WO2002093046A1 - Joint mecanique - Google Patents
Joint mecanique Download PDFInfo
- Publication number
- WO2002093046A1 WO2002093046A1 PCT/GB2002/002162 GB0202162W WO02093046A1 WO 2002093046 A1 WO2002093046 A1 WO 2002093046A1 GB 0202162 W GB0202162 W GB 0202162W WO 02093046 A1 WO02093046 A1 WO 02093046A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- seal
- seal face
- textured
- mechanical seal
- face
- Prior art date
Links
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
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
- F16J15/3404—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member and characterised by parts or details relating to lubrication, cooling or venting of the seal
- F16J15/3408—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member and characterised by parts or details relating to lubrication, cooling or venting of the seal at least one ring having an uneven slipping surface
- F16J15/3424—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member and characterised by parts or details relating to lubrication, cooling or venting of the seal at least one ring having an uneven slipping surface with microcavities
-
- 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
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
- F16J15/3404—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member and characterised by parts or details relating to lubrication, cooling or venting of the seal
- F16J15/3408—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member and characterised by parts or details relating to lubrication, cooling or venting of the seal at least one ring having an uneven slipping surface
- F16J15/3412—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member and characterised by parts or details relating to lubrication, cooling or venting of the seal at least one ring having an uneven slipping surface with cavities
Definitions
- This invention relates to mechanical seals used to seal equipment with rotating components.
- a mechanical seal comprises a "floating" component which is mounted so as to be axially movable around the rotary shaft of, for example, a pump and a “static” component which is axially fixed, typically being secured to a housing.
- the floating component has a flat annular end face, i.e. its seal face, directed towards a complementary seal face of the static component.
- the floating component is urged towards the static component to close the seal faces together to form a sliding face seal, usually by means of one or more spring members.
- one of the floating and static components rotates; this component is referred to as the rotary component.
- the other of the floating and static components does not rotate and is referred to as the stationary component.
- the sliding interface between the rotary and stationary components is particularly important to the operational performance of the mechanical seal.
- the varying conditions at the sliding interface between a pair of mechanical seal faces, are well documented.
- the term "fluid film” is often used to describe the lubrication characteristics at the sliding interface. It is commonly understood that the action of a rotating component sliding against a stationary component can create undesirable operational conditions. Such conditions include the generation of heat, increased equipment power consumption, increased component wear and ultimately reduced component operational life.
- An etched surface across the entire radial seal face width can, in some circumstances, lead to static seal face leakage. This is due to the respective distance between any two micropores and the hydrostatic effects of the fluid film under media pressure.
- a mechanical seal to provide sealing between a rotatable shaft and a housing, the seal having a stationary part for connection to the housing and a rotary part for rotation with the shaft, mating sealing faces being carried by said stationary and rotary parts, said rotary parts being for mounting on the drive shaft for rotation therewith, at least one seal face having a textured portion and a non-textured portion, the non-textured portion acting as a sealing dam
- edge of the sealing dam is positioned at or close to the seal face balance diameter.
- the sealing dam may be radially positioned on the lower pressure side of the seal face relative to the textured portion.
- the sealing dam may be radially positioned on the higher pressure side of the seal face relative to the textured portion.
- the sealing dam may cover up to 99 per cent of the seal face area and correspondingly the textured surface may cover up to 99 per cent of the seal face area.
- the textured surface consists of micropores or indentations in the surface of the seal face.
- micropores or indentations may be evenly distributed in the area of the seal face adjacent to the sealing dam. Alternatively they may be randomly distributed in the area of the seal face adjacent to the sealing dam.
- Figure 1 illustrates an end view of a prior art seal face design extracted from US 6,046,430 (Etsion).
- Figure 2 is a graph which compares the typical start up torque required to overcome the ringing or sticking effect of a conventional "non-textured" seal face to that of a micropore “textured” seal face which is textured across its entire radial length, over a range of process pressures using water as a process media.
- Figure 3 is a graph which corresponds to Figure 2 but uses a nitrogen gas as the process media.
- Figure 4 is a partial longitudinal cross section through a single cartridge mechanical seal of the invention.
- Figure 5 is a sectional view showing the invention and corresponding to
- Figure 6 is a partial longitudinal cross section through a double cartridge mechanical seal of the invention.
- Figure 7 is a cross section through a seal face showing a sealing dam and typical micropore indentations in its surface.
- Figure 8a is an end view of a seal face with a surface texture across its entire radial cross section.
- Figure 8b corresponds to Figure 8a and part of Figure 6 and is an end view of a seal face of the invention with a portion of its seal face encompassing a sealing dam and a surface textured portion.
- Figure 1 shows a prior art arrangement as previously mentioned.
- Figure 3 clearly shows a similar torque difference between a fully textured seal face and a conventional seal face when starting a mechanical seal operating in nitrogen gas.
- the rotary and axially floating seal face (1) is spring biased towards a static stationary seal face (2).
- the rotary seal face (1) is allowed to slide on the static seal face (2).
- the interface between the rotary seal face (1) and stationary seal face (2) forms sealing area (3).
- This sealing area (3) is the primary seal that prevents the process media (4) from escaping from the process chamber (5).
- the process media (4) is sealed by a sleeve elastomer (6) in contact with the shaft (7) and sleeve (8). This has been termed the first secondary sealing area (9).
- the second secondary sealing area (10) is formed between stationary seal face (2) and stationary gland (11) using elastomer (12).
- the third secondary sealing area (13) is formed between the rotary seal face (1) and the sleeve (8) using elastomer (14).
- the fourth secondary sealing area (15) is formed between the gland (11) and the process chamber (5) using gasket (16).
- At least one of the two sealing faces, rotary (1) and stationary (2) has a partly micropore textured surface (17).
- Said micropore textured surface, in single seal operation, preferably extends radially inwardly from the outside diameter terminating at the sealing dam.
- the invention illustrated in Figure 4 therefore offers a cartridge mechanical seal with at least one set of mechanical seal faces which are textured across only part of the radial cross section.
- Figure 5 shows the section at the mechanical seal faces which corresponds to Figure 4.
- Figure 5 illustrates an inwardly positioned sealing dam (18) since the micropore textured surface (17) is positioned radially outwardly to the sealing dam (18).
- This seal dam (18) invention provides an adequate, non- textured sealing surface for static applications.
- the sealing dam (18) It is considered advantageous to locate the edge of the sealing dam (18) at or close to the seal balance diameter (19). It is further advantageous, although not essential, for the radially largest part of the sealing dam (18) to coincide with the mechanical seal face balance line (19). The sealing dam (18) therefore protrudes radially inwardly allowing the micropore surface (17) to be lubricated by the process fluid (4). From the single seal design in Figure 4, the process fluid (4) is often at a higher pressure than the inner most part of the seal face (3). This radially inner most part of a single seal design is often termed the atmospheric side of the seal face (3).
- the sealing dam to balance diameter ratio can be changed to suit specific applications. Likewise the percentage seal face area coverage of the sealing dam and textured surface can be changed to create optimised conditions at the fluid film, for given process conditions.
- the radially smallest part of the sealing dam (18) can be designed to coincide with the mechanical seal face balance diameter (19).
- the sealing dam (18) therefore protrudes radially outwardly allowing the micropore surface (17) adjacent to the lower pressure or atmospheric side of the seal faces (3). This is shown in Figure 6, assuming the barrier pressure (20) is lower than the process pressure (4).
- Hydrostatic fluid film conditions between the mechanical seal faces (3) are a known and well-documented fact of mechanical seal design.
- the hydrostatic fluid film conditions between any two mating seal faces (3) may be approximated as a linear pressure drop.
- the linear pressure drop creates an axially thicker fluid film at the higher pressure outer or inner most radial side of the seal faces (3).
- the fluid film then reduces in a linear axially manner to the radially lower pressure side of the seal faces (3). At the lower pressure side of the seal faces the fluid film is said to be "thin".
- Figure 6 illustrates the invention applied to a double cartridge mechanical seal. From Figure 6 the stationary and axially floating seal face (2) is spring biased towards an axially static rotary seal face (1). The rotary face (1) is allowed to slide on the stationary seal face (2). The interface between the rotary seal face (1) and stationary seal face (2) forms sealing area (3). This sealing area (3) is the primary seal that prevents the process media (4) from escaping from the process chamber (5).
- the second primary seal is made in the barrier media chamber (20) on the outboard side of the mechanical seal.
- the stationary and axially floating seal face (21) is spring biased towards an axially static rotary seal face (22).
- the rotary face (22) is allowed to slide on the stationary seal face (21).
- the interface between the rotary seal face (22) and stationary seal face (21) forms sealing area (23).
- This sealing area (23) is the primary seal that prevents the barrier media from escaping from the barrier media chamber (20).
- the sealing dam (24) is positioned approximately radially outwardly of the seal face balance diameter (25), whilst the textured surface (26) is positioned adjacent to the barrier media in the barrier media chamber (20).
- Figure 7 shows a cross section through a seal face of the invention.
- the micropore indentations (27) have been shown as spherical indentations which penetrate the surface in depth up to, but preferably less than, the radius of the spherical indentation. It is considered self evident that the surface indentations could be of any physical shape, but ideally be of a symmetrical nature (viewed on the end of the seal face) and of any physical depth.
- the seal face comprises of a sealing dam portion (24) and a textured portion (26)
- the spacing of the micropore indentations (27) has minimal influence on the static sealability of the seal face. It is therefore possible to distribute the micropore indentations (27) so that they are positioned as close to each other as physically possible.
- the micropore indentations (27) could cover up to 95% of the designated textured surface area (26).
- This invention therefore allows the optimum dynamic performance of the mechanical seal without increasing the physical radial cross section (28) of the seal face. This reduces heat generation, power consumption and seal face wear in comparison to a conventional mechanical seal.
- the mean ringing force may be approximated to lie on the radius midway between the outside radius (Rmax) of the seal face and inside radius (Rmin) of the seal face.
- This is mean radius (Rmean) is shown in Figure 8a.
- Figure 8b shows the mean radius (Rmean), where the ringing force acts, on a seal face of the invention when the micropore surface (17) is on the radially most inner part of the seal face (3). Comparing Figures 8a and 8b, for the same seal face radial cross section, the mean radius is smaller in that of the invention ( Figure 8b).
- Torque is derived from Force and Radius. If we assume the same amount of surface indentations in the two designs, the force will be constant. If the mean radius of the invention reduces, then the torque required to overcome the ringing effect in the invention will be proportionally smaller.
- This reduction in torque, of the invention is significant, and reduces the likelihood of damaging the seal face in equipment start up conditions.
- the invention may be employed for at least one seal face, for both rotary seals and stationary seals, single, double or triple mechanical seals, whether designed in a cartridge or component seal format. It is also considered self evident that the invention may be used with metallic components as well as non-metallic components. Some types of equipment rotate the housing and have a stationary shaft. It is considered that the invention can be similarly applied to such designs.
- the invention may be employed for seal designs with hydraulically balanced seal faces as well as hydraulically unbalanced seal faces.
- the textured micropore portion of the seal face may differ between each set of faces.
- the micropore portion may be on the inner radial portion of at least one seal face in contact with the process media (4) and on the outer radial portion of at least one seal face in contact with the barrier media (20).
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mechanical Sealing (AREA)
Abstract
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0111716A GB0111716D0 (en) | 2001-05-15 | 2001-05-15 | A mechanical seal with a textured seal face |
GB0111716.7 | 2001-05-15 | ||
GB0200147A GB0200147D0 (en) | 2001-05-15 | 2002-01-02 | A mechanical seal with a textured seal face |
GB0200147.7 | 2002-01-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002093046A1 true WO2002093046A1 (fr) | 2002-11-21 |
Family
ID=26246072
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB2002/002162 WO2002093046A1 (fr) | 2001-05-15 | 2002-05-15 | Joint mecanique |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2002093046A1 (fr) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2006070205A1 (fr) * | 2004-12-30 | 2006-07-06 | Aes Engineering Limited | Joint rotatif |
CN103470762A (zh) * | 2013-08-20 | 2013-12-25 | 浙江工业大学 | 倾斜渐变多孔端面非接触式机械密封结构 |
CN104154235A (zh) * | 2014-05-07 | 2014-11-19 | 清华大学 | 螺旋分布收敛型微孔织构机械密封 |
WO2015031474A1 (fr) * | 2013-08-27 | 2015-03-05 | Eaton Corporation | Composite pour bague d'étanchéité permettant une meilleure étanchéité hydrodynamique |
WO2015041048A1 (fr) * | 2013-09-18 | 2015-03-26 | イーグル工業株式会社 | Composant coulissant |
US9714712B2 (en) | 2014-08-15 | 2017-07-25 | Eaton Corporation | Hydrodynamic mating ring with integrated groove inlet pressure control |
US9970478B2 (en) | 2013-09-18 | 2018-05-15 | Eagle Industry Co., Ltd. | Sliding parts |
EP3627011A4 (fr) * | 2017-05-19 | 2021-01-20 | Eagle Industry Co., Ltd. | Composant coulissant |
US11035411B2 (en) | 2017-07-14 | 2021-06-15 | Eagle Industry Co., Ltd. | Sliding parts |
US11125334B2 (en) | 2016-12-21 | 2021-09-21 | Eaton Intelligent Power Limited | Hydrodynamic sealing component and assembly |
US11248707B2 (en) | 2017-05-19 | 2022-02-15 | Eagle Industry Co., Ltd | Sliding component |
US11708911B2 (en) | 2017-10-03 | 2023-07-25 | Eagle Industry Co., Ltd. | Sliding component |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4925490A (en) * | 1987-12-28 | 1990-05-15 | Tanken Seiko Kabushiki Kaisha | Mechanical seal using pore-dispersed material, and pore-dispersed cemented carbide and method for manufacturing same |
EP0466076A2 (fr) * | 1990-07-09 | 1992-01-15 | Ebara Corporation | Garniture à bague glissante avec rainures hélicoidales |
EP0470409A1 (fr) * | 1990-07-18 | 1992-02-12 | Ebara Corporation | Garniture mécanique d'étanchéité sans contact |
US5092612A (en) * | 1986-10-28 | 1992-03-03 | Pacific Wietz Gmbh & Co. Kg | Contactless pressurizing-gas shaft seal |
US5435574A (en) * | 1986-10-28 | 1995-07-25 | Pacific Wietz Gmbh & Co. Kg | Contactless pressurizing-gas shaft seal |
US5664787A (en) * | 1994-03-22 | 1997-09-09 | Nippon Pillar Packing Co., Ltd. | Non-contacting shaft sealing device |
EP0935086A2 (fr) * | 1998-02-06 | 1999-08-11 | John Crane Inc. | Garniture d'étanchéité lubrifiée au gaz pour faibles vitesses de rotation |
US6046430A (en) * | 1996-09-30 | 2000-04-04 | Surface Technologies Ltd. | Bearing having micropores, and design method therefor |
US6341782B1 (en) * | 2000-03-03 | 2002-01-29 | Surface Technologies Ltd | Lubricated seals having micropores |
-
2002
- 2002-05-15 WO PCT/GB2002/002162 patent/WO2002093046A1/fr not_active Application Discontinuation
Patent Citations (9)
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US5092612A (en) * | 1986-10-28 | 1992-03-03 | Pacific Wietz Gmbh & Co. Kg | Contactless pressurizing-gas shaft seal |
US5435574A (en) * | 1986-10-28 | 1995-07-25 | Pacific Wietz Gmbh & Co. Kg | Contactless pressurizing-gas shaft seal |
US4925490A (en) * | 1987-12-28 | 1990-05-15 | Tanken Seiko Kabushiki Kaisha | Mechanical seal using pore-dispersed material, and pore-dispersed cemented carbide and method for manufacturing same |
EP0466076A2 (fr) * | 1990-07-09 | 1992-01-15 | Ebara Corporation | Garniture à bague glissante avec rainures hélicoidales |
EP0470409A1 (fr) * | 1990-07-18 | 1992-02-12 | Ebara Corporation | Garniture mécanique d'étanchéité sans contact |
US5664787A (en) * | 1994-03-22 | 1997-09-09 | Nippon Pillar Packing Co., Ltd. | Non-contacting shaft sealing device |
US6046430A (en) * | 1996-09-30 | 2000-04-04 | Surface Technologies Ltd. | Bearing having micropores, and design method therefor |
EP0935086A2 (fr) * | 1998-02-06 | 1999-08-11 | John Crane Inc. | Garniture d'étanchéité lubrifiée au gaz pour faibles vitesses de rotation |
US6341782B1 (en) * | 2000-03-03 | 2002-01-29 | Surface Technologies Ltd | Lubricated seals having micropores |
Non-Patent Citations (1)
Title |
---|
ETSION I ET AL: "A MODEL FOR MECHANICAL SEALS WITH REGULAR MICROSURFACE STRUCTURE", TRIBOLOGY TRANSACTIONS, THE SOCIETY, PARK RIDGE, IL,, US, vol. 3, no. 39, July 1996 (1996-07-01), pages 677 - 683, XP001094562, ISSN: 1040-2004 * |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2006070205A1 (fr) * | 2004-12-30 | 2006-07-06 | Aes Engineering Limited | Joint rotatif |
GB2436778A (en) * | 2004-12-30 | 2007-10-03 | Aes Eng Ltd | Rotary seal |
GB2436778B (en) * | 2004-12-30 | 2009-06-03 | Aes Eng Ltd | Rotary seal |
CN103470762A (zh) * | 2013-08-20 | 2013-12-25 | 浙江工业大学 | 倾斜渐变多孔端面非接触式机械密封结构 |
US10337619B2 (en) | 2013-08-27 | 2019-07-02 | Eaton Intelligent Power Limited | Seal ring composite for improved hydrodynamic seal performance |
WO2015031474A1 (fr) * | 2013-08-27 | 2015-03-05 | Eaton Corporation | Composite pour bague d'étanchéité permettant une meilleure étanchéité hydrodynamique |
CN107269705A (zh) * | 2013-09-18 | 2017-10-20 | 伊格尔工业股份有限公司 | 滑动部件 |
US9970478B2 (en) | 2013-09-18 | 2018-05-15 | Eagle Industry Co., Ltd. | Sliding parts |
EP3284982B1 (fr) * | 2013-09-18 | 2024-03-20 | Eagle Industry Co., Ltd. | Composant coulissant |
JP2017166701A (ja) * | 2013-09-18 | 2017-09-21 | イーグル工業株式会社 | しゅう動部品 |
WO2015041048A1 (fr) * | 2013-09-18 | 2015-03-26 | イーグル工業株式会社 | Composant coulissant |
US9829043B2 (en) | 2013-09-18 | 2017-11-28 | Eagle Industry Co., Ltd. | Sliding parts |
US9915289B2 (en) | 2013-09-18 | 2018-03-13 | Eagle Industry Co., Ltd. | Sliding parts |
JPWO2015041048A1 (ja) * | 2013-09-18 | 2017-03-02 | イーグル工業株式会社 | しゅう動部品 |
CN104154235A (zh) * | 2014-05-07 | 2014-11-19 | 清华大学 | 螺旋分布收敛型微孔织构机械密封 |
US9714712B2 (en) | 2014-08-15 | 2017-07-25 | Eaton Corporation | Hydrodynamic mating ring with integrated groove inlet pressure control |
US11125334B2 (en) | 2016-12-21 | 2021-09-21 | Eaton Intelligent Power Limited | Hydrodynamic sealing component and assembly |
EP3627011A4 (fr) * | 2017-05-19 | 2021-01-20 | Eagle Industry Co., Ltd. | Composant coulissant |
US11053975B2 (en) | 2017-05-19 | 2021-07-06 | Eagle Industry Co., Ltd | Sliding component |
US11248707B2 (en) | 2017-05-19 | 2022-02-15 | Eagle Industry Co., Ltd | Sliding component |
US11035411B2 (en) | 2017-07-14 | 2021-06-15 | Eagle Industry Co., Ltd. | Sliding parts |
US11708911B2 (en) | 2017-10-03 | 2023-07-25 | Eagle Industry Co., Ltd. | Sliding component |
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