A gasket can be used to seal the interface between components in a range of fluid assemblies (e.g., industrial, automotive aerospace, life science, oil, gas, etc.). The interfacing components typically each include a flange surrounding an opening communicating with a fluid chamber. A controlled-compression gasket typically comprises a rigid retainer having the primary role of preventing over-compression of seal elements during installation into the fluid assembly.
A gasket is provided wherein the retainer comprises a plurality of rigid balls interconnected to form an integral retaining structure. The interconnection of the balls is preferably accomplished by a polymeric matrix (that is compressible and flexible). The balls prevent over-compression of the gasket, and the polymeric matrix provides the retainer with an almost infinite number of elbows or joints. This combination allows the gasket to flex in the field to conform to different flange-surface geometries (e.g., planar, pitted, curved, stepped, etc.) without any compromise on over-compression protection. The matrix can be the same material as, and molded at the same time as, the gasket's sealing elements. And the gasket can be manufactured “flat” even when intended for installation between non-planar (e.g., pitted, curved, stepped, etc.) flange surfaces.
Referring now to the drawings, and initially to
The gasket 10 seals the interface between these flange surfaces 26 and 27, to prevent leakage from (or into) the fluid chamber 23. The gasket 10 can be adapted to accommodate a planar flange interface (
The gasket 10 is shown isolated from (and not yet installed in) the fluid assembly 20 in
The gasket 10 comprises a retainer 30 comprising a plurality of balls 31 that are interconnected to form an integral retaining structure 32. “Integral” in the present context means that the structure 32 is a one-piece part that does not need further assembly for installation. The structure 32 is preferably (but not necessarily) formed in one-piece during the gasket-manufacturing process. In the illustrated embodiment, for example, a polymeric matrix 33 interconnects the balls 31 to form the integral retaining structure 32.
The retaining structure 32 has opposed radial faces 34 and 35, an outer axial edge 36 that extends axially between and radially around the faces 34/35, and an inner axial edge 37, that extends axially between and radially within the faces 34/35. The radial faces 34 and 35 contact the respective flange surfaces 26 and 27 in the fluid assembly 20, the distance therebetween defines the installation compression limit. The inner axial edge 37 defines an aperture 38 that corresponds to the gasket opening 18.
The retainer 30 and/or the retaining structure 32 can further comprise holes 39 corresponding to the fastener holes 19 in the gasket 10 and/or the fastener holes 28 in the fluid assembly 20 (See
The gasket 10 additionally comprises a sealing rim 40 that encircles the retainer's inner axial edge 37. The rim 40 can have a proximate stem portion 41 adjacent the retainer edge 37 and a distal bead portion 42 projecting radially inward therefrom. The bead portion 42 can have a circular or bulb (in cross-section) shape that extends axially beyond one or both of the retainer faces 34/35. In the illustrated embodiment, the bead portion 42 defines the inner perimeter 17 of the gasket 10.
The gasket 10 can further comprise a peripheral hem 50 around the retainer's outer axial edge 36 and/or surrounding ledges 60 within the retainer's holes 19 (See
Referring now to
The matrix 33 is preferably a polymeric material (e.g., rubber) that is flexible and can also (and usually will) be compressible at the minimum flange pressure. The polymeric matrix can be introduced during a molding step to encapsulate the balls 31, and/or fill the spaces therebetween and therearound so that the retaining structure 32 is a substantially solid, continuous (other than designed openings and holes) part. In the illustrated retainer 30, the matrix 33 is level with the “poles” of the balls 31 and forms the adjoining regions of the respective radial face 34/35. In some sealing situations, it may be undesirable for the polymeric matrix 33 to extend axially beyond the balls 31, as this may introduce a false sense of adequate compression during installation. On the other hand, total-ball encapsulation could offer positive corrosion resistance characteristics, as the balls 31 would not be exposed to the environment.
The flexible polymeric matrix 33 provides the retainer 30 (and thus the gasket 10) with a hinge, elbow, or joint between each adjacent ball 31 in the retaining structure 32. In other words, the gasket 10 has a two-way grid of joints, each of which can be flexed in plural directions, to conform to a particular surface. Thus the gasket 10 can conform to an enormous number of different surface profiles (e.g., this number being at least, and probably greater than, the factorial of the number of balls 31).
Specifically, for example, the retainer 30 can easily accommodate flat smooth flange surfaces (see e.g.,
With a stepped flange surface, such as shown in
The balls 31 can be spherical, and conventional ball-bearings can easily used to manufacture the retainer 30. That being said, the tough tolerances typically imposed upon bearings will often not need to be so strict for the balls 31 forming the retaining structure 32. Discrete units that have chips or scrapes, or ones that are more oblong or egg-shaped may work acceptably well in many sealing situations (see e.g.,
The dimensions of the balls 31 can depend upon manufacturing methods, sealing situations, and ball-array arrangements within the retaining structure 32. Some or all of the balls 31 can each have a diameter of between 0.10 cm and 0.30 cm, between 0.10 cm and 0.15 cm, between 0.15 cm and 0.17 cm, and/or between 0.15 and 0.20 cm. Additionally or alternatively, at least some or all of the balls 31 can have a diameter greater than 0.10 cm and/or less than 0.30 cm. In the case of non-spherical units 31, the diameter can be considered the dimension most likely to define the axial distance between the radial faces 34 and 35 in the retaining structure 32.
The ball density (i.e., the number of balls 31 per unit surface area of the face 34/35 of the retaining structure 32), and/or the ball-to-matrix ratio (i.e., the total volume occupied by the balls 31 versus the total volume occupied by the matrix 33) can differ depending upon manufacturing concerns and/or sealing situations. Generally, there should be enough balls 31 to provide suitable rigidity and acceptable over-compression protection, and enough matrix material to provide structural integrity and acceptable flexibility. And the relative cost of the balls 31 versus the polymeric matrix 32, may make it economically desirable to minimize one rather than the other.
The illustrated gasket 10 can have a ball density (i.e., number of balls 31 per unit surface area of the retaining structure 32) can be twenty to seventy balls (31) per cm2 and/or thirty to sixty balls (31) per cm2. Additionally or alternatively, the retaining structure 32 can have a ball density of less than seventy balls (31) per cm2 and/or greater than twenty balls (31) per cm2. The balls 31 can (but need not) be relatively evenly distributed throughout the retaining structure 32.
Referring now to the 6th (
Also in each of these methods, a molding step is performed wherein polymeric material is introduced to form the matrix 33 interconnecting the balls 31. (See
The sealing rim 40, the peripheral hem 50, and/or the ledges 60 can be formed during the same molding step that forms the matrix 33. Thus, the elements 40/50/60 can be made from the same polymeric material as the matrix 33. This approach not only eliminates separate molding steps, but will in many cases promote the bonding of the elements 40/50/60 to the retainer 30. Specifically, for example, the matrix 33, the rim 40, the hem 50, and the ledges 60 are all formed in one-piece together, whereby the gasket 10 does not have any tear-susceptible seams, welds, or adhesive bonds.
In the method shown in
In the method shown in
In the method shown in
In the methods shown in the 7th and 8th drawing sets, any cutting, machining, or stamping is performed prior to the molding step. This may be preferred if such activity causes the polymeric material introduced during molding to be susceptible to rips or tears. If this is not a concern, post-mold cutting of the openings 38 and 39 (and/or other features) may be a suitable approach. Also, forming the rim 40, the hem 50, and/or the ledges 60 during separate molding or other steps is possible and contemplated, and may even be preferred if advantages can be gained by using different matrix and sealing materials.
One may now appreciate that the gasket 10, retainer 30, and/or the retaining surface 32 can accommodate a large range of different flange contours, without any compromise on over-compression protection. Moreover, there is no need for the mold platform 70 (or other manufacturing equipment) to anticipate the profile of the flange interface. This may prove particularly useful when, for example, surfaces have unintended irregular contours (as opposed to designed) that must be accommodated in the fluid assembly 20.
Although the gasket 10, the retainer 30, the balls 31, the retaining structure 32, the matrix 33, sealing elements 40, 50, 60, related components, equipment, methods, and/or steps have been shown and described with respect to a certain embodiments, equivalent alterations and modifications should occur to others skilled in the art upon review of this specification and drawings. If an element (e.g., component, assembly, system, device, composition, method, process, step, means, etc.), has been described as performing a particular function or functions, this element corresponds to any functional equivalent (i.e., any element performing the same or equivalent function) thereof, regardless of whether it is structurally equivalent thereto. And while a particular feature may have been described with respect to less than all of the embodiments, such feature can be combined with one or more other features of the other embodiments.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US2009/045371 | 5/28/2009 | WO | 00 | 12/23/2010 |
Number | Date | Country | |
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61075159 | Jun 2008 | US | |
61145135 | Jan 2009 | US | |
61148148 | Jan 2009 | US |