US20100310363A1

US20100310363A1 - Turbocharger

Info

Publication number: US20100310363A1
Application number: US12/745,351
Authority: US
Inventors: Yoshimitsu Matsuyama; Hiroshi Tange
Original assignee: IHI Corp
Current assignee: IHI Corp
Priority date: 2007-12-12
Filing date: 2008-11-12
Publication date: 2010-12-09
Also published as: KR20100087376A; JP2009144546A; EP2233718A4; WO2009075057A1; CN101896705A; EP2233718A1; EP2233718B1; KR101196248B1

Abstract

Turbulence of fluid in a turbine impeller outlet is reduced with a simple structure so as to improve efficiency of a turbine.

In a turbocharger comprising a turbine housing 1 having a scroll passage 8 outwardly of an exhaust nozzle 9 which in turn is arranged outwardly of a turbine impeller 4 rotatably supported on a bearing housing 3, the exhaust nozzle 9 having a plurality of nozzle vanes 15 between front and rear exhaust introduction walls on sides of the bearing and turbine housings 3 and 1, respectively, a vane shaft for each of the nozzle vanes 15 extending at least through the front exhaust introduction wall 10 and being rotatably supported, pressing means 23 is arranged between the respective vane shafts 16 and the bearing housing 3 to urge the vane shafts 16 toward the rear wall 11 to displace the nozzle vanes 15 toward the rear wall 11.

Description

TECHNICAL FIELD

The present invention relates to a turbocharger which is simple in structure and which can reduce turbulence of fluid in a turbine impeller outlet to improve efficiency of a turbine.

BACKGROUND ART

FIG. 1 shows a conventional variable displacement turbocharger to which the invention is applied. In the turbocharger, turbine and compressor housings 1 and 2 are integrally assembled through a bearing housing 3 by fastening bolts 3 a and 3 b, a turbine impeller 4 in the turbine housing 1 being connected to a compressor impeller 5 in the compressor housing 2 by a turbine shaft 7 rotatably supported via a bearing 6 in the bearing housing 3.
As shown in FIG. 2 in enlarged scale, the bearing housing 3 is provided, on its turbine housing 1 side, with an exhaust nozzle 9 by which fluid (exhaust gas) introduced into a scroll passage 8 in the turbine housing 1 is guided to a turbine impeller 4.
The exhaust nozzle 9 comprises front and rear exhaust introduction walls 10 and 11 respectively on sides of the bearing and turbine housings 3 and 1 and integrally assembled together with a required distance between them by, for example, three fixing members 12 arranged circumferentially. Upon assembling of the turbine and bearing housings 1 and 3, an attachment member 13 fixed on a front surface of the front wall 10 (side surface of the bearing housing 3) is clamped by the housings 1 and 3 to fix the exhaust nozzle 9. Upon the assembling, the exhaust nozzle 9 is positioned with respect to the bearing housing 3 by a positioning pin 14.
Arranged between the front and rear walls 10 and 11 are a plurality of nozzle vanes 15 each rotatably supported at least on the front wall 10 by a vane shaft 16 extending through the front wall 10. In the example shown in FIG. 2, each of the nozzle vanes 15 is supported in a cantilever manner by the vane shaft 16 arranged on the vane 15 on the side of the bearing housing 3 to extend through the front wall 10. Alternatively, as shown in FIG. 1, each of the nozzle vanes 15 may be dually supported by vane shafts 16 and 28 on opposite sides of the vane 15 extending through the front and rear walls 10 and 11, respectively.
In FIG. 1, reference numerals 17 a, 17 b, 17 c and 17 d designate a linked transmission mechanism for varying an opening angle of the nozzle vanes 15 for capacity control; and 18, a scroll passage in the compressor housing 2.
Provided between the turbine housing 1 and the rear wall 11 of the exhaust nozzle 9 is a gap 19 which is, by nature, is unwanted and which is however is provided for countermeasure to, for example, possible thermal deformation of the turbine housing 1 between during being hot and during being cold and possible variations in accuracy of parts to be assembled.
The gap 19 may disadvantageously cause the exhaust gas in the scroll passage 8 to vainly leak to a turbine impeller outlet 20, resulting in lowering of turbine efficiency. Thus, in order to block the gap 19, it has been proposed to arrange sealing piston rings 21 between an outer surface of a downstream extension 11′ of the rear wall 11 and an inner surface 1′ of the turbine housing 1 confronting the extension 11′ so as to prevent the gas leakage and absorb thermal deformation (see Patent Literature 1).
In Patent Literature 1, as best shown in FIG. 2, formed on the outer periphery of the extension 11′ of the rear wall 11 is an annular groove 22 into which generally two sealing piston rings 21 are inserted with their closed gaps being not aligned or overlapped with each other, thereby providing a sealing device. The piston rings 21 are pressed at their outer peripheries against the inner surface 1′ of the turbine housing 1 by spring force of the piston rings themselves to prevent the gas leakage.
[Patent Literature 1] JP 2006-125588A

SUMMARY OF INVENTION

Technical Problems

In the conventional turbochargers, as shown in FIG. 2, some sealing device has been devised to prevent gas leakage from the gap 19; however, even with such devised sealing device, it is difficult and limitative to substantially improve turbine efficiency.
Thus, the inventors have made various researches and experiments on factors other than the gas leakage affecting the turbine efficiency to find out that the more the exhaust gas in the turbine impeller outlet 20 is turbulent, the more the turbine efficiency is lowered and that the less the exhaust gas in the turbine impeller outlet 20 is turbulent, the more the turbine efficiency is improved.
The invention was made in view of the above and has its object to provide a turbocharger which is simple in structure and which can reduce turbulence of fluid in a turbine impeller outlet to improve turbine efficiency.

Solution to Problems

The invention is directed to a turbocharger with a turbine housing having a scroll passage outwardly of an exhaust nozzle which in turn is arranged outwardly of a turbine impeller rotatably supported on a bearing housing, said exhaust nozzle having a plurality of nozzle vanes between front and rear exhaust introduction walls on sides of the bearing and turbine housings, respectively, a vane shaft for each of said nozzle vanes extending at least through the front wall and being rotatably supported, characterized in that it comprises pressing means arranged between the respective vane shafts and the bearing housing for urging the respective vane shafts toward the rear wall to displace the nozzle vanes toward the rear wall.
In the turbocharger, said pressing means may be a disc spring between the vane shafts and the bearing housing.
In the turbocharger, said pressing means may be a coiled spring between each of the vane shafts and the bearing housing.
In the turbocharger, each of said nozzle vanes may be supported in a cantilever manner by the vane shaft on one side of the vane extending through the front wall.
In the turbocharger, each of said nozzle vane may be dually supported by vane shafts on opposite sides of the vane extending through the front and rear walls, respectively.
In the turbocharger, each of said nozzle vane may be dually supported by vane shafts on opposite sides of the vane, one of the vane shafts extending through the front wall, the other of the vane shafts being embedded in the rear wall.

ADVANTAGEOUS EFFECTS OF INVENTION

According to a turbocharger of the invention which comprises pressing means between the bearing housing and the respective vane shafts of the nozzle vanes for urging the respective vane shafts toward the rear wall to displace the nozzle vanes toward the rear wall, a clearance between the nozzle vanes and the rear wall can be minimized by the simple structure, resulting in advantageous effect that turbulence of the fluid in the turbine impeller outlet can be reduced to substantially improve efficiency of the turbine.

BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 is a sectional side view showing a conventional turbocharger;

FIG. 2 is a sectional side view showing the nozzle and its vicinity in FIG. 1;

FIG. 3 is a sectional side view showing a nozzle and its vicinity according to an embodiment of the invention;

FIG. 4 is a side view showing the disc spring in FIG. 3;

FIG. 5 is a sectional side view showing a nozzle and its vicinity according to a further embodiment of the invention;

FIG. 6 is a sectional side view showing a further embodiment of the vane shafts which support the nozzle vane;

FIG. 7 is a sectional side view showing a still further embodiment of the vane shafts which support the nozzle vane;

FIG. 8 is a diagram for showing conditioning conventional and claimed turbochargers to have substantially same pressure ratios between upstream and downstream sides of turbine impeller;

FIG. 9 is a diagram showing velocity distribution of exhaust gas in radial positions in comparison of the conventional turbocharger with the claimed turbocharger; and

FIG. 10 is a diagram showing turbine efficiency in comparison of the conventional turbocharger with the claimed turbocharger.

REFERENCE SIGNS LIST

1 turbine housing
3 bearing housing
4 turbine impeller
5 compressor impeller
8 scroll passage
9 exhaust nozzle
10 front exhaust introduction wall
11 rear exhaust introduction wall
15 nozzle vane
16 vane shaft
20 turbine impeller outlet
23 pressing means
24 disc spring
27 coiled spring
28 vane shaft
28′ vane shaft

DESCRIPTION OF EMBODIMENTS

Embodiments of the invention will be described in conjunction with the attached drawings.
FIG. 3 shows an embodiment of the invention applied to the turbocharger shown in FIG. 2 with nozzle vanes 15 being arranged between front and rear exhaust introduction walls 10 and 11 of an exhaust nozzle 9 and each being supported in a cantilever manner by a vane shaft 16 arranged on a side of the vane 15 and extending through the front wall 10, comprising pressing means 23 arranged between a front end 16′ (right end in FIG. 3) of the vane shaft 16 of each of the nozzle vanes 15 and a rear surface 3′ of a bearing housing 3 (between a nozzle link plate 16 a referred to hereinafter and the rear surface 3′) to urge the respective vane shafts 16 toward the rear wall 11 to thereby keep the respective nozzle vanes 15 always in a displaced state toward the rear wall 11.
The pressing means 23 shown in FIG. 3 is in the form of a disc spring 24 which urges the respective vane shafts 16 toward the rear wall 11. As shown in FIG. 4, the disc spring 24 is frustconical and has inner and outer peripheral edges 25 and 26 mutually offset with respect to an axis of the spring to thereby provide a doughnut shape, an axial height H of the disc spring 24 with the frustconical shape being set to be greater than a distance between the respective front ends 16′ of the respective vane shafts 16 and the rear surface 3′ of the bearing housing 3.
The respective front ends 16′ of the vane shafts 16 extend through and are retained by inner ends of nozzle link plates 16 a (shaft support members) arranged between the front wall 10 and the rear surface 3′ of the bearing housing 3. The respective nozzle link plates 16 a are pivoted about the vane shafts 16 by rotating a drive ring (not shown); the respective vane shafts 16 (nozzle vanes 15) are rotated integrally with the respective nozzle link plates 16 a through the pivotal movements of the nozzle link plates 16 a. Since the disc spring 24 is arranged in a compressed state between the front ends 16′ of the respective vane shafts 16 and the rear surface 3′ of the bearing housing 3, the elastic force of the disc spring 24 causes the vane shafts 16 to be urged toward the rear wall 11, the nozzle vanes 15 being displaced toward the rear wall 11.
FIG. 5 shows a further embodiment of pressing means 23 which has a coiled spring 27 between respective front ends 16′ of vane shafts 16 and a rear surface 3′ of a bearing housing 3 so as to urge the respective vane shafts 16 toward a rear exhaust introduction wall 11.
FIG. 6 shows a case where vane shafts 16 and 28 on opposite sides of each of nozzle vanes 15 extend through front and rear exhaust introduction walls 10 and 11, respectively, so that the nozzle vanes 15 are dually supported by the vane shafts 16 and 28 on the walls 10 and 11; also in this case, pressing means 23 comprising a disc spring 24 or coiled springs 27 shown in FIG. 5 may be arranged between the front ends 16′ of the vane shafts 16 and a rear surface 3′ of a bearing housing 3 so as to urge the respective vane shafts 16 toward the rear wall 11.
FIG. 7 shows a case where vane shafts 16 and 28′ are provided on opposite sides of each of nozzle vanes 15, one 16 of the vane shafts extending through a front exhaust wall 10, the other vane shaft 28′ not extending through but being embedded in a rear exhaust introduction wall 11 so that the nozzle vanes 15 are dually supported by the vane shafts 16 and 28′; also in this case, pressing means 23 comprising a disc spring 24 or coiled springs 27 as shown in FIG. 5 may be arranged between front ends 16′ of the vane shafts 16 and a rear surface 3′ of a bearing housing 3 so as to urge the respective vane shafts 16 toward the rear wall 11.
Mode of operation of the embodiments shown in FIGS. 3-7 is as follows.
When the pressing means 23 comprising the disc spring 24 shown in FIGS. 3 and 4 or the coiled springs 27 shown in FIG. 5 is arranged between the front ends 16′ of the vane shafts 16 of the nozzle vanes 15 and the rear surface 3′ of the bearing housing 3, the respective vane shafts 16 are always urged by the pressing means 23 toward the rear wall 11, so that the respective nozzle vanes 15 are retained in their displaced positions toward the rear wall 11.
More specifically, there exist inherently clearances between the nozzle vanes 15 and the front and rear exhaust introduction walls 10 and 11 so as to make the nozzle vanes 15 pivotable and rotatable; and the clearances may be different between individual turbochargers. Then, as mentioned in the above, the respective vane shafts 16 are urged by the pressing means 23 toward the rear wall 11, so that the respective nozzle vanes 15 are displaced toward the rear wall 11 by the clearance. As a result, the respective nozzle vanes 15 contact the rear wall 11 with the clearance between the nozzle vanes 15 and the rear wall 11 being minimized.
In the embodiments shown in FIGS. 3, 6 and 7, the rear surface 3′ of the bearing housing 3 has a circumference in the form of frustoconical surface 3 a′ (forwardly and outwardly tapered surface). The disc spring 24 is arranged with its outer circumference being between the frustoconical surface 3 a′ and the nozzle link plates 16 a and extending along the frustoconical surface 3 a′. This makes it easy to ensure a space for the disc spring 24 without broadening the distance between the rear surface 3′ and the nozzle link plates 16 a.
On the conditioning that a conventional turbocharger (conventional one) and a turbocharger of the invention (claimed one) are made to have substantially same pressure ratios between upstream and downstream sides of turbine impeller 4 as shown in FIG. 8, the inventors determined velocity distribution of exhaust gas at radial positions in turbine impeller outlet 20 through numerical analysis. The results are shown in FIG. 9.
As is clear from FIG. 9, in comparison with the conventional one, the claimed one has radially flattened flow velocity distribution with less deviation. This means that the claimed one has less turbulence of exhaust gas in turbine impeller outlet 20 in comparison with the conventional one.
Moreover, turbine efficiency was compared between the claimed and conventional ones through numerical analysis. As a result, it was found out as shown in FIG. 10 that the claimed one has turbine efficiency improved by about 10% relative to the conventional one.
The exhaust gas in the scroll passage 8 passes through the nozzle vanes 15 of the exhaust nozzle 9 into the turbine impeller 4. Because of such exhaust gas flow being a complex three-dimensional stream, it is much difficult to find out factors in turbulence of the exhaust gas in the turbine impeller outlet 20.
However, as mentioned in the above, when the clearance between the respective nozzle vanes 15 and the rear wall 11 is minimized by urging the respective vane shafts 16 toward the rear wall 11, then the velocity distribution of the exhaust gas at radial positions in the turbine impeller outlet 20 becomes flattened to reduce the turbulence of the exhaust gas in the turbine impeller outlet 20, whereby the turbine efficiency can be improved. Thus, it was found out that the clearance between the respective nozzle vanes 15 and the rear wall 11 is one of factors affecting turbulence of the exhaust gas in the turbine impeller outlet 20.
Thus, according to the invention, by the above-mentioned simple structure that the pressing means 23 is arranged between the bearing housing 3 and the respective vane shafts 16 of the nozzle vanes 15, the nozzle vanes 15 are displaced toward the rear wall 11 to keep in the minimized state the clearance between the respective nozzle vanes 15 and the rear wall 11, whereby the turbulence of the fluid in the turbine impeller outlet 20 can be reduced to substantially improve the efficiency of the turbine.
It is to be understood that the invention is not limited to the above embodiments and that various changes and modifications may be made without departing form the scope of the invention. For example, though the sealing device in the form of the piston rings 21 for the gap 19 has been exemplified in the above embodiments, there is no restriction or limitation on construction of the sealing device.

INDUSTRIAL APPLICABILITY

A turbocharger according to the invention can be applied to displace nozzle vanes toward a rear exhaust introduction wall to minimize clearance between the respective nozzle vanes and the rear wall, thereby reducing turbulence of fluid in a turbine impeller outlet to improve efficiency of a turbine.

Claims

1. A turbocharger with a bearing housing having a scroll passage outwardly of an exhaust nozzle which in turn is arranged outwardly of a turbine impeller rotatably supported on the bearing housing, said exhaust nozzle having a plurality of nozzle vanes between front and rear exhaust introduction walls on sides of the bearing and turbine housings, respectively, a vane shaft for each of said nozzle vanes extending at least through the front wall and being rotatably supported, characterized in that it comprises pressing means arranged between the respective vane shafts and the bearing housing for urging the respective vane shafts toward the rear wall to displace the nozzle vanes toward the rear wall.

2. A turbocharger as claimed in claim 1, wherein said pressing means is a disc spring between the vane shafts and the bearing housing.

3. A turbocharger as claimed in claim 1, wherein said pressing means is a coiled spring between each of the vane shafts and the bearing housing.

4. A turbocharger as claimed in claim 1, wherein each of said nozzle vanes is supported in a cantilever manner by the vane shaft on one side of the vane extending through the front wall.

5. A turbocharger as claimed in claim 1, wherein each of said nozzle vanes is dually supported by vane shafts on opposite sides of the vane extending through the front and rear walls, respectively.

6. A turbocharger as claimed in claim 1, wherein each of said nozzle vanes is dually supported by vane shafts on opposite sides of the vane, one of the vane shafts extending through the front wall, the other vane shaft being embedded in the rear wall.

7. A turbocharger as claimed in claim 2, wherein each of said nozzle vanes is supported in a cantilever manner by the vane shaft on one side of the vane extending through the front wall.

8. A turbocharger as claimed in claim 3, wherein each of said nozzle vanes is supported in a cantilever manner by the vane shaft on one side of the vane extending through the front wall.

9. A turbocharger as claimed in claim 2, wherein each of said nozzle vanes is dually supported by vane shafts on opposite sides of the vane extending through the front and rear walls, respectively.

10. A turbocharger as claimed in claim 3, wherein each of said nozzle vanes is dually supported by vane shafts on opposite sides of the vane extending through the front and rear walls, respectively.

11. A turbocharger as claimed in claim 2, wherein each of said nozzle vanes is dually supported by vane shafts on opposite sides of the vane, one of the vane shafts extending through the front wall, the other vane shaft being embedded in the rear wall.

12. A turbocharger as claimed in claim 3, wherein each of said nozzle vanes is dually supported by vane shafts on opposite sides of the vane, one of the vane shafts extending through the front wall, the other vane shaft being embedded in the rear wall.