This application claims priority under 35 U.S.C. §119 to European Application No. 04405762.8 filed in Europe on Dec. 8, 2004, and as a continuation application under 35 U.S.C. §120 to PCT/CH2005/000694 filed as an International Application on Nov. 24, 2005 designating the U.S., the entire contents of which are hereby incorporated by reference in their entireties.
1. Field
A stator arrangement, or distributor, of a turbine machine, for example, of an exhaust gas turbine or a compressor is disclosed. In an exhaust gas turbine which is exposed to axial incident flow, such a distributor is connected upstream of the moving blades of the turbine and has guide blades in the exhaust gas-carrying flow channel which are arranged axial-symmetrically to the turbine axis and which can each be pivoted around a radially guided axis, and a pivoting device which moves the guide blades around the pivot axis. With this distributor, by pivoting the guide blades, the size of the cross section area of the flow channel through which the exhaust gas flows can be changed and the exhaust gas turbine can be adapted to changing exhaust gas flows, as occur for example in partial load operation of an internal combustion engine which delivers an exhaust gas.
2. Background Information
A distributor is described for example in DE 100 13 335 A1. In this distributor, concentrically to the moving wheel of the turbine there is a setting ring which is located radially outside in the flow channel. A blade shaft which is guided out of the flow channel through the housing wall radially to the outside is attached to each of the guide blades. The blade shaft is supported to pivot around the pivot axis with its part which is guided to the outside. The pivoting device contains a setting ring which is located outside the flow channel and which can be pivoted around the turbine axis, and adjusting levers which transmit torque from the setting ring to the blade shaft of each guide blade.
The adjusting levers are slipped with one end onto the blade shaft. With the other end the adjusting levers are guided in the grooves of the setting ring. The grooves are bordered by two radially guided groove walls, with a distance from one another which is somewhat greater than the diameter of the ends of the adjusting levers, which ends are made as a ball head and are guided in the grooves.
Due to the rotational and pivoting motion, the ball head of the adjusting lever is moved on the surface of the groove walls. Based on the point support of the balls in the grooves of the adjusting lever, very high Hertzian stresses can occur in spite of moderate normal forces. The relative movements of the balls on the surface of the groove walls and the high surface pressures can lead to wear on the sliding partners in operation.
Patents U.S. Pat. No. 5,316,438 and U.S. Pat. No. 4,867,635 and patent disclosure document DE 1 503 527 A1 disclose distributors with adjustable guide blades. The adjustment mechanisms of these distributors have adjusting devices which transmit force from a setting ring to the shafts of the guide blades to adjust the guide blades. The adjusting levers are provided on one end with a ball head and engage ball sockets with it in the region of the setting rings.
A stator component, or distributor, for a turbine machine is disclosed wherein a surface which acts on a ball head of adjusting levers for transmission of torque to a blade shaft of each guide blade is configured as ball socket, the ball socket being formed at least partially from slide elements which are arranged to be able to move translationally. Such features can yield a uniform, large-area pressure distribution by which the wear of the parts which press on one another can be distinctly reduced.
In an exemplary embodiment, there are guide shoes in grooves of a setting ring, which are configured as a ball socket and in which the ball heads of the adjusting levers are located. For an exemplary embodiment, the guide shoes can be easily and very economically produced.
Various exemplary embodiments of a distributor are detailed below using the drawings, wherein like elements have been designated by like reference numbers, and wherein:
The shaft on whose one end the turbine blade carrier is mounted is routed gas-tight out of the housing to a bearing point which is not shown and on its other end bears a compressor wheel which is likewise not specifically shown in
The turbine housing contains a gas inlet housing 71 with an inlet opening arranged axial-symmetrically and a gas exit housing 72 with a radially aligned exit opening. Between the inlet and outlet opening a flow channel which is bordered by the turbine housing extends. Hot gas from an exhaust gas source which is not shown, especially an internal combustion engine, is supplied through the inlet opening. This hot gas is first routed in a section of the flow channel which is aligned in the direction of the turbine axis. In this section the exhaust gas is routed over the guide blades 11 and the moving blades 61. Downstream of the moving blades the exhaust gas enters a section of the flow channel which is bordered by the gas exit housing and in which it is routed radially to the outside away from the axis and is finally removed from the turbine housing via the exit opening.
The distributor is held on a support ring 73 which is clamped between the gas inlet housing 71 and the gas exit housing 72. Furthermore, a relief ring which is thermally decoupled from the support ring is clamped between the two housings and borders the flow channel radially to the outside in the region of the guide blades 11 and in this way shields the support ring against the direct action of hot exhaust gases and thus thermally relieves it. Each guide blade 11 forms a unit with the attached blade shaft 12. The blade shaft is guided out of the flow channel radially to the outside through the housing wall. The blade shaft with its outwardly guided part is mounted to be able to turn around the radially pointed pivot axis which is shown by the broken line. The rotary motion is initiated by a setting ring 3 which is located outside the flow channel and which can turn around the turbine axis and by adjusting levers 2 which transmit torque from the setting ring 3 to the blade shaft 12 of each guide blade.
The part of the blade shaft 12 which is guided to the outside is supported at two locations 13 which are arranged radially offset against one another. The two bearing points 13 are located in the support ring 73 which is used as a section of the housing.
The adjusting lever 2 is connected on one end by a plug connection to the blade shaft 12. As
In the exemplary embodiments shown in the figures, the groove 4 in the peripheral direction is bordered by essentially radially guided groove walls 41 which run parallel to one another. In the exemplary embodiment shown, the middle plane between the two groove walls runs exactly in the radial direction, while the two groove walls which run parallel to one another deviate slightly from the radial direction. As is shown in
When the adjusting ring 3 for adjusting the guide blades 1 is turned, the slide elements 51 are pushed from the ball head in the groove 4 in the plane of the groove surfaces 41. If the setting ring in
By a small projection which runs peripherally at least partially on the axial edge of the groove, the ball head which is inserted into the groove in the radial direction, i.e. from underneath in
The two slide elements 51 can be fitted independently of one another between the ball head 25 and the respective groove walls 41. For facilitated installation, the two slide elements can also be made as the legs of a guide shoe 5 which additionally encompasses a connecting piece 53 which holds the two legs together.
Alternatively to the illustrated exemplary embodiment with the slide elements 51, the ball socket can also be inlet directly into the groove walls. In any case, the freedom of motion of the adjusting lever with respect to the setting ring would have to be ensured by other means. For example, for this purpose the adjusting lever can include an elastically stretchable shaft which can stretch and bend up to a certain degree.
Due to the flattened regions on the bottom of the adjusting lever 26 and on the guide shoe 53 in the exemplary embodiment illustrated, the guide shoe after installation cannot turn relative to the adjusting lever. The flattened regions which are spaced apart from one another can however prevent the limited wobbling which can be desired for operation of the positioning device, but allow more extensive twisting which could lead to loosening of the connection between the ball head and the ball socket in an extreme case. The locking against rotation by the flattened region can also provide protection against loss which prevents the mounted guide shoe from falling off the adjusting lever and being lost.
In this embodiment, due to the flattening of the ball head, the height B of the guide shoe and the radial groove height in the setting ring can be reduced. In order to prevent rotation of the guide shoe and possible loosening of the connection between the ball head and the ball socket, there is an anti-rotation device 54 which can be made as an additional, flattened leg. If there is addition axial flattening of the ball head on the end of the adjusting lever, the axial depth of the grooves 4 can be reduced.
In an alternate exemplary embodiment, the distributor can be configured for producing a pretwist in the intake region of the compressor. This compressor can be used for example in an exhaust gas turbochargers. The pretwist distributor can include a pivotable setting ring which transmits torque to the blade shafts of the guide blades via adjusting levers as described herein.
It will be appreciated by those skilled in the art that the present invention can be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The presently disclosed embodiments are therefore considered in all respects to be illustrative and not restricted. The scope of the invention is indicated by the appended claims rather than the foregoing description and all changes that come within the meaning and range and equivalence thereof are intended to be embraced therein.
Number | Date | Country | Kind |
---|---|---|---|
04405762 | Dec 2004 | EP | regional |
Number | Name | Date | Kind |
---|---|---|---|
3303992 | Johnson | Feb 1967 | A |
3954349 | Abild | May 1976 | A |
3972644 | Johnson | Aug 1976 | A |
4239450 | Geitner et al. | Dec 1980 | A |
4430043 | Knight et al. | Feb 1984 | A |
4684319 | Sasaki | Aug 1987 | A |
4836746 | Owsianny et al. | Jun 1989 | A |
4867635 | Tubbs | Sep 1989 | A |
5025629 | Woollenweber | Jun 1991 | A |
5316438 | Tubbs | May 1994 | A |
20040009061 | McDonald | Jan 2004 | A1 |
Number | Date | Country |
---|---|---|
1 503 527 | Aug 1969 | DE |
1503527 | Aug 1969 | DE |
100 13 335 | Sep 2001 | DE |
Number | Date | Country | |
---|---|---|---|
20080107520 A1 | May 2008 | US |
Number | Date | Country | |
---|---|---|---|
Parent | PCT/CH2005/000694 | Nov 2005 | US |
Child | 11806647 | US |