GB2196706A - Sealing devices - Google Patents
Sealing devices Download PDFInfo
- Publication number
- GB2196706A GB2196706A GB08625908A GB8625908A GB2196706A GB 2196706 A GB2196706 A GB 2196706A GB 08625908 A GB08625908 A GB 08625908A GB 8625908 A GB8625908 A GB 8625908A GB 2196706 A GB2196706 A GB 2196706A
- Authority
- GB
- United Kingdom
- Prior art keywords
- seal
- sealing device
- annular metallic
- circumferential portion
- metal
- 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.)
- Withdrawn
Links
- 238000007789 sealing Methods 0.000 title claims abstract description 36
- 239000002184 metal Substances 0.000 claims description 9
- 229910001026 inconel Inorganic materials 0.000 claims description 4
- 238000009987 spinning Methods 0.000 claims description 3
- 230000015556 catabolic process Effects 0.000 description 2
- 238000006731 degradation reaction Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
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
- F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
- F16J15/3284—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Gasket Seals (AREA)
Abstract
A sealing device for providing a seal between a concentric outer member (1) and inner member (3) which slides in a bore in the outer member e.g. a reactor standpipe in a nuclear fuelling maching, comprises an annular metallic seal (15) having a flat annular part (17) which is clamped to the outer member and a curved annular part (19) which forms an interference fit with the outer surface of the inner member and is held in engagement with that surface by tensile hoop stress in the seal. <IMAGE>
Description
SPECIFICATION
Sealing devices
This invention relates to sealing devices. In particular the invention relates to sealing devices capable of providing a gas tight seal between two concentric components.
Such a seal is required for example in a nuclear fuelling machine, a nose portion of which must slide onto and seal onto a reactor standpipe during refuelling operations. The sealing device used to provide this seal must be capable of operating at high ambient temperatures, high ionising radiation levels, and high reactor gas pressures, and furthermore must be capable of being coupled and uncoupled many thousand times without degradation of the sealing performance or degradation of the surfaces of the mating components. A sealing device which has been used for many years for this purpose comprises an elastomeric O-ring- seal backed by a circular section metal O-ring, this metal O-ring limiting the leak rate from the nose unit in the event of failure of the primary elastomeric O-ring seal.As the safety requirements of such nuclear fuelling machines have increased over the years, it has been found that the reactor gas leakage rates from such a known sealing device are too high.
It is an object of the present invention to provide a sealing device suitable for use in a nuclear fuelling machine, which has a lower leakage rate than previously used sealing devices.
According to the present invention a sealing device includes an annular metallic seal, a first circumferential portion of the seal being substantially planar, and the other circumferential portion of the seal being curved out of the plane of the first portion such that the other portion operates as an interference fit garter on a component to be sealed by the device.
One sealing device in accordance with the invention will now be described, by way of example only, with reference to the accompanying drawings in which:
Figure 1 is a schematic diagram of the sealing device in use in a nuclear fuelling machine, only part of the machine being shown.
Figure 2 is a section through a component of the sealing device, the component being shown on a different scale to that of Fig. 1, and
Figure 3 shows a detail of the component shown in Fig. 2 on a increased scale.
Referring firstly to Fig. 1, the sealing device is designed to seal a nose unit 1 carried on the lower end of a nuclear fuelling machine onto a nuclear reactor standpipe 3, this nose unit 1 sliding and sealing onto the standpipe 3 during refuelling operations. The sealing device comprises upper 5 and lower 7 annular housings, these being bolted onto the nose unit 1 of the fuelling machine by high temperature bolts 9, there typically being six or more such bolts positioned round the nose unit 1. A proprietory static metal C-ring 11 provides a static seal between the upper housing 5 and the nose unit 1.The upper housing 5 carries an elastomeric O-ring 13, which in use of the sealing device provides a primary seal between the nose unit 1 and the standpipe 3 for operation up to 300"C. Clamped between the upper 5 and lower 7 housings there is provided a metal garter seal 15 whose form is described in more detail hereafter, this seal 15 constituting a back-up seal between the nose unit 1 and standpipe 3 in the event of failure of the primary seal 13 due to for example fault conditions in which the ambient temperature of the sealing device may reach 600"C. A further metal C-ring 16 is provided between the seal 15 and upper housing 5 to close the secondary leak path between these components.
Turning now also to Figs. 2 and 3, the seal 15 comprises a ring of age hardened Inconel (RTM) 718. The outer portion 17 of the ring is substantially planar, such that in use of the seal 15, this portion may readily be clamped between the upper and lower housings 5, 7.
The inner portion 19 of the ring is smoothly curved out of the plane of the portion 17, such that in use of the seal the portion 19 of the ring operates as an interference fit garter on the standpipe 3. The seal 15 will typically be formed by cold spinning in several stages from an annealed sheet of Inconel (RTM) 718, the seal ring thus formed being subsequently heat treated so as to anneal the ring and finally age harden it.
Using a small amount of grease to lubricate standpipe 3 prior to each engagement by the nose unit 1 of the fuelling machine, it is found that repeated engagement and disengagement of the standpipe 3 and the nose unit 1 causes the surface finish of the standpipe to improve due to the burnishing/polishing action of the seal 15, the seal 15 is being found to operate satisfactorily with the slightest trace of lubricant.
During fault conditions such as reverse flow gas leading to construction of the O-ring 13 constituting the primary seal, the back-up seal 15 has been found to be able to withstand the thermal movements of the standpipe 3 and the nose unit 1. Under these conditions an adequate seal is maintained at ambient temperatures up to 600"C, reactor gas pressures of 600psig being held in intense ionising radiation fields.
It will be appreciated that whilst the sealing device described herebefore by way of example uses the seal 15 as a back up seal, in some applications a sealing device in accordance with the invention may use such an annular metallic seal as a primary seal at pressures up to 1500psig.
It will also be appreciated that the curved portion of such a seal which in use operates as an interference fit garter may be on the inner or the outer circumferential portion of the seal.
It will also be appreciated that a sealing device in accordance with the invention may be used to provide a seal to components of other than circular cross section, for example components of oval cross section the annular metallic seal deflecting to accomodate such a component, the seal being resilient enough to maintain its sealing properties.
Claims (5)
1. A sealing device including an annular metallic seal, a first circumferential portion of the seal being substantially planar, and the other circumferential portion of the seal being curved out of the plane of the first portion such that the other portion operates as an interference fit garter on a component to be sealed by the device.
2. A sealing device according to Claim 1 in which the annular metallic seal forms a backup seal, the primary seal being constituted by an elastomeric O-ring.
3. A sealing device according to either of the preceding Claims in which said first circumferential portion is the outer circumferential portion.
4. A sealing device according to any one of the preceding Claims in which the annular metallic seal is formed by a cold spinning process from an annealled sheet of metal.
5. A sealing device substantially as hereinbefore described with reference to the accompanying drawings.
5. A sealing device according to Claim 4 in which said metal is Inconel (RTM).
6. A sealing device substantially as hereinbefore described with reference to the accompanying drawings.
CLAIMS
Ammendments to the claims have been filed, and have the following effect:
Claims 1 to 6 above have been deleted or textually amended.
New or textually amended claims have been filed as follows:
1. A sealing device to provide a seal between an outer member having a bore therein and an Inner member which can slide within the bore, the sealing device comprising an annular metallic seal having a first circumferential portion which is substantially planar and is arranged for attachment to the outer member; and a second circumferential portion which is curved out of the plane of the first portion towards the centre of the annulus such that the second portion operates as a garter which is an interference fit round the inner member.
2. A sealing device according to Claim 1, in which the annular metallic seal is formed from an annealed sheet of metal by a cold spinning process.
3. A sealing device according to Claim 2, in which the metal is Inconel (registered Trade
Mark).
4. A sealing device according to any preceding claim, in which the annular metallic seal forms a back-up seal, and a primary seal is constituted by an elastomeric O-ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08625908A GB2196706A (en) | 1986-10-29 | 1986-10-29 | Sealing devices |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08625908A GB2196706A (en) | 1986-10-29 | 1986-10-29 | Sealing devices |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB8625908D0 GB8625908D0 (en) | 1986-12-03 |
| GB2196706A true GB2196706A (en) | 1988-05-05 |
Family
ID=10606510
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08625908A Withdrawn GB2196706A (en) | 1986-10-29 | 1986-10-29 | Sealing devices |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2196706A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0441015A1 (en) * | 1990-02-07 | 1991-08-14 | Cooper Industries, Inc. | Annular sealing apparatus |
| FR2755040A1 (en) * | 1996-10-31 | 1998-04-30 | Aerospatiale | METHOD OF MANUFACTURING BY COLD FLUOTURNING AN INCONEL 718 ALLOY PART |
| EP2971880A4 (en) * | 2013-03-15 | 2016-11-30 | Little Engine Llc | WEAR-RESISTANT COMBINED SEAL |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB899552A (en) * | 1958-04-05 | 1962-06-27 | Goetzewerke | Gasket |
| GB957720A (en) * | 1959-06-23 | 1964-05-13 | Siemens Ag | Improvements in or relating to releasable fluid-tight joints |
| GB982975A (en) * | 1960-04-06 | 1965-02-10 | Geartight Unions Ltd | Improvements in or relating to sealing means |
| GB1436753A (en) * | 1972-05-26 | 1976-05-26 | Atomenergi Ab | Seal for pressure vessels |
| GB2065796A (en) * | 1979-12-18 | 1981-07-01 | Mtu Friedrichshafen Gmbh | Sealing element |
| GB2145482A (en) * | 1983-08-22 | 1985-03-27 | Heat Transfer Technology | Sealing joints between consenting member |
-
1986
- 1986-10-29 GB GB08625908A patent/GB2196706A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB899552A (en) * | 1958-04-05 | 1962-06-27 | Goetzewerke | Gasket |
| GB957720A (en) * | 1959-06-23 | 1964-05-13 | Siemens Ag | Improvements in or relating to releasable fluid-tight joints |
| GB982975A (en) * | 1960-04-06 | 1965-02-10 | Geartight Unions Ltd | Improvements in or relating to sealing means |
| GB1436753A (en) * | 1972-05-26 | 1976-05-26 | Atomenergi Ab | Seal for pressure vessels |
| GB2065796A (en) * | 1979-12-18 | 1981-07-01 | Mtu Friedrichshafen Gmbh | Sealing element |
| GB2145482A (en) * | 1983-08-22 | 1985-03-27 | Heat Transfer Technology | Sealing joints between consenting member |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0441015A1 (en) * | 1990-02-07 | 1991-08-14 | Cooper Industries, Inc. | Annular sealing apparatus |
| US5066029A (en) * | 1990-02-07 | 1991-11-19 | Cooper Industries, Inc. | Annular sealing apparatus |
| FR2755040A1 (en) * | 1996-10-31 | 1998-04-30 | Aerospatiale | METHOD OF MANUFACTURING BY COLD FLUOTURNING AN INCONEL 718 ALLOY PART |
| EP0841107A1 (en) * | 1996-10-31 | 1998-05-13 | AEROSPATIALE Société Nationale Industrielle | Process for manufacturing by cold spinning a workpiece made of inconel 718 alloy |
| EP2971880A4 (en) * | 2013-03-15 | 2016-11-30 | Little Engine Llc | WEAR-RESISTANT COMBINED SEAL |
Also Published As
| Publication number | Publication date |
|---|---|
| GB8625908D0 (en) | 1986-12-03 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |