GB2069631A - A sealing element - Google Patents

A sealing element Download PDF

Info

Publication number
GB2069631A
GB2069631A GB8104113A GB8104113A GB2069631A GB 2069631 A GB2069631 A GB 2069631A GB 8104113 A GB8104113 A GB 8104113A GB 8104113 A GB8104113 A GB 8104113A GB 2069631 A GB2069631 A GB 2069631A
Authority
GB
United Kingdom
Prior art keywords
sealing element
metal jacket
filler material
element according
jacket
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Withdrawn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
GB8104113A
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.)
Reinz Dichtungs GmbH
Original Assignee
Reinz Dichtungs GmbH
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 Reinz Dichtungs GmbH filed Critical Reinz Dichtungs GmbH
Publication of GB2069631A publication Critical patent/GB2069631A/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Withdrawn legal-status Critical Current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
    • 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
    • F16J15/128Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal covering

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Gasket Seals (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A sealing element comprises a ring-shaped outer metal jacket (2) having a circular radial cross-section and edges (2a and 2b) extending along a seam of the jacket. A filler material (3) is mechanically supported and hermetically sealed in the metal jacket, thereby preventing extrusion of the filler material and preventing penetration of chemically reactive agents to the filler material. In some embodiments the metal jacket is hermetically sealed by sealing the seam edges of the jacket together. In other embodiments, the filler material is received in an inner metal jacket which is sealingly enclosed by the outer metal jacket. <IMAGE>

Description

SPECIFICATION A sealing element This invention relates to improvements in or relating to sealing elements comprising a metal jacket containing a filler material.
In known sealing elements of this kind, e.g.
filled sealing rings, type C, according to DIN 7603, the metal jacket does not fully enclose the filler material either when supplied or when installed, so that the filler may come into contact with the media to be sealed and the structural components as well as the atmospheric environment When known sealing rings of this kind are used to seal joints which are exposed to high thermal stress, satisfactory sealing usually is not achieved because the temperature resistance of the filler materials used is too low, i.e. at high operating temperatures the materials are subject to oxidation and so lose their sealing effectiveness.
An all-metal seal, e.g. solid metal ring, cannot be used because of the low recovery characteristics of the metal, as defined by the elasticity module, which results in thermal dilatation of structural components.
While structurally elastic metallic sealing elements, such as embossed metal gaskets, exhibit high recovery properties at room temperatures, practically all these properties are lost at high temperature due to thermal relaxation.
Therefore, an object of the invention is to provide a sealing element that can withstand high temperatures and is chemically resistant.
According to the present invention, there is provided a sealing element comprising a metal jacket containing a filler material, in which element the filler material is mechanically supported and hermetically sealed in the jacket, thereby preventing extrusion of the filler material and penetration of chemically reactive media to the filler material during use of the element.
In one form of the invention, the metal jacket is hermetically sealed by sealing two edges of the jacket together along a seam. For example, in one embodiment, the seam edges of the metal jacket are butted together and joined. In another embodiment, the seam edges of the metal jacket are sealed together by a metal sealing strip extending along the seam, the metal sealing strip preferably being disposed inside the metal jacket between the filler material and the metal jacket. In a further embodiment, the seam edges of the metal jacket are outwardly flanged and crimped together. In yet another embodiment, the seam edges of the metal jacket are overlapped and sealed together, the overlapped seam edges preferably overlapping over a circumferential angle of not more than about 45".
In another form of the invention, the filler material is received in an inner metal jacket which is enclosed by an outer metal jacket.
If desired, the filler material may be received in an innermost metal jacket which is enclosed by an intermediate metal jacket which is itself enclosed by an outer metal jacket.
Conveniently, each of the metal jackets has two adjacent edges thereof extending along a seam, the seams of adjacent jackets being staggered relative to one another to provide hermatic sealing of the filler material within the jackets.
Desirably, the metal jacket or jackets are of adequate thickness to protect the sealing element from mechanical damage prior to or during use.
In a preferred application of the sealing element, the element is ring-shaped and has a substantially circular cross-section.
The filler material may comprise an elastic or plastic gasket material, such as graphite, asbestos and/or clay.
Due to the construction of a sealing element embodying the invention the filler material is neither in contact with the medium to be sealed nor with the structural components nor the ambient atmosphere. Consequently, the filler material is protected from extraneous influences. For example, a material normally subject to oxidation in a normal environment at high temperatures, like graphite, will maintain its good recovery characteristics at room temperature as well as at very high temperatures. For this reason, a sealing element embodying the invention has proven its outstanding performance in actual use on joints which are subject to high temperatures, e.g. sealing applications on exhaust turbocharger flanges.
In order that the invention may be readily understood, embodiments thereof will now be described, by way of example, with reference to the accompanying drawings, in which: Figure 1 is a plan view of a ring-shaped sealing element embodying the invention; Figure 2 is a radial cross-sectional view of part of the sealing element of Fig. 1 taken on the line ll-ll of Fig. 1; and Figures 3 to 7 are cross-sectional views similar to Fig. 2 of various other embodiments of a sealing element in accordance with the invention.
Referring now to the drawings, Fig. 1 shows a ring-shaped sealing element 1 embodying the invention, designed for use on joints subject to high temperature stress, for example exhaust turbocharger flanges, or joints requiring high resistance to chemical attack at high temperatures.
As shown in Fig. 2, the sealing element of Fig. 1 is of circular radial cross-section and comprises a toroidal body of a filler material 3 sealingly encased by an outer metal jacket 2.
The two edges 2a, 2b extending along a seam of the jacket 2 are butted and joined together so as hermetically to enclose the filler material within the metal jacket 2.
The filler material 3 comprises an elastic or plastic gasket material (preferably composed by graphite, asbestos and/or clay). The performance of the sealing elements has been tested and proven in practical applications in sealing exhaust turbocharger flanges, the an nular sealing ring having inner diameter of approximately 45.3 mm and an outer diameter of approximately 51.9 mm for this particu lar purpose.
In the embodiment shown in Fig. 3, the filler material is shaped to allow a contact area or seam 4 between the two edges 2a, 2b of the outer metal jacket to be hermetically sealed by an inner metal sealing strip 5 which extends along the seam and, as shown in Fig.
3, bridges the edges 2a, 2b at the seam 4.
Fig. 4 shows another embodiment of a sealing element in accordance with the invention, in which an additional inner metal jacket 6 is disposed immediately inside the outer metal jacket 2. The filler material 3 is contained within the inner jacket 6 contacting the inner surface of the metal jacket 6 and extending into a gap left at the seam 7 between edges 6a and 6b. The outer metal jacket 2 is sealingly arranged around the inner metal jacket 6 such that the respective seams 7 and 4 do not coincide. As shown in Fig. 3, the seam 7 is diametrically opposite the seam 4.
A further embodiment of a sealing element in accordance with the invention is illustrated in Fig. 5, wherein the single outer metal jacket 2 has seam edges 2a, 2b which are outwardly flanged and crimped together.
As shown in Fig. 6, another sealing element embodying the invention is formed with three concentric metal jackets. The filler material is received within and extends into the seam 8 between the two edges of an innermost metal jacket 9, around which an intermediate inner metal jacket 6 is sealingly disposed. The intermediate metal jacket 6 is similar sealingly engaged within the outer metal jacket 2. The metal jackets 9, 6 and 2 are arranged around the filler material such that the respective seams of adjacent metal jackets are in staggered, non-overlapping relationship, although as shown in Fig. 6 the seam 8 of the innermost metal jacket 9 is radially aligned with the seam 4 of the outer metal jacket 2.
Fig. 7 illustrates a sealing element embodying the invention and including a single outer metal jacket 2 formed sealing-tightly around the filler material 3. The edges 2a and 2b of the jacket overlap and are resiliently prestressed to form a tight seal, the degree of overlap being such that the overlap area subtends an angle of not more than approximately 45 at the part which would form the centre of the cross-section were the crosssection circular. The overlap may subtend an angle of between 10 and 45t and preferably between 20 and 30 .
Each of the embodiments described above is provided with a jacket or jackets of adequate thickness to prevent mechanical damage prior to as well as during use of the sealing element.
The filler material 3 is so tightly enclosed within the metal jacket or jackets that damage by extraneous external conditions, for example oxidation caused by contact with air, is prevented and the filler material retains the good recovery characteristic inherent therein, resulting in a high operating reliability and long life for a sealing element embodying the invention.
Advantageously, the filler material 3 is provided in a pressed form conforming to the internal cross-sectional shape within the metal jacket or jackets in each embodiment as shown in Figs. 2 to 7.

Claims (11)

1. A sealing element comprising a metal jacket containing a filler material, in which element the filler material is mechanically supported and hermetically sealed in the jacket, thereby preventing extrusion of the filler material and penetration of chemically reactive media to the filler material during use of the element.
2. A sealing element according to claim 1, wherein the metal jacket is hermetically sealed by sealing two edges of the jacket together along a seam.
3. A sealing element according to claim 2, wherein the seam edges of the metal jacket are butted together and joined.
4. A sealing element according to claim 2, wherein the seam edges of the metal jacket are sealed together by a metal sealing strip extending along the seam.
5. A sealing element according to claim 4, wherein the metal sealing strip is disposed inside the metal jacket between the filler material and the metal jacket.
6. A sealing element according to claim 2, wherein the seam edges of the metal jacket are outwardly flanged and crimped together.
7. A sealing element according to claim 2, wherein the seam edges of the metal jacket are overlapped and sealed together.
8. A sealing element according to claim 7, wherein the seam edges overlap over a circumferential angle of not more than about 45".
9. A sealing element according to claim 1 or 2, wherein the filler material is received in an inner metal jacket which is enclosed by an outer metal jacket.
10. A sealing element according to claim 1 or 2, wherein the filler material is received in an innermost metal jacket which is enclosed by an intermediate metal jacket which is itself enclosed by an outer metal jacket.
11. A sealing element according to claim 9 or 10, wherein each of the metal jackets has two adjacent edges thereof extending along a seam, the seams of adjacent jackets being staggered relative to one another to provide hermetic sealing of the filler material within the jackets.
1 2. A sealing element according to any preceding claim, wherein the metal jacket or jackets are of adequate thickness to protect the sealing element from mechanical damage prior to or during use.
1 3. A sealing element according to any preceding claim, wherein the element is ringshaped.
1 4. A sealing element according to claim 13, wherein the element has a substantially circular cross-section.
1 5. A sealing element according to any preceding claim, wherein the filler material comprises an elastic or plastic gasket material, such as graphite, asbestos and/or clay.
1 6. A sealing element substantially as hereinbefore described with reference to, and as illustrated in, the accompanying drawings.
1 7. Any novel feature or combination of features herein disclosed.
GB8104113A 1980-02-15 1981-02-10 A sealing element Withdrawn GB2069631A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19803005792 DE3005792A1 (en) 1980-02-15 1980-02-15 SEALING ELEMENT

Publications (1)

Publication Number Publication Date
GB2069631A true GB2069631A (en) 1981-08-26

Family

ID=6094751

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8104113A Withdrawn GB2069631A (en) 1980-02-15 1981-02-10 A sealing element

Country Status (4)

Country Link
JP (1) JPS571864A (en)
DE (1) DE3005792A1 (en)
FR (1) FR2476259A1 (en)
GB (1) GB2069631A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2512155A1 (en) * 1981-08-28 1983-03-04 Lechler Elring Dichtungswerke FLAT SEAL AND MANUFACTURING METHOD THEREOF
WO1988009890A1 (en) * 1987-06-10 1988-12-15 Heilmeier & Weinlein Fabrik Für Oel-Hydraulik Gmbh Screw-type valve housing
GB2326680A (en) * 1997-06-25 1998-12-30 Europ Gas Turbines Ltd High temperature compliant seal
FR2840968A1 (en) * 2002-06-13 2003-12-19 Commissariat Energie Atomique High temperature graphite sealing joint comprises flexible graphite core held in shape by two metal cups, whole assembly enclosed in sealed jacket
LU101292B1 (en) * 2019-06-30 2020-12-30 BigRep GmbH Sealing element and sealing arrangement

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6199772A (en) * 1984-10-19 1986-05-17 Fuji Seikou Kk Composite seal material for vacuum devices
DE3528614A1 (en) * 1985-08-09 1987-02-19 Goetze Ag FLAT GASKET, ESPECIALLY CYLINDER HEAD GASKET FOR COMBUSTION ENGINES
JPH0526383Y2 (en) * 1985-11-21 1993-07-02
DE102014203430A1 (en) * 2014-02-26 2015-08-27 Siemens Aktiengesellschaft Liquid metal plain bearings
DE102017100402A1 (en) * 2016-12-21 2018-06-21 Endress+Hauser SE+Co. KG Sealing ring and pressure transducer with at least one such sealing ring

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB333478A (en) * 1929-11-25 1930-08-14 Albert Georg Wilhelm Iseler Improvements in joint-making packing
FR993123A (en) * 1949-06-03 1951-10-26 Metalloplastic seal
BE757953A (en) * 1969-10-24 1971-04-23 Verrieres Appliquees S E V A S INDUCED ELASTICITY SEAL
US3820799A (en) * 1972-08-16 1974-06-28 Commissariat Energie Atomique Resilient metal gasket
JPS53123354U (en) * 1977-03-10 1978-09-30
JPS54127967U (en) * 1978-02-28 1979-09-06

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2512155A1 (en) * 1981-08-28 1983-03-04 Lechler Elring Dichtungswerke FLAT SEAL AND MANUFACTURING METHOD THEREOF
WO1988009890A1 (en) * 1987-06-10 1988-12-15 Heilmeier & Weinlein Fabrik Für Oel-Hydraulik Gmbh Screw-type valve housing
US5063961A (en) * 1987-06-10 1991-11-12 Heilmeier & Weinlein Fabrik Fur Oel-Hydroaulik Gmbh & Co. Screw-type valve housing
GB2326680A (en) * 1997-06-25 1998-12-30 Europ Gas Turbines Ltd High temperature compliant seal
GB2326680B (en) * 1997-06-25 2001-03-28 Europ Gas Turbines Ltd High temperature compliant seal
FR2840968A1 (en) * 2002-06-13 2003-12-19 Commissariat Energie Atomique High temperature graphite sealing joint comprises flexible graphite core held in shape by two metal cups, whole assembly enclosed in sealed jacket
WO2003106869A3 (en) * 2002-06-13 2004-04-01 Commissariat Energie Atomique Flexible graphite sealing joint with metal jacket for high temperature
US7255353B2 (en) 2002-06-13 2007-08-14 Commissariat A L'energie Atomique Flexible graphite sealing joint with metal jacket for high temperature
CN100383438C (en) * 2002-06-13 2008-04-23 原子能委员会 Flexible graphite sealing joint with metal jacket for high temperature
LU101292B1 (en) * 2019-06-30 2020-12-30 BigRep GmbH Sealing element and sealing arrangement
WO2021001113A1 (en) * 2019-06-30 2021-01-07 BigRep GmbH Sealing element and sealing arrangement

Also Published As

Publication number Publication date
DE3005792A1 (en) 1981-08-20
JPS571864A (en) 1982-01-07
FR2476259A1 (en) 1981-08-21
JPS622188B2 (en) 1987-01-19

Similar Documents

Publication Publication Date Title
US2580546A (en) Jacketed gasket
SU1720503A3 (en) Stuffing box seal
US4603892A (en) Tight connection device
GB2069631A (en) A sealing element
KR960003784A (en) In-line filter for tube
KR880004267A (en) Absolute safety fireproof sealing assembly
US20060181032A1 (en) Hybrid gasket
GB2105797A (en) Rotary shaft seal
US4582094A (en) Insulation for hot gas piping
CA1047063A (en) Electrically insulating pipe coupling
US4576387A (en) Rotary joint device with floating seal ring for a cryogenic fluid
US4245012A (en) Sodium sulfur battery seal
US3583730A (en) Dual fire resistant seal
CA1243054A (en) Gaskets
US4778074A (en) Composite material and metal canister
SU1386042A3 (en) Hermetic joint for two pipes
US4567504A (en) Semiconductor component with a disc-shaped case
JPS6340693Y2 (en)
JP2548658Y2 (en) Spiral wound gasket
JPH0239116Y2 (en)
KR840003343A (en) Valve Sealing Device
JP2742888B2 (en) Electrical insulating gasket
JPH0432553Y2 (en)
JP2945872B2 (en) Spiral wound gasket
JPS6043016B2 (en) semiconductor equipment

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)