GB2188121A - Retaining rings - Google Patents

Retaining rings Download PDF

Info

Publication number
GB2188121A
GB2188121A GB8610557A GB8610557A GB2188121A GB 2188121 A GB2188121 A GB 2188121A GB 8610557 A GB8610557 A GB 8610557A GB 8610557 A GB8610557 A GB 8610557A GB 2188121 A GB2188121 A GB 2188121A
Authority
GB
United Kingdom
Prior art keywords
ring
extending portion
annular
housing
retaining
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Withdrawn
Application number
GB8610557A
Other versions
GB8610557D0 (en
Inventor
John Fredrick Leonard
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of GB8610557D0 publication Critical patent/GB8610557D0/en
Priority to DE19873708949 priority Critical patent/DE3708949A1/en
Priority to FR8703781A priority patent/FR2596115A1/en
Publication of GB2188121A publication Critical patent/GB2188121A/en
Withdrawn legal-status Critical Current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
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/10Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
    • 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
    • F16J15/32Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/3268Mounting of 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
    • F16J15/32Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/3284Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
    • F16J15/3288Filamentary structures, e.g. brush seals

Abstract

In locating an annular ring 14 in an annular housing 10, a retaining ring 16 is provided which has a first radially extending portion 18 and a second axially extending portion 20 which in combination are capable of providing an enhanced retaining force when used in conjunction with a loading means 26, 40. In other embodiments the ring 16 has an L-shape or U-shape cross-section. <IMAGE>

Description

SPECIFICATION Improvements in or relating to retaining means This invention relates to an improved apparatus for locating orsealing and is particularly relevant to the location of annular rings in annular housings.
One well known method of locating annular rings in an annular housing is shown in Figure A, in which a retaining ring is fixedly attached to an extended portion of the housing and is provided with at least one portion which acts to retain the ring in the housing. Such a retaining ring may for example be attached to the housing by for example riveting or bolting. One major disadvantage ofthe above method of retaining isthatlittle or no load can be exerted on the annular ring by the retaining ring in orderto ensure a good location ofthe annular ring in the housing. A further disadvantage is that if the annular ring is ever exchanged for one of a slightly different width, then either spacing washers will be required upon re-assembly or it will be necessary to provide new bolting holes.
An alternative solution to the above mentioned problem is to ruse a bellville washer as shown in Figure B. Such a washer is shaped so that its outer edge is spaced axially from its inner edge. In operation, the washer is used in conjunction with a clamping means of any conventional form such that one edge of the washer acts against the annular ring and the other edge acts againstthe clamping means such that when a clamping load is applied bythe clamping means, the ring is deformed in such a mannerthatthe clamping load is transferred to the annular ring to retain the annular ring in the housing.
This solution, whilst overcoming the disadvantages of the above mentioned solution still suffers from a number of disadvantages.
One disadvantage of the above solution resides in the change of size of the inner and outer diameters of the washer during deformation. During deformation, the inside diametertends to reduce and the outside diametertendsto become larger. Changing inner and outer washer diameters can cause location problems and may result in an uneven load being applied to the annular ring.
Furtherto this, the amount of spring force available from the washer is severely limited by the amount of axial deformation the washer is capable of accommodating before the material is stretched beyond its elastic limit on the outer diameter or the washer is flattened.
An object of the present invention isto provide an appartusfor retaining an annular ring in a housing which reduces and possibly eliminates the disadvantages of the above two mentioned methods.
The present invention will now be particularly described with reference to the accompanying drawings, in which: Figure lisa cross-sectional view of a first type of spring ring shown in its deformed position in a typical installation.
Figure2 is a cross-sectional view of the spring ring shown in Figure 1 in its relaxed position.
Figure 3 is a cross-sectional view of a second shape of spring ring positioned in a second installation.
Figure 4 is a cross-sectional view of a third shape of spring ring positioned in a third installation.
Referringto Figure 1,an annularhousing 10 is provided with a recess 12 into which an annular ring 14 is positioned. The spring ring shown generally at 16 comprises one generally radiallyextending portion 18 and one generally axially extending portion 20. A clamping means, shown generally at 22 comprises a second annular ring 24which is urged into contact with the annular housing 10 by a plurality of nuts 26 and bolts 28 circumferentially spaced around the ring 24 and housing 10. The second ring is provided with a recess at 30 having an end face 32. In operation, the generally radially extending portion 18 of the spring ring 16 is deformed axially whilst the generally axially extending portion 20 is deformed radially to provide a retaining force capable of retaining the annular ring 14 in the housing 10.Deformation of the spring ring 16 is achieved by tightening the nuts and bolts 26,28 such that the end face 32 of the recess acts on the free end 34 of the axially extending portion 20 and hence urges the radially extending portion 18 into contact with the annular ring 14. Furthertightening ofthe nuts and bolts 26,28 will increase the deformation of the spring ring 16 such that the axially extending portion 20 isforced up againstthe radially inwardly facing face 36 of recess 30. Any additional tightening of the nuts and bolts 26,28 will theteafter result in axial deformation of the radially extending portion 18.
In such a deformed position, the spring ring will exert a force F1 on the annular ring 14 and F2 on the second annular ring 24 which in combination act to resist the axial and circumferential movement of the annular ring 14.
It has been found that the addition of the axially extending portion 20 greatly increases the retaining force which is exertable on the annular ring 14for a given axial displacement of the radially extending portion. Further to this, the outside diameter of the spring ring 16 is restrained by the inside diameter of the second ring 24, this aids location of the ring and assists in providing an even retaining force.
Turning now to Figure 2, it will be seen that when the ring is relaxed the axially extending portion 20 extends along a plane which is substantially parallel to the longitudinal centre line 42 of the ring 16 to aid assembly and the radially extending portion 18 is angled relative to the radial plane 45 by an amount 0.
It will be appreciated that other angles could be used.
A second shape of spring ring 16 is shown in Figure 3. The ring is substantiallythe same shape as that shown in Figures 1 and 2 exceptforthe addition of a loading flange 38 at one end ofthe axially extending portion 20 In its relaxed position the radially extending portion 18 is bent towards the axially extending portion 20. A nut 26, bolt 28 and loading tab 40 are provided on the housing 10 and are positioned to communicate with the loading flange 38.
In operation, the nut 26 and bolt 28 are progressively tightened such that the loading tab 40 and loading flangeare pulledtowardsthe housing 10 in the direction of arrow 5. This in turn brings the radially extending portion 18 into contact with the ring 14. Furthertightening ofthe nuts and bolt 26,28 will result in a progressively larger retaining force being extended on the ring 14. The spring ring 16 may be shaped and positioned such that the axially extending portion comes into contact with the housing 10 when loaded, thus increasing the retaining force.
Referring now to Figure 4, a third shape of spring ring 16 comprises two generally radially extending portions 42,44 and one generally axially extending portion 46 which acts to join the two portions 42,44 together. Each portion is angled from the radial plane 45 by an amountl2i.The housing loins provided with a retaining flange 54 at one end and a threaded portion 58 at another which cooperates with a similarly threaded retaining ring 48.
In operation, the retaining ring 48 is tightened down the thread 58 such that the spring ring 16 is deformed and a retaining force exerted on the annular ring 14.
Itwill be appreciated that the annular ring 14 may take any form, such as for example a brush seal of the type described in British Patent No. 1,450,553.
A pair of such seals are shown in Figure 4at50 and 52. In operation, the inside edge of the brush seal 50 52 act against the outside diameter ofthe shaft 56to effect a seal.
It will also be appreciated thatthe spring rings 16 described in this specification may be used as seals, in which the ring 16 acts to prevent a fluid or gas from leaking past the ring 16.

Claims (5)

1. A ring for use in combination with a clamping means to retain a body in a housing, said ring having a generally radially extending portion, which in operation is urged against the body by the action of the clamping means and being provided with a generally axially extending portion.
2. A ring according to claim 1 in which the generally extending portion is deformed axially and the generally axially extending portion is deformed radially by the action of the clamping means.
3. A ring according to either of the preceding claims in which the generally axially extending portion is provided with a free end against which the clamping means acts.
4. A ring according to claim 1 or claim 2 in which a second generally radially extending portion is provided against which the clamping means acts.
5. A ring substantially as herein described with referenceto Figures 1 to 4 of the accompanying drawings.
GB8610557A 1986-03-21 1986-04-30 Retaining rings Withdrawn GB2188121A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE19873708949 DE3708949A1 (en) 1986-03-21 1987-03-19 HOLDING RING FOR LOCATING A COMPONENT
FR8703781A FR2596115A1 (en) 1986-03-21 1987-03-19 Improvement to retention means

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8607072A GB8607072D0 (en) 1986-03-21 1986-03-21 Retaining means

Publications (2)

Publication Number Publication Date
GB8610557D0 GB8610557D0 (en) 1986-06-04
GB2188121A true GB2188121A (en) 1987-09-23

Family

ID=10595033

Family Applications (2)

Application Number Title Priority Date Filing Date
GB8607072A Pending GB8607072D0 (en) 1986-03-21 1986-03-21 Retaining means
GB8610557A Withdrawn GB2188121A (en) 1986-03-21 1986-04-30 Retaining rings

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB8607072A Pending GB8607072D0 (en) 1986-03-21 1986-03-21 Retaining means

Country Status (2)

Country Link
JP (1) JPS62233507A (en)
GB (2) GB8607072D0 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5577887A (en) * 1994-07-06 1996-11-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Metallic lip seal and turbo jet engine equipped with said seal
EP2853784A1 (en) * 2013-09-30 2015-04-01 MTU Aero Engines GmbH Brush sealing for a turbo engine
KR20150144628A (en) * 2014-06-17 2015-12-28 두산중공업 주식회사 Brush seal assembly
US9951871B2 (en) 2014-06-17 2018-04-24 Doosan Heavy Industries Construction Co., Ltd. Brush seal assembly
US10738656B2 (en) 2017-04-07 2020-08-11 MTU Aero Engines AG Sealing assembly for a gas turbine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1309939A (en) * 1969-10-22 1973-03-14 Allinquant F M Seals in telescopic hydraulic shock absorbers
GB1315990A (en) * 1969-12-18 1973-05-09 Illinois Tool Works Spring washers
GB2140534A (en) * 1983-05-18 1984-11-28 Kitamura Valve Mfg Co Ltd A trunnion-type valve assembly
GB2163497A (en) * 1984-08-22 1986-02-26 Terence Peter Nicholson Ring seals
US4637506A (en) * 1983-06-02 1987-01-20 Valeo Clutch release bearing and assembly tool for same

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1309939A (en) * 1969-10-22 1973-03-14 Allinquant F M Seals in telescopic hydraulic shock absorbers
GB1315990A (en) * 1969-12-18 1973-05-09 Illinois Tool Works Spring washers
GB2140534A (en) * 1983-05-18 1984-11-28 Kitamura Valve Mfg Co Ltd A trunnion-type valve assembly
US4637506A (en) * 1983-06-02 1987-01-20 Valeo Clutch release bearing and assembly tool for same
GB2163497A (en) * 1984-08-22 1986-02-26 Terence Peter Nicholson Ring seals

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5577887A (en) * 1994-07-06 1996-11-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Metallic lip seal and turbo jet engine equipped with said seal
EP2853784A1 (en) * 2013-09-30 2015-04-01 MTU Aero Engines GmbH Brush sealing for a turbo engine
US10240472B2 (en) 2013-09-30 2019-03-26 MTU Aero Engines AG Brush seal for a turbomachine
KR20150144628A (en) * 2014-06-17 2015-12-28 두산중공업 주식회사 Brush seal assembly
KR101616620B1 (en) * 2014-06-17 2016-04-28 두산중공업 주식회사 Brush seal assembly
US9951871B2 (en) 2014-06-17 2018-04-24 Doosan Heavy Industries Construction Co., Ltd. Brush seal assembly
US10738656B2 (en) 2017-04-07 2020-08-11 MTU Aero Engines AG Sealing assembly for a gas turbine

Also Published As

Publication number Publication date
JPS62233507A (en) 1987-10-13
GB8607072D0 (en) 1986-04-30
GB8610557D0 (en) 1986-06-04

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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)