CN202391683U - High-pressure air cylinder chamber seal structure of reciprocating-type piston compressor - Google Patents

High-pressure air cylinder chamber seal structure of reciprocating-type piston compressor Download PDF

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Publication number
CN202391683U
CN202391683U CN2011204805660U CN201120480566U CN202391683U CN 202391683 U CN202391683 U CN 202391683U CN 2011204805660 U CN2011204805660 U CN 2011204805660U CN 201120480566 U CN201120480566 U CN 201120480566U CN 202391683 U CN202391683 U CN 202391683U
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CN
China
Prior art keywords
annular
reciprocating
circular groove
piston compressor
pressure air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn - After Issue
Application number
CN2011204805660U
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Chinese (zh)
Inventor
朱为宇
张国芬
黄顺良
邵健
徐伟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuxi Compressor Co Ltd
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Wuxi Compressor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuxi Compressor Co Ltd filed Critical Wuxi Compressor Co Ltd
Priority to CN2011204805660U priority Critical patent/CN202391683U/en
Application granted granted Critical
Publication of CN202391683U publication Critical patent/CN202391683U/en
Anticipated expiration legal-status Critical
Withdrawn - After Issue legal-status Critical Current

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Abstract

The utility model provides a high-pressure air cylinder chamber seal structure of a reciprocating-type piston compressor, which realizes the seal reliability, using safety and processing economy of the high-pressure air cylinder chamber. The high-pressure air cylinder chamber seal structure of the reciprocating-type piston compressor comprises a cylinder body and a high-pressure air cavity. The high-pressure air cylinder chamber seal structure of the reciprocating-type piston compressor is characterized in that an inner end surface and an outer end surface of a technology hole of the cylinder body are respectively provided with an inner end annular groove and an outer end annular groove; an outer annular surface of an outer convex circle of a drain plug with the outer convex circle is fit with an annular surface of the inner end annular groove; the annular surface of the inner end annular groove, which is close to the outer end annular grove, is provided with an annular oblique gasket; the outer convex circle of the drain plug is provided with an oblique surface which corresponds to the annular oblique gasket and has the same obliquity with the annular oblique gasket; an end cover covers the outer end annular groove of the cylinder body; the outer annular surface of the end cover clings to the annular surface of the outer end annular surface; a bolt penetrates through the end cover and is in threaded connected with the connecting part of the drain plug; and the outer annular surface of the connecting part of the drain plug clings to the inner annular surface of the technology hole.

Description

A kind of reciprocating-piston compressor high pressure cylinder cavity seal
Technical field
The utility model relates to the technical field of the sealing configuration of reciprocating-piston compressor, is specially a kind of reciprocating-piston compressor high pressure cylinder cavity seal.
Background technique
Reciprocating-piston compressor is a kind of every profession and trade that is widely used in, through changing the universal machine that the gas in the jar volume realizes that gas pressure increases.In some mesohigh petrochemical equipment technological process and special circumstances, require gas pressure high especially, require usually to reach more than the 10MPa, generally use the forging cylinder could satisfy usage requirement.Usually the forging cylinder can be divided into induction part, cylinder chamber part and discharge portion, and induction part has three chambers that link to each other respectively with discharge portion.They are respectively that two air valve chambeies and one advance (row) air cavity.For two air valve chambeies and the exhaust port that is communicated with the forging cylinder, can only begin from the cylinder body outside to form the gas in the jar passage, thereby produce a processing technology hole at the cylinder body end face through machining.In actual production, all can take suitable sealing configuration to seal.Particularly some explosive occasions especially will be noted the structural design here, do not allow the potential safety hazard that exists seal failure, explosion hazard gases to leak.
Existing sealing configuration mainly contains following dual mode:
Mode one is as shown in Figure 1: through between plug 1 and the cylinder body 2 be threaded and the outside weldings weld seam realize the sealing.These structure existing problems:
1. because employing is threaded, and processing only relies on tapping to solve, precision is difficult for guaranteeing.
2. owing to adopt welded structure to dismantle.
3. the weld seam melting zone is little, is prone to produce weld cracking or welding stress, and weld seam only depends on surface seepage to detect can't guarantee fully that its defective can come to light fully.
4. right-hand member air flue hole is a high-pressure section, and left end is the normal pressure part, though this kind sealing means structure is simple, uncertain factor is many.Rely on screw thread pretightening force and welding to be had potential safety hazard by motive sealing.
Mode two is as shown in Figure 2: it is through applying bigger pretightening force to the bolt 3 that is uniformly distributed with, and with flange 4 being pressed on the cylinder body 2 ' tightly, realizes sealing through the annular taper liner between flange 4 and the cylinder body 2 ' 5.These structure existing problems:
1. owing to adopt the blank flange structure, physical dimension is bigger, and the bolt arrangement difficulty causes the cylinder profile to increase, and is less economical.
2. right-hand member air flue hole is a high-pressure section, and left end is the normal pressure part, relies on the pretightening force of bolt to seal, and for by movable sealing structure, has big potential safety hazard.
Summary of the invention
To the problems referred to above, the utility model provides a kind of reciprocating-piston compressor high pressure cylinder cavity seal, and it realizes the reliability of high pressure cylinder cavity seal, the Security and the Economics of Processing of use.
A kind of reciprocating-piston compressor high pressure cylinder cavity seal; Its technological scheme is such: it comprises cylinder body, heavy pressure gas chamber; It is characterized in that: the auxiliary hole interior edge face of said cylinder body, exterior edge face are respectively arranged with inner circular groove, outer end circular groove; The outer ring surface of outer dome that has the plug of the outer dome anchor ring of said inner circular groove of fitting, said inner circular groove is provided with annular taper liner near the anchor ring of outer end circular groove, and the corresponding said annular taper liner of the outer dome of said plug is provided with the inclined-plane of same slope; The end cap lid is loaded on the outer end circular groove of said cylinder body; The outer ring surface of said end cap is close to the anchor ring of said outer end circular groove, and the said end cap rear thread of bolt-through connects the attachment portion of said plug, and the outer ring surface of the attachment portion of said plug is close to the inner ring surface of said auxiliary hole.
It is further characterized in that: be provided with O type circle between the outer ring surface of the attachment portion of said plug and the inner ring surface of said auxiliary hole;
Said annular taper liner is specially the annular taper liner of alloy aluminum.
After adopting the said structure of the utility model; High-pressure gas pressure in the heavy pressure gas chamber is pressed in the outer dome of plug in the inner circular groove of cylinder; The annular taper liner fits tightly the inner circular groove of plug, cylinder respectively, accomplishes sealing, and whole sealing configuration is the active sealing configuration: do not rely on the external world and apply pretightening force; The simple structure that relies on self pressure to reach self-locking and realize sealing; It realizes the reliability of high pressure cylinder cavity seal, the Security of use, and total only has higher requirements to the precision of annular taper liner with the inclined-plane of the corresponding said annular taper liner of plug, and other finished surface required precisions are lower; Reduced the processing technology requirement, its Economics of Processing is good.
Description of drawings
Fig. 1 is the structural representation of the sealing means one of existing sealing configuration;
Fig. 2 is the structural representation of the sealing means two of existing sealing configuration;
Fig. 3 is the structural representation of the utility model.
Embodiment
See Fig. 3; It comprises cylinder body 2, heavy pressure gas chamber 6; Auxiliary hole 7 interior edge faces of cylinder body 2, exterior edge face are respectively arranged with inner circular groove 8, outer end circular groove 9; The outer ring surface of outer dome 10 that has the plug 1 of the outer dome anchor ring of inner circular groove 8 of fitting, inner circular groove 8 is provided with annular taper liner 5 near the position of outer end circular groove 9, and the outer dome 10 corresponding annular taper liners 5 of plug 1 are provided with the inclined-plane 11 of same slope; End cap 4 lids are loaded on the outer end circular groove 9 of cylinder body 2; The outer ring surface of end cap 4 is close to the anchor ring of outer end circular groove 9, and bolt 3 runs through the attachment portion 12 that end cap 4 rear threads connect plug 1, and the outer ring surface of the attachment portion 12 of plug 1 is close to the inner ring surface of auxiliary hole 7.Be provided with O type circle 13 between the outer ring surface of the attachment portion 12 of plug 1 and the inner ring surface of auxiliary hole 7; Annular taper liner 5 is specially the annular taper liner of alloy aluminum.

Claims (3)

1. reciprocating-piston compressor high pressure cylinder cavity seal; It comprises cylinder body, heavy pressure gas chamber; It is characterized in that: the auxiliary hole interior edge face of said cylinder body, exterior edge face are respectively arranged with inner circular groove, outer end circular groove; The outer ring surface of outer dome that has the plug of the outer dome anchor ring of said inner circular groove of fitting, said inner circular groove is provided with annular taper liner near the anchor ring of outer end circular groove, and the corresponding said annular taper liner of the outer dome of said plug is provided with the inclined-plane of same slope; The end cap lid is loaded on the outer end circular groove of said cylinder body; The outer ring surface of said end cap is close to the anchor ring of said outer end circular groove, and the said end cap rear thread of bolt-through connects the attachment portion of said plug, and the outer ring surface of the attachment portion of said plug is close to the inner ring surface of said auxiliary hole.
2. a kind of reciprocating-piston compressor high pressure cylinder cavity seal according to claim 1 is characterized in that: be provided with O type circle between the outer ring surface of the attachment portion of said plug and the inner ring surface of said auxiliary hole.
3. a kind of reciprocating-piston compressor high pressure cylinder cavity seal according to claim 1 and 2, it is characterized in that: said annular taper liner is specially the annular taper liner of alloy aluminum.
CN2011204805660U 2011-11-28 2011-11-28 High-pressure air cylinder chamber seal structure of reciprocating-type piston compressor Withdrawn - After Issue CN202391683U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011204805660U CN202391683U (en) 2011-11-28 2011-11-28 High-pressure air cylinder chamber seal structure of reciprocating-type piston compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011204805660U CN202391683U (en) 2011-11-28 2011-11-28 High-pressure air cylinder chamber seal structure of reciprocating-type piston compressor

Publications (1)

Publication Number Publication Date
CN202391683U true CN202391683U (en) 2012-08-22

Family

ID=46666613

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011204805660U Withdrawn - After Issue CN202391683U (en) 2011-11-28 2011-11-28 High-pressure air cylinder chamber seal structure of reciprocating-type piston compressor

Country Status (1)

Country Link
CN (1) CN202391683U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102384071A (en) * 2011-11-28 2012-03-21 无锡压缩机股份有限公司 High-pressure air cylinder chamber seal structure of reciprocating type piston compressor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102384071A (en) * 2011-11-28 2012-03-21 无锡压缩机股份有限公司 High-pressure air cylinder chamber seal structure of reciprocating type piston compressor
CN102384071B (en) * 2011-11-28 2014-12-10 无锡压缩机股份有限公司 High-pressure air cylinder chamber seal structure of reciprocating type piston compressor

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C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20120822

Effective date of abandoning: 20141210

RGAV Abandon patent right to avoid regrant