CN104747736B - A kind of synchronous mode is dismounted from seal structure - Google Patents
A kind of synchronous mode is dismounted from seal structure Download PDFInfo
- Publication number
- CN104747736B CN104747736B CN201510031666.8A CN201510031666A CN104747736B CN 104747736 B CN104747736 B CN 104747736B CN 201510031666 A CN201510031666 A CN 201510031666A CN 104747736 B CN104747736 B CN 104747736B
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- CN
- China
- Prior art keywords
- housing
- chipware
- sealing
- sealing drum
- sealing ring
- 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.)
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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
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
-
- 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
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
- F16K1/32—Details
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Details Of Reciprocating Pumps (AREA)
Abstract
The invention belongs to field of fluid machinery, it is related to a kind of synchronous mode dismounting from seal structure.Structure of the present invention includes housing (1), sealing ring (2), fixing screws (3), sealing drum (4), chipware (5), sealing ring (6), sealing ring (7), valve body (8), screw (9), sealing ring (10), spring (11), valve core (12), push rod (13), moulding (14), locating rod (15), gag lever post (16), limit spring (17), fluid intake (18), fluid issuing (19), step auricle (20) and aperture (21) etc..Wherein, chipware (5) can be the fluid machinery that pump or valve etc. have inner flow passage.
Description
Technical field
A kind of synchronous mode dismounting belongs to field of fluid machinery from seal structure, is related to a kind of design dismounted from seal structure.
Background technology
Dismounting from seal structure in field of fluid machinery, especially Aviation Fuel system it is in an increasingly wide range of applications.
There is lot of advantages from the product of seal structure using dismounting, product maintenance can be significantly improved, reliability is improved.
Dismounting is varied from seal structure, in Aviation Fuel system, have using it is synchronous open or self-styled fluid intake and
Demand of the dismounting of fluid issuing from seal structure.
The content of the invention
The purpose of the present invention:A kind of synchronous mode dismounting is provided from seal structure, reduction dismounting improves reliable from seal structure flow resistance
Property, it is provided simultaneously with error-disable function.
Technical scheme:Scheme such as Fig. 1.Housing 1 is sealed in fluid system configuration by sealing ring 2;Screw 3 will
Sealing drum 4 and chipware 5 are fixed on housing 1;Sealing ring 6 seals sealing drum 4 and body clearance;Sealing ring 7 is by chipware and close
Sealed tube clearance seal;Valve body 8 is arranged on housing 1 by screw 9, and sealing therebetween is ensured by sealing ring 10;Spring 11
The top that valve core 12 inside valve body 8 is compressed and makes the push rod 13 on valve core 12 contact chipware 5, moulding
14 ensure sealing therebetween when valve core 12 contacts housing 1;Locating rod 15, which is arranged on sealing drum 4, to be used to be oriented to;Gag lever post
16 and limit spring 17 be arranged on housing 1 on.Push rod 13 designs suitably sized, loads the assembly of sealing drum 4 and chipware 5
Or when extracting housing 1, fluid intake 18 and fluid issuing 19 are synchronously opened or closed.The overhanging step auricle 20 of gag lever post 16 blocks
On sealing drum 4 and chipware 5, do not deviate from the aperture 21 time limit coremaking part 5 on housing 1 in locating rod 15, prevent it close from deviating from
Sealed tube 4;Locating rod 15 rotates to an angle when deviating from the aperture 21 on housing 1 and chipware 5 can be deviate from into sealing drum 4;Step
The limitation sealing drum 4 of auricle 20 can not deviate from housing 1 all the time.
Beneficial effects of the present invention:The present invention can be extensively using fluid-mechanic system, especially aircraft fuel system.This hair
It is bright easy to implement, it is possible to decrease dismounting improves reliability from seal structure flow resistance, being capable of systematically mistake proofing.
Brief description of the drawings:
Fig. 1 is that vortex weakens structure and method schematic diagram in a kind of pump spiral case;
1- housings, 2- sealing rings, 3- screws, 4- sealing drums, 5- chipwares, 6- sealing rings, 7- sealing rings, 8- valve bodies,
9- screws, 10- sealing rings, 11- springs, 12- valve cores, 13- push rods, 14 moulding, 15- positioning, 16- gag lever posts, the spacing bullets of 17-
Spring, 18- fluid intakes, 19- fluid issuings, 20- step auricles, 21- apertures.
Embodiment
Scheme such as Fig. 1.Housing 1 is sealed in fluid system configuration by sealing ring 2;Screw 3 consolidates sealing drum 4 and chipware 5
Determine onto housing 1;Sealing ring 6 seals sealing drum 4 and body clearance;Sealing ring 7 is by chipware and sealing drum clearance seal;Valve
Housing 8 is arranged on housing 1 by screw 9, and sealing therebetween is ensured by sealing ring 10;Spring 11 will be arranged on valve body 8
The top that internal valve core 12 compresses and makes the push rod 13 on valve core 12 contact chipware 5, moulding 14 is contacted in valve core 12
Ensure sealing therebetween during housing 1;Locating rod 15, which is arranged on sealing drum 4, to be used to be oriented to;Gag lever post 16 and limit spring 17 are pacified
On housing 1.Push rod 14 designs suitably sized, when making the assembly loading of sealing drum 4 and chipware 5 or extracting housing 1, stream
Body entrance 18 and fluid issuing 19 are synchronously opened or closed.The overhanging step auricle 20 of gag lever post 16 is stuck in sealing drum 4 and chipware 5
On, do not deviate from the aperture 21 time limit coremaking part 5 on housing 1 in locating rod 15, prevent it from deviating from sealing drum 4;Locating rod 15 takes off
Sealing drum 4 can be deviate from by chipware 5 by being rotated to an angle when going out the aperture 21 on housing 1;Step auricle 20 limits sealing drum 4
All the time housing 1 can not be deviate from.
Claims (4)
1. a kind of synchronous mode is dismounted from seal structure, it is characterised in that housing (1) is sealed to mounting structure by the first sealing ring (2)
On;Sealing drum (4) and chipware (5) are fixed on housing (1) by screw (3);Second sealing ring (6) is by sealing drum (4) and housing
Clearance seal;3rd sealing ring (7) is by chipware and sealing drum clearance seal;Valve body (8) is arranged on housing by screw (9)
(1) on, the sealing between valve body (8) and housing (1) is ensured by the 4th sealing ring (10);Spring (11) will be arranged on valve
The internal valve core (12) of housing (8) is compressed, and the push rod (13) on valve core (12) is contacted the tops of chipware (5);Moulding
(14) it is arranged on valve core (12), when valve core (12) contacts housing (1), the moulding (14) ensures valve core (12) and shell
Sealing between body (1);Locating rod (15) is arranged on sealing drum (4), for being oriented to;Gag lever post (16) and limit spring (17)
On housing (1).
2. synchronous mode dismounting according to claim 1 is from seal structure, wherein, push rod (13) makes close with suitably sized
When the assembly of sealed tube (4) and chipware (5) loads or extracts housing (1), fluid intake (18) and fluid issuing (19) are synchronously beaten
Open or close and close.
3. synchronous mode dismounting according to claim 1 or 2 is from seal structure, wherein, the overhanging step auricle of gag lever post (16)
(20) it is stuck on sealing drum (4) and chipware (5), does not deviate from aperture (21) time limit coremaking part on housing (1) in locating rod (15)
(5) it, is prevented from deviating from sealing drum (4);Being rotated to an angle during aperture (21) in locating rod (15) abjection housing (1) can be with
By chipware (5) abjection sealing drum (4);Step auricle (20) limitation sealing drum (4) can not deviate from housing (1) all the time.
4. synchronous mode dismounting according to claim 3 is from seal structure, wherein, described chipware (5) is valve or pump.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510031666.8A CN104747736B (en) | 2015-01-21 | 2015-01-21 | A kind of synchronous mode is dismounted from seal structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510031666.8A CN104747736B (en) | 2015-01-21 | 2015-01-21 | A kind of synchronous mode is dismounted from seal structure |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104747736A CN104747736A (en) | 2015-07-01 |
CN104747736B true CN104747736B (en) | 2017-08-04 |
Family
ID=53587842
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510031666.8A Active CN104747736B (en) | 2015-01-21 | 2015-01-21 | A kind of synchronous mode is dismounted from seal structure |
Country Status (1)
Country | Link |
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CN (1) | CN104747736B (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4318667A (en) * | 1979-09-27 | 1982-03-09 | Sundstrand Corporation | Actuating mechanism for fluid pump inlet closure valve |
CN2197527Y (en) * | 1994-08-24 | 1995-05-17 | 赵宝善 | Self shut-off and fast mounting/dismounting valve |
CN2584889Y (en) * | 2002-10-25 | 2003-11-05 | 北京建大流体技术研究院 | Whirlwind centrifugal constant-pressure spray fire pumps |
CN201856897U (en) * | 2010-09-10 | 2011-06-08 | 新乡航空工业(集团)有限公司 | Oil supply pump free from oil drainage in process of disassembling aircraft oil tank |
CN103437852A (en) * | 2013-08-13 | 2013-12-11 | 中国航空工业集团公司沈阳发动机设计研究所 | Filter screen-integrated chip annunciator structure |
CN203347963U (en) * | 2013-01-05 | 2013-12-18 | 中国航空工业集团公司西安飞机设计研究所 | Split fuel pump |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8939736B2 (en) * | 2011-11-30 | 2015-01-27 | Walbro Engine Management, L.L.C. | Fuel pump assembly |
-
2015
- 2015-01-21 CN CN201510031666.8A patent/CN104747736B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4318667A (en) * | 1979-09-27 | 1982-03-09 | Sundstrand Corporation | Actuating mechanism for fluid pump inlet closure valve |
CN2197527Y (en) * | 1994-08-24 | 1995-05-17 | 赵宝善 | Self shut-off and fast mounting/dismounting valve |
CN2584889Y (en) * | 2002-10-25 | 2003-11-05 | 北京建大流体技术研究院 | Whirlwind centrifugal constant-pressure spray fire pumps |
CN201856897U (en) * | 2010-09-10 | 2011-06-08 | 新乡航空工业(集团)有限公司 | Oil supply pump free from oil drainage in process of disassembling aircraft oil tank |
CN203347963U (en) * | 2013-01-05 | 2013-12-18 | 中国航空工业集团公司西安飞机设计研究所 | Split fuel pump |
CN103437852A (en) * | 2013-08-13 | 2013-12-11 | 中国航空工业集团公司沈阳发动机设计研究所 | Filter screen-integrated chip annunciator structure |
Also Published As
Publication number | Publication date |
---|---|
CN104747736A (en) | 2015-07-01 |
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