KR20140067817A - Gas seal assembly - Google Patents
Gas seal assembly Download PDFInfo
- Publication number
- KR20140067817A KR20140067817A KR1020120135554A KR20120135554A KR20140067817A KR 20140067817 A KR20140067817 A KR 20140067817A KR 1020120135554 A KR1020120135554 A KR 1020120135554A KR 20120135554 A KR20120135554 A KR 20120135554A KR 20140067817 A KR20140067817 A KR 20140067817A
- Authority
- KR
- South Korea
- Prior art keywords
- sleeve
- sealing
- force
- gas
- sealing sleeve
- Prior art date
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
- F16J15/38—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member sealed by a packing
Abstract
Description
The present invention relates to an assembly, and more particularly, to a gas seal assembly.
In general, gas-tight assemblies can be used to seal gas to internal components in a device that uses gas. In particular, the gas seal assembly can be used in a device that compresses and uses a gas such as a compressor. Such gas seal assemblies can be constructed by various components.
Particularly, such a gas chamber assembly is disclosed in US Patent No. 6,601,854 entitled Shaft seal (Applicant: DRESSER-RAND COMPANY). Hereinafter, a conventional gas chamber assembly will be described in detail with reference to FIG.
1 is a cross-sectional view showing a conventional
Referring to FIG. 1, a conventional
At this time, in the case of the gas chamber assembly formed as described above, the type of product is complicated and the driving method can be complicated. Particularly, the gas chamber assembly formed as described above can increase the processing cost and the number of assembly work due to an increase in the number of parts. Therefore, it is necessary to simplify the structure of the gas chamber assembly formed as described above.
Embodiments of the present invention seek to provide a gas chamber assembly that is simple in structure.
According to an aspect of the present invention, there is provided an internal combustion engine comprising: a rotating sealing sleeve inserted into and installed in an inner sleeve; a sealing sleeve installed to be in contact with the rotating sealing sleeve; and a pressing member urging the sealing sleeve toward the rotating sealing sleeve in contact with the sealing sleeve A seal housing having a sleeve, a seal sleeve spaced apart from the seal sleeve by a predetermined distance, one surface of the force sleeve being disposed below the bottom surface, and at least two And a resilient portion provided between the threaded housing and the force sleeve to provide a restoring force to the force sleeve.
The apparatus may further include a first sealing portion disposed at a portion where the inner sleeve and the rotating sealing sleeve contact each other and installed to be inserted into the inner sleeve.
The rotating sealing sleeve and the sealing sleeve may be in surface contact with each other.
The apparatus may further include a sealing member installed between the sealing sleeve and the force sleeve, the second sealing member contacting the sealing sleeve and the force sleeve.
In addition, at least one of the force sleeve and the thread housing may have an elastic part insertion groove into which a part of the elastic part is inserted.
The at least two third sealing portions may be provided between the force sleeve and the bottom surface of the threaded housing such that the third sealing portions are spaced from each other by a predetermined distance in the longitudinal direction of the inner sleeve.
The bottom surface of the seal housing having the at least two or more third sealing portions may be formed to be inclined in both directions about the at least two or more third sealing portions.
In addition, the inclination formed on the bottom surface of the seal housing may be formed to be higher in the longitudinal direction of the rotary shaft between the at least two or more third sealing portions.
In addition, the force sleeve may include a movable block provided with the elastic portion, spaced apart from the threaded housing by a predetermined distance, and a support block formed to be bent from the movable block to the bottom side of the threaded housing.
The embodiments of the present invention can effectively block the flow of the gas generated along the rotation axis of the rotation shaft with a simple structure. In addition, embodiments of the present invention can reduce the number of parts compared to conventional gas-seal assemblies, thereby simplifying the assembly process and reducing the fabrication cost and the number of assemblies.
In addition, embodiments of the present invention can simplify the structure by utilizing the leverage effect that the ringage mechanism necessary for effectively blocking the gas has to have.
1 is a cross-sectional view showing a conventional gas chamber assembly.
2 is a cross-sectional view illustrating a gas seal assembly according to an embodiment of the present invention.
3 is a sectional view showing the operation of the gas chamber assembly shown in Fig.
4 is an enlarged cross-sectional view showing part A of FIG.
BRIEF DESCRIPTION OF THE DRAWINGS The present invention will become more apparent from the following detailed description taken in conjunction with the accompanying drawings, in which: FIG. The present invention may, however, be embodied in many different forms and should not be construed as being limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. Is provided to fully convey the scope of the invention to those skilled in the art, and the invention is only defined by the scope of the claims. It is to be understood that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. In the present specification, the singular form includes plural forms unless otherwise specified in the specification. It is noted that the terms "comprises" and / or "comprising" used in the specification are intended to be inclusive in a manner similar to the components, steps, operations, and / Or additions. The terms first, second, etc. may be used to describe various elements, but the elements should not be limited by terms. Terms are used only for the purpose of distinguishing one component from another.
2 is a cross-sectional view showing a
The
Particularly, the
The
Meanwhile, the
The
Specifically, the
When the first sealing
Meanwhile, the first sealing
At this time, since the O-ring or U-shaped chamber corresponds to a general configuration, a detailed description will be omitted. Hereinafter, the case where the
The
The
Meanwhile, the
The
Further, the
In addition, the
The
The
The
Meanwhile, the second insertion groove 150a may be formed in the portion of the
The
The
Further, the
The
Hereinafter, for the sake of convenience of explanation, the case where at least two or more
The
The
Hereinafter, the
When the
The
At this time, the bottom surface of the threaded
The bottom surface of the
The
The
At least one of the
Particularly when the elastic
Hereinafter, the operation of the
3 is a sectional view showing the operation of the
3 and 4, the
Such a compressor must shut off the gas flowing into the rotary shaft S when rotating the rotary shaft S due to its life or the like. Therefore, the
Specifically, when the rotary shaft S rotates, an external gas may flow into the interior through an impeller (not shown). At this time, the gas introduced into the inside can flow in the longitudinal direction of the rotation axis S.
Particularly, in the case of the above-described flowing gas, it is possible to flow between the outer case C and the
The gas may also flow into the space between the
At this time, the gas flowing in the space between the
The gas flowing through the space between the
On the other hand, in the case of the above-mentioned flowing gas, the pressure can be increased toward the impeller side in the longitudinal direction of the rotating shaft S on which the impeller is installed. Further, the gas may be formed to have a smaller pressure as it moves away from the impeller side about the longitudinal direction of the rotary shaft (S).
Therefore, the flow of air may occur due to the pressure difference as described above. At this time, the flow of the air as described above can remove the lubricant supplied to the rotating shaft (S). Particularly, when the lubricant is removed as described above, wear of the rotation shaft S may occur due to rotation of the rotation shaft S, and thus the service life of the rotation shaft S may be shortened.
At this time, in order to prevent the above-described problems, the gas can be prevented from flowing through the first to
However, since the space between the
Specifically, the rotating sealing
At this time, the sealing
When the
When the restoring force is provided from the
The sealing
When the
The
At this time, the
On the contrary, when the
Therefore, when the
Meanwhile, when the supporting
Therefore, the
In addition, the
Although the present invention has been described in connection with the above-mentioned preferred embodiments, it is possible to make various modifications and variations without departing from the spirit and scope of the invention. Accordingly, it is intended that the appended claims cover all such modifications and variations as fall within the true spirit of the invention.
100: gas chamber assembly 140: sealing sleeve
110: inner sleeve 150: force sleeve
111: first body part 160: thread housing
112: first coupling portion 161: support projection
113: seat groove 170: second sealing portion
114: first insertion groove 180: third sealing portion
120: rotating sealing sleeve 190: positioning sleeve
130: first sealing portion 193: sixth sealing portion
131: first sealing member 195: elastic member
132: first elastic member
Claims (9)
A sealing sleeve installed to contact the rotating sealing sleeve;
A force sleeve contacting the sealing sleeve to apply the sealing sleeve to the rotating sealing sleeve side;
An actual housing disposed at a predetermined distance from the force sleeve and the sealing sleeve, the one side of the force sleeve being disposed below the bottom;
At least two third sealing portions provided between the force sleeve and the bottom surface of the seal housing; And
And an elastic portion provided between the threaded housing and the force sleeve to provide a restoring force to the force sleeve.
And a first sealing portion disposed at a portion where the inner sleeve and the rotating sealing sleeve contact each other and installed to be inserted into the inner sleeve.
Wherein the rotating sealing sleeve and the sealing sleeve are in surface contact with each other.
And a second sealing portion disposed between the sealing sleeve and the force sleeve, the second sealing portion contacting the sealing sleeve and the force sleeve.
At least one of the force sleeve and the thread housing,
And an elastic part insertion groove into which a part of the elastic part is inserted.
Wherein the at least two third sealing portions are disposed between the force sleeve and the bottom surface of the seal housing so as to be spaced apart from each other by a predetermined distance in the longitudinal direction of the inner sleeve.
Wherein a bottom surface of the seal housing having at least two or more third sealing portions is formed to be inclined in both directions about a center between the at least two or more third sealing portions.
Wherein a slope formed on a bottom surface of the seal housing is formed to be heightened in the longitudinal direction of the rotation shaft between the at least two or more third seal portions.
The force sleeve
A moving block provided with the elastic portion and spaced apart from the threaded housing at a predetermined interval; And
And a support block formed to be bent from the movable block to a bottom surface side of the seal housing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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KR1020120135554A KR20140067817A (en) | 2012-11-27 | 2012-11-27 | Gas seal assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020120135554A KR20140067817A (en) | 2012-11-27 | 2012-11-27 | Gas seal assembly |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
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KR1020160027137A Division KR101695255B1 (en) | 2016-03-07 | 2016-03-07 | Gas seal assembly |
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Publication Number | Publication Date |
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KR20140067817A true KR20140067817A (en) | 2014-06-05 |
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Application Number | Title | Priority Date | Filing Date |
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KR1020120135554A KR20140067817A (en) | 2012-11-27 | 2012-11-27 | Gas seal assembly |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112517557A (en) * | 2020-12-18 | 2021-03-19 | 河北华丰能源科技发展有限公司 | Online cleaning device for gas pipeline |
-
2012
- 2012-11-27 KR KR1020120135554A patent/KR20140067817A/en active Application Filing
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112517557A (en) * | 2020-12-18 | 2021-03-19 | 河北华丰能源科技发展有限公司 | Online cleaning device for gas pipeline |
CN112517557B (en) * | 2020-12-18 | 2022-03-18 | 河北华丰能源科技发展有限公司 | Online cleaning device for gas pipeline |
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