CN220101601U - Mechanical seal composite open-cell foam medium sealing ring structure of turbine pump - Google Patents

Mechanical seal composite open-cell foam medium sealing ring structure of turbine pump Download PDF

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CN220101601U
CN220101601U CN202321691935.XU CN202321691935U CN220101601U CN 220101601 U CN220101601 U CN 220101601U CN 202321691935 U CN202321691935 U CN 202321691935U CN 220101601 U CN220101601 U CN 220101601U
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ring
mechanical seal
cell foam
open
foam
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马学忠
李聪聪
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Lanzhou University of Technology
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Lanzhou University of Technology
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Abstract

The utility model relates to the technical field of fluid sealing, in particular to a mechanical seal composite open-cell foam medium sealing ring structure of a turbine pump, which comprises a movable ring and a static ring of the mechanical seal, wherein flushing holes leading to the outer diameter side from the bottom surface of the movable ring are uniformly distributed in the circumferential direction of the movable ring, annular grooves are formed in the outer diameter sides of the movable ring and the static ring, and foam mediums are embedded in the flushing holes and the annular grooves of the movable ring and the static ring. The sealing ring is favorable for strengthening heat transfer of the sealing end face and reducing the temperature of the end face.

Description

Mechanical seal composite open-cell foam medium sealing ring structure of turbine pump
Technical Field
The utility model relates to the technical field of fluid sealing, in particular to a mechanical sealing composite open-cell foam medium sealing ring structure of a turbine pump.
Background
Turbopumps are the core components of rocket engines, while mechanical seals are critical to their performance as an important component of the turbopump. The mechanical seal rotates at a high speed under the actual working condition, the end face of the seal ring can generate great friction heat and viscous shearing heat, and the stirring heat is added, so that the temperature of the end face is too high, and a series of problems such as thermal deformation of the end face, vaporization of an end face liquid film, thermal cracking of the end face and the like are caused. Therefore, in order to ensure the reliability of the turbo pump, a higher demand is placed on the mechanical seal of the turbo pump. Currently, the use of new seal ring structures is an effective way to study mechanical seals.
Qia et al (DOI: 10.1115/1.4006063) have built a mechanical seal three-dimensional thermodynamic model of a "U" shaped notch and have analyzed the thermal mixing and heat transfer characteristics within the "U" notch in detail. And discusses the heat transfer path and cooling mechanism of the gap. Zhang Weizheng et al (DOI: 10.11949/0438-1157.20221377) established a three-dimensional thermal fluid dynamic lubrication model of annular groove and spiral groove composite end face configuration, analyzed the law of influence of groove geometry parameters on the temperature field and sealing performance under the two models, and revealed the influence mechanism of the flow state on the end face groove cooling effect. Both documents essentially reduce the end surface temperature by changing the shape of the sealing end surface, but the two documents also belong to the traditional processing method, and have a certain cooling effect but are not obvious enough.
Disclosure of Invention
The utility model aims to provide a mechanical seal composite open-cell foam medium sealing ring structure of a turbine pump, which is beneficial to strengthening heat transfer of a sealing end face and reducing the temperature of the end face.
The technical scheme of the utility model is as follows: the utility model provides a compound open cell foam medium sealing ring structure of turbopump mechanical seal, includes mechanical seal's movable ring and quiet ring, the circumferencial direction evenly distributed of movable ring has the flushing hole that leads to the external diameter side from the ring bottom surface, and the external diameter side of movable ring and quiet ring all is provided with a pair of annular arch, is located the annular channel that forms between a pair of annular arch, all imbeds foam medium in the annular channel of flushing hole and movable ring and quiet ring.
Further, the annular channel of the moving ring is arranged between the flushing hole and the end surface matched with the stationary ring, and the annular channel of the stationary ring is arranged between the bottom surface of the stationary ring and the end surface matched with the moving ring.
Further, the axial height of the annular channel is 1-10mm, and the radial depth is 1-8mm.
Further, the flushing hole is in an L-shaped straight hole, a straight inclined hole or a bent hole; the cross section of the flushing hole is square, round or polygonal.
Further, the aperture selection range of the flushing holes is 2-6 cm, and the number of the openings is 8-30.
Further, the foam medium is an open-cell foam metal material or an open-cell foam nonmetal material.
Further, the open-cell foam metal material is copper foam, aluminum foam or nickel foam; the open-cell foam nonmetallic material is foam graphite or foam ceramic.
Further, the porosity of the open-cell foam medium is selected to be 50% -97%, and the pore density is selected to be 10 PPI-95 PPI.
Further, the foam medium between the flushing hole and the annular channel is connected in a pressure fixing, bonding or brazing mode.
Further, the mechanical seal of the turbine pump is a contact mechanical seal or a non-contact mechanical seal.
Compared with the prior art, the utility model has the following advantages:
1. the sealing ring is embedded into the flushing hole and between the grooves of the tooth-shaped structures of the movable ring and the static ring through the open-cell foam medium, so that the mechanical sealing ring structure of the turbine pump is effectively improved, the heat convection between the sealing medium and the end face of the ring is enhanced, and the temperatures of the end face and the end face liquid film are reduced. The problems of thermal deformation, liquid film gasification, thermal cracking and the like generated by the end surfaces of the dynamic ring and the static ring when the mechanical seal of the turbine pump rotates at a high speed in the prior art are solved.
2. The sealing ring utilizes the advantages of large specific surface area, good permeability, strong turbulence effect, high heat transfer efficiency and the like of the open-cell foam material, and greatly reduces heat generated by friction and fluid viscosity shearing, so that the service life of the mechanical seal of the turbine pump is prolonged by the vortex.
3. The seal ring can be applied to a contact turbine pump mechanical seal or a non-contact turbine pump mechanical seal.
Drawings
FIG. 1 is a schematic view of the structure of the present utility model
FIG. 2 is a schematic view of an "L" shaped flushing hole in the moving ring of the present utility model;
FIG. 3 is a schematic view of a straight bore of greater than 90 degrees in the moving ring of the present utility model;
FIG. 4 is a schematic view of a straight inclined hole in the moving ring of the present utility model;
FIG. 5 is a schematic view of a circular curved bore in a moving ring according to the present utility model;
FIG. 6 is a schematic representation of the structure of an open cell foam media of the present utility model with porosity;
FIG. 7 is a schematic representation of another open cell foam media structure of the present utility model;
FIG. 8 is a schematic representation of the structure of a double layer open cell foam media of the present utility model;
in the figure: the device comprises an A-moving ring, a B-stationary ring, a 1-ring bottom surface, a 2-outer diameter side, 3- 'L' -shaped flushing holes, 4-annular channels, 5-foam media, 6-straight holes with the angle of more than 90 degrees, 7- 'straight' -shaped inclined holes and 8-round bent holes.
Detailed Description
In order to make the above features and advantages of the present utility model more comprehensible, embodiments accompanied with figures are described in detail below, but the present utility model is not limited thereto.
Referring to fig. 1 to 8
The utility model provides a compound open cell foam medium sealing ring of turbopump mechanical seal, includes mechanical seal's rotating ring A and quiet ring B, the circumferencial direction evenly distributed of rotating ring has the flushing hole that leads to rotating ring external diameter side 2 from ring bottom surface 1, and the external diameter side of rotating ring and quiet ring all is provided with the ring channel 4 that forms "tooth" column structure, all imbeds foam medium 5 in the ring channel of flushing hole and rotating ring and quiet ring. When the sealing moving ring rotates at a high speed, under the drive of the centrifugal force of fluid, a low-temperature medium in the sealing cavity flows in from the opening of the bottom surface of the moving ring, the sealing medium is fully contacted with the foam material, and then flows back to the sealing cavity from the opening of the outer diameter side; when the movable ring rotates at a high speed, the traction sealing cavity medium flows outside the dynamic and static rings, so that the low-temperature sealing medium enters the foam material. Because the foam material has the advantages of large specific surface area, good permeability, strong turbulence effect, high heat transfer efficiency and the like, the sealing ring structure is greatly improved, the heat convection between the sealing medium and the ring end face is enhanced, and the temperature of the sealing ring end face is reduced.
In this embodiment, the annular channel of the moving ring is disposed between the flushing hole and the end face that mates with the stationary ring, and the annular channel of the stationary ring is disposed between the ring bottom face of the stationary ring and the end face that mates with the moving ring.
In this embodiment, the axial height of the annular channel is 1-10mm, and the radial depth is 1-8mm.
In this embodiment, the flushing hole is an "L" shaped straight hole (refer to fig. 2), an "in-line" inclined hole (refer to fig. 3) or a curved hole (refer to fig. 5), or may be a straight hole at other angles (refer to fig. 4); the section shape of the flushing hole is square, round or polygonal.
In this embodiment, the aperture selection range of the flushing holes is 2-6 cm, and the number of the openings is 8-30.
In this embodiment, the foam medium is an open-cell foam metal material, such as copper foam, aluminum foam, or nickel foam. The foam medium may also be an open-cell foam nonmetallic material, such as graphite foam or ceramic foam.
In this embodiment, the porosity of the open-cell foam medium is selected to be 50% -97%, and the pore density is selected to be 10 ppi-95 ppi.
In this embodiment, the foam medium in the flushing hole, and the foam medium in the annular channels of the moving ring and the static ring are connected with the annular surface by pressure fixing, bonding or brazing.
In this embodiment, the mechanical seal of the turbo pump may be a contact type mechanical seal or a non-contact type mechanical seal.
Working principle:
when the mechanical seal moving ring of the turbine pump rotates at a high speed, the low-temperature medium in the seal cavity flows in from the ring bottom surface open pore of the moving ring under the drive of the centrifugal force of fluid, fully contacts with the open-pore foam material, and flows back to the seal cavity from the outer diameter side open pore. Meanwhile, the dynamic ring rotates to drag the sealing cavity medium to flow outside the dynamic ring and the static ring, so that the low-temperature sealing medium enters the foam material, the foam material has large specific surface area, good permeability, strong turbulence effect and high heat transfer efficiency, and the heat convection between the sealing medium and the end face of the ring is enhanced, thereby reducing the temperature of the end face of the sealing ring. Compared with a similar fluid dynamic pressure type mechanical seal structure, the mechanical seal structure of the utility model greatly reduces heat generated by friction and fluid viscosity shearing, so that the service life of the mechanical seal of the turbine pump is prolonged.
If the utility model discloses or relates to components or structures fixedly connected with each other, then unless otherwise stated, the fixed connection is understood as: detachably fixed connection (e.g. using bolts or screws) can also be understood as: the non-detachable fixed connection (e.g. riveting, welding), of course, the mutual fixed connection may also be replaced by an integral structure (e.g. integrally formed using a casting process) (except for obviously being unable to use an integral forming process).
In addition, terms used in any of the above-described aspects of the present disclosure to express positional relationship or shape have meanings including a state or shape similar to, similar to or approaching thereto unless otherwise stated.
Any part provided by the utility model can be assembled by a plurality of independent components, or can be manufactured by an integral forming process.
The foregoing description is only of the preferred embodiments of the utility model, and all changes and modifications that come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.

Claims (10)

1. The utility model provides a compound open cell foam medium sealing ring structure of turbopump mechanical seal, includes mechanical seal's rotating ring and quiet ring, its characterized in that, the circumferencial direction evenly distributed of rotating ring has the flushing hole that leads to the external diameter side from the ring bottom surface, and the external diameter side of rotating ring and quiet ring all is provided with the annular channel, all imbeds foam medium in the annular channel of flushing hole and rotating ring and quiet ring.
2. The mechanical seal composite open-cell foam media seal ring structure of a turbopump of claim 1 wherein the annular channel of the moving ring is disposed between the flushing orifice and the end face that mates with the stationary ring, the annular channel of the stationary ring being disposed between the ring bottom face of the stationary ring and the end face that mates with the moving ring.
3. The mechanical seal composite open cell foam media seal ring structure of a turbopump of claim 1 or 2 wherein the annular channel has an axial height of 1-10mm and a radial depth of 1-8mm.
4. The mechanical seal composite open-cell foam media seal ring structure of a turbopump according to claim 1 or 2, wherein the flushing holes are in the form of "L" straight holes, "straight" inclined holes or curved holes; the cross section of the flushing hole is square, round or polygonal.
5. The mechanical seal composite open-cell foam medium sealing ring structure of the turbine pump according to claim 4, wherein the aperture of the flushing holes is selected to be 2-6 cm, and the number of the open cells is selected to be 8-30.
6. The turbopump mechanical seal composite open cell foam media seal ring structure of claim 1 wherein the foam media is an open cell foam metal material or an open cell foam non-metal material.
7. The turbopump mechanical seal composite open-cell foam media seal ring structure of claim 6 wherein the open-cell foam metal material is copper foam, aluminum foam or nickel foam; the open-cell foam nonmetallic material is foam graphite or foam ceramic.
8. The mechanical seal composite open-cell foam media sealing ring structure of a turbopump of claim 5, wherein the open-cell foam media has a porosity value ranging from 50% to 97% and a cell density value ranging from 10ppi to 95 ppi.
9. The mechanical seal composite open-cell foam medium sealing ring structure of the turbopump according to claim 1, wherein foam medium between the flushing holes and the annular channels is connected in a pressure fixing, bonding or brazing mode.
10. The mechanical seal composite open-cell foam media seal ring structure of a turbopump of claim 1, wherein the mechanical seal of the turbopump is a contact mechanical seal or a non-contact mechanical seal.
CN202321691935.XU 2023-06-30 2023-06-30 Mechanical seal composite open-cell foam medium sealing ring structure of turbine pump Active CN220101601U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202321691935.XU CN220101601U (en) 2023-06-30 2023-06-30 Mechanical seal composite open-cell foam medium sealing ring structure of turbine pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202321691935.XU CN220101601U (en) 2023-06-30 2023-06-30 Mechanical seal composite open-cell foam medium sealing ring structure of turbine pump

Publications (1)

Publication Number Publication Date
CN220101601U true CN220101601U (en) 2023-11-28

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202321691935.XU Active CN220101601U (en) 2023-06-30 2023-06-30 Mechanical seal composite open-cell foam medium sealing ring structure of turbine pump

Country Status (1)

Country Link
CN (1) CN220101601U (en)

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