WO1984000058A1 - Joint d'etancheite elastique possedant des organes auxiliaires d'elasticite - Google Patents

Joint d'etancheite elastique possedant des organes auxiliaires d'elasticite Download PDF

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Publication number
WO1984000058A1
WO1984000058A1 PCT/US1983/000878 US8300878W WO8400058A1 WO 1984000058 A1 WO1984000058 A1 WO 1984000058A1 US 8300878 W US8300878 W US 8300878W WO 8400058 A1 WO8400058 A1 WO 8400058A1
Authority
WO
WIPO (PCT)
Prior art keywords
gasket
along
auxiliary
resilient
ridges
Prior art date
Application number
PCT/US1983/000878
Other languages
English (en)
Inventor
Charles Martin Warren
Original Assignee
Dow Chemical Co
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 Dow Chemical Co filed Critical Dow Chemical Co
Priority to AU17716/83A priority Critical patent/AU1771683A/en
Priority to BR8307415A priority patent/BR8307415A/pt
Priority to JP50231783A priority patent/JPS59500980A/ja
Publication of WO1984000058A1 publication Critical patent/WO1984000058A1/fr

Links

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
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/021—Sealings between relatively-stationary surfaces with elastic packing
    • F16J15/022—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material
    • F16J15/024—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material the packing being locally weakened in order to increase elasticity
    • 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
    • F16J15/02—Sealings between relatively-stationary surfaces

Definitions

  • an elongate strip or elliptical tube of flexible resilient material having auxiliary resilience means along its length said elongate strip or elliptical tube preferably having a flange portion along one or both edges thereof.
  • the elongate strip may be straight, or curved, or may be embodied as a structure having the general overall shape of a triangle, square, rectangle, polygon, circle, or ellipse.
  • the flange portions may lie in substantially the same general plane in which the elongate strip lies, or may be skewed from, or offset from the plane of the elongate sheet.
  • Figure 1 may be considered as a top view of a horizontally-positioned series of compartments (1) with gaskets or seals (2) between the compartments, or may be considered as a side view of a vertically-stacked series of compartments (1).
  • the series of compartments is shown as being held in place between end members (8) by tensioned rods (7), though other suitable means for maintaining the positions of the compartments may be used.
  • Figure 2 is a view of Figure 1 taken along offset line A-A of Figure 1 and shows a rectangular shape of gasket (2) along an exposed edge of one of the compartments (1) which is, itself, shown to be of a "picture-frame" type of configuration. Holes (9) may be provided in a flanged portion (11) of gasket (2) for fastening purposes.
  • Figure 3 is a enlarged cross-section view of a cutaway portion of Figure 1 to reveal in greater detail the positioning of an embodiment of gasket (2) between two compartments (1) and to show use of holes (9) for fastening gasket (2) in place along the outer perimeter of a surface of a compartment divider (5).
  • the divider When installed, the divider provides a space (4) which is distinct from spaces (3) within the compartments (1).
  • the means for fastening the flanged portion of gasket (2) and divider (5) is shown as a bolt-means, though other means may be used.
  • Figure 4 is an enlarged cross-section view of a portion of gasket (2) to demonstrate positioning of metal spring means (6) which may be (and preferably are) used within an elliptically-shaped embodiment of gasket (2) having an elliptically-shaped centrally- located, opening (10) running the length of the gasket.
  • the spring means (6) is described in Figure 5.
  • Figure 5 illustrates an end-view or cross- sectional view of a preferred metal spring means for use inside various embodiments of the resilient gaskets of the present invention to provide auxiliary resiliency.
  • the springs represent two elongate strips of spring steel which are curved along their length with the concave surfaces facing each other, forming an elliptically shaped area between them. When under compression the curved surfaces are forced closer together. As shown, the curved strips have a small distance between their cooperating edges to expedite movement of the edges when the springs are compressed; other means or configurations for obtaining expedient movement of the edges may be used.
  • the metal spring means are made of "spring steel" though any material which will undergo numerous compression- decompression cycles may be used. Other metal spring configurations may be used.
  • Figure 6 illustrates, in cross-section, an embodiment wherein the gasket (2), having a flange-like extension (11) is provided with auxiliary resiliency means (12) as well an internal void area (10) and a stiffening edge (13) opposite the flange (11).
  • the spring steel means of Figure 5 may also be used within the area (10) as an auxiliary resiliency means along with, or instead of, the auxiliary resiliency means (12).
  • the auxiliary resiliency means (12) illustrate a plurality of resilient ridges or beads on the effective sealing surfaces of gasket (2).
  • the auxiliary means (12) may comprise a single ridge or bead, but preferably comprises a plurality of such ridges or beads which are parallel to each other.
  • the ridges (12) may also be used, if desired, along the flange (11).
  • the stiffening edge (13) may be used for structural purposes, such as for helping to avoid side-ways distortion of the gasket or as an aid in positioning the gasket during installation.
  • the stif- fening edge (13 ⁇ may be thick enough, itself, to augment the total area of seal when gasket (2) is totally compressed, but should not be. so thick that it will prevent the main effective portion of gasket (2) from
  • flanged portion (11) is illustrated as being an offset (bent) member attached obliquely, but it may also be a sub ⁇ stantially straight or flat member attached at a dif ⁇ ferent angle than that shown in Figure 6. Furthermore, the flanged portion (11) may be curved, as viewed in cross-section. .Various configurations of the flanged portion (11) may be used, depending on the process equipment in which it is to be used.
  • Figure 7 illustrates an embodiment wherein the only auxiliary resiliency means for gasket (2) is that of a plurality of ridges or beads (12) positioned on the effective seal-surfaces of gasket (2) and arranged parallel to each other. If desired, the ridges or beads (12) may also be positioned along flange (11). In some cases a single ridge or bead (12) may be used along each sealing surface, but a plurality of such ridges or beads is generally preferred. The ridges (12) do not have to be at right angles to gasket (2).
  • Figure 8 illustrates an embodiment wherein the gasket (2) is circular and has ridges or beads (12) concentrically-located along the effective sealing surfaces of the gasket.
  • the flange (11) is illustrated as an off-set, oblique member, but other configurations may be used.
  • the drawing is not to scale and it will be realized that the central open area within the gasket may be much larger, relative to the entire dimensions, than is illustrated.
  • Figure 9 is a cross-sectional view of gasket (2) taken along line B-B of Figure 8 to more clearly show the ridges or beads (12) and to show the relative position of flange (11).
  • Figure 10 is a cross-sectional view of a gasket (2) having paired counter-biased ridges or beads (12) which are intentionally made to be at an acute angle to gasket (2).
  • gasket (2) having paired counter-biased ridges or beads (12) which are intentionally made to be at an acute angle to gasket (2).
  • three pairs of counter-biased ridges (12) arranged so that they bend toward the central portion (14) of gasket (2) when the configuration becomes compressed between two compartments, each compressed ridge over ⁇ lapping the ridge toward which it bends. Only one such counter-biased pair of ridges along each side may be used, but a plurality of two or more such pairs is preferable.
  • an angle _A which is counter-biased to an angle (_LB) for the-out ⁇ side (i.e., the third) pair of ridges (12).
  • _LB angle for the-out ⁇ side (i.e., the third) pair of ridges (12).
  • the acute angle for the counter-biased pairs of ridges may effectively be any angle less than 90°, it is preferable that it be in the range of about 75° to about 80°.
  • angles L& and_LB it is most preferred to use a value of about 11° ⁇ 1°.
  • re ⁇ silient gasketing material having auxiliary resiliency means comprising at least one of the following:
  • Resilient ridges or beads positioned along the effective sealing surfaces of the gasketing material, said ridges or beads being substantially parallel or concentric to each other; 2. Resilient ridges or beads positioned along the effective sealing surfaces of the gasketing material, said ridges or beads being substantially parallel or concentric to each other, said gasketing material containing a hollow portion (especially a hollow portion that is elliptical in cross-section) running internally through the gasketing material;
  • Spring members comprising elongate strips which are curved along their length, the curved portions forming, when viewed in cross-section, an elliptical shape, said spring members being positioned within a hollow portion of a gasket material which hollow portion conforms to the dimensions of said spring members; 4. Spring members positioned internally within an elongated gasket material, along the length of the gasket, said spring members responding resil- iently to compression and decompression forces acting on the gasket; 5. Resilient ridges or beads as in Item 2 above, along with spring members as in Item 3 or 4 above.
  • the resilient gasketing material may be made of natural or synthetic rubber or resilient polymers, taking into account the environment to which the gasket is to be exposed.
  • Polychloroprene rubber is usually a good choice as it has the ability to withstand contact with a large number of chemicals and can withstand moderately high temperatures.
  • Rubbery formulations based on polybutene, polybutadiene, polyisoprene, fluoropoly ers, polyvinylchloride, polysilicones, and the like may be used in many applications.
  • the rubber formulations generally contain fillers or other additives to enhance their physical and chemical properties. Rubbery formulations covered with fluoropolymers or other flexible coatings or sheaths are within the purview of the present invention.
  • the resilient gasketing material can be pre ⁇ pared by molding-in the auxiliary resiliency means of the present invention. In some cases, it may be best to extrude, cast or mold the gasketing material as sections, including (if desired) the resilient ridges or beads, and then inserting the spring members between the sections and bonding the sections together. In other cases, the internally-positioned spring members may be included during the casting or molding operation.
  • the flanges are preferably formed along with the gasket, but may be formed separately and then bonded to, or anchored to, the gasket. *
  • the general configuration of the gasket can be that of straight gaskets or curved gaskets or may be continuous gaskets for use along triangular, square, rectangular, polygonal, circular, or elliptical surfaces.
  • Figures 1-10 illustrate certain embodi ⁇ ments (not to scale) of the present invention, it will be understood that variations may be made without de ⁇ parting from the inventive concept expressed herein. For instance, more than one hollow portion may be used within the gasket and the internally-positioned spring members may be used in more than one area of the gasket.
  • Equipment in which these gaskets can be used may be, in size, from very small to very large and the concomitant gasket is conveniently sized for the par ⁇ ticular equipment.
  • One of the greatest advantages of the present gaskets is that the gaskets, when used in very large structures are easily fastened in place by use of the flanges and a series of compartments can be more easily pressed together, horizontally, without having the gasket droop, sag, or slip out of place during the placement of the compartments.
  • the flanges can serve as gasketing for internal parts of the equip ⁇ ment, such as compartment dividers or separators, while serving to hold the main portion of the gasket in place.

Landscapes

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

Abstract

Matériau formant un joint d'étanchéité flexible et élastique (2) pourvu d'organes auxiliaires d'élasticité tels que des arêtes ou des bourrelets (12) ou des organes de ressort (6) positionnés à l'intérieur. Les joints d'étanchéité (2) peuvent être droits ou courbés ou être produits en continu, par exemple sous forme de rectangles ou de cercles. Les joints d'étanchéité présentent de préférence des rebords (11).
PCT/US1983/000878 1982-06-14 1983-06-06 Joint d'etancheite elastique possedant des organes auxiliaires d'elasticite WO1984000058A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
AU17716/83A AU1771683A (en) 1982-06-14 1983-06-06 Flanged compression gasket
BR8307415A BR8307415A (pt) 1982-06-14 1983-06-06 Gaxeta elastica,tendo meio de elasticidade auxiliar
JP50231783A JPS59500980A (ja) 1982-06-14 1983-06-06 フランジ付き圧縮ガスケット

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US38841582A 1982-06-14 1982-06-14

Publications (1)

Publication Number Publication Date
WO1984000058A1 true WO1984000058A1 (fr) 1984-01-05

Family

ID=23534037

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1983/000878 WO1984000058A1 (fr) 1982-06-14 1983-06-06 Joint d'etancheite elastique possedant des organes auxiliaires d'elasticite

Country Status (4)

Country Link
EP (1) EP0111546A4 (fr)
KR (1) KR860001694B1 (fr)
WO (1) WO1984000058A1 (fr)
ZA (1) ZA834233B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3344734A1 (de) * 1983-12-10 1985-06-20 Kaco Gmbh + Co, 7100 Heilbronn Dichtelement fuer flachdichtungen
EP0686792A1 (fr) * 1994-06-10 1995-12-13 Commissariat A L'energie Atomique Système à joint d'étanchéité comprimé entre deux portées non parallèles

Citations (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE48428C1 (fr) *
NL93033C (fr) * 1900-01-01
US1674038A (en) * 1924-04-18 1928-06-19 Clifton A Glass Floating roof for oil tanks
GB475755A (en) * 1936-12-23 1937-11-25 Henri Lancery Improvements in pipe joints
US2195046A (en) * 1937-03-10 1940-03-26 Frank A Best Flexible and resilient beaded strip and method of manufacturing the same
US2306160A (en) * 1938-07-29 1942-12-22 Freyssinet Eugene Packing device
US2315588A (en) * 1941-12-04 1943-04-06 American Steel & Wire Co Top seal for pavement joints
US2753074A (en) * 1950-03-06 1956-07-03 Interpa Corp Registered Trust Container seals or closures
DE958482C (de) * 1953-08-27 1957-02-21 Bosch Gmbh Robert Elektrische Dichtung fuer Abschirmgehaeuse
US2859496A (en) * 1957-04-16 1958-11-11 Westinghouse Electric Corp Refrigeration apparatus
SU122999A1 (ru) * 1957-10-19 1958-11-30 В.С. Белобров Торовое уплотнение
US2914212A (en) * 1957-08-01 1959-11-24 Hammond Iron Works Floating roof weather seal
US2923984A (en) * 1960-02-09 Astragal mounting
FR1239365A (fr) * 1959-07-09 1960-08-26 Expl S Ind Soc Gen Joint d'étanchéité travaillant entre deux espaces à pression également très élevée
GB862917A (en) * 1958-02-19 1961-03-15 Juan Andres Arecheta Mota Improvements in or relating to apparatus for sealing a joint between two opposed surfaces
US3026367A (en) * 1959-05-08 1962-03-20 Tech Wire Prod Inc Shielding and mounting strip
US3038732A (en) * 1958-04-07 1962-06-12 Texas Pipe Line Company Inflatable seal bushing for pipeline casing
US3040393A (en) * 1957-08-05 1962-06-26 Baldwin Montrose Chemical Comp Vacuum insertable strip
US3247312A (en) * 1963-12-26 1966-04-19 Borg Warner Shielding enclosure for electrical equipment
FR1473325A (fr) * 1966-02-04 1967-03-17 Joint d'étanchéité
US3398977A (en) * 1965-02-13 1968-08-27 Yoneda Rikizo Pipe coupling
US3501868A (en) * 1964-01-31 1970-03-24 Equipment Moderne Ind Par Appl Sealing joints
US3508587A (en) * 1966-09-29 1970-04-28 Hans A Mauch Tubular structural member
US3554567A (en) * 1966-03-16 1971-01-12 Carrier Corp Fluid seal
US3591190A (en) * 1969-05-23 1971-07-06 Fred Winay Clinch seals
US3591963A (en) * 1968-06-18 1971-07-13 Entwicklungsring Sued Gmbh Inflatable seal for aircraft jet engines
US3604716A (en) * 1968-12-03 1971-09-14 Jacques Webert Self-tightening seal
US3812316A (en) * 1973-03-28 1974-05-21 Gen Electric Door seal gasket for combined microwave and self-cleaning oven
US3926332A (en) * 1973-02-14 1975-12-16 Nippon Kakokicompany Limited Sealing structure for a liquid storage vessel having a floating head
US4143883A (en) * 1978-02-07 1979-03-13 Controlex Corporation Of America Push-pull control with spring-loaded seal

Patent Citations (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2923984A (en) * 1960-02-09 Astragal mounting
NL93033C (fr) * 1900-01-01
SE48428C1 (fr) *
US1674038A (en) * 1924-04-18 1928-06-19 Clifton A Glass Floating roof for oil tanks
GB475755A (en) * 1936-12-23 1937-11-25 Henri Lancery Improvements in pipe joints
US2195046A (en) * 1937-03-10 1940-03-26 Frank A Best Flexible and resilient beaded strip and method of manufacturing the same
US2306160A (en) * 1938-07-29 1942-12-22 Freyssinet Eugene Packing device
US2315588A (en) * 1941-12-04 1943-04-06 American Steel & Wire Co Top seal for pavement joints
US2753074A (en) * 1950-03-06 1956-07-03 Interpa Corp Registered Trust Container seals or closures
DE958482C (de) * 1953-08-27 1957-02-21 Bosch Gmbh Robert Elektrische Dichtung fuer Abschirmgehaeuse
US2859496A (en) * 1957-04-16 1958-11-11 Westinghouse Electric Corp Refrigeration apparatus
US2914212A (en) * 1957-08-01 1959-11-24 Hammond Iron Works Floating roof weather seal
US3040393A (en) * 1957-08-05 1962-06-26 Baldwin Montrose Chemical Comp Vacuum insertable strip
SU122999A1 (ru) * 1957-10-19 1958-11-30 В.С. Белобров Торовое уплотнение
GB862917A (en) * 1958-02-19 1961-03-15 Juan Andres Arecheta Mota Improvements in or relating to apparatus for sealing a joint between two opposed surfaces
US3038732A (en) * 1958-04-07 1962-06-12 Texas Pipe Line Company Inflatable seal bushing for pipeline casing
US3026367A (en) * 1959-05-08 1962-03-20 Tech Wire Prod Inc Shielding and mounting strip
FR1239365A (fr) * 1959-07-09 1960-08-26 Expl S Ind Soc Gen Joint d'étanchéité travaillant entre deux espaces à pression également très élevée
US3247312A (en) * 1963-12-26 1966-04-19 Borg Warner Shielding enclosure for electrical equipment
US3501868A (en) * 1964-01-31 1970-03-24 Equipment Moderne Ind Par Appl Sealing joints
US3398977A (en) * 1965-02-13 1968-08-27 Yoneda Rikizo Pipe coupling
FR1473325A (fr) * 1966-02-04 1967-03-17 Joint d'étanchéité
US3554567A (en) * 1966-03-16 1971-01-12 Carrier Corp Fluid seal
US3508587A (en) * 1966-09-29 1970-04-28 Hans A Mauch Tubular structural member
US3591963A (en) * 1968-06-18 1971-07-13 Entwicklungsring Sued Gmbh Inflatable seal for aircraft jet engines
US3604716A (en) * 1968-12-03 1971-09-14 Jacques Webert Self-tightening seal
US3591190A (en) * 1969-05-23 1971-07-06 Fred Winay Clinch seals
US3926332A (en) * 1973-02-14 1975-12-16 Nippon Kakokicompany Limited Sealing structure for a liquid storage vessel having a floating head
US3812316A (en) * 1973-03-28 1974-05-21 Gen Electric Door seal gasket for combined microwave and self-cleaning oven
US4143883A (en) * 1978-02-07 1979-03-13 Controlex Corporation Of America Push-pull control with spring-loaded seal

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP0111546A4 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3344734A1 (de) * 1983-12-10 1985-06-20 Kaco Gmbh + Co, 7100 Heilbronn Dichtelement fuer flachdichtungen
EP0686792A1 (fr) * 1994-06-10 1995-12-13 Commissariat A L'energie Atomique Système à joint d'étanchéité comprimé entre deux portées non parallèles
FR2721085A1 (fr) * 1994-06-10 1995-12-15 Commissariat Energie Atomique Système à joint d'étanchéité comprimé entre deux portées non parallèles.
US5655752A (en) * 1994-06-10 1997-08-12 Commissariat A L'energie Atomique System with imperviousness joint compressed between two non-parallel bearings

Also Published As

Publication number Publication date
KR860001694B1 (ko) 1986-10-17
EP0111546A1 (fr) 1984-06-27
KR840005528A (ko) 1984-11-14
ZA834233B (en) 1985-01-30
EP0111546A4 (fr) 1984-10-29

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