INTERNAL-COMBUSTION ENGINE PISTON RING, PROCESS FOR OBTAINING A PISTON RING, AND INTERNAL-COMBUSTION ENGINE

Abstract

A piston ring for an internal-combustion engine may include a body having a substantially annular external surface and a physical vapor deposition coating layer disposed on the external surface. The body may include a gap defined between a first end and a second end. The piston ring may also include a first half in a region of the gap and a second half opposite the first half. The coating layer of the first half may have a thickness gradient, and the coating layer may define a greater thickness in a vicinity of the first end and the second end and a reduced thickness in regions further away from the vicinity of the first end and the second end. The coating layer of the second half may have a uniform thickness.

Claims

1. A piston ring for internal-combustion engines, comprising: a body having a substantially annular external surface and a physical vapor deposition coating layer disposed on the external surface, the body including a gap defined between a first end and a second end, a first half defined by a circumferential angle of 180° adjacent to the gap and a second half defined by a portion of the external surface between a circumferential angle of 90° and 270°, wherein the coating layer of the first half has a thickness gradient, the thickness gradient of the coating layer defining a greater thickness in regions adjacent to a vicinity of the first end and the second end and a reduced thickness in regions further away from the vicinity of the first end and the second end, and wherein the coating layer of the second half has a uniform thickness.

2. The piston ring as claimed in claim 1, wherein the thickness gradient has a thickness of at least 15 microns in the regions further away from the vicinity of the first end and the second end and a thickness of at least 55 microns in the regions adjacent to the vicinity of the first end and the second end.

3. The piston ring as claimed in claim 1, wherein the coating layer of the first half in the regions further away from the vicinity of the first end and the second end is approximately 2% to 10% less thick than the coating layer of the regions adjacent to the vicinity of the first end and the second end.

4. The piston ring as claimed in claim 1, wherein the coating layer of the first half in a region adjacent to the vicinity of the first end has a thickness of at least 55 microns and in a region adjacent to the vicinity of the second end has a thickness of at least 55 microns.

5. The piston ring as claimed in claim 1, wherein the coating layer of the second half has a uniform thickness of at least 15 microns.

6. The piston ring as claimed in claim 1, wherein the external surface is a sliding surface.

7. A method for coating an internal-combustion engine piston ring, comprising: fastening at least one piston ring on a rotary table, the at least one piston ring including a gap positioned opposite at least one physical vapor deposition source of coating material; performing a first rotation movement of the rotary table about a central axis while the at least one piston ring is stationary in relation to the rotary table, and receiving a first deposition of coating material on an external surface of the at least one piston ring in a region defined by a circumferential angle of 180° adjacent to a center of the gap by rotating the rotary table; performing a relative rotation movement by performing the first rotation movement of the rotary table and performing a second rotation movement of the at least one piston ring on the rotary table such that the at least one physical vapor deposition source of coating material promotes a second deposition of coating material entirely along the external surface of the at least one piston ring; and wherein performing the first rotation movement and performing the relative rotation movement are alternated and wherein the first rotation movement and the second rotation movement are in opposite directions.

8. The method as claimed in claim 7, further comprising placing a physical barrier between the gap and the at least one source of coating material after at least one of performing the first rotation movement and performing the relative rotation movement.

9. The method as claimed in claim 7, wherein the first deposition of coating material forms substantially two thirds of a final thickness of a coating layer.

10. The method as claimed in claim 7, wherein a coating material of the first deposition is different a coating material of the second deposition.

11. An internal-combustion engine, comprising: at least one piston ring including: a body defining a substantially annular external surface and including a gap defined between a first end and a second end, the external surface having a first portion defined by a circumferential angle along the body of 180° adjacent to a center of the gap, and a second portion defined by a circumferential angle along the body of between 90° and 270° from the center of the gap; a physical vapor deposition coating layer disposed on the external surface; wherein the coating layer disposed on the first portion has a thickness gradient defining a greater thickness in a region of the first end and the second end than a further region spaced away from the region of the first end and the second end; and wherein the coating layer disposed on the second portion has a uniform thickness.

12. The internal-combustion engine as claimed in claim 11, wherein the coating layer has a thickness of at least 15 microns in the further region spaced away from the first end and the second end and a thickness of at least 55 microns in the region of the first end and the second end.

13. The internal-combustion engine as claimed in claim 11, wherein the thickness gradient of the coating layer extends from a respective one of the first end and the second end to the second portion of the external surface, and wherein the coating layer is approximately 2% to 10% less thick towards the second portion than at the external surface adjacent to the first end and the second end.

14. The internal-combustion engine as claimed in claim 11, wherein the coating layer of the second portion has a uniform thickness of at least 15 microns.

15. The internal-combustion engine as claimed in claim 11, wherein the external surface is a sliding surface.

16. The method as claimed in claim 7, wherein performing the first rotation movement and receiving the first deposition of coating material is followed by performing the relative rotation movement.

17. The method as claimed in claim 7, wherein the first rotation movement is one of the clockwise and counterclockwise, and the second rotation movement is the other of clockwise and counterclockwise.

18. The method as claimed in claim 7, wherein receiving the first deposition of coating material includes forming a coating layer via physical vapor deposition on the external surface with a varying thickness that increases towards the gap.

19. The piston ring as claimed in claim 1, wherein the coating layer disposed on the first half has a maximum thickness in a region of 10° and 350° from a center of the gap.

20. The piston ring as claimed in claim 19, wherein the coating layer diminishes in thickness from the region of 10° and 350° towards the first end and the second end, respectively.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0022] The present invention will be described below in greater detail on the basis of an illustrative embodiment represented the drawings. The Figures show:

[0023] FIG. 1 shows a schematic representation of a piston ring obtained by means of the coating process described in the present invention;

[0024] FIG. 2 shows a graphic representation of the pressure distribution from 0° to 360° for a piston ring;

[0025] FIG. 3 shows a schematic representation of the conventional PVD process;

[0026] FIG. 4 shows a schematic representation of step 1 of the PVD process of the present invention;

[0027] FIG. 5 shows a schematic representation of step 2 of the PVD process of the present invention;

[0028] FIG. 6 shows a schematic representation of the use of a physical barrier in the PVD process; and

[0029] FIG. 7 shows a schematic representation of the thickness of the coating layer of the piston ring for the prior art and for the present invention.

DETAILED DESCRIPTION

[0030] The present invention relates to a piston ring 1 and to a process for deposition of a coating capable of guaranteeing a variable thickness of the coating layer 5 on the external surface 2 of the piston ring 1 such that an adjacent region in the vicinity of the ends 31, 32 of a gap 3 of the ring 1 comprises a coating layer 5 that is thicker than the coating layer in the opposite region in the vicinity of the ends 31, 32 of the ring 1 and, furthermore, with a reduction in the thickness of the coating layer 5 in the vicinity of the ends 31, 32 of the gap 3 of the ring 1, thus providing a piston ring 1 with a high level of durability owing to the excellent resistance and to the high level of thickness in the region of greatest wear of the ring.

[0031] As is also known, the entire piston ring 1 is provided with a gap 3, the existence of which guarantees the possibility of mounting the ring in a groove of an internal-combustion engine piston. For the purposes of a better definition of the present invention, the region of the gap 3 of the ring is defined by two ends 31, 32, also known as extremities of the ring. Taking, for example, the center of the gap 3, it may be assumed that this is a total angle of 10°. Thus, the center of the gap 3 will be defined as a zero-degree (0°) angle or a 360° angle. Therefore, each end is positioned at 5° from the center of the gap 30.

[0032] In this context, the limit of the first end 31 is positioned at 5° from the center of the gap 3 and the limit of the second end 32 is positioned at 355° from the center of the gap, or −5° from said center. For the purposes of a better understanding of the present invention, the degrees will be measured in the clockwise direction, starting from the center of the gap 3 of the piston ring 1.

[0033] In a much simpler way, which will set forth better as the description continues, the process of the present invention consists in performing a first deposition, by PVD, over substantially half the external surface 2 of the ring 1, followed by a second deposition, also by PVD, over the entire external surface 2 of the ring 1, it being possible for the first deposition and the second deposition to be alternated.

[0034] More specifically, the first deposition is performed in the region of the ring 1 included between the areas defined by the angles 0° to 90° and 270° to 360°, starting from the center of the gap 3 of the ring 1. Alternately, it may be stated that the surface that receives the first deposition is defined by the 180° adjacent to the center of the gap 3. Said 180° adjacent to the center of the gap will henceforth be called a first half 21 of the ring 1. The opposite portion of the ring 1 will henceforth be called a second half 22 and naturally comprises the portion of the external surface 2 defined by the angles from 90° to 270°.

[0035] As may be seen in FIG. 1, the piston ring 1 comprises a substantially annular metallic external surface 2, this surface acting as sliding portion at the interface between the ring 1 and a cylinder lining. The piston ring 1 illustrated in the present invention preferably comprises a compression ring for the first piston groove or, furthermore, a compression ring for the second piston groove.

[0036] Notably, the process of the PVD coating of the present invention is provided with a chamber 55 specially designed for this type of deposition, comprising at least one source 52 of coating material 53 and at least one rotary table 50 to which at least one piston ring 1 is fastened.

[0037] The chamber 55 preferably, but optionally, comprises an even number of sources 52 of coating material 53. Alternatively, the present invention may be constituted by an uneven number of sources 52. The selection of one, two, three, four, five, six, seven, eight, nine, ten, etc. sources 52 may depend on various specific requirements. For example, in a possible embodiment illustrated in FIG. 3, 4, or 5, four 4 sources may be arranged symmetrically and at uniform distances so as to allow a balanced deposition over all the components to be coated. In sum, in simple terms, the number of sources 52 changes independently of the number of rings 1.

[0038] Regarding the number of rings to be deposited, there is no limitation other than the area available on the rotary table. Thus, it is possible for one ring 1 or for a plurality of rings to be deposited. The greater the number of sources 52, the greater will be the speed of deposition of the coating material 53 and, therefore, the greater the efficiency of the process.

[0039] Regarding the rotary table 50, rotation thereof may be either clockwise or counterclockwise. Moreover, although a first rotation movement W1 of the rotary table 50 and a second rotation movement W2 of the piston ring 1 are given, it should be mentioned that both may rotate in different directions or in the same direction, and that this direction may be either clockwise or counterclockwise.

[0040] Usually, the PVD process for coating piston rings 1, illustrated in FIG. 3, comprises the fastening of at least one ring 1 on a rotary table 50 such that the rotary table performs a first rotation movement W1 about its central axis 51 and the ring 1 performs a second rotation movement W2 on the rotary table 50, the ring 1 receiving a deposition of coating material over the entire external surface 2, from 0° to 360°.

[0041] In the conventional PVD process, the speed of the rotation movements is maintained constant, thereby defining a uniform thickness of coating 5 over the entire external surface 2 of the piston ring 1.

[0042] The PVD process described in the prior art is performed in accordance with the conventional process, but at a varying speed of rotation. Thus, when the first half 21 of the ring 1 is opposite a source 52 of coating material 53, the speed of rotation is reduced, thereby guaranteeing that the first half 21 of the ring 1 has a coating layer 5 that is thicker than the second half 22 of the external surface 2 of the ring 1.

[0043] However, in addition to the disadvantage in terms of precise control of the speed of rotation, the prior-art PVD process has the further disadvantage that the vicinity of ends 31, 32 of the gap 3 of ring 1 have a thicker coating layer 5, thereby increasing contact pressures between the ends 31, 32 of the ring 1 and the cylinder.

[0044] The coating process proposed by the present invention comprises the application of a coating using a PVD process performed as at least two steps, which may be alternated in terms of sequence of execution.

[0045] As may be seen in FIG. 4, in step 1 of the coating process the piston ring 1 is fastened to the rotary table 50 such that the first half 21 of the ring 1 lies opposite the source 52 of coating material 53. In this step, only the rotary table 50 performs the first rotation movement W1 about the central axis 51, while the piston ring 1 remains stationary in relation to the rotary table 50. The objective of this first step is a first deposition of the coating material 53 and it achieves around 2/3 (two thirds) of the final thickness of the coating layer 5.

[0046] In step 2 of the process, shown in FIG. 5, not only the rotary table 50 but also the piston ring 1 perform a rotation movement. The rotary table 50 performs a first rotation movement W1 about the central axis 51 while the piston ring 1 performs a second rotation movement W2 on the rotary table 50. In this step, there is a second deposition of the coating material 53 over the entire external surface 2 from 0° to 360° of the ring 1. Thus, the first half 21 of the ring 1 will achieve the final thickness of the coating layer 5, which will be thicker in relation to the second half 22 of the ring 1. Alternatively, it should be noted that, between step 1 and step 2, the rings may receive a finishing process, which may be machining, lapping, grinding, sanding, honing, brushing, inter alia.

[0047] FIG. 6 shows that the PVD coating process further ensures that the thickness of the coating layer 5 in the vicinity of the first end 31 and in the vicinity of the second end 32 is preferably, but optionally, from 2% to 10% thinner than the thickness of the coating layer in the adjacent regions in the vicinity of the ends 31, 32 of the ring 1.

[0048] In a preferred construction, a physical barrier 54 is inserted between the ends 31, 32 of the gap 3 of the ring 1 so as to obstruct a fraction of the coating material 53 applied by the source 52, this resulting in a reduction in the thickness of the coating layer 5 in the vicinity of the first end 31 and in the vicinity of the second end 32 of the gap 3 of the ring 1.

[0049] In a second embodiment, the reduction in the thickness of the coating layer 5 in the vicinity of the ends 31, 32 of the gap 3 may be obtained by carrying out a machining process in such a manner as to remove the material after the coating process. Preferably, but optionally, the machining processes used may be the process of brushing or lapping.

[0050] The reduction in the thickness of the coating layer in the vicinity of the ends 31, 32 aims to reduce the contact pressure so as to allow better lubrication and consequently less wear of the ring 1.

[0051] The division of the PVD coating process into two steps enables the process parameters to be adjusted in such a manner as to reduce compressive stresses applied during deposition of the material 53, resulting in greater thicknesses of the coating layer 5. This trick of optimizing the stresses in the coating layer 5 is not possible with the PVD process known in the prior art, thus, it is possible to achieve thicknesses greater than the 50 microns described in the prior art. It is also feasible to achieve thicknesses of 70 microns, or even thicknesses greater than 100 microns. It should be noted that any value below 110 microns may be obtained.

[0052] Furthermore, the process of the present invention allows different materials to be applied during the first and the second steps. For example, in the first step it is possible to apply a material with high wear resistance while in the second step it is possible to apply a material with low sliding wear and less wear resistance.

[0053] Naturally, the layers which can be applied by PVD methods are not restricted to the chemical composition thereof, i.e. layers of nitrides, carbides and other compounds can also be applied, for example CrN, TiN, NbN, CrCN, CrCN, inter alia. The solution described in the present invention can also be applied when the layer obtained by PVD has a multi-layer or superstructure architecture, i.e. multi- or nano-layers of CrN/NbN independent of the thickness of the individual layers that form these multi-layers. Another design that can also be applied is, during steps 1 and 2 of deposition, possibly applying materials of different chemical composition or microstructure, for example a thick coating of CrN is applied in the adjacent region in the vicinity of the ends (31, 32) and, on this material, a different material, for example a layer of non-hydrogenated amorphous carbon, or any other material.

[0054] These advantages cannot be achieved using the processes described in the prior art as they are continuous processes and constitute only one step. Thus, the PVD coating process proposed by the present invention is based on the present technology but has a more advantageous process methodology that consequently results in a product of which the performance level differs, at least in terms of durability.

[0055] The piston ring 1 obtained by means of the PVD coating process proposed by the present invention is such that the first half 21 of the ring 1 has a thickness gradient for the coating layer 5 starting from at least 15 microns at 90° and 270° and ending at at least 15 microns in the adjacent regions in the vicinity of the ends 31, 32 of the gap 3. It should furthermore be noted that the vicinity of the ends 31, 32 have a coating layer 5 that is approximately 2% to 10% thinner than the adjacent regions in the vicinity of the ends 31, 32, and thus the vicinity of the first end 31 has a thickness of at least 55 microns and the vicinity of the second end 32 a thickness of at least 55 microns. Furthermore, the second half 22 of the ring, i.e. between 90°, 180°, and 270°, has a coating layer of uniform thickness of at least 15 microns.

[0056] A preferred embodiment having been described, it must be understood that the scope of the present invention encompasses other possible variations and is limited only by the content of the appended claims, which include the possible equivalents.