Patent Application
20200300161
The invention relates to a turbocharger having an integrated position securement of a housing and to a method for producing such a turbocharger.
Major forces act on components of an exhaust gas turbocharger because of rotating components. In order to secure the housing and stator components of turbochargers against a rotation and an axial displacement, additional components and connecting elements, such as dowel pins or screws are generally required. Because of the further components, the number of parts increases substantially, which leads to an expensive installation and a high material expenditure.
An object of one aspect of the present invention is to provide a turbocharger having an integrated position securement of a housing and a method for producing such a turbocharger, which reduces the installation expenditure and the number of parts.
According to one aspect of the invention, a turbocharger having a housing and at least one stator is proposed. The housing and/or the stator comprises or comprise an inner housing component and an outer housing component, with which an inner section directly lies against a lateral portion of the inner housing component and covers the lateral portion. The respective lateral portion and the respective inner portion are formed such that together they form a positive-locking connection, which fixes the respective inner housing component and the respective outer housing component against a relative positional change relative to one another along a longitudinal axis of the turbocharger and/or against a rotation about this longitudinal axis. Furthermore, the respective inner housing component and/or the respective outer housing component is at least partly produced by additive manufacturing. By using additive manufacturing methods such as a 3D printing method, the position securement can be directly integrated in the components. Advantageous in this is for example that the component number is reduced and, as a consequence, the weight of the turbocharger and the production costs are also lowered. In addition to this, installation errors can be avoided by way of a positive-locking connection. Altogether, the installation and maintenance expenditure is optimised because of lighter and/or segmented components. Through the positive-locking connection, the containment safety and thus the product safety of the turbocharger improve additionally.
Preferentially, the turbocharger is designed so that the lateral section of an inner housing component and/or the inner section of an outer housing component are produced or were created entirely by additive manufacturing. This is particularly favourable since the forces, against which a position securement is employed, act on the lateral sections of the two housing components. In this way, the position securement can be exactly matched to the requirements of the respective turbocharger.
In an advantageous embodiment version it is provided that the lateral section comprises at least one positioning element that projects from the lateral section. In addition, the inner section comprises at least one recess, which is formed corresponding to the positioning element, so that together these form a positive-locking connection. In an exemplary embodiment of the invention it is provided that the positioning element is formed as a positioning lug and the recess as a groove. Further, an embodiment is favourable in which the positioning elements are formed as at least one spline and the recesses as at least one spline hub. In a further advantageous version it is provided according to the invention that the positioning element is partly or entirely formed as a wavy spline and the recess as a wavy spline hub.
By integrating positioning elements in the housing components, these can be fixed relative to one another in a circumferential direction. Additional connecting elements, such as dowel pins or screws can be omitted because they are no longer necessary. By shaping and arranging the individual positioning elements, an exact and unambiguous orientation of the housing components can be defined besides the position securement, as a result of which errors during the installation can be avoided.
The turbocharger according to one aspect of the invention is formed in an embodiment version so that a plug-turn connection or a bayonet connection is integrated in the lateral section and the inner section, which establishes a positive-locking connection between the inner housing component and the outer housing component. By integrating positioning elements in the housing components, these can be fixed in a longitudinal direction relative to one another.
Furthermore, the measures for the position securement described above can have positive effects on the containment safety for example in the case of a moving blade loss or rotor bursting. Thus, the shearing load screws of a containment-relevant flange connection can be prevented in that the torsional forces resulting from the failure are directly transmitted via the positive-locking connection of the components.
Furthermore it is advantageous when the inner housing component and/or the outer housing component is or are segmented and it is provided, furthermore, in a further development of the present turbocharger that hollow spaces are integrated in the inner housing component and/or the outer housing components. By dividing the components into segments and/or the specific introduction of hollow spaces, the installation and the maintenance expenditure can be reduced in particular in large turbochargers by way of a lower individual weight resulting from this. The segmenting or introduction of hollow spaces can be combined with the measures described above.
In a preferred embodiment of the invention, crash elements or a honeycomb structure for absorbing potential or kinetic energy of components during a component failure are integrated in the inner housing component and/or the outer housing component. Advantageous in this is that the crash elements or the honeycomb structure are directly integrated in the safety-relevant components. In this way, the crash elements or the honeycomb structure reduce the kinetic energy of the rotor fragments emitted in the event of a failure upon impacting on the housing structure by way of targeted deformation. Because of this, escaping of failing components from the turbocharger housing is prevented.
According to one aspect of the invention, a method for producing a turbocharger described above is proposed in which the inner housing component and/or the outer housing component are produced at least partly or entirely by additive manufacturing in particular by a 3D printing method. By an additive manufacture, the inner housing component and the outer housing component can be exactly matched to the requirements of the optimal position securement. For this reason, the installation expenditure, the weight and the costs of the turbocharger can be reduced and an adequate containment safety ensured at the same time.
In a preferred embodiment of the method, the lateral section and/or the inner section are entirely produced by additive manufacturing in particular by a 3D printing method. Particularly favourable in this is that the forces against which a position securement is employed act against the lateral portions of the two housing components. Thus, the position securement can be exactly matched to the requirements of the respective turbocharger.
Other advantageous further developments of the invention are marked in the subclaims or are shown in more detail by way of the figures together with the description of the preferred embodiment of the invention. It shows:
In
A sectional view of a turbocharger housing 1 with a bayonet closure 8 is shown in
Thus, while there have shown and described and pointed out fundamental novel features of the invention as applied to a preferred embodiment thereof, it will be understood that various omissions and substitutions and changes in the form and details of the devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those elements and/or method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.
| Number | Date | Country | Kind |
|---|---|---|---|
| 10 2019 107 093.7 | Mar 2019 | DE | national |
