1. Technical Field
The invention relates to a process and an apparatus for casting a piston for an internal combustion engine.
2. Related Art
In pistons of internal combustion engines, the strength of the so-called piston-pin bores, in which the piston pin is accommodated for connection with a piston rod, is of particular importance. The required strength can be achieved in particular by rapid quenching of the casting. According to the current procedure, such quenching only takes place outside the mold, when the piston as a whole has solidified to such an extent that it can be removed from the so-called mold.
DE 10 2005 027 540 A1 relates to a process for the production of a piston for internal combustion engines, in which the casting mould is opened before the melt in the region of a feeder has solidified. The piston can subsequently be removed and cooled outside the casting mold.
The object underlying the invention is to provide a process and an apparatus for casting pistons for internal combustion engines, with which the strength, in particular in the region of the piston-pin bores, can be improved.
Accordingly, after boundary layer solidification in the region of at least one piston-pin bore, at least one sleeve provided there is withdrawn and that region is cooled. As a result, the region of the piston-pin bores, in particular the largely cylindrical inner face thereof, can be cooled and quenched more quickly than is possible with the current procedure, so that the strength in those regions is advantageously increased. To that end, it is necessary to wait for only a certain degree of boundary layer solidification, which allows a sleeve provided there to be withdrawn without jeopardizing the shape of the piston in that region. A sleeve is substantially a largely cylindrical or slightly conical casting core which, during casting, keeps free the space subsequently intended for the piston pin and around which the material that surrounds the subsequent piston-pin bore is accordingly molded. With regard to the expression piston-pin bore, it is to be emphasized that this does not necessarily have to be formed by boring as a procedure according to the process. Rather, it is conventionally two substantially cylindrical openings in which the two ends of a piston pin are accommodated, while the piston rod is located between them in the assembled state.
Accordingly, the material surrounding the piston-pin bores can be cooled and quenched by the procedure according to the invention more quickly than has been possible hitherto, so that more rapid and more directed solidification is possible, which results in increased strength. In other words, the rate of solidification of the piston material in particular in the region of the piston-pin bores is increased, which leads to quenching and increased strength. Furthermore, directed solidification can also be produced by means of the described procedure in other regions of the piston.
It is at present preferred to carry out cooling of the piston-pin bores by means of compressed air. Initial considerations have shown that the compressed-air lines required therefor can be provided for all sizes of piston, in particular diesel pistons.
It is further preferred in this connection that a cooling agent that is to be supplied, in particular compressed air, is supplied through at least one core provided between the piston-pin bores and/or through at least one sleeve. Such a core or sleeve has sufficient space, even in the case of small piston types, for compressed-air lines and nozzles or openings to be provided. In particular, the core can advantageously have at least one outlet opening for the cooling medium pointing towards the respective sleeve. There are preferably provided on the core on at least one side, preferably on both sides, two openings, in particular in the form of bores, which are arranged “one behind the other” according to the representation shown in the accompanying figures discussed hereinbelow and which consequently are visible in the figures as only one bore. In other words, the two bores are in different places in the radial direction and, for example, symmetrical relative to the piston axis. Furthermore, a common supply line or separate supply lines to the different bores can be present.
The start of the supply of cooling agent can be initiated particularly efficiently if the above-mentioned outlet openings are freed by the withdrawal of the particular sleeve in question.
It has further been found to be advantageous to configure such a core to be withdrawable. As a result, in particular after initial cooling of the region of the piston-pin bores, further cooling agent, in particular compressed air, can be supplied through the core, preferably to a lesser extent, so that the region between the piston-pin bores can also be cooled. In other words, the core is not withdrawn at first, and the material that is in contact with the core until the core is withdrawn is cooled in order to achieve increased strength there too. Cooling agent can subsequently be supplied simultaneously by way of the core and at least one sleeve. Alternatively, it has been found to be advantageous, after the core has been withdrawn, for cooling of the core space, that is to say the region which is in contact with the core until it is withdrawn, to be carried out by supplying cooling agent through only one sleeve. Cooling to a lesser extent can accordingly be effected by supplying cooling agent, in particular compressed air, through precisely one sleeve.
The object mentioned above is further achieved by the casting apparatus having at least one sleeve, which can be withdrawn from the region of a piston-pin bore, and a device for cooling the region of the piston-pin bores. The advantages mentioned above can be achieved by such an apparatus. The preferred embodiments of the apparatus according to the invention correspond to the process features described above.
A preferred exemplary embodiment of the invention is discussed in greater detail below. In the drawings:
The casting apparatus or mold 20 for a piston 10 shown schematically in section in
As is shown in
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In
Number | Date | Country | Kind |
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10 2010 003 345 | Mar 2010 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2011/054531 | 3/24/2011 | WO | 00 | 12/21/2012 |
Publishing Document | Publishing Date | Country | Kind |
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WO2011/117343 | 9/29/2011 | WO | A |
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Number | Date | Country | |
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20130092342 A1 | Apr 2013 | US |