CN201568568U - Sealing structure at pressure end of turbocharger - Google Patents
Sealing structure at pressure end of turbocharger Download PDFInfo
- Publication number
- CN201568568U CN201568568U CN2009202597083U CN200920259708U CN201568568U CN 201568568 U CN201568568 U CN 201568568U CN 2009202597083 U CN2009202597083 U CN 2009202597083U CN 200920259708 U CN200920259708 U CN 200920259708U CN 201568568 U CN201568568 U CN 201568568U
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- China
- Prior art keywords
- seal ring
- sealing
- pressure side
- boss
- impeller
- Prior art date
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- Expired - Fee Related
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Abstract
Disclosed is a sealing structure at a pressure end of a turbocharger, which comprises a gland (1), an impeller (2) and oil seal cover (3). The gland (1) is provided with a sealing circular groove in which a sealing ring (11) is arranged. A boss (21) is arranged on a hub of the impeller (2). The boss (21) is provided with the sealing circular groove in which a sealing ring (22) is arranged. The oil seal cover (3) is sleeved around the sealing ring (11) and the sealing ring (22). An oil slinger (31) is arranged on the position between the sealing ring (11) and the sealing ring (22) on the oil seal cover (3). The utility model has the advantages of compact structure, double independent sealing and good sealing effect.
Description
Technical field
The utility model relates to turbosupercharger pressure side structure, particularly a kind of turbosupercharger pressure side sealing configuration.
Background technique
At present, the sealing means of turbosupercharger pressure side generally is to adopt the piston type sealing, arranges seal ring in the pressure side of turbosupercharger, and the main effect of seal ring is that the gas of sealing in gas compressor and the turbine case leaks to the intermediate oil pocket.This seal ring have only just play a part under special circumstances the sealing machine oil, because the turbosupercharger wheel back of the body at its two ends (pressing the back of the body and the whirlpool back of the body) in normal operation locates that certain gas pressure is all arranged, machine oil is can not flow to the high pressure district from low pressure zone, but in real work, because sometimes the turbosupercharger air-intake negative-pressure is too big or dead time is long, is prone in the bearing support lubricant oil and breaks through the fault of seal ring to the pressure side seepage.As shown in Figure 3-4, in order to strengthen the sealability of pressure side, the turbosupercharger that has at present adopts adorns double seal ring (41,42) structure on the pressure side stuffing box gland, but because stuffing box gland position compactness, double seal ring (41,42) is difficult to arranged apart, cause double seal ring in fact only to play the effect of a seal ring, make sealing effect not good.
Summary of the invention
The purpose of this utility model is to overcome the above-mentioned deficiency of prior art and a kind of turbosupercharger pressure side sealing configuration is provided, and its compact structure can form double independently sealing.
The technical solution of the utility model is: a kind of turbosupercharger pressure side sealing configuration, it comprises stuffing box gland, impeller and oil sealing cap, stuffing box gland is provided with closure gasket groove, in its closure gasket groove seal ring is installed, the wheel hub of impeller is provided with boss, boss is provided with closure gasket groove, in its closure gasket groove seal ring is installed.
The further technological scheme of the utility model is: described oil sealing cap is ridden and is enclosed within seal ring and seal ring periphery.
The utility model further technological scheme is: the position on the described oil sealing cap between seal ring and seal ring also is provided with gets rid of oilhole.
The also further technological scheme of the utility model is: the boss on the wheel hub of described impeller is provided with ring-shaped step corresponding to the position of getting rid of oilhole.
The utility model compared with prior art has following characteristics:
1, the seal ring on the wheel hub of seal ring on the utility model stuffing box gland and impeller is arranged apart, forms double independently sealing, its good sealing effect;
2, get rid of oilhole on the oil sealing cap, can avoid the pressure side leakage of oil to produce, reach better sealing effect.
Below in conjunction with the drawings and specific embodiments detailed structure of the present utility model is further described.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is the enlarged view of Fig. 1 along the A line;
Fig. 3 is the schematic representation of existing turbosupercharger pressure side sealing configuration;
Fig. 4 is the enlarged view of Fig. 3 along the B line.
Embodiment
Embodiment
As shown in the figure: a kind of turbosupercharger pressure side sealing configuration, it comprises stuffing box gland 1, impeller 2 and oil sealing cap 3, stuffing box gland 1 is provided with closure gasket groove, seal ring 11 is installed in its closure gasket groove, the wheel hub of impeller 2 is provided with boss 21, boss 21 is provided with closure gasket groove, seal ring 22 is installed in its closure gasket groove, oil sealing cap 3 is ridden and is enclosed within seal ring 11 and seal ring 22 peripheries, position on the oil sealing cap 3 between seal ring 11 and seal ring 22 also is provided with gets rid of oilhole 31, and boss 21 is provided with ring-shaped step 211 corresponding to the position of getting rid of oilhole 31.
The utility model is not limited to above-mentioned concrete structure, so long as just drop within the protection domain of the present utility model at the turbosupercharger pressure side sealing configuration that is provided with seal ring 22 on the wheel hub of impeller 2.
Claims (5)
1. turbosupercharger pressure side sealing configuration, it comprises stuffing box gland (1), impeller (2) and oil sealing cap (3), stuffing box gland (1) is provided with closure gasket groove, seal ring (11) is installed in its closure gasket groove, it is characterized in that: the wheel hub of impeller (2) is provided with boss (21), boss (21) is provided with closure gasket groove, and seal ring (22) is installed in its closure gasket groove.
2. turbosupercharger pressure side sealing configuration according to claim 1 is characterized in that: described oil sealing cap (3) is ridden and is enclosed within seal ring (11) and seal ring (22) periphery.
3. turbosupercharger pressure side sealing configuration according to claim 1 and 2 is characterized in that: be positioned at position between seal ring (11) and the seal ring (22) on the described oil sealing cap (3) and also be provided with and get rid of oilhole (31).
4. turbosupercharger pressure side sealing configuration according to claim 1 and 2 is characterized in that: the boss (21) on the wheel hub of described impeller (2) is provided with ring-shaped step (211) corresponding to the position of getting rid of oilhole (31).
5. turbosupercharger pressure side sealing configuration according to claim 3 is characterized in that: the boss (21) on the wheel hub of described impeller (2) is provided with ring-shaped step (211) corresponding to the position of getting rid of oilhole (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202597083U CN201568568U (en) | 2009-12-10 | 2009-12-10 | Sealing structure at pressure end of turbocharger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202597083U CN201568568U (en) | 2009-12-10 | 2009-12-10 | Sealing structure at pressure end of turbocharger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201568568U true CN201568568U (en) | 2010-09-01 |
Family
ID=42660854
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009202597083U Expired - Fee Related CN201568568U (en) | 2009-12-10 | 2009-12-10 | Sealing structure at pressure end of turbocharger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201568568U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101975185A (en) * | 2010-10-21 | 2011-02-16 | 湖南天雁机械有限责任公司 | Compressor seal structure of small turbocharger |
| CN103375427A (en) * | 2012-04-16 | 2013-10-30 | 三星泰科威株式会社 | Oil seal of compressor |
| US9874217B2 (en) | 2012-01-13 | 2018-01-23 | Cummins Ltd. | Turbomachine shaft sealing arrangement |
-
2009
- 2009-12-10 CN CN2009202597083U patent/CN201568568U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101975185A (en) * | 2010-10-21 | 2011-02-16 | 湖南天雁机械有限责任公司 | Compressor seal structure of small turbocharger |
| US9874217B2 (en) | 2012-01-13 | 2018-01-23 | Cummins Ltd. | Turbomachine shaft sealing arrangement |
| CN103375427A (en) * | 2012-04-16 | 2013-10-30 | 三星泰科威株式会社 | Oil seal of compressor |
| CN112253534A (en) * | 2012-04-16 | 2021-01-22 | 韩华压缩机株式会社 | Oil seal for compressor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100901 Termination date: 20121210 |