This application claims priority under 35 USC 119 to German Patent Appl. No. 10 2016 116 815.7 filed on Sep. 8, 2016, the entire disclosure of which is incorporated herein by reference.
The invention relates to a method for coating a cylinder of an internal combustion engine and to a cylinder for an internal combustion engine.
Cylinders of internal combustion engines are coated with a plasma spray to reduce wear caused by the oscillating movement of the piston in the cylinder.
EP 2 112 359 B1 discloses a cylinder with a piston running surface that is roughened with grooves or a spiral profile. The roughened structure has undercuts that result in an increase of an adhesive surface area and an improved adhesion for a coating of the cylinder.
EP 1 334 268 B1 discloses a cylinder with a piston running surface that has a thread-like structure that comprises two undulating shapes for improved adhesion of the coating.
EP 1 225 324 B1 discloses a cylinder for an internal combustion engine where the piston running surface has a coating consisting of an alloy. The piston running surface is roughened to have obliquely running teeth for improved adhesion of the coating.
However, particles of the coating material reflect during the coating operation and cause undefined embedding of the particles of the coating material occurs. The particles are reflected on surfaces that are configured in the cylinder of what is known as a honing run-out and bearing pedestals. These reflections lead to an inhomogeneous layer configuration caused by embedding of the reflected particles. This inhomogeneous coating leads in a further machining process or finishing process, such as honing of the cylinder, to ruptures and surface damage. As a result, the cylinder becomes unserviceable and can no longer be used.
It is an object of the invention to provide an improved method for coating a cylinder of an internal combustion engine. It is a further object of the invention to specify an improved cylinder for an internal combustion engine.
The invention relates to a method for coating a cylinder of an internal combustion engine. The cylinder may be in a crankcase of the internal combustion engine and may have a cylinder lining surface section with a piston running surface that is configured to face an interior space of the cylinder and along which a piston of the internal combustion engine can be moved. The cylinder may have further surfaces that adjoin the interior space. In particular, the cylinder has a bearing section surface of a bearing section that is provided for mounting a crankshaft of the internal combustion engine, and a run-out section surface of a run-out section that is between the bearing section and the running surface section. The further surface may face the interior space and may receive a defined structure in a first step, and the coating may take place by spraying the piston running surface in a second step. The advantage of the method of the invention is that the further surfaces of the cylinder that are not configured as a piston running surface receive a defined structure that is configured for a defined reflection of particles that are produced during an application of the coating. Thus, a substantially improved cylinder surface can be achieved in the region of the piston running surface. A reject rate is reduced and therefore production costs can be lowered substantially. The further surface may be the bearing section surface and/or a run-out section surface of the run-out section. The run-out surface may adjoin the piston running surface directly, and is therefore in direct contact with the latter. The bearing section surface serves for reflection, since it is transverse, usually perpendicular, to the piston running surface.
The coating may be a thermally resistant and mechanically resistant plasma coating.
An extraction of reflected particles takes place in a step that follows the second step or happens virtually at the same time. The extraction of the reflected particles leads to an ensured elimination of the reflected particles.
The defined structure may be removed in a further step that follows the second step or next step. After the coating has taken place, the defined structure on the further surface, in particular on the bearing section surface and/or the run-out surface, no longer has a function and can be removed to avoid a possible stress concentration that might otherwise be produced in a manner that is dependent on the defined structure. A further advantage is achieved in improved reworking of the cylinder, since the defined structure can be ruled out as a disruptive factor during reworking.
The removal of the coating that is applied on the further surface can take place at the same time as the removal of the applied defined structure. Thus, a cost saving is achieved by reducing the number of method steps.
The defined structure may be produced with the aid of a spindle process, a circular machining operation or a helical machining operation.
The defined structure may be produced by a tooth-shaped structure. A side surface of the tooth lies at an angle to the spraying jet. Thus, the teeth direct the particles striking thereon in a defined direction into the interior space of the cylinder, and thus in a direction that faces away from the piston running surface. The particles then can be removed simply, for example, by extraction. The defined structure may have an angle between two adjacent teeth with a value of between 0° and 90°.
The invention also relates to a cylinder for an internal combustion engine. The cylinder has a cylinder lining surface section with a piston running surface that is configured to face an interior space of the cylinder and along which a piston of the internal combustion engine can be moved. The cylinder has further surfaces that adjoin the interior space, in particular a bearing section surface of a bearing section that is provided for mounting a crankshaft of the internal combustion engine, and a run-out section surface of a run-out section that is between the bearing section and the cylinder lining surface section. The cylinder has a defined structure at least temporarily. A high quality coated piston running surface can be achieved by the at least temporarily defined structure. This reduces wear of the piston running surface and therefore leads to an increase in the service life of the cylinder.
Further advantages, features and details of the invention result from the following detailed description and the drawings. The features and combinations of features mentioned in the preceding text and the features and combinations of features mentioned in the following text and/or shown in the figure can be used in the specified combination, in other combinations or on their own, without departing from the scope of the invention.
The cylinder 1 is hollow and has an interior space 3, in which a piston oscillates during operation of the internal combustion engine 2. A coating is applied in a region of a cylinder lining surface section 4 of the cylinder 1 on a piston running surface 5 that faces the interior space 3 to reduce wear between the cylinder 1 and the piston. The cylinder lining surface section 4 is the section of the cylinder 1 that is in contact with the piston or its piston rings during operation.
The cylinder 1 is in a crankcase 7 and comprises a bearing section surface 13 of a bearing section 6 of the crankcase 7. The bearing section 6 is provided for mounting a crankshaft (not shown in greater detail) of the internal combustion engine 2, and a run-out section 8 which is configured between the bearing section 6 and the cylinder lining surface section 4.
A plasma coating in the form of a spray coating is applied on the specially prepared piston running surface 5. The special preparation of the piston running surface 5 is to achieve improved adhesion of the coating on the piston running surface 5.
The method for coating is carried out by way a lance 9 that has an opening 10 for accommodating a spray jet 11 of coating material. The lance 9 rotates about its lance axis 12 and moves axial along the lance axis 12 while coating the cylinder 1, as indicated by the movement arrows 19.
In accordance with the prior art, particles 15 of the coating reflect and accumulate in an undefined and uncontrolled manner on the piston running surface 5 in the region on the bearing section surface 13 of the bearing section 6 that faces the interior space 3, and on a run-out section surface 14 of the run-out section 8 that faces the interior space 3.
This means that the method according to the invention has the configuration of the defined structure 16 on the bearing section surface 13 and the run-out section surface 14 in a first step. The coating which is a plasma coating in the present exemplary embodiment is applied, in particular, to the piston running surface 5 in a second step of the method according to the invention. That is to say, in other words, spraying of the piston running surface 5 takes place. During the coating or directly following it, the extraction of the reflected particles 15 takes place, of the plasma particles in the present exemplary embodiment.
On account of the spray jet 11, the further surfaces 13, 14 which are configured so as to face the interior space 3, that is to say, in particular, the bearing section surface 13 and the run-out section surface 14, are likewise sprayed with the coating material, that is to say with plasma. That is to say, said further surfaces 13, 14 likewise have a coating.
After the coating and the extraction, the bearing section surface 13 and the run-out section surface 14 are machined further, the coating which has likewise accumulated there being removed. The defined structure 16 is likewise removed at the same time as said removal.
The defined structure 16 might likewise also be removed following the removal of the accumulated coating.
The defined structure 16 has a constant pitch P with a value of greater than or equal to 1. In the present exemplary embodiment, it has been produced in a spindle process. It might likewise also be configured in a circular machining operation or a helical machining operation.
Number | Date | Country | Kind |
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10 2016 116 815.7 | Sep 2016 | DE | national |