CN202326200U - Spring-compensating four-space rotor pump - Google Patents
Spring-compensating four-space rotor pump Download PDFInfo
- Publication number
- CN202326200U CN202326200U CN2011203882138U CN201120388213U CN202326200U CN 202326200 U CN202326200 U CN 202326200U CN 2011203882138 U CN2011203882138 U CN 2011203882138U CN 201120388213 U CN201120388213 U CN 201120388213U CN 202326200 U CN202326200 U CN 202326200U
- Authority
- CN
- China
- Prior art keywords
- eccentric
- rotor
- central axis
- rotor shaft
- compensating disc
- 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.)
- Expired - Fee Related
Links
Images
Landscapes
- Rotary Pumps (AREA)
Abstract
The utility model relates to a spring-compensating four-space rotor pump. The spring-compensating four-space rotor pump comprises a pump body, a rotor shaft and a driven rotor, wherein the rotor shaft is mounted in a center through hole of the pump body, and the driven rotor is mounted in an eccentric semi hole of the pump body. An eccentric end cover which is closed and fixed by use of at least three screws is arranged at the external end face of the eccentric semi hole, the external end face of the driven rotor is adhered to the front plane of a compensation plate, locating pins and pagoda-shaped springs are arranged between the back face of the compensation plate and the eccentric end cover, an eccentric distance t exists between the central axis of the rotor shaft and the central axis of the driven rotor, four contact points are synchronously formed between four equi-cambered working segments of the rotor shaft and six equi-cambered surfaces of the driven rotor, four axially-extended sealing tapes are formed from the contact points, four dynamic spaces, namely an A dynamic space, a B dynamic space, a C dynamic space and a D dynamic space, are formed by combining the sealing tapes with the bottom face of the eccentric semi hole and the front plane of the compensation plate, and a supporting rebound force is generated through a way that the pagoda-shaped springs support a boss at the inner side of the eccentric end cover and support the back face of the compensation plate, so that the end face sliding of the four dynamic spaces is ensured to be always in effective sealing.
Description
Technical field
The utility model belongs to mechanical engineering field, relate to a kind of with mechanical energy convert into fluid pressure can the transformation of energy displacement pump, be meant that especially a kind of spring compensates four Space Rotor pumps.
Background technique
Known displacement pump main structure form has: plunger pump, screw pump, Roots pump and sliding vane pump.Have the high advantage of efficient as displacement pump, but all exist its efficient of long-time running wearing and tearing back obviously to reduce, cause the main cause of above-mentioned defective to be that movable isolation of end face between hyperbaric chamber and the low pressure chamber fail to play effective sealing.The undersized easy heat expansion of end face fit tolerance is stuck firmly; The end face fit tolerance is oversize then fails to play effective sealing; And long-time running wearing and tearing back sealing effect is poorer, and the production line of having to stop is changed pumping unit, causes very big direct waste and indirect loss.
Summary of the invention
The purpose of the utility model provides a kind of spring and compensates four Space Rotor pumps; The technology that possesses end wear sealing compensation and gauge wear sealing compensation simultaneously; To realize being in good movable isolating seal state for a long time between hyperbaric chamber and the low pressure chamber; Remedy the deficiency of existing technology, fill up the technological gap that displacement pump possesses end wear sealing compensation and gauge wear sealing compensation simultaneously.To achieve these goals, the utility model provides following technological scheme:
A kind of spring compensates four Space Rotor pumps; Comprise the pump housing and be installed on rotor shaft and off-centre half hole that is installed in the pump housing on the central through bore of the pump housing from rotor; Eccentric half outer end of hole face has eccentric end cap next airtight fixing with at least three screw; Pasting the horizontal frontal plane of compensating disc from the exterior edge face of rotor, locating stud and pagoda shape spring are arranged between the back side of compensating disc and the eccentric end cap, it is characterized in that: described rotor shaft comprises four five equilibrium cambered surface active sections and does not have the keyway shaft part and the shaft with keyway section; The inner end of four five equilibrium cambered surface active sections is pasting bottom surface, eccentric half hole, and the exterior edge face of four five equilibrium cambered surface active sections is being pasted by the horizontal frontal plane of compensating disc; Describedly comprise complete section of five five equilibrium cambered surfaces, the size equal uniform of the width of full section both ends of the surface and the both ends of the surface width of four five equilibrium cambered surface active sections from rotor; Be with " O " type ring recess in the central through bore on the described pump housing; Has eccentric distance t between the central axis in the central axis of central through bore and eccentric half hole; A crescent shape suction inlet UNICOM on the bottom surface, eccentric half hole import, and another crescent shape row mouthful UNICOM outlet; The central axis of described rotor shaft and have eccentric distance t between the centre of rotor axis; Four five equilibrium cambered surface active sections of rotor shaft and from four point of contact of synchronized generation between five five equilibrium cambered surfaces of rotor; Cross point of contact and form four axially extended sealing strips; In conjunction with the horizontal frontal plane of eccentric bottom surface, half hole and compensating disc, constitute A, B, C and four dynamic spaces of D; Has eccentric distance t between the central axis of the central axis of the band on the described compensating disc " O " type ring recess through hole and band " O " type ring recess cylindrical; The outer ring that can hold pagoda shape spring in the back side re-entrant angle of compensating disc; The inner ring of pagoda shape spring is enclosed within on the inboard boss of eccentric end cap, and the eccentric positioning hole and the locating stud of compensating disc are slidingly matched.
The beneficial effect of the utility model is: the support rebounding force that is supported on the inboard boss of eccentric end cap by means of pagoda shape spring and is asking the back side of compensating disc to produce, the end face of guaranteeing four dynamic spaces slides and is in effective sealing all the time.Rotor shaft and from four axially extended sealing strips of rotor synchronized generation, constitute A, B, C and four dynamic spaces of D and possessed the gauge wear sealing compensation simultaneously, guarantee to be in for a long time between hyperbaric chamber and the low pressure chamber good movable isolating seal state.Possess in the time of end wear sealing compensation and gauge wear sealing compensation, realize being in good movable isolating seal state for a long time between hyperbaric chamber and the low pressure chamber.
Description of drawings
Fig. 1 is the sectional drawing of the utility model integral body through axis;
Fig. 2 is the sectional drawing in W-W cross section among Fig. 1;
Fig. 3 is an inner rotor shaft 1 and the relative position relation of four dynamic spaces of synchronized generation that are in operation from rotor 2;
Fig. 4 is with respect to Fig. 3, and rotor shaft 1 is rotated counterclockwise 50 degree around central axis O2, from the relative position relation of rotor 2 after eccentric axis O1 is rotated counterclockwise 40 degree;
Fig. 5 is with respect to Fig. 3, and rotor shaft 1 is rotated counterclockwise 100 degree around central axis O2, from the relative position relation of rotor 2 after eccentric axis O1 is rotated counterclockwise 80 degree;
Fig. 6 is with respect to Fig. 3, and rotor shaft 1 is rotated counterclockwise 150 degree around central axis O2, from the relative position relation of rotor 2 after eccentric axis O1 is rotated counterclockwise 120 degree;
Fig. 7 is with respect to Fig. 3, and rotor shaft 1 is rotated counterclockwise 200 degree around central axis O2, from the relative position relation of rotor 2 after eccentric axis O1 is rotated counterclockwise 160 degree;
Fig. 8 is with respect to Fig. 3, and rotor shaft 1 is rotated counterclockwise 250 degree around central axis O2, from the relative position relation of rotor 2 after eccentric axis O1 is rotated counterclockwise 200 degree;
Fig. 9 is with respect to Fig. 3, and rotor shaft 1 is rotated counterclockwise 300 degree around central axis O2, from the relative position relation of rotor 2 after eccentric axis O1 is rotated counterclockwise 240 degree;
Figure 10 is with respect to Fig. 3, and rotor shaft 1 is rotated counterclockwise 350 degree around central axis O2, from the relative position relation of rotor 2 after eccentric axis O1 is rotated counterclockwise 280 degree.
Figure 11 is the exterior perspective view of rotor shaft 1.
Figure 12 is a rotor shaft 1 and from the camberline construction drawing of rotor 2.
Embodiment
In conjunction with accompanying drawing and embodiment, further structure and the working principle to the utility model elaborates.
A kind of spring compensates four Space Rotor pumps; Comprise the pump housing 4 and be installed on rotor shaft 1 and off-centre half hole 42 that is installed in the pump housing 4 on the central through bore 41 of the pump housing 4 from rotor 2; 42 exterior edge faces, eccentric half hole have the screw 8 of at least three of eccentric end cap 5 usefulness airtight fixing; Pasting the horizontal frontal plane of compensating disc 6 from the exterior edge face of rotor 2; Locating stud 7 and pagoda shape spring 9 are arranged between the back side of compensating disc 6 and the eccentric end cap 5; It is characterized in that: described rotor shaft 1 comprises four five equilibrium cambered surface active sections 13 and does not have keyway shaft part 11 and exterior edge face that the inner end of 12, four five equilibrium cambered surfaces of shaft with keyway section active section 13 is pasting bottom surface, eccentric half hole 40, four five equilibrium cambered surfaces active section 13 is being pasted by the horizontal frontal plane of compensating disc 6; Describedly comprise complete section of five five equilibrium cambered surfaces, the size equal uniform of the width of full section both ends of the surface and the both ends of the surface width of four five equilibrium cambered surface active sections 13 from rotor 2; Central through bore on the described pump housing 4 is with " O " type ring recess for 41 li; Has eccentric distance t between the central axis in the central axis of central through bore 41 and eccentric half hole 42; Crescent shape suction inlet 47 UNICOMs on the bottom surface, eccentric half hole 40 import 46, and another crescent shape row mouthful 48 UNICOMs outlet 49; The central axis of described rotor shaft 1 and have eccentric distance t between the central axis of rotor 2; Four five equilibrium cambered surface active sections of rotor shaft 1 and from four point of contact of synchronized generation between five five equilibrium cambered surfaces of rotor 2; Cross point of contact and form four axially extended sealing strips; Horizontal frontal plane in conjunction with bottom surface, eccentric half hole 40 and compensating disc 6 constitutes A, B, C and four dynamic spaces of D; Has eccentric distance t between the central axis of band " O " the type ring recess through hole 61 on the described compensating disc 6 and the central axis of band " O " type ring recess cylindrical 62; The outer ring that can hold pagoda shape spring 9 in the back side re-entrant angle of compensating disc 6; The inner ring of pagoda shape spring 9 is enclosed within on the inboard boss of eccentric end cap 5, and the eccentric positioning hole 67 and the locating stud 7 of compensating disc 6 are slidingly matched.
" O " type circle in all " O " type ring recess plays the motive sealing effect at position of living in.
Installation steps and working principle:
The shaft with keyway section 12 of rotor shaft 1 is 40 1 sides from bottom surface, off-centre half hole, pass central through bore 41 and are slidingly matched with it, and the inner end of four five equilibrium cambered surface active sections 13 is pasting bottom surface, eccentric half hole 40.Be placed in eccentric half hole 42 from rotor 2 and be slidingly matched; Also pasting bottom surface, eccentric half hole 40 from the inner end of rotor 2; Make the central axis O2 of rotor shaft 1 and between the eccentric axis O1 of rotor 2, have eccentric distance t; Four five equilibrium cambered surface active sections 13 of rotor shaft 1 and from four point of contact of synchronized generation between five five equilibrium cambered surfaces of rotor 2; Cross point of contact and form four axially extended sealing strips, the horizontal frontal plane in conjunction with bottom surface, eccentric half hole 40 and compensating disc 6 constitutes A, B, C and four dynamic spaces of D.Even can guarantee that still four axially extended sealing strips form synchronously after using uniform wear for a long time, guarantee the radially effectively sealing all the time of four dynamic spaces;
Has eccentric distance t between the eccentric axis O1 of the central axis O2 of the band on the compensating disc 6 " O " type ring recess through hole 61 and band " O " type ring recess cylindrical 62; The outer ring that can hold pagoda shape spring 9 in the back side re-entrant angle of compensating disc 6, the eccentric positioning hole 67 and the locating stud 7 of compensating disc 6 are slidingly matched.The horizontal frontal plane of compensating disc 6 inwardly, band " O " type ring recess through hole 61 is inserted in from no keyway shaft part 11 1 ends of rotor shaft 1 and is slidingly matched, band " O " type ring recess cylindrical 62 is slidingly matched with eccentric half hole 42.
Locating stud 7 is fastened on the eccentric end cap 5 inboard faces, and the inner ring of pagoda shape spring 9 is enclosed within on the inboard boss of eccentric end cap 5, and band " O " the type ring recess through hole 51 on the eccentric end cap 5 is inserted in from no keyway shaft part 11 1 ends of rotor shaft 1 and is slidingly matched.At least three screw 8 along the outer circular edge of eccentric end cap 5, on the outside end face with airtight off-centre half hole 42 that is fixed on the pump housing 4 of eccentric end cap 5 shimmings 54.
The back side of compensating disc 6 has positioning hole 67 and locating stud 7 to be slidingly matched, and locating stud 7 is fixedly connected with eccentric end cap 5, thereby compensating disc 6 can only be made axial slip with respect to eccentric end cap 5." O " type circle in all " O " type ring recess plays the motive sealing effect at position of living in.
The support rebounding force that is supported on the inboard boss of eccentric end cap by means of pagoda shape spring and is asking the back side of compensating disc to produce; The horizontal frontal plane of compensating disc is close to the exterior edge face of two rotors all the time; Then force the inner end of two rotors also to be close to bottom surface, eccentric half hole, guarantee that the end face slip of four dynamic spaces is in effective sealing all the time.
During work, external force drives rotor shaft 1 rotation through shaft with keyway section 12, stirs then from rotor 2 rotations.From both rotating center deviation distances of rotor 2 and rotor shaft 1 is eccentric distance t; Four five equilibrium cambered surface active sections 13 of rotor shaft 1 and from four axially extended sealing strips of synchronized generation between five five equilibrium cambered surfaces of rotor 2; Horizontal frontal plane in conjunction with bottom surface, eccentric half hole 40 and compensating disc 6 constitutes A, B, C and four dynamic spaces of D.During rotation, A, B, C and four dynamic spaces of D along with rotation will become a big side gradually and be crescent shape suction inlet 47, lead to import 46; One side that will diminish gradually along with rotation of A, B, C and four dynamic spaces of D is a crescent shape row mouth 48, leads to outlet 49.Rotor shaft 1 continuously rotation order about A, B, C and four dynamic spaces of D go round and begin again accomplish inhale, row's work.
Among Figure 12, illustrate rotor shaft 1 and from the camberline working process of rotor 2 by means of CAD:
Setting-out X of elder generation and vertical with it line Y1 and line Y2, intersection point is respectively O1, O2, and O1 and O2 are 6mm at a distance of get eccentric distance t distance here for eccentric distance t.;
With O1 is the center of circle, and R1 is that radius is made basic circle R1.Here getting the R1 radius is 60mm;
An intersection point with basic circle R1 and line X is the center of circle, and R2 is that radius is made arc section R2, is the center of circle again with O1, and arc section R2 is displayed around O1 five five equilibriums annular.Here getting the R2 radius is 33mm;
The distance that is extended to R3 with the intersection point of arc section R2 and line X is the center of circle, is that the intersection point that radius is crossed arc section R2 and line X is made arc section R3 with R3, is the center of circle again with O2, with arc section R3 around O2 quartering annular display.Here getting the R3 radius is 50mm;
Choose two arc section R3 and an arc section R2 respectively, the tangent arc section R4 that does of four lines gets the R4 radius here and is approximately 4.8mm;
With R5 is that radius is made two adjacent arc section R2 of arc section R5 connection respectively, and the R5 radius is 40mm here.
Article four, arc section R4 alternately with four point of contact of five arc section R2 synchronized generation, cross point of contact and form four axially extended sealing strips, constitute A, B, C and four dynamic spaces of D.Even after using uniform wear for a long time, four point of contact of synchronized generation form four axially extended sealing strips can guarantee that still four axially extended sealing strips form synchronously, and that guarantees four dynamic spaces radially is in effective sealing all the time.
The both ends of the surface width of four five equilibrium cambered surface active sections 13 of rotor shaft 1 and size equal uniform from the both ends of the surface width of rotor 2; Here getting the both ends of the surface width all is 50mm; The inner end of two rotors is all pasting bottom surface, eccentric half hole 40, and the horizontal frontal plane of compensating disc 6 is pasting the exterior edge face of two rotors simultaneously.The support rebounding force that is supported on the inboard boss of eccentric end cap 5 by means of pagoda shape spring 9 and is asking the back side of compensating disc 6 to produce; The horizontal frontal plane of compensating disc 6 is close to the exterior edge face of two rotors all the time; Then force the inner end of two rotors also to be close to bottom surface, eccentric half hole 40, guarantee that the end face slip of four dynamic spaces is in effective sealing all the time.
Claims (1)
1. a spring compensates four Space Rotor pumps; Comprise the pump housing (4) and be installed in the rotor shaft (1) on the central through bore (41) of the pump housing (4) and be installed on off-centre half hole (42) of the pump housing (4) from rotor (2); Exterior edge face, eccentric half hole (42) has eccentric end cap (5) next airtight fixing with at least three screw (8); Pasting the horizontal frontal plane of compensating disc (6) from the exterior edge face of rotor (2); Locating stud (7) and pagoda shape spring (9) are arranged between the back side of compensating disc (6) and the eccentric end cap (5); It is characterized in that: described rotor shaft (1) comprises four five equilibrium cambered surface active sections (13) and do not have keyway shaft part (11) and shaft with keyway section (12), and the inner end of four five equilibrium cambered surface active sections (13) is pasting bottom surface, eccentric half hole (40), and the exterior edge face of four five equilibrium cambered surface active sections (13) is being pasted by the horizontal frontal plane of compensating disc (6); Describedly comprise complete section of five five equilibrium cambered surfaces, the size equal uniform of the width of full section both ends of the surface and the both ends of the surface width of four five equilibrium cambered surface active sections (13) from rotor (2); " O " type ring recess is with in central through bore (41) lining on the described pump housing (4); Has eccentric distance t between the central axis in the central axis of central through bore (41) and eccentric half hole (42); Crescent shape suction inlet (47) UNICOM on the eccentric bottom surface, half hole (40) import (46), and another crescent shape row mouthful (48) UNICOM outlet (49); The central axis of described rotor shaft (1) and have eccentric distance t between the central axis of rotor (2); Four five equilibrium cambered surface active sections of rotor shaft (1) and from four point of contact of synchronized generation between five five equilibrium cambered surfaces of rotor (2); Cross point of contact and form four axially extended sealing strips; In conjunction with the horizontal frontal plane of bottom surface, eccentric half hole (40) and compensating disc (6), constitute A, B, C and four dynamic spaces of D; Has eccentric distance t between the central axis of band " O " the type ring recess through hole (61) on the described compensating disc (6) and the central axis of band " O " type ring recess cylindrical (62); The outer ring that can hold pagoda shape spring (9) in the back side re-entrant angle of compensating disc (6); The inner ring of pagoda shape spring (9) is enclosed within on the inboard boss of eccentric end cap (5), and the eccentric positioning hole (67) of compensating disc (6) is slidingly matched with locating stud (7).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011203882138U CN202326200U (en) | 2011-09-30 | 2011-09-30 | Spring-compensating four-space rotor pump |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011203882138U CN202326200U (en) | 2011-09-30 | 2011-09-30 | Spring-compensating four-space rotor pump |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202326200U true CN202326200U (en) | 2012-07-11 |
Family
ID=46438182
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2011203882138U Expired - Fee Related CN202326200U (en) | 2011-09-30 | 2011-09-30 | Spring-compensating four-space rotor pump |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN202326200U (en) |
-
2011
- 2011-09-30 CN CN2011203882138U patent/CN202326200U/en not_active Expired - Fee Related
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102182673A (en) | Four-line synchromesh spring compensation combination pump | |
CN102192142B (en) | Annular air bag compensation sealing four-space rotor pump | |
CN202370827U (en) | Disc spring compensating five-wire meshed rotor pump | |
CN202326200U (en) | Spring-compensating four-space rotor pump | |
CN202326204U (en) | Cylinder spring compensation five-space rotor pump | |
CN202326203U (en) | Cylindrical spring compensation four-space rotor pump | |
CN202040077U (en) | Four-line synchromesh spring-compensation combination pump | |
CN202326201U (en) | Spring compensating five-space rotor pump | |
CN102182674B (en) | Five-wire synchronous meshing spring compensation combined pump | |
CN202370825U (en) | Cylindrical spring compensating four-wire meshed rotor pump | |
CN202250811U (en) | Spring compensating three-dimensional space rotor pump | |
CN202040076U (en) | Three-line synchromesh spring-compensation combination pump | |
CN202040075U (en) | Five-wire synchromesh spring compensating unit pump | |
CN102182677B (en) | A kind of four line engagement inner pressuring sealing new pump | |
CN202082094U (en) | Annular air bag compensation seal four-space rotor pump | |
CN202531418U (en) | Seal compensating three-space rotor pump for pressure airbag | |
CN202284535U (en) | Three-space rotor pump with cylindrical spring for compensation | |
CN202326202U (en) | Five-space rotor pump adopting pressure air bag for seal compensation | |
CN202228347U (en) | Pressure air bag compensation sealing three-space rotor pump | |
CN202370824U (en) | Five-line-meshed rotor pump compensated by cylindrical spring | |
CN202194822U (en) | Novel pump adopting five-line meshing and internal-pressure sealing | |
CN202082093U (en) | Annular airbag compensating sealing five-space rotor pump | |
CN202187910U (en) | Novel four-wire meshing internal pressure seal pump | |
CN202370829U (en) | Ring-shaped air bag compensating internal and external gear pump | |
CN202250812U (en) | Five-dimensional space internal pressure balance canned-rotor pump |
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: 20120711 Termination date: 20120930 |