GB2210939A - Flexible ring seal - Google Patents

Flexible ring seal Download PDF

Info

Publication number
GB2210939A
GB2210939A GB8823989A GB8823989A GB2210939A GB 2210939 A GB2210939 A GB 2210939A GB 8823989 A GB8823989 A GB 8823989A GB 8823989 A GB8823989 A GB 8823989A GB 2210939 A GB2210939 A GB 2210939A
Authority
GB
United Kingdom
Prior art keywords
strip
ring seal
flexible ring
coiled
envelope
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
GB8823989A
Other versions
GB8823989D0 (en
GB2210939B (en
Inventor
Terence Peter Nicholson
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.)
Specialist Sealing Ltd
Original Assignee
Specialist Sealing 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 Specialist Sealing Ltd filed Critical Specialist Sealing Ltd
Publication of GB8823989D0 publication Critical patent/GB8823989D0/en
Publication of GB2210939A publication Critical patent/GB2210939A/en
Application granted granted Critical
Publication of GB2210939B publication Critical patent/GB2210939B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/06Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/10Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
    • F16J15/12Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering
    • F16J15/121Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal reinforcement
    • F16J15/125Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal reinforcement generally perpendicular to the surfaces
    • 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
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/021Sealings between relatively-stationary surfaces with elastic packing
    • F16J15/022Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material
    • 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
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L23/00Flanged joints
    • F16L23/16Flanged joints characterised by the sealing means
    • F16L23/18Flanged joints characterised by the sealing means the sealing means being rings
    • F16L23/20Flanged joints characterised by the sealing means the sealing means being rings made exclusively of metal

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Gasket Seals (AREA)

Abstract

A flexible ring seal particularly intended for sealing the joints between the flanges of glass-lined pressure vessels and their associated piping systems comprises a coiled strip (1, 2) of flexible material which is enclosed within an envelope (5) of low friction co-efficient inert material such as PTFE. The strip has at least one transverse convolution and side margins of increased thickness such that in the coiled structure the adjacent convoluted parts are separated by air spaces. Further, there is preferably provided a closure ring (6) which faces the radially innermost coil of the coiled structure to prevent accidental entry of the envelope into a groove which is formed by a convolution. The strip may be made of stainless steel or any other ferrous or non-ferrous metal or alloy preferably capable of imparting resilience to the strip. Alternatively the coiled strip may be made of synthetic plastics or elastomeric material which may have an embedded metal reinforcing strip.

Description

FLEXBLE RING SEAL" This invention relates to a flexible ring seal which has been specifically but not exclusively devised for sealing the joints between the flanges of glass lined pressure vessels and their associated piping systems The need for a flexible ring seal arises because after gloss powder has been sprayed on these pressure vessels and their ancillary equipment a great deal of distortion occurs when the glass is fused and becomes an integral part of the vessel and/or equipment Consequently the space to be sealed between the flange connections varies considerably in thickness and a successful seal nust be able to adjust to the variation Currently used ring seals are unsatisfactory.
@irstly, in view of lack of flexibility it is most difficult to obtain an efficient sealing fit, and to achieve this many man-hours of work may be needed which is extremely expensive. Secondly the known ring seals constitute a health hazard because asbestos is extensively used in their construction In particular, asbestos millboard, which is one of the most dangerous forms of asbestos is a commonly used ingredient The general ob e ct of the invention is to provide a more flexible and efficient ring seal for this and other similar sealing purposes and also one which is safe and easy to manufacture.
In accordance with the invention a flexible ring seal comprises a coiled strip of flexible arterial enclosed within an envelope ntade of an inert material having a low friction co-efficient, the strip having at least one transverse convolution and side margins of increased thickness such that in the coiled structure the adjacent convoluted parts are separated by air spaces.
The strip may be made of stainless steel or any other ferrous or non-ferrous metal or alloy preferably capable of imparting resilience to the strip. The convoluted base strip may comprise layers laminated together.
Alternatively the coiled strip may be made of synthetic plastics or elastoineric material which may have an embedded metal reinforcing strip.
Also, for the purpose of preventing possible entrance under pressure of part of the envelope into the groove formed by the convoluted part of an adjacent coil of the strip, the ring seal may further comprise a groove closure ring.
Some embodiments of the invention are hereinafter described by reference to the accompanying drawings in which: Fig. 1 is a cross-section of a irietal-fabricated strip preparatory to coiling; Fig. 2, analogous to Fig. 1, illustrates an alternative profile strip; Fig. 3 is a radial cross-section of the train part of a ring seal utilising the strip shown in Fig. 2; Fig. 4 is a fragmentary radial cross-section of a complete ring seal utilising the strip shown in Fig. 1; Figs. 5, 6 and 7 are cross-sections of three typical groove closure rings; Figs 8 and 9 are fragmentary radial cros s-sections of two other ring seal embodiments;; Figs. 10 and 11 are radial cross-sections Of the coiled strip forming the main part of two other ring seal embodiments Fig 12 is a fragmentary plan view of a ring seal; and' Fig 13 is a cross s section, analogous to Fig. 1, illustrating a further strip profile The ring seals according to the invention which are to be described coinpr ise a coiled strip structure which is enclosed in an envelope made of PTFE . When this structure is made ol metal it comprises, as shown in Fig, 1 or Fig. 2, an assembly of three metal strips namely two rectangular section strips 1 made of solid drawn metal (wire) and a roll-forried strip 2 of uniforri thickness, which is thin in relation to its width and formed centrally with at least one arch-shaped convolution 11 (a single convolution being illustrated) . t opposite sides of the central convolution 11 are respective plane flanges 12, lying in a common plane, with the convoluted intermediate region lying entirely on one side of this plane.
As this formed strip 2 leaves the rolling machine it is fed through two guide rollers onto which the two wires 1 are fed accurately onto positions in contact with the respecttive side flanges 12, with the outside edges of the rectangular wires aligned with the outside edges of the flanges. The wires are secured to the flanges by resistance welds 3 at regular intervals, for example 10 millinieters These wires form side niargins for the strip, of increased thickness. The convolution 11 and margins are of substantially equal height in the illustrated strips.
As the coiripound strip leaves the machine, globules of brazing paste 4 are deposited in the corners between the convolution of the strip 2 and the wires 1.
After the colnpcrundd strip leaves the machine, having been welded and "pasted" it is fed onto the mandrel of a coiling machine and wound upon it, the end of the strip being welded at both sides to the coil when a first coi ] has been established. The mandrel is then expanded so as to grip the coiled strip firmly, whereupon further coiling occurs, the inside diameter of the ring being controlled by the diameter of the mandrel, until the desired outside diameter is attained.
The strip 1, 2 is Argon-arc welded at the intended final point of contact between the strip and its last wound coil and is severed from the coil structure which is then removed from the mandrel and transferred to a high temperature furnace which is characterised by vacuum and an inert atmosphere. This causes the brazing paste to become liquid and to flow by capillary action to forni a continuous brazed fillet along the junction between the innermost sides of the wires 1 and the convolution of the strip 2.
However, to improve the flexibility of the structure, especially when the ring sisal will be required to operate in extremely severe environmental conditions it is preferable before the structure is brazed at high temperature -- to apply an adhesive, preferably by roller, to both end faces of the ring, whereafter the ring is lowered into a fluidized bed of brazing powder and then brazed at high temperature.
This results in d complete, integral, flexible metal 5 tru c ture Another expedient which niay be employed to increase flexibility is to form perforations spaced along the strip prior to form rolling, these perforations preferably having the form of slots which are elongated transversely across the strip.Typically for a strip which is 9.83 mm wide, the slots measure 1.57 nim by 6.6 itiin, the interval between adjacent sides of the slots being 1.57 mm. Also greater flexibility can be achieved if the strip 2 is of laminated formation and formed preferably of three, four or five equal thickness layers After the coil has cooled and has been removed from the furnace, it is highly lapped to remove any nodules of brazing snaterial and the inner start and outer finish of the coil are dressed to meet final specification requirements.
In figs. 1 and 2 typical dimensions of the wires 1 and the strip 2 are indicated for two compound strips whereof the central convolutions are somewhat i'iffere-ntly shaped, different radii A, B and C being indieated, Fig. 3 illustrates the coiled structure which is formed by coiling the compound strip which is formed as shown in Fig. 2.
The coiled structure is enclosed within an envelope 5 made of inert low friction co-efficient Inaterial such as PTFE, This envelope may be made either from a ring which has been slit radially inwards or two rings fused or bonded together at its inside diameter, as shown in Fig. 4, or it may be milled instead of slit as shown in Figs. 8 and 9. Slit envelopes are usually used for lower pressure applications, and milled envelopes for higher pressure ones.
Whichever envelope 5 is used, and although it is unnecessary from the operational point of view, it is desirable to fit, around the inside diameter of the coiled structure, a closure ring 6 as shown for instance in Fig. 4. This ring 6 may typically be dimensioned and have one annular rib 6A as also shown in Fig. 5 or Fig.
6 or it may alternatively be shaped as shown in Fig. 7) which again shows typical relative dimensions, or Fig. 9 and have two annular ribs 6A which face the grooves of the innermost coil.
Note that Fig. 9 shows a strip with three convolutions 11, all lying on the same side of the plane of the flanges 12 and not exceeding the height of the margins 1 when relaxed.
The purpose of the closure ring 6 is to prevent any possibility of the envelope 5 being forced under pressure into the adjacent groove or grooves formed by the or each convolution with a consequent risk of splitting of the envelope.
Suitable alloys which can be employed in the fabrication of the coiled structures described above are for instance, the Niinonic and Inconel alloys, Waspalloy, Hastelloy and similar other alloys of which the resilience characteristic can be greatly enhanced by an ageing process.
If desired, there may be welded to one face of the ring seal one or more radial metal tabs 7 (Fig. 12) conveniently there are four such tabs equally spaced around the outer circumference of the ring seal.
The coiled structure need not necessarily wholly consist of metallic material but may instead comprise a coiled transversely convoluted strip of synthetic plastic or elastomeric Inaterial having side margins M of increased thi ckness with adjoining coils adhesively secured to one another and preferably incorporating an embedded metallic reinforcing strip R extending into the thicker margins as illustrated in Figs. 10 and 11.
In cross section the strip may have one or more convolutions, in general an odd number of conuolut: ions as can be seen for example in Ei9urzs. S 1 and 11 Figure 13 shows a further metal ring seal with three convolutions in the strip cross section. Each convolution is semicircular in cross section and the convolutions are nterconnected by straight regions The outermost convolutions are connected to the side flanges by utar joggled or dog-leg regions 10.
Typical dimensions in millimeters are shown, by way of example only, in F i gi)re 13. In this seal the convolutions all lie on one side of the plane of the flanges, but the two outer convolutions are higher than the margins and nest in the convolutions of the adjacent layer of the coil, This seal is made in a manner similar to that described with reference to the seal shown in Figure 1 and is provided with a low-friction envelope as already described.
As a background to the invention it should be mentioned that it is a recognised fact that as the diameter of a flange connection increases so does the di.stortic)n of the flange faces and this increases the problem of obtaining an adequate seal.To cope with this probleni when utilising the metallic mode of construction which has been described with reference to Figs, 1 to 7 inclusive, varations can be made in the width, thickness and other dlrnensions of the roll-formed strip and the wires, as well as in its convoluted shape and in the number of coil turns, Similar considerations apply to the dimensions, shapes and coil turns Of the embodiments which are made of synthetic plastic or elastomeric material and enable the characteristics of the ring seal to be adjusted to aliricist all the requirements of the operational environment, The success of the ring seal derives principally from the air 5 pace which is available between the or each convolution and the adjacent parts of the coil and it is the availability of this space which allows the ring seal when under compression to conform with the utmost flexibility to the changing dimension between the flanges to be sealed.In this connection it should be realised that the ring seal does not act in the same manner as a block of inert cellular material which can readily be compressed In fact it is a very complex resilient structure such that under compression the convolutions become flat and this has the effect of forcibly increasing the diameter of the apex of each of the convoiutions. However this compressing effect is resisted by the natural hoop strength Of the material w,ith the consequence that when the compression node is re ] eased it tennis to return very closely to its original dimension In addition to the hoop strength which is inherent in the convolutions there is also a double parabolic spring effect ori either side of the cipex Of each convolution which also reacts to the compress ion mode, thereby ensuring that the low friction co-efficient material (PTFE) is forced into the mating faces to guarantee a perfect seal. This is of critical importance when the ring seal is to be used in highly corrosive env irotTilents

Claims (14)

  1. CLAIMS 1. A flexible ring seal comprising a coiled strip of flexible material enclosed within an envelope of low friction inert material, the strip having at least one transverse convolution and side margins of increased thickness such that in the coiled structure the adjacent convoluted parts are separated by air spaces.
  2. 2 A flexible ring 5 eal as claimed in Claim 1 in which the coiled strip coiriprises a uniform thickness Inetal base strip having at least one transverse convolution and metallic wires attached by welding at each 5 ide of the convolutions to form said increased thickness side margins
  3. 3. A flexible ring seal as claimed in Claims 2 in which the base strip is comprised of layers which are laniinated together.
  4. 4. A flexible ring seal as claimed in any of Claims 1 to 3 in which the strip is formed with perforations along its length
  5. 5. A flexible ring seal as claimed in Claim 4 in which the perforations are slots which are extended transversely of the strip..
  6. 6. A flexible ring seal as claimed in Claim 1 in which the strip is made of synthetic plastic or elastomeric material.
  7. 7. A flexible ring seal as claimed in Claim 6 in which the synthetic plastic or elastomeric material is reinforced by a metal strip embedded therein,
  8. 8. 4 flexible ring seal in accordance with any of Claims 1 to 7 including a groove closure ring which is located radially inwardly of the radially inneflriost coil of the strip.
  9. 9. A flexible ring seal in accordance with any of Claims 1 to 8 in which the envelope of low friction inert material is initially radially slit inwards or formed of two rings which are bonded or fused together at its inside diameter.
  10. 10. A flexible ring seal in accordance with any of Claims 1 to 8 in which the envelope is fornied by milling prior to fitting around the coiled structure.
  11. ii, A flexible metal seal in accordance with any of Claims 1 to 5 wherein metal tabs are welded to the outer edge of the coiled structure and extend radially thereof.
  12. 12 A flexible ring seal coniprised of a coiled metallic structure substantially as hereinbefore described with reference to, and as shown in, any of Figs 1 to 9 and Fig. 12 of the accompanying drawings
  13. 13 g flexible ring seal coniprised of a coiled structure made of synthetic plastic or elastomeric material substantially as hereinbefore described with reference to, and as shown in, Figs. 10 and 11 of the accompanying drawings.
  14. 14. A flexible ring seal comprising a coiled metallic structure enclosed within an envelope of low friction innert material, substantially as described with reference to Figure e 13 15 of the accompanying drawl rigs
GB8823989A 1987-10-13 1988-10-13 Flexible ring seal Expired - Fee Related GB2210939B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB878724010A GB8724010D0 (en) 1987-10-13 1987-10-13 Flexible ring seal

Publications (3)

Publication Number Publication Date
GB8823989D0 GB8823989D0 (en) 1988-11-23
GB2210939A true GB2210939A (en) 1989-06-21
GB2210939B GB2210939B (en) 1991-05-01

Family

ID=10625245

Family Applications (2)

Application Number Title Priority Date Filing Date
GB878724010A Pending GB8724010D0 (en) 1987-10-13 1987-10-13 Flexible ring seal
GB8823989A Expired - Fee Related GB2210939B (en) 1987-10-13 1988-10-13 Flexible ring seal

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB878724010A Pending GB8724010D0 (en) 1987-10-13 1987-10-13 Flexible ring seal

Country Status (3)

Country Link
CA (1) CA1337823C (en)
GB (2) GB8724010D0 (en)
WO (1) WO1989003491A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2246822A (en) * 1990-08-06 1992-02-12 Specialist Sealing Ltd Static seal
US5558347A (en) * 1990-12-31 1996-09-24 Specialist Sealing Limited Seal
EP2264338A1 (en) * 2009-06-18 2010-12-22 Rolls-Royce PLC A compliant element

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992012365A1 (en) * 1990-12-31 1992-07-23 Specialist Sealing Limited Seal

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1350380A (en) * 1970-07-17 1974-04-18 Corrugated Packing Sheet Metal Sealing ring
DE2618804C3 (en) * 1976-04-29 1978-11-23 Kempchen & Co Gmbh, 4200 Oberhausen All-metal seal
DE3149753C2 (en) * 1981-12-16 1983-12-01 Kempchen & Co Gmbh, 4200 Oberhausen Sealing ring for flange seals
GB2185295B (en) * 1986-01-15 1989-01-05 Chemical Reactor Services Ltd Gaskets

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2246822A (en) * 1990-08-06 1992-02-12 Specialist Sealing Ltd Static seal
US5195759A (en) * 1990-08-06 1993-03-23 Specialist Sealing Ltd. Static seal
GB2246822B (en) * 1990-08-06 1994-03-30 Specialist Sealing Ltd Static seal
US5558347A (en) * 1990-12-31 1996-09-24 Specialist Sealing Limited Seal
EP2264338A1 (en) * 2009-06-18 2010-12-22 Rolls-Royce PLC A compliant element
US8950751B2 (en) 2009-06-18 2015-02-10 Rolls-Royce Plc Compliant element

Also Published As

Publication number Publication date
WO1989003491A1 (en) 1989-04-20
GB8823989D0 (en) 1988-11-23
CA1337823C (en) 1995-12-26
GB8724010D0 (en) 1987-11-18
GB2210939B (en) 1991-05-01

Similar Documents

Publication Publication Date Title
US4189819A (en) Method of manufacturing metallic spirally wound gaskets
CA1127566A (en) Wire-reinforced hose and method of making same
US5082296A (en) Spiral wound gasket and fabrication method thereof
US20050139280A1 (en) Composite pressure pipe
GB2075616A (en) Annular gasket
US5634254A (en) Method for manufacturing swaging rings
US5913522A (en) Spirally-bound flange seal with separate soft layers
CA1337823C (en) Flexible ring seal
US6619668B1 (en) Static metal gasket and method of manufacturing it
EP0472324B1 (en) Static seal
US4127277A (en) Spiral wound gasket assembly and method
US4640455A (en) Method of making a metal seal for flanged joints and a seal made by said method
EP0992719B1 (en) Filler material for spiral wound gasket and spiral wound gasket
US4677839A (en) Apparatus for shaping a spiral catalyst support
JP2006515049A (en) Sealed joint with plate-like internal structure for use at very high temperatures
EP0122260B1 (en) High pressure bellows capsule and method of making same
JPH06294482A (en) Pressure tube
US20040089360A1 (en) Flexible metal hose assembly and method of making the same
US2442311A (en) Composite compressible gasket
JPH08219291A (en) Metal covered gasket
JPS6199772A (en) Composite seal material for vacuum devices
DE2910802A1 (en) FLEXIBLE COATING FOR PIPES AND THE LIKE
JPS61153084A (en) Ceramic lining hose
GB2316720A (en) Gasket
JPH05215242A (en) Static seal

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19971013