The field to which the disclosure generally relates includes turbochargers for use with internal combustion engines and more particularly, includes turbochargers with an exhaust driven rotary turbine that drives a compressor to charge an engine's air intake system.
An exhaust driven turbocharger may be used with an internal combustion engine to compress air delivered to the engine's intake air system. The turbocharger may include a compressor rotor driven by a connected turbine rotor. The compressor may include a housing that channels intake aft and the turbine may include a housing that channels exhaust gases. The compressor housing may be spaced apart from the turbine housing by a bearing housing containing bearings that support a shaft connecting the turbine rotor to the compressor rotor.
The compressor rotor, the shaft and the turbine rotor may rotate at speeds that approach hundreds of thousands of revolutions per minute. In addition, the turbine rotor operates in a high temperature exhaust gas environment, wherein heat may be transferred to the other turbocharger system components. Under these harsh, and increasingly demanding operating conditions, the lifespan of a turbocharger is expected to match that of the engine with which it operates. To accomplish that challenge, the design of a turbocharger and its components must be robust to survive as expected, while still being cost effective. As a result, a turbocharger is designed to exacting tolerances and standards.
To reduce friction in the bearings, the bearing housing may include an oil delivery system to provide lubrication. Oil may be provided by the associated engine's pressurized oil delivery system and may be channeled through the bearing housing to the bearings and other rotating parts. The oil may then be collected and allowed to drain back to the engine's sump. Maintaining the integrity of the lubrication circuit is essential so that the oil level in the associated engine is not depleted, and so that oil does not enter unwanted areas.
A product according to a number of variations may inhibit oil from entering a turbocharger compressor. A compressor wheel may be disposed in a wheel chamber of a housing to rotate at a range of speeds. The compressor wheel may be surrounded by a collection volute with a diffuser channeling air from the wheel chamber to the collection volute. A shaft may extend through the housing and may be connected to the compressor wheel. The shaft may be supported by a bearing that may be lubricated through an oil circuit. A pressure differential between the wheel chamber and the oil circuit may inhibit oil from entering the wheel chamber. The pressure differential may be maintained during rotation of the compressor wheel at a low end of the range of speeds by a collar disposed near a tip of the compressor wheel at an entrance to the diffuser. The pressure differential may maintain oil in the lubrication circuit.
Other illustrative variations within the scope of the invention will become apparent from the detailed description provided herein. It should be understood that the detailed description and specific examples, while disclosing variations within the scope of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
Select examples of variations within the scope of the invention will become more fully understood from the detailed description and the accompanying drawings, wherein:
In a number of illustrative variations of turbocharger systems for internal combustion engines, oil migration into the compressor housing is impeded. Referring to
Referring additionally to
The bearing housing 24 may include an annular groove 42 located at a position that is radially outside the circumferential tip 20 of compressor wheel 14 and opens to the diffuser 38. A collar 44 may be annular in shape with an axially disposed leg 46 and an integral radial disposed leg 48, and may be configured to operate to provide an active diffuser. In the illustration of
The collar 44 may be biased to slide outward in the groove 42 by a spring 50 that is positioned in a chamber of the groove 42 as shown in
The collar 44 may have a groove (not shown), with a seal or seals to inhibit pressure leakage around the collar 44. An opening 54 may be bored in the bearing housing 24 between the diffuser 38 and the groove 42 with a port 56 opening to the groove 42 behind the retainer 52. The opening 54 may allow pressure to communicate from the diffuser 38 to the groove 42 to assist in moving the collar 44 into the groove 42 as pressure builds in response to increased rotational speed of the compressor wheel 14. A vent 58 opening may be bored through the bearing housing 24 into the groove 42 to allow air to escape from behind the collar 44. The vent 58 may extend to a point outside the bearing housing 24 or to a point inside the bearing housing 24. Through the foregoing structure, pressure is provided both at relatively low rotational speeds and relatively high rotational speeds, sufficient to inhibit leakage of oil from the bearing housing 24 to the compressor wheel chamber 34. At higher rotational speeds of the compressor wheel 14, the diffuser 38 is not obstructed by the sliding collar 44, optimizing flow efficiency.
Referring additionally to
As shown in
Referring to
A collar 124 may be annular in shape with an axial directed leg 126 positioned in the axially extending groove section 120 and an integral radial directed leg 128 positioned at least partially in radially extending groove section 122, and may be configured to operate in providing an active diffuser. The collar 124 may be configured with a spring section 130 in leg 126 to bias the radial inside end 132 of leg 128 outward from the groove 118, and into the diffuser 110 near the circumferential tip 134 of the compressor wheel 102. This may narrow the width of the flow channel provided by the diffuser 110 which may result in an increase in pressure within the compressor wheel chamber 112 including on the back 136 side of the compressor wheel 102. An increase in pressure may assist in maintaining oil in the bearing housing section 108 and inhibit migration of oil past the insert wall 116 into compressor wheel cavity 112. When the compressor wheel 102 may rotate at speeds above the low end of its rotational speed range, the pressure may overcome the force of spring section 130 compressing the collar 124 and fully moving the leg 128 into the groove section 122. As a result, the diffuser may be open from the tip 134 radially outward, without restricting flow. The collar 124 may be formed as one piece from a thermoplastic or other material suitable for the application including the spring section 130. The leg 128 may be held in the groove section 122 by a retainer 138 and the leg 126 may be held in the groove section 120 by a retainer 140.
Through the foregoing illustrative variations, a turbocharger system may be provided with an active diffuser responsive to pressure generated by a compressor wheel to retain oil in a bearing housing by maintaining a pressure differential between the compressor wheel's cavity and the bearing housing. The following description of variants is only illustrative of components, elements, acts, products and methods considered to be within the scope of the invention and is not in any way intended to limit such scope by what is specifically disclosed or not expressly set forth. Components, elements, acts, products and methods may be combined and rearranged other than as expressly described herein and still are considered to be within the scope of the invention.
Variation 1 may involve a product that may inhibit oil from entering a turbocharger compressor. A compressor wheel may be disposed in a wheel chamber of a housing to rotate at a range of speeds. The compressor wheel may be surrounded by a collection volute with a diffuser channeling air from the wheel chamber to the collection volute. A shaft may extend through the housing and may be connected to the compressor wheel. The shaft may be supported by a bearing that may be lubricated through an oil circuit. A pressure differential between the wheel chamber and the oil circuit inhibits oil from entering the wheel chamber. The pressure differential may be maintained during rotation of the compressor wheel at a low end of the range of speeds by a collar disposed near a tip of the compressor wheel at an entrance to the diffuser. The pressure differential may maintain oil in the lubrication circuit.
Variation 2 may include a product according to variation 1 and may include a spring biasing the collar toward the wheel. During rotation of the wheel at speeds above the low end of the range of speeds, the pressure differential may cause the collar to slide to compress the spring.
Variation 3 may include a product according to variation 2 wherein during rotation of the wheel at the low end of the range of speeds the spring may bias the collar to direct air from a tip of the wheel to a shaft side of the wheel, to increase pressure on the shaft side of the wheel.
Variation 4 may include a product according to variation 2 or 3 wherein the spring may be disposed in a chamber of the housing behind the collar and wherein a vent may extend from the chamber and through the housing.
Variation 5 may include a product according to any of variations 1 through 4 and may include a retainer engaged in the housing. The retainer may hold the collar in a groove of the housing. An opening may extend through the housing from the diffuser to the groove. The opening may enter the groove at a port located between the retainer and the collar.
Variation 6 may include a product according to any of variations 1 through 5 wherein the collar may be disposed in a groove of the housing. The collar may include a cavity. An opening may extend through the housing from the diffuser to the groove. The opening may enter the groove at a port that is aligned with the cavity.
Variation 7 may include a product according to variation 1 wherein the collar may include a disk section extending along the diffuser and a spring section joining with the disk section and biasing the disk section to vary the diffuser in response to the pressure differential.
Variation 8 may involve a product for use with a turbocharger. A compressor wheel may be connected to and may rotate with a shaft. The compressor wheel may be disposed in a compressor housing. A bearing may be disposed in a bearing housing and may rotatably support the shaft. The bearing housing may include an annular groove formed in a radial location outside a circumferential tip of the compressor wheel. A collar may be disposed in the annular groove. The collar may slide in the groove in an outward direction when the compressor wheel rotates at a relatively slow speed and the collar may slide in the groove in an inward direction when the compressor wheel rotates at a relatively fast speed.
Variation 9 may include a product according to variation 8 and may include a spring biasing the collar in the outward direction. During rotation of the compressor wheel at the relatively fast speed, a pressure differential may cause the collar to slide in the inward direction.
Variation 10 may include a product according to variation 8 or 9 wherein during rotation of the compressor wheel at the relatively low speed, a spring may cause the collar to slide in the outward direction.
Variation 11 may include a product according to any of variations 8 through 10 and may include a retainer engaged in the bearing housing. The retainer may hold the collar in the annular groove of the bearing housing.
Variation 12 may include a product according to variation 11 wherein an opening may extend through the bearing housing from a diffuser channel to the annular groove. The opening may enter the annular groove at a port located between the retainer and the collar.
Variation 13 may include a product according to any of variations 8 through 12 wherein the collar may include a cavity. An opening may extend through the bearing housing from a diffuser channel to the annular groove. The opening may enter the annular groove at a port. The port may be aligned with the cavity.
Variation 14 may include a product according to variation 8 and may include a diffuser channel. The collar may include a disk section extending along the diffuser channel and a spring section joining with the disk section. The spring section may bias the disk section to vary the diffuser channel in response to a pressure generated by the compressor wheel.
Variation 15 may involve a turbocharger system and may include a housing assembly having a compressor wheel cavity and a bearing cavity. A compressor wheel may be rotatably disposed in the compressor wheel cavity. A bearing may be disposed in the bearing cavity. A shaft may be connected to the compressor wheel and may extend through the bearing for support. The compressor wheel may include a circumferential tip. A diffuser channel may extend through the housing assembly from the compressor wheel cavity to a collection volute. The housing assembly may have an annular groove facing the diffuser channel near the circumferential tip. A collar may be slidably disposed in the annular groove. The collar may slide into and out of the diffuser channel in response to a pressure generated by a rotational speed of the compressor wheel.
Variation 16 may include a turbocharger assembly according to variation 15 and may include a spring disposed in the annular groove behind the collar and biasing the collar out of the annular groove.
Variation 17 may include a turbocharger assembly according to variation 16 and may include a retainer engaged in the housing assembly, the retainer may hold the collar in the annular groove.
Variation 18 may include a turbocharger assembly according to variation 17 wherein an opening may extend through the housing assembly from the diffuser channel to the annular groove. The opening may enter the annular groove at a port located between the retainer and the collar.
Variation 19 may include a turbocharger assembly according to variation 15 wherein the collar may include a cavity with an opening extending through the housing assembly from the diffuser channel to the annular groove. The opening may enter the annular groove at a port that is aligned with the cavity.
Variation 20 may include a turbocharger assembly according to variation 15 wherein the collar may include a disk section extending along the diffuser channel and a spring section joining with the disk section and biasing the disk section to vary the diffuser channel in response to a pressure generated by a rotational speed of the compressor wheel.
The above description of select variations within the scope of the invention is merely illustrative in nature and, thus, variations or variants thereof are not to be regarded as a departure from the spirit and scope of the invention.
Number | Name | Date | Kind |
---|---|---|---|
916427 | Fee | Mar 1909 | A |
3289919 | Wood | Dec 1966 | A |
3728857 | Nichols | Apr 1973 | A |
3784318 | Davis | Jan 1974 | A |
3874677 | Ludwig et al. | Apr 1975 | A |
4219305 | Mount et al. | Aug 1980 | A |
4236867 | Morris | Dec 1980 | A |
4257733 | Bandukwalla et al. | Mar 1981 | A |
4265589 | Watson et al. | May 1981 | A |
4378194 | Bandukwalla | Mar 1983 | A |
4460310 | Plunkett | Jul 1984 | A |
4472107 | Chang et al. | Sep 1984 | A |
4611969 | Zinsmeyer | Sep 1986 | A |
4828454 | Morris et al. | May 1989 | A |
4932835 | Sorokes | Jun 1990 | A |
5297928 | Imakiire et al. | Mar 1994 | A |
6139262 | Ravidranath | Oct 2000 | A |
6368077 | Meyerkord et al. | Apr 2002 | B1 |
6857845 | Stabley et al. | Feb 2005 | B2 |
6966746 | Cardenas et al. | Nov 2005 | B2 |
7252474 | Belokon et al. | Aug 2007 | B2 |
7326027 | Skoch et al. | Feb 2008 | B1 |
20050175446 | Garner | Aug 2005 | A1 |
20110255963 | Kim | Oct 2011 | A1 |