GB2528836A - Mechanical seal control mechanism - Google Patents

Mechanical seal control mechanism Download PDF

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Publication number
GB2528836A
GB2528836A GB1411427.6A GB201411427A GB2528836A GB 2528836 A GB2528836 A GB 2528836A GB 201411427 A GB201411427 A GB 201411427A GB 2528836 A GB2528836 A GB 2528836A
Authority
GB
United Kingdom
Prior art keywords
seal
floating
face
longitudinally
heat
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.)
Granted
Application number
GB1411427.6A
Other versions
GB2528836B (en
GB201411427D0 (en
Inventor
Carl-Eiler Rodgrigues
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AES Engineering Ltd
Original Assignee
AES Engineering Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by AES Engineering Ltd filed Critical AES Engineering Ltd
Priority to GB1411427.6A priority Critical patent/GB2528836B/en
Publication of GB201411427D0 publication Critical patent/GB201411427D0/en
Priority to US14/743,031 priority patent/US20150377359A1/en
Publication of GB2528836A publication Critical patent/GB2528836A/en
Application granted granted Critical
Publication of GB2528836B publication Critical patent/GB2528836B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/34Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/3436Pressing means
    • F16J15/346Pressing means the pressing force varying during operation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/10Shaft sealings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/10Shaft sealings
    • F04D29/12Shaft sealings using sealing-rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/34Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/3436Pressing means
    • F16J15/3452Pressing means the pressing force resulting from the action of a spring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/34Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/3496Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member use of special materials

Abstract

A mechanical seal control mechanism is provided. The mechanical seal comprises: one or more seal faces under axial contact through a spring biasing means (12 in Figure 1); a longitudinally floating first member (7 in Figure 1); a longitudinally non-floating member (3 in Figure 1); a longitudinally floating seal face (9 in Figure 1); an a longitudinally non-floating second seal face (10 in Figure 1). The seal includes a thermally responsive element 14, which reduces or negates face contact pressure at the sealing interface 13 when heat is generated within the seal above a predetermined temperature. The thermally responsive element may take the form of a bimetal 14 or a shape memory alloy spring (17 in Figure 6).

Description

MECHANICAL SEAL CONTROL MECHANISM
Field of the Invention
The present invention relates to a mechanical seal control mechanism and particularly to the use of a smart material with the ability to convert temperature S change into a reduction in face contact pressure within a mechanical seal in the undesired operating condition commonly referred to as dry running".
Background to the Invention
A mechanical seal generally comprises a rotating member attached to the pump shaft and a stationary member attached to the pump housing. The rotating member is in relative contact with the stationary member, which provides the seal. Both the rotating member and the stationary member are commonly referred to in the mechanical sealing industry as seal faces'. A basic operating principle of mechanical seals is that the seal faces require a fluid film' that provides a lubricant between them in order to function correctly.
The operating condition of dry running" occurs between the seal faces when a fluid film' is not present to lubricate them. This results in the faces being in direct contact while in operation and thus generating heat. This heat can cause the faces to wear and the contacting elastomers to distort and melt, in turn causing the mechanical seal to fail.
Reducing face contact pressure or friction between the rotary and stationary faces during periods of dry running can reduce heat generation, face wear and elastomer damage.
Current solutions include; Polycrystalline Diamond Coatings adhered to the faces with the aim to reduce face contact wear by increasing hardness.
Amorphous Diamond-Like Coatings adhered to the faces with the aim to reduce face temperature through decreased friction.
Dual seals providing a "stable" lubrication from a dedicated system, and do not rely on the process fluid, however they can still falter through the system fluid finishing or the system being inadvertently shut off.
Problems still exist with these solutions including; cost, reliability and application limitations.
Statements of the Invention
The present invention relates to a device whereby the face contact pressure caused by the spring pressure is negated by the force produced when the thermally activated Smart Material shape is altered.
The aforementioned "Smart Material" may comprise a Bimetal, Shape Memory Alloy (for example Nitinol) or Shape Memory Polymer. Additionally, the smart material may comprise a combination of one or more those items. A "smart material" is intended to be a shape-memory material that is sensitive to thermal changes such that it increases or decreases in size and/or shape when subjected to a change in temperature. Preferably, the change is a two-way change, although it may be desirable to employ a one-way shape-change material in certain circumstances. The advantage of a two-way change is that where the material has changed shape upon heating to reduce the face contact pressure, upon the system cooling, the pressure can be increased to retain the integrity of the seal.
A problem is addressed by distinguishing the condition of dry running from normal operating conditions and implementing a mechanical system able to reduce or eliminate face pressure through separation of the faces. An advantage of using a smart material to address this problem is that it can be incorporated into an element of the seal mechanism and so have a direct effect on the seal faces. Additionally, it may be possible to retrofit such parts into existing seal mechanisms.
Additionally, when utilising a bimetal or shape memory alloy it can be used within seals operating at differing temperatures by specifying the material to alter shape at the appropriate temperature. This provides an advantage in that the system can be operated at predetermined temperatures to provide a predetermined thermal response.
Brief Description of the Drawings
The accompanying drawings are as follows:-Figure 1 shows a cross sectional side view profile of a typical mechanical seal Figure 2 shows an enlarged cross sectional side view profile of a typical mechanical seal in operational conditions using the first embodiment of a bimetal Figure 3 shows an enlarged cross sectional side view profile of a typical mechanical seal in dry running conditions using the first embodiment of a bimetal Figure 4 shows an enlarged cross sectional side view profile of a typical mechanical seal in operational conditions using the second embodiment of a bimetal Figure 5 shows an enlarged cross sectional side view profile of a typical mechanical seal in dry running conditions using the second embodiment of a bimetal Figure 6 shows an enlarged cross sectional side view profile of a typical mechanical seal in operational conditions using an SMA Spring Figure 7 shows an enlarged cross sectional side view profile of a typical mechanical seal in dry running conditions using an SMA Spring
Detailed Description of the Drawings
The invention will now be described by way of examples only, with reference to the accompanying drawings.
Figure 1 shows a cross sectional side view profile of a typical mechanical seal 1, that comprises of a pump housing 2, a longitudinally non floating member the gland 3 which is fixed to said pump housing, the atmosphere 4, a shaft 5 which axially aligns with the said gland, a process fluid 6 contained within the said pump housing, a longitudinally floating second member the shaft sleeve 7 which attaches axially to the said shaft, an elastomeric sealing member a rotary 0-ring 8, a longitudinally floating seal face the rotary 9, a longitudinally non floating seal face the stationary 10, a secondary elastomeric sealing member a stationary 0-ring 11, and a spring biasing means 12.
In operation, the stationary floating seal face 10 is energized by the spring 12 causing the seal face 9 to contact said stationary seal face 10. Between said seal faces 9 and 10 a fluid film of lubrication is provided by the process fluid being pumped 6.
Figure 2 shows an enlarged cross sectional side view profile of a typical mechanical seal in operational conditions with fluid 6, present between the faces 13. It shows the first embodiment using a bimetal 14, and circlip 15 in normal operational conditions.
Figure 3 shows an enlarged cross sectional side view profile of a typical mechanical seal in dry running conditions with no fluid 6, present between the faces 13, causing initial direct contact. It shows the first embodiment using a bimetal 14, and circlip 15 to fit said bimetal. In this condition a reduction in pressure between the seal faces is obtained by negating the spring biasing means through deflection of the disc acting on the stationary seal face, moving the faces away from each other. When faces reach a predetermined temperature, the bimetal deflects. When the faces return to predetermined temperature the bimetal returns to their original shape.
Figure 4 shows an enlarged cross sectional side view profile of a typical mechanical seal in operational conditions with fluid 6, present between the faces 13. It shows the second embodiment of a bimetal 15, altering the location within the seal, acting directly on the face forcing a gap between them.
Figure 5 shows an enlarged cross sectional side view profile of a typical mechanical seal in dry running conditions with no fluid 6, present between the faces 13, causing initial direct contact. It shows the second embodiment of a bimetal 15, the alternative location offers a faster response to temperature changes.
Figure 6 shows an enlarged cross sectional side view profile of a typical mechanical seal in operational conditions with fluid 4. It shows the third embodiment of a Smart Memory Alloy Spring 17 in normal operational conditions.
Figure 7 shows an enlarged cross sectional side view profile of a typical mechanical seal in dry running conditions with no fluid 6, present between the faces 16, causing initial direct contact. It shows the third embodiment of a Smart Memory Alloy Spring 17 in dry running operation conditions where heat is present. A reduction in face pressure is initiated through the heat transfer to the back face and into the spring 17.
On heating the spring contracts, opening the faces 16 and when temperature is normalised the spring extends to normal working lengths. :io

Claims (9)

  1. Claims 1. A mechanical seal comprising of one or more seal faces under axial contact through a spring biasing means, a longitudinally floating first member, a longitudinally non-floating member, a longitudinally floating seal face, a longitudinally non-floating second seal face, and comprises a thermally responsive element, which reduces or negates face contact pressure when heat is generated within the seal above a predetermined temperature threshold.
  2. 2. A device according to claim 1, wherein the said element comprises a Smart Material.
  3. 3. A device according to claim 1 or claim 2, wherein the temperature threshold correlates with the maximum operating temperature of the contacting elastomers.
  4. 4. A device according to any one of claims 1 to 3, wherein the heat is generated through contact between said floating seal face and said second non-floating seal face and that heat is linked to the thermally responsive element.
  5. 5. A device according to any preceding claim, where the thermal response is predetermined to suit the application and, when in use, the thermal response alters the pressure on the one or more seal faces.
  6. 6. A device according to claim 4, wherein heat is generated as a result of direct face contact on the one or more seal faces without lubrication.
  7. 7. A device according to claim 6, wherein, when in use, the heat generated is as a result of misalignment of the one or more seal faces.
  8. 8. A device according to any preceding claim, wherein the face contact is caused through a loss in chamber pressure.
  9. 9. A device according to any preceding claim, wherein the device comprises one or more elements from a group comprising: a spring; disc; wire; sheet; or ring.
GB1411427.6A 2014-06-26 2014-06-26 Mechanical seal control mechanism Active GB2528836B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB1411427.6A GB2528836B (en) 2014-06-26 2014-06-26 Mechanical seal control mechanism
US14/743,031 US20150377359A1 (en) 2014-06-26 2015-06-18 Mechanical seal control apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1411427.6A GB2528836B (en) 2014-06-26 2014-06-26 Mechanical seal control mechanism

Publications (3)

Publication Number Publication Date
GB201411427D0 GB201411427D0 (en) 2014-08-13
GB2528836A true GB2528836A (en) 2016-02-10
GB2528836B GB2528836B (en) 2017-12-27

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB1411427.6A Active GB2528836B (en) 2014-06-26 2014-06-26 Mechanical seal control mechanism

Country Status (2)

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US (1) US20150377359A1 (en)
GB (1) GB2528836B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107420550A (en) * 2017-06-01 2017-12-01 武汉船用机械有限责任公司 A kind of rotary sealing appts

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10232551B2 (en) * 2016-04-15 2019-03-19 Cc3D Llc Head and system for continuously manufacturing composite hollow structure

Citations (5)

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JPS60143276A (en) * 1983-12-29 1985-07-29 Matsushita Electric Ind Co Ltd Mechanical seal device
SU1413342A1 (en) * 1987-01-04 1988-07-30 Всесоюзное Научно-Производственное Объединение Турбохолодильной,Газоперекачивающей И Газотурбинной Техники "Союзтурбогаз" Turbo-machine shaft seal unit
JPH11351149A (en) * 1998-06-09 1999-12-21 Mitsubishi Heavy Ind Ltd Shaft seal device for pump
US20080079222A1 (en) * 2006-09-28 2008-04-03 Gm Global Technology Operations, Inc. Temperature adaptive radial shaft seal assemblies using shape memory alloy elements
FR2985296A1 (en) * 2012-01-04 2013-07-05 Jspm PASSIVE STOP SEALING DEVICE FOR SHAFT JOINT SYSTEM OF PRIMARY MOTOR PUMP GROUP

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US4429854A (en) * 1982-11-26 1984-02-07 Smith International, Inc. Dual squeeze seal gland
US4948151A (en) * 1986-10-10 1990-08-14 Atomic Energy Of Canada Limited Rotary end face seal assembly
US4990054A (en) * 1989-12-13 1991-02-05 Westinghouse Electric Corp. Device incorporating micro-porous membrane for venting gases from seal assembly of a reactor coolant pump
US5024452A (en) * 1990-01-16 1991-06-18 Westinghouse Electric Corp. Reactor coolant pump having thermally stabilized hydrostatic sealing assembly
DK172996B1 (en) * 1997-05-27 1999-11-01 Apv Fluid Handling Horsens As Centrifugal pump with shaft seal
US6428011B1 (en) * 1998-09-16 2002-08-06 Aes Engineering Limited Mechanical seals
JP2003506632A (en) * 1999-08-06 2003-02-18 ルーク ファールツォイク−ヒュドラオリク ゲーエムベーハー ウント コンパニー カーゲー CO2 compressor
FI116803B (en) * 2001-04-27 2006-02-28 Crane John Safematic Oy Device in a mechanical seal
FR2832204B1 (en) * 2001-11-14 2004-04-02 Syegon SEALING RING FOR A FLUID CIRCUIT

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60143276A (en) * 1983-12-29 1985-07-29 Matsushita Electric Ind Co Ltd Mechanical seal device
SU1413342A1 (en) * 1987-01-04 1988-07-30 Всесоюзное Научно-Производственное Объединение Турбохолодильной,Газоперекачивающей И Газотурбинной Техники "Союзтурбогаз" Turbo-machine shaft seal unit
JPH11351149A (en) * 1998-06-09 1999-12-21 Mitsubishi Heavy Ind Ltd Shaft seal device for pump
US20080079222A1 (en) * 2006-09-28 2008-04-03 Gm Global Technology Operations, Inc. Temperature adaptive radial shaft seal assemblies using shape memory alloy elements
FR2985296A1 (en) * 2012-01-04 2013-07-05 Jspm PASSIVE STOP SEALING DEVICE FOR SHAFT JOINT SYSTEM OF PRIMARY MOTOR PUMP GROUP

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107420550A (en) * 2017-06-01 2017-12-01 武汉船用机械有限责任公司 A kind of rotary sealing appts
CN107420550B (en) * 2017-06-01 2019-07-05 武汉船用机械有限责任公司 A kind of rotary sealing appts

Also Published As

Publication number Publication date
GB2528836B (en) 2017-12-27
GB201411427D0 (en) 2014-08-13
US20150377359A1 (en) 2015-12-31

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