The invention relates to a bearing housing body group of an exhaust-gas turbocharger, as per the preamble of Claim 1.
Within the context of downsizing programmes for internal combustion engines, ever smaller and more compact exhaust-gas turbochargers are the preferred embodiments. However, the oil quantity required for the function of mounting the rotor cannot be reduced to the same extent as the external dimensions. Relatively small exhaust-gas turbochargers therefore tend in particular to oil up at the compressor side at certain operating points, since the volume available in the bearing housing for discharging the oil is relatively small.
It is therefore an object of the present invention to create a bearing housing body group of an exhaust-gas turbocharger as per the preamble of claim 1 which permits a compact design of the exhaust-gas turbocharger with a simultaneous improvement of the compressor-side oil sealing,
Said object is achieved by means of the features of Claim 1.
In contrast to known bearing housing body groups, in which the bearing housing cover is fastened by means of conventional connecting techniques such as screws or circlips, the design of the fastening device according to the invention as a bayonet connection has the advantage that the space between the axial bearing and the housing cover of the bearing housing body group can be designed to be so large that oil can flow out unhindered, and the oil pressure can be depleted in an unhindered fashion to the same value as that in the crankcase of the engine.
The subclaims relate to advantageous refinements of the invention.
The bayonet connection of the body group according to the invention may, in a particularly preferred embodiment, have a web arrangement on the housing cover and an associated groove arrangement in the housing opening, with an arrangement of three webs being preferable, which three webs may be arranged uniformly on the periphery of a web ring of the housing cover, with a spacing of 120° conventionally being provided.
The groove arrangement of the housing opening may, for this purpose, have three part-ring grooves which are separated from one another by webs and which are provided in each case with an insertion recess into which the webs of the web arrangement can be inserted and come to rest, and latch, in a recess at the end of the part-ring grooves.
For fixing, it is necessary merely for the housing cover, after the positioning of the webs with respect to the insertion recesses, to be moved axially by a defined distance, such that the webs can be rotated into the part-ring grooves in the circumferential direction by a defined angle in the rotational direction of the rotor. Having arrived in said position, the axial pushing force can be removed and the webs come to rest in an axial recess at the end of the part-ring grooves, such that latching takes place and a backward rotation is reliably prevented.
In one particularly preferred embodiment, the housing cover is provided with a holding groove for an O-ring. Here, the holding groove may be open at one end side or closed at both end sides.
In the case of the groove of the housing cover being open at one side, the O-ring is axially compressed during the fixing of said housing cover in the bearing housing, which axial compression of the O-ring firstly provides an axial force component for increasing the axial clamping force and secondly ensures the sealing action, whereas a groove for the O-ring which is closed at both sides provides merely a radial compression for the sealing function.
Furthermore, in a further particularly preferred embodiment, it is possible to arrange a spring plate in the bearing housing between the housing cover and the axial bearing, which spring plate fixes the axial bearing axially.
The spring plate may preferably be designed as a plate spring.
Further details, advantages and features of the present invention can be gathered from the following description of exemplary embodiments on the basis of the drawing, in which:
The body group 1 has a housing 2 for a bearing arrangement (not illustrated in any more detail in the figures) of a rotor shaft 3.
The body group 1 also comprises a turbine wheel 4 on one end 5 of the rotor shaft 3, while a compressor wheel 6 is arranged on the opposite end 7 of the rotor shaft 3.
The housing cover 8 can be fixed at the compressor side in a compressor-wheel-side housing opening 10 by means of a fastening device 9.
According to the invention, the fastening device 9 is designed as a bayonet connection which has a web arrangement 11 on the housing cover 8 and a groove arrangement 12 in the housing opening 10 of the housing 2.
Of the web arrangement,
The annular groove arrangement 12 has a number of insertion recesses corresponding to the number of webs 11, that is to say in the example, three such insertion recesses. of which the insertion recesses 13 and 14 can be seen in the illustration of
The housing cover 8 may also have a holding groove 15 (see
The embodiment of the holding groove 15 which can be seen in
The embodiment according to
However, the embodiment of
It can correspondingly be seen from the illustration of
In addition to the written disclosure of the invention, reference is hereby explicitly made to the diagrammatic illustration of said invention in
Number | Date | Country | Kind |
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102008031349.1 | Jul 2008 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US09/48763 | 6/26/2009 | WO | 00 | 12/16/2010 |