The present invention relates to improvements in bearings for turbochargers, and, more specifically, improved lubrication and methods of lubrication for bearings for turbochargers.
Turbochargers are well known in the art and are generally used for supplying pressurized air to an internal combustion engine to increase performance. Turbochargers generally comprise a turbine wheel and a compressor wheel on a shared shaft. Bearings, including journal bearings or ball bearings, are used to support the shaft during high speed rotation. The turbine wheel is positioned in a housing shaped to promote passage of exhaust gases from the internal combustion engine over the turbine, in turn causing high speed rotation of the turbine and the associated shaft. This high speed rotation of the shaft then drives the compressor wheel. Generally, the compressor is surrounded by a compressor housing, allowing the rotating compressor to draw in and compress ambient air for subsequent supply to the associated internal combustion engine. The support shaft and bearings are generally housed within a center housing, located between the turbine housing and the compressor housing.
Due to the high rotational speeds of the turbocharger support shaft, considerable effort is placed on maintaining proper operation of the support shaft bearings. For ball bearings, in particular, it is necessary to provide lubrication to the rolling surfaces in order to prevent bearing ring overheating and premature raceway damage. In addition, the high heat of the exhaust gases from the internal combustion engine poses additional problems of thermal transfer to surrounding systems, itself requiring lubrication, often in the form of engine oil, in order to cool the turbocharger system, including the bearings. A further consideration is over-supply of lubricating oil to the bearing, particularly ball bearings, in an effort to address the transient nature of the turbocharger environment. This over-supply may result in reduction of operating efficiency through viscous losses.
Lubrication, once again, often in the form of engine oil, is supplied through ports or “jets” often located in the bearing outer ring or the center housing. The bearing supports are often spaced far apart on the support shaft to maintain low vibration and high rigidity of the system, with the oil supply holes located between the two bearing elements. These oil jets provide oil for both lubrication of the bearing and for cooling of the system.
Generally, cooling demand far exceeds lubrication demand. Volumetric flow within the bearing cavity is controlled by orifice size, input pressure or other restriction methods. In this arrangement, the bearing operates with oil quantity in excess of its optimal value with respect to lubrication function resulting in viscous loss. In addition, all oil used for cooling of the shaft passes through the bearing raceways. Engine oil often contains a level of contamination higher than recommended for proper bearing function, therefore, with the increased volume of possibly contaminated oil passing through the bearing contact zone the probability of indirect damage is high.
Finally, as discussed, numerous configurations and types of bearings have been used to address the issue of reduced friction losses at high speeds, in combination with the thermal transient conditions of a turbocharger operating environment. Increased friction in the support bearings have also been associated with “turbo lag”. “Turbo lag” is generally identified as the delayed response associated with a turbocharger coming to an operating speed wherein pressurized air is effectively supplied to the internal combustion engine and is as a result of the time taken for the exhaust gas driving the turbocharger to come to high enough pressure for the turbine rotor to overcome the rotational inertia of the turbocharger system. Any friction losses, such as due to over-supply of lubricant, may increase this phenomena. Conversely, reduction of friction losses will reduce the time and incidence of “turbo lag”. Reduction of these frictional losses is identified as desirable in the marketplace.
The example aspect of the invention described comprises an improved ball assembly for a turbocharger assembly. The turbocharger assembly comprising an outer turbocharger housing, a turbine positioned in a turbine housing with the turbine housing joined with the turbocharger housing by any variety of means, including bolts, with the turbine, in turn, positioned on a rotary shaft. The example embodiment also comprises a compressor positioned on the rotary shaft in a compressor housing, the compressor housing similarly assembled with the turbocharger housing on an opposite end from the turbine housing. Included is a center housing assembled between the compressor housing and the turbine housing, within an inner cavity in the turbocharger housing, and at least two ball bearings positioned towards opposing ends on the rotary shaft between the turbine and the compressor, the ball bearings comprising an outer ring with an outer bearing raceway, a plurality of balls, a ball retainer and an inner ring with an inner bearing raceway. A lubricant reservoir and channel is formed in the turbocharger housing, with at least one bearing lubrication port connected to the reservoir, the port positioned in the center housing between the bearings directed toward lubricating at least one of the bearings and at least one turbocharger cooling port connected to the reservoir, the port positioned in the center housing outside of the bearings, directing lubricant away from the bearings and toward cooling and lubrication of the turbocharger system. The assembly also includes a lubricant exhaust port in the center housing, and a lubricant exhaust port in the outer turbocharger housing to return the lubricant to a central lubricant sump.
A further example embodiment of the invention has the center housing formed as a hollow shaft, forming the bearing outer rings, in which are formed outer bearing raceways. The lubrication and cooling port are positioned through this hollow shaft on opposite ends of each of the bearings.
A further example embodiment of the invention includes having a spacer located between the bearing inner rings. Alternatively, the bearing inner rings may be elongated, extending toward each other and abutting at a point between the two bearings.
The above mentioned and other features and advantages of the embodiments described herein, and the manner of attaining them, will become apparent and be better understood by reference to the following description of at least one example embodiment in conjunction with the accompanying drawings. A brief description of those drawings now follows.
Identically labeled elements appearing in different ones of the figures refer to the same elements but may not be referenced in the description for all figures. The exemplification set out herein illustrates at least one embodiment, in at least one form, and such exemplification is not to be construed as limiting the scope of the claims in any manner.
In the foregoing description, example embodiments are described. The specification and drawings are accordingly to be regarded in an illustrative rather than in a restrictive sense. It will, however, be evident that various modifications and changes may be made thereto, without departing from the broader spirit and scope of the present invention.
In addition, it should be understood that the figures illustrated in the attachments, which highlight the functionality and advantages of the example embodiments, are presented for example purposes only. The architecture or construction of example embodiments described herein is sufficiently flexible and configurable, such that it may be utilized (and navigated) in ways other than that shown in the accompanying figures.
Although example embodiments have been described herein, many additional modifications and variations would be apparent to those skilled in the art. It is therefore to be understood that this invention may be practiced otherwise than as specifically described. Thus, the present example embodiments should be considered in all respects as illustrative and not restrictive.
| Number | Date | Country | |
|---|---|---|---|
| 61317551 | Mar 2010 | US |