CN220539927U - Supercharging rotor wing - Google Patents

Supercharging rotor wing Download PDF

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Publication number
CN220539927U
CN220539927U CN202322194161.6U CN202322194161U CN220539927U CN 220539927 U CN220539927 U CN 220539927U CN 202322194161 U CN202322194161 U CN 202322194161U CN 220539927 U CN220539927 U CN 220539927U
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CN
China
Prior art keywords
ring body
liquid
ring
pressurizing
booster
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Active
Application number
CN202322194161.6U
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Chinese (zh)
Inventor
张华�
黄军
孙兵
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Jiangsu Jinhai Yulong Fluid Technology Co ltd
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Jiangsu Jinhai Yulong Fluid Technology Co ltd
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Application filed by Jiangsu Jinhai Yulong Fluid Technology Co ltd filed Critical Jiangsu Jinhai Yulong Fluid Technology Co ltd
Priority to CN202322194161.6U priority Critical patent/CN220539927U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The utility model relates to a mechanical seal's technical field especially relates to a booster rotor, and it is including setting up the ring body on rotating member, the axis of ring body and rotating member axis form relative eccentric setting on not same straight line, be provided with a plurality of booster grooves on the lateral wall of the eccentric big head one side of ring body. This application has can reduce to encroach on and seal the liquid chamber space, guarantees the liquid capacity, and then guarantees mechanical seal pressure boost temperature control and lubricated effect.

Description

Supercharging rotor wing
Technical Field
The application relates to the technical field of mechanical seals, in particular to a supercharging rotor wing.
Background
I developed and filed before publication No. CN110821880A: the utility model provides a force transmission bi-polar face collection dress formula mechanical seal, mediate movable ring and mediate quiet ring friction seal connection, the gland opposite side is equipped with cold quiet ring seat, cold quiet ring seat is connected with cold quiet ring, cold movable ring and cold quiet ring friction seal connection, cold movable ring and mediate movable ring joint respectively in the rotating part both sides that lead to in, and the through-hole on the rotating part is passed and is supported cold movable ring and mediate movable ring respectively to the spring, rotating part passes cold quiet ring seat in cold quiet ring one side and forms the elasticity pressure portion, the locking snare is established in the elasticity pressure portion outside and is connected with cold quiet ring seat by the locating piece, the screw that the ring was established passes locating piece and locking ring and compresses tightly the elasticity pressure portion, the gland is equipped with the liquid passageway at its two opposite faces, the pump shaft passes from quick-witted seal structure middle part.
However, in the actual production and use process, part of user feedback is limited due to the working environment, and the pumping ring can be additionally arranged on the rotating part, so that the effect of self-circulation sealing liquid is realized, and the durability of the mechanical seal is ensured. However, the pumping ring commonly used in the market is a spiral groove type pumping ring, but in order to ensure a normal pumping effect, the outer side wall of the pumping ring needs to be attached to the inner wall of the gland, so that the space of a liquid sealing cavity in the gland is compressed, and then liquid in the gland is reduced, and the normal mechanical sealing effect is affected.
Disclosure of Invention
In order to solve the technical problem, the application provides a booster rotor, which has the advantages of being capable of reducing the occupation of the space of a liquid sealing cavity, guaranteeing the liquid capacity and further guaranteeing the mechanical sealing effect.
In order to achieve the above purpose, the technical scheme of the utility model is as follows:
the utility model provides a booster rotor, includes the ring body of setting on rotating member, the axis of ring body and rotating member axis form relative eccentric setting on not same straight line, be provided with a plurality of booster tanks on the lateral wall of the eccentric big head one side of ring body.
According to the technical scheme, the central axis of the ring body and the central axis of the rotating part are not in the same straight line, so that the ring body is eccentrically arranged relative to the rotating sleeve, the rotating part can drive the ring body to eccentrically rotate when rotating, the inner space of the gland is changed due to rotation, liquid in the gland can be sent out from one liquid channel and sucked into the other liquid channel (similar to an eccentric cam pump principle, a pumping effect is achieved), compared with a traditional spiral groove type ring body, the eccentric design ring body reduces the space of an internal liquid sealing cavity of the gland, the liquid capacity is ensured not to be too low, the liquid lubrication temperature control effect is ensured, and the mechanical sealing effect is ensured; and when the setting of booster groove can prevent that the ring body from eccentrically rotating, because of the unbalanced centre of gravity leads to it to produce the disturbance to rotating parts, and then lead to the existence of rotating parts bending condition, play dynamic balance effect, and then guarantee life.
As a preferable scheme of the method, the pressurizing grooves are arranged at equal intervals along the circumference of the ring body in a staggered mode.
The technical scheme is realized, so that liquid flowing out of the liquid channel can flow to the medium side and the atmosphere side respectively after being guided by the pressurizing groove, the liquid can be forced to circulate cooling media at two sides, and the temperature control efficiency of the liquid is ensured.
As a preferable mode of the present application, the groove depth of the pressurizing groove is gradually increased in a direction approaching the end face opening thereof.
According to the technical scheme, the bottom wall of the pressurizing tank forms an inclined plane, so that liquid can be pushed to two sides obliquely under the guiding effect of the pressurizing tank after entering from the liquid inlet, and the situation that liquid at dead angles in the sealing cavity cannot circulate is reduced.
As a preferred solution of the present application, the number of the pressurizing grooves of the ring body near the atmosphere side is greater than the number of the pressurizing grooves of the ring body near the medium side.
According to the technical scheme, more liquid is supplied to the atmosphere side than the medium side, so that the atmosphere side pressure is larger than the medium side, and a certain pressure can be generated on the moving ring of the medium side, and the moving ring of the medium side can meet the requirement of medium sealing with a certain pressure.
In summary, the present application includes at least one of the following beneficial technical effects:
1. the central axis of the ring body and the central axis of the rotating part are not in the same straight line, so that the ring body is eccentrically arranged relative to the rotating sleeve, the rotating part can drive the ring body to eccentrically rotate when rotating, the inner space of the gland is changed due to rotation, liquid in the gland can be sent out from one liquid channel and sucked into the other liquid channel (similar to an eccentric cam pump principle, and a pumping effect is realized), compared with the traditional spiral groove type ring body, the eccentric design ring body reduces the space of an inner liquid sealing cavity of the gland, so that the liquid capacity is ensured not to affect the liquid lubrication and the temperature control effect too low, and the mechanical sealing effect is ensured;
2. the arrangement of the pressurizing groove can prevent the ring body from generating disturbance to the rotating component due to unbalanced gravity center when the ring body eccentrically rotates, so that the rotating component is curved, a dynamic balance effect is achieved, and the service life is further ensured;
3. the liquid on the air side is supplied more than the liquid on the medium side, so that the air side pressure is higher than the medium side pressure, and the air side pressure can generate a certain pressure on the moving ring on the medium side, and the moving ring on the medium side can meet the sealing of the medium with a certain pressure.
Drawings
In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic overall structure of an embodiment of the present application.
Fig. 2 is a side view of an embodiment of the present application.
Reference numerals: 1. a ring body; 2. a pressurizing tank.
Detailed Description
The present application is described in further detail below in conjunction with figures 1-2.
The embodiment of the application discloses a booster rotor. Referring to fig. 1, the booster rotor includes a ring body 1 disposed on a rotating member, where the ring body 1 may be integrally formed with the rotating member, and may be detachably assembled on the rotating member, so that the rotating member may rotate while following the rotation of the rotating member to be sealed. Simultaneously the axis of rotating member and the axis of rotating member are not on same straight line, and then make the ring platform set up for rotating the cover is eccentric, and then can drive ring body 1 eccentric rotation when making rotating member rotate, and then make gland inner space because of rotating, and lead to the inner space to change, thereby can be with the liquid in the gland from one of them liquid channel out, inhale liquid (like eccentric cam pump principle, realization pumping effect) in another liquid channel, and the ring body 1 of this kind of eccentric design compares for traditional helical groove formula ring body 1, it has reduced the inside liquid cavity space that seals of invasion gland, thereby guarantee that liquid capacity can not be too low influence liquid lubrication and accuse temperature effect.
Meanwhile, in order to prevent the ring body 1 from eccentrically rotating, the rotating component is disturbed due to unbalanced gravity center, and then the rotating component is bent, a plurality of pressurizing grooves 2 are formed in the side wall of one side of the eccentric big end of the ring body 1, the pressurizing grooves can be axially arranged through the pump body and can also be axially arranged without the pump body, the pressurizing grooves 2 can adjust the gravity center of the ring body 1, the dynamic balance effect is further ensured, the pressurizing grooves 2 can accelerate the internal space to change like pulses, and the pumping pressure of the ring body 1 is further improved. The length of booster tank is less than the ring body in this embodiment, and then makes the booster tank not run through the pump body axial setting, and a plurality of booster tanks 2 are equidistant crisscross to be set up along ring body 1 circumference, and then make the liquid that flows out from the liquid passageway flow to medium side (medium ring one side) and atmosphere side (cold ring one side) respectively after the direction of booster tank 2 to guarantee that liquid can circulate to the cooling medium of both sides, thereby guarantee lubrication and the accuse temperature effect of liquid. Meanwhile, the number of the pressurizing grooves of the ring body 1 close to the atmosphere side is larger than the number of the pressurizing grooves 2 of the ring body 1 close to the medium side, so that liquid supplied to the atmosphere side is more than liquid supplied to the medium side, the atmosphere side pressure is larger than the medium side, a certain pressure can be generated on the moving ring of the medium side, and the moving ring of the medium side can meet the requirement of medium sealing with a certain pressure. And the groove depth of each pressurizing groove 2 is gradually increased along the direction close to the opening of the end face of the pressurizing groove, so that the bottom wall of the pressurizing groove 2 forms an inclined plane, and then liquid can be sent out to two sides in an inclined manner under the guiding effect of the pressurizing groove 2 after entering from the liquid inlet, so that the situation that the liquid at dead angles in a sealing cavity cannot circulate is reduced.
The implementation principle of the booster rotor wing is as follows: the axis of ring body and the axis of rotating member are not on same straight line, and then make the ring platform set up for rotating the cover is eccentric, and then can drive ring body 1 eccentric rotation when making rotating member rotate, and then make gland inner space because of rotating, and lead to the inner space change, thereby can be with the liquid in the gland from one of them liquid channel out, inhale liquid (like eccentric cam pump principle, realize the pumping effect) in another liquid channel, and the ring body 1 of this kind of eccentric design compares for traditional spiral groove formula pumping ring, it has reduced the inside liquid chamber space of sealing of invasion gland, thereby guarantee that liquid capacity can not the too low effect liquid lubrication and accuse temperature effect, thereby guarantee mechanical seal effect. When the pressurization groove 2 is arranged to prevent the ring body 1 from eccentrically rotating, the rotation part is disturbed due to unbalanced gravity center, so that the rotation part is bent, a dynamic balance effect is achieved, and the service life is further guaranteed.
The number of the pressurizing grooves of the ring body 1 close to the atmosphere side is larger than the number of the pressurizing grooves 2 of the ring body 1 close to the medium side, and the liquid fed into the atmosphere side is more than the liquid fed into the medium side, so that the atmosphere side pressure is larger than the medium side, and the ring body can generate certain pressure on the moving ring of the medium side, and the moving ring of the medium side can meet the sealing of the medium with certain pressure.
The foregoing are all preferred embodiments of the present application, and are not intended to limit the scope of the present application in any way, therefore: all equivalent changes in structure, shape and principle of this application should be covered in the protection scope of this application.

Claims (4)

1. A booster rotor, characterized in that: the rotary part comprises a ring body (1) arranged on the rotary part, wherein the central axis of the ring body (1) and the central axis of the rotary part are not in the same straight line to form relative eccentric arrangement, and a plurality of pressurizing grooves (2) are formed in the side wall of one side of the eccentric big head of the ring body (1).
2. The booster rotor of claim 1, wherein: the length of the pressurizing grooves (2) is smaller than the axial width of the ring body (1), and the pressurizing grooves (2) are arranged at equal intervals along the circumferential direction of the ring body (1).
3. A booster rotor according to claim 1 or 2, characterized in that: the groove depth of the pressurizing groove (2) gradually increases along the direction close to the opening of the end face.
4. The booster rotor of claim 2, wherein: the number of the pressurizing grooves of the ring body (1) close to the atmosphere is larger than the number of the pressurizing grooves (2) of the ring body (1) close to the medium.
CN202322194161.6U 2023-08-15 2023-08-15 Supercharging rotor wing Active CN220539927U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322194161.6U CN220539927U (en) 2023-08-15 2023-08-15 Supercharging rotor wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322194161.6U CN220539927U (en) 2023-08-15 2023-08-15 Supercharging rotor wing

Publications (1)

Publication Number Publication Date
CN220539927U true CN220539927U (en) 2024-02-27

Family

ID=89973819

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322194161.6U Active CN220539927U (en) 2023-08-15 2023-08-15 Supercharging rotor wing

Country Status (1)

Country Link
CN (1) CN220539927U (en)

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