Sealing-coupled apparatus of turbocharger

Abstract

A sealing-coupled apparatus of a turbocharger may include a vane cover installed in front of a turbine vane set in a turbine housing, the vane cover configured to cover the turbine vane and to define a fluid passage through which a fluid may be fed to an outlet hole extending in the turbine housing, and a sealing member having a tubular shape with a predetermined thickness, the sealing member being engaged with a front end of the vane cover and having an annular groove formed around an outer circumferential surface of the sealing member, with a sealing ring fitted over the groove and spacing the vane cover apart from the turbine housing in a radial direction.

Claims

1. A sealing-coupled apparatus of a turbocharger, the apparatus comprising: a vane cover installed in front of a turbine vane set in a turbine housing, the vane cover configured to cover the turbine vane and to define a fluid passage through which a fluid is fed to an outlet hole extending in the turbine housing; and a sealing member having a tubular shape with a predetermined thickness, the sealing member being engaged with a front end of the vane cover and having an annular groove formed around an outer circumferential surface of the sealing member, with a sealing ring fitted over the groove and spacing the vane cover apart from the turbine housing in a radial direction, wherein the sealing member is provided with a step formed around an outer circumferential surface of an end of the sealing member at which the sealing member is combined with the vane cover, such that a thickness of the end of the sealing member is reduced by the step, the sealing member being combined with the vane cover, with a gasket set in the step.

2. The sealing-coupled apparatus of the turbocharger of claim 1, wherein the turbine housing is provided with a protruding ring formed by protruding inwardly to a predetermined height in a radial direction along an inner circumferential surface of the outlet hole at a location spaced apart from the sealing member by a predetermined distance, and wherein the protruding ring is configured to be a stopper preventing the sealing member from being removed into the outlet hole.

3. A sealing-coupled apparatus of a turbocharger, the apparatus comprising: a vane cover installed in front of a turbine vane set in a turbine housing, the vane cover configured to cover the turbine vane and to define a fluid passage through which a fluid is fed to an outlet hole extending in the turbine housing; and a sealing member having a tubular shape with a predetermined thickness, the sealing member being engaged with a front end of the vane cover and having an annular groove formed around an outer circumferential surface of the sealing member, with a sealing ring fitted over the groove and spacing the vane cover apart from the turbine housing in a radial direction, wherein the sealing member is provided with screw threads and the vane cover is provided with thread grooves, so that the vane cover and the sealing member are combined with each other in a screw engagement.

4. The sealing-coupled apparatus of the turbocharger of claim 3, wherein the turbine housing is provided with a protruding ring formed by protruding inwardly to a predetermined height in a radial direction along an inner circumferential surface of the outlet hole at a location spaced apart from the sealing member by a predetermined distance, and wherein the protruding ring is configured to be a stopper preventing the sealing member from being removed into the outlet hole.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a sectional view illustrating a sealing-coupled apparatus of a turbocharger according to an exemplary embodiment of the present invention.

(2) FIG. 2 is a sectional view illustrating a protruding ring formed in a turbine housing of FIG. 1.

(3) FIG. 3 is a sectional view illustrating a screw engagement of a sealing member with a vane cover.

(4) FIG. 4 is a sectional view illustrating a gasket set in a step of the sealing member.

(5) It should be understood that the appended drawings are not necessarily to scale, presenting a somewhat simplified representation of various features illustrative of the basic principles of the invention. The specific design features of the present invention as disclosed herein, including, for example, specific dimensions, orientations, locations, and shapes will be determined in part by the particular intended application and use environment.

(6) In the figures, reference numbers refer to the same or equivalent parts of the present invention throughout the several figures of the drawing.

DETAILED DESCRIPTION

(7) Reference will now be made in detail to various embodiments of the present invention(s), examples of which are illustrated in the accompanying drawings and described below. While the invention(s) will be described in conjunction with exemplary embodiments, it will be understood that the present description is not intended to limit the invention(s) to those exemplary embodiments. On the contrary, the invention(s) is/are intended to cover not only the exemplary embodiments, but also various alternatives, modifications, equivalents and other embodiments, which may be included within the spirit and scope of the invention as defined by the appended claims.

(8) Hereinbelow, a sealing-coupled apparatus of a turbocharger according to exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings.

(9) FIG. 1 is a view illustrating a sealing-coupled apparatus of a turbocharger according to an exemplary embodiment of the present invention. As shown in FIG. 1, the sealing-coupled apparatus of the turbocharger according to the exemplary embodiment of the present invention includes: a vane cover 500 installed in front of a turbine vane 300 set in a turbine housing 100, the vane cover 500 functioning to cover the vane 300 and to define a fluid passage through which a fluid is fed to an outlet hole 110 extending in the housing 100, and a sealing member 700 having a tubular shape with a predetermined thickness, the sealing member 700 being engaged with a front end of the cover 500 and having an annular groove 710 formed around an outer circumferential surface of the sealing member 700, with a sealing ring 730 fitted over the groove 710 and spacing the cover 500 apart from the housing 100 in a radial direction.

(10) The turbine vane 300 is provided on an end of a vane shaft 310 and is set in the housing 100 by both the vane shaft 310 and a vane base ring 200. In operation, a fluid is introduced into the housing 100 via an inlet hole 130 of the housing 100 and is compressed by the vane 300, and is discharged to the outside of the housing 100 via the outlet hole 110. The vane cover 500 is set in front of the vane 300 and defines the fluid passage through which the fluid is fed to the outlet hole 110 extending in the housing 100. Here, the vane cover 500 has a shape suitable to efficiently cover the vane 300, so the shape of the cover 500 corresponds to the shape of the vane 300. The cover 500 has a flat disc shape at a part surrounding the blades of the vane 300 and has a tubular shape at a central part thereof such that the tubular part of the cover 500 forms the fluid passage extending to the outlet hole 130.

(11) The sealing member 700 having a tubular shape with a predetermined thickness is engaged with the front end of the cover 500. The outer circumferential surface of the sealing member 700 is grooved in a circumferential direction, so the annular groove 710 is formed around the outer circumferential surface of the sealing member 700. The sealing ring 730 having a shape corresponding to the shape of the groove 710 is fitted over the groove 710, and seals the junction between the housing 100 and the sealing member 700, thereby preventing a fluid (for example, exhaust gas) from leaking into the outlet hole 110 via the junction. Further, the sealing ring 730 fitted over the groove 710 spaces the cover 500 apart from the housing 100 at a predetermined interval in a radial direction. In an exemplary embodiment of the present invention, the sealing member 700 is installed in the turbine housing 100 in such a way that, although thermal deformation of the housing 100 during operation under high temperature conditions may be transferred to the sealing member 700, the cover 500 is efficiently isolated from the thermal deformation of the housing 100. Accordingly, the present invention can prevent damage or breakage of both the vane 300 and the cover 500, which may be caused by a thermal deformation of the housing 100 during operation under high temperature conditions, so the present invention can increase the durability and operational reliability of the turbocharger.

(12) Further, in the housing 100, at a location spaced apart from the sealing member 700 by a predetermined distance, a protruding ring 131 is formed by protruding inwardly to a predetermined height in a radial direction along the inner circumferential surface of the outlet hole 110, as shown in FIG. 2. The protruding ring 131 functions as a stopper preventing the sealing member 700 from being removed into the outlet hole 110 during operation. Accordingly, even when the turbocharger is repeatedly operated under high temperature conditions and operational vibrations and shock occur in the turbocharger, the protruding ring 131 can efficiently prevent the sealing member 700 from being removed into the outlet hole 110. Thus, in an exemplary embodiment of the present invention, heat from the housing 100 is transferred only to the sealing member 700, so the present invention can increase the durability of parts of the turbocharger.

(13) As shown in FIG. 1, respective steps 750 may be formed on the cover 500 and the sealing member 700 at corresponding locations, so that the cover 500 and the sealing member 700 may be combined with each other by a sliding engagement. Alternatively, as shown in FIG. 3, screw threads 770 may be formed around the outer circumferential surface of the step of the sealing member 700, and thread grooves 510 may be formed around the inner circumferential surface of the step of the cover 500, so that the cover 500 and the sealing member 700 may be combined with each other in a screw engagement. Here, screw threads may be formed on the cover 500 and thread grooves may be formed on the sealing member 700.

(14) As a further alternative, a step 750 may be formed around the outer circumferential surface of the end of the sealing member 700 at which the sealing member 700 is combined with the cover 500, as shown in FIG. 4. Due to the step 750, the thickness of the end of the sealing member 700 is reduced. In this case, the sealing member 700 may be combined with the cover 500, with a gasket 900 having a U-shaped, V-shaped or C-shaped cross-section set in the step 750. Here, the method of combining the sealing member 700 with the cover 500 may be freely changed according to operational conditions and designing requirements of the turbocharger.

(15) The above-mentioned sealing-coupled apparatus of the turbocharger according to an exemplary embodiment of the present invention is advantageous in that, unlike a conventional technique in which an insert functioning as a vane cover is installed and a sealing structure is provided on the outlet of the insert, the sealing-coupled apparatus of this invention is formed by combining a vane cover having no sealing structure with a sealing member produced separately from the cover. Thus, the sealing-coupled apparatus of this invention can efficiently prevent leakage of a fluid and can avoid direct transfer of the thermal deformation of a turbine housing exposed to high temperature conditions during operation to the vane cover, thereby preventing damage or breakage of a turbine vane due to the thermal deformation of the housing during operation under high temperature conditions, and increasing the durability and operational reliability of the turbocharger.

(16) For convenience in explanation and accurate definition in the appended claims, the terms “upper”, “lower”, “inner” and “outer” are used to describe features of the exemplary embodiments with reference to the positions of such features as displayed in the figures.

(17) The foregoing descriptions of specific exemplary embodiments of the present invention have been presented for purposes of illustration and description. They are not intended to be exhaustive or to limit the invention to the precise forms disclosed, and obviously many modifications and variations are possible in light of the above teachings. The exemplary embodiments were chosen and described in order to explain certain principles of the invention and their practical application, to thereby enable others skilled in the art to make and utilize various exemplary embodiments of the present invention, as well as various alternatives and modifications thereof. It is intended that the scope of the invention be defined by the Claims appended hereto and their equivalents.