reduces the weight of the piston so reducing the power requirement. In addition, the friction losses in contact between the piston and the associated cylinder or liner are reduced as a result of the reduced area of the 80 bearing surfaces in comparison with a conventional piston having a continuous skirt.

Because the surfaces are adequately lubricated, their spacing can be kept at a constant maximum without the need for an increase in surface area at the centres of the surfaces. These measures together reduce the cost of the piston and improve the performance of an engine fitted with the piston.

Referring next to Figures 3 and 5, the modified piston shown therein is generally similar to the piston of Figures 1, 2 and 4 and parts common to Figures 3 and 5 and Figures 1, 2 and 4 are given the same reference numerals, but with the subscript a, and will not be described in detail. In this modified embodiment, the bearing surfaces 5 remote from the crown 2 are each replaced by a pair of circumferentially spaced generally rectangular sectors 9. Instead of a single gudgeon pin boss 6 being provided, a pair of spaced gudgeon pin bosses 6a are provided and each sector 9 of each pair of sectors is connected to an associated boss 6a by a strut 7a (which may be formed as described below with reference to Figs.

1 OA and 1 OB). The sectors 9 are provided with cha mfe rs in the sa me way as the bea ring su rface and may have the cross-sectional dimensions as described above with reference to Figure 6. The sectors 9 are axially aligned.

A metallic ring 10, shown in broken line in 110 Figures 3 and 5, interconnects the four sectors 9 and ads to control the expansion of the sectors 9 in a radial direction.

The piston of Figures 3 and 5, operates in generally the same way as the piston of Figures 1, 2 and 4 with generally the same advantages. Since, however, the sectors 9 have a lesser area than the bearing surface 5, there will be a further reduction in both weight and friction with conseqential advantages.

Referring next to Figures 7, 8 and 9, the second piston comprises a crown 12 surrounded by a ring band 13 including grooves for receiving piston rings (not shown). A single gudgeon pin boss 16 is provided which defines a gudgeon pin bore (see Fig. 8).

The piston is provided, on each side of a plane including the piston axis and the gudgeon pin bore axis, with a crown-end thrust surface 14 and a thrust surface 15 remote from the crown end. The two thrust surfaces are connected by a skirt portion 14a, as best seen in Figures 7 and 8. The thrust surface 15 remote from the crown end is connected to the gudgeon pin bore by struts 17 (see Fig. 8) while the crown-end thrust surface 14 is connected to the ring band 13. Thus a single member is formed having a crown end connected to the ring band 13 and having the lower end connected to the gudgeon pin boss 16 by the struts 17. The axially extending lateral edges 18 of the composite member define respective apertures leading to a circumferential cavity S (see Fig. 8) extending between the composite member and the remainder of the piston.

Because the lower bearing surface in this embodiment and the lower surface or surfaces 5, 9 of the embodiments of Figures 1 to 6 are supported only by the respective struts 7, 17, these struts are highly loaded. In order to prevent any possibility of strut failure, the struts may be flanged so they have, for example, T-cross-section of Figure 1 OA or the ±cross-section of Figure 1 OB.

The bearing surfaces 14, 15 and the skirt portion 14a are symmetrically disposed about a plane including the piston axis and normal to the gudgeon pin bore axis (i.e. the plane of Fig. 8). The bearing surface 15 remote from the crown is of greater circumferential extent than the skirt 1 4a and the crown end bearing surface 14, which are of equal circumferential extent. For example, the bearing surfaces 15 remote from the crown may have an arcuate extent of 901 and have their ends spaced from one another by 901 (see Fig. 9).

In use, the piston slides in a cylinder or liner of an internal combustion engine which may be a diesel engine an Otto-cycle engine or a two-stroke engine. The lateral thrust is taken on the bearing surfaces 14, 15. A chamfer 18 provided on the lower edge of the bearing surface 15 ensures a flow of lubricant to and over the surface and this chamfer may be dimensioned and arranged as described above with reference to Figure 6.

The piston of Figures 7, 8 and 9 has the advantages of lightness, low friction and low cost which characterises the pistons of Figures 1 to 5. The struts 17 hold the bearing surfaces 14, 15 rigidly positioned without the need for any further connections between the lateral edges and the gudgeon pin boss.

It will be appreciated, that more than two bearing surfaces may be provided on both sides of the plane including the piston and gudgeon pin bore axes. For example, as in Figures 3 and 5, three such surfaces may be provided, or four or more surfaces.

Claims

1. A piston for an internal combustion engine comprising a crown, a gudgeon pin bore and, on both sides of a plane including the gudgeon pin bore axis and the piston axis, at least two bearing surfaces, one bearing surface or group of bearing surfaces being towards the crown end of the piston and being spaced by an axially and 3 GB 2 105 439 A 3 circumferentially extending gap from the remaining surface or surfaces in an axial direction, the bearing surfaces being disposed about a plane including the piston axis and normal to the gudgeon pin bore axis, and extending only partially 50 around the piston.

2. A piston according to claim 1 wherein each bearing surface has generally the shape of a segment of a cylinder.

3. A piston according to claim 4, wherein a single crown-end bearing surface is provided and a single remaining bearing surface is provided, spaced by a gap from said crown-end bearing surface.

4. A piston according to claim 2, wherein a 60 single crown-end bearing surface is provided and two remaining bearing surfaces are provided, the two remaining surfaces being circumferentially spaced but axially aligned.

5. A piston according to claim 4, wherein the two remaining surfaces are symmetrically disposed on either side of a plane including the piston axis and normal to the gudgeon pin axis.

6. A piston according to claim 3 or claim 4 wherein the two remaining bearing surfaces to one side of the plane containing the piston and gudgeon pin bore axes and the two remaining surfaces to the other side of said plane are interconnected by a metallic band extending around the piston.

7. A piston according to any one of claims 1 to 6 wherein the or each remaining surface has two generally parallel circumferentially extending edges and wherein at least one of said edges is provided with a chamfer for directing lubricant over said surface during reciprocation of the piston.

8. A piston according to claim 7 wherein the or each chamfer is planar or curved in planes including the piston axis.

9. A piston according to claim 7 or claim 8 wherein the or each remaining surface is barrelled so that said surface is curved in planes including the piston axis for directing lubricant over said surface during reciprocation.

10. A piston for an internal combustion engine comprising a crown, a ring band and, on both sides of a plane including the gudgeon pin bore axis and the piston axis, two bearing surfaces or groups of bearing surfaces extending only partially around the piston on either side of a plane including the piston axis and normal to the gudgeon pin bore axis, one bearing surface or group of bearing surfaces being supported by the ring band and the other bearing surface or group of bearing surfaces being spaced from the ring band and being carried on a strut or struts.

11. A piston according to claim 10, wherein there is provided a single bearing surface connected to the ring band and depending therefrom and wherein there is provided a single bearing surface carried on a strut or struts.

12. A piston according to claim 10 wherein the ring band bearing surface and the strut-connected bearing surface are interconnected by a skirt portion to form a single generally part-cylindrical member having one end connected to the ring band and the other end carried on a strut or struts, the member having circumferentially-spaced generally axially extending edges defining respective apertures leading to a circumferentially extending cavity between the member and the remainder of the piston.

13. A piston according to any one of claims 10 to 12, and including a gudgeon pin boss or bosses defining the gudgeon pin bore, the or each strut being connected at one end to the gudgeon pin boss.

14. A piston according to claim 13 wherein two struts are provided.

15. A piston according to any one of claims 10 to 14 wherein the or each strut has a crosssection of T-shape or ±shape and is cast integrally with the remainder of the piston.

16. A piston substantially as hereinbefore described with reference to Figures 1, 2,4 and 6 or Figures 3, 5 and 6 or Figures 7, 8 and 9 or to Figures 1, 2,4 and 6 or Figures 3, 5 and 6 or Figures 7, 8 and 9 as modified by Figures 1 OA or 1 OB of the accompanying drawings.

Printed for Her Majesty's Stationery Office by the Courier Press, Leamington Spa, 1983. Published by the Patent Office, 25 Southampton Buildings, London, WC2A lAY, from which copies may be obtained.