The invention relates to an exhaust-gas turbocharger according to the preamble of claim 1.
Known exhaust-gas turbochargers with a so-called wastegate arrangement have a flap plate which can be actuated by means of a control capsule and a lever mechanism and which regulates the throughput of a bypass opening which leads directly from the inlet region of the spiral of the turbine housing to the outlet out of the turbine. Since the spiral is heated up very intensely by the hot exhaust gases, in particular in said inlet region, sealing problems arise in said known designs on account of said thermal loadings, which sealing problems are exacerbated in that the flap plate, in the open state, is impinged on directly by the main flow of the exhaust gas discharged by the turbine wheel.
Furthermore, the spindle shaft of known exhaust-gas turbochargers with a wastegate arrangement runs perpendicular to the charger axis, such that the regulating rod together with the control capsule is aligned substantially axially with respect to the charger axis, which leads in part to space problems and therefore to problems during the installation of the exhaust-gas turbocharger.
It is therefore an object of the present invention to create an exhaust-gas turbocharger of the type specified in the preamble of claim 1 which can be better adapted to different installation situations and which enables an improvement in the sealing action of the wastegate arrangement.
Said object is achieved by means of the features of claim 1.
Subclaims 2 to 5 relate to advantageous refinements of the invention.
Claims 6 to 9 present a wastegate arrangement as an object which can be dealt with independently.
In particular, the arrangement of the spindle shaft parallel to the charger axis makes it possible for the regulating rod to be arranged substantially at right angles with respect to the charger axis and to thereby position the control capsule radially, which yields installation space advantages for certain installation conditions.
Furthermore, it is made possible for the bypass opening to be arranged at one end of a bypass duct whose other end is flow-connected to the spiral of the turbine housing. This results in cooling of the exhaust-gas flow impinging on the flap plate, which increases the sealing action since thermal decoupling of the flap plate is made possible at least to a certain extent by means of the bypass duct, which acts as a cooling path.
Furthermore, the provision of a line or bypass duct of said type provides greater freedom for positioning the flap, which in a particularly preferred embodiment permits an arrangement outside the exhaust-gas main flow passing from the turbine wheel, which yields a further improvement of the sealing action of the flap plate.
Furthermore, it is made possible for the turbine housing to be formed as a sheet-metal housing, which above all yields production advantages and therefore cost advantages.
Further details, advantages and features of the present invention will emerge from the following description of exemplary embodiments on the basis of the appended drawing, in which:
A description of all other components, which of course likewise encompasses said exhaust-gas turbocharger 1, may however be omitted for the explanation of the principles of the present invention.
The exhaust-gas turbocharger 1 according to the invention is therefore explained in detail below on the basis of a description of a juxtaposition of
The wastegate arrangement 5 comprises a control capsule 6, a regulating rod 7 which can be moved by the control capsule 6, a lever 8 which is connected to the regulating rod 7 by means of a guide piece 9, and a spindle shaft 10.
The spindle shaft 10 is connected at one end to the lever 8 and at the other end to a spindle 11 which bears a flap plate 12 for opening and closing a bypass opening 13.
As can be seen in particular from
Furthermore, the regulating rod 7 is arranged substantially at right angles to the charger axis L, as can be seen from
As is also illustrated in detail in
As illustrated in
In addition to the above written disclosure of the invention, reference is hereby additionally explicitly made to the diagrammatic illustration thereof in
Number | Date | Country | Kind |
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102009012309.1 | Mar 2009 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US10/25840 | 3/2/2010 | WO | 00 | 8/31/2011 |