1. Field
The technology of the present application relates to seals, and more specifically, to seals for ports or glands.
2. Background
Assorted systems may use fluids or gases (generally referred to as “media” or “process media”) to maintain pressure. These pressurized systems often have ports and fittings to allow the introduction of media to charge the system. It is generally necessary to provide a seal between any port and fitting in the system to prevent pressure loss by the escape of some or all of the media passing through the port or fitting.
Ports traditionally include machined, internally threaded passages, while fittings traditionally include external threads that mate with the threaded passages of the port. The threads of the port matingly receive the threads of the fitting to form a joint, where closing of the joint is accomplished by applying an appropriate torque to the fitting aligned with the port.
When a seal is employed between the fitting and port, the joint formed is closed to prevent leakage of media and pressure drops. As shown in
Some seals known in the art, such as seal 50 illustrated in
Accordingly, a seal for providing a bubble tight seal between a port and fitting without requiring high levels of torque and which is not expensive to manufacture or prone to breaking is desirable.
Embodiments disclosed herein address the above stated needs by providing an annular seal having an upper protruding portion protruding upwardly from the portion of the seal body proximate the opening in the seal and a lower protruding portion protruding downwardly from the portion of the seal body proximate the opening in the seal and in a direction perpendicular to the lower annular-shaped surface of the seal body.
The foregoing, as well as other features, utilities, and advantages of the invention will be apparent from the following more particular description of a preferred embodiment of the invention as illustrated in the accompanying drawings.
The technology of the present application will be further explained with reference to
The inner wall 105 includes a groove 106, which, as illustrated, is centered on the inner wall 105 between the upper face 102 and lower face 103. In one aspect of the embodiment, the groove has a V-shape. Other shapes, such as a U-shape, also may be used in the seal of the instant application. In one aspect of the embodiment described herein, the size of the mouth of the groove 106 is substantially equal to the distance between the upper face 102 and the lower face 103. However, the size of the mouth of the groove 106 may be smaller or larger than the distance between the upper face 102 and lower face 103. The depth of the groove 106, i.e., the distance into the inner wall 105 the groove 106 penetrates, also may vary. In one embodiment, the depth that the groove 106 extends into the inner wall 105 is farther than the location where the protruding portions, discussed in greater detail below, begin.
As also shown in
As illustrated in
As also illustrated in
As noted above, in one aspect of the embodiment described herein, the upper protruding portion 107 and lower protruding portion 108 are located entirely above and below, respectively, the groove 106. In other words, the distance from the inner wall 105 to the point at which the upper protruding portion 107 and lower protruding portion 108 begin to protrude from the upper face 102 and lower face 103, respectively, is shorter than the distance the groove 106 extends into the inner wall 105.
In the illustrated aspect of the embodiment described herein, the lower protruding portion 108 protrudes away from the lower face 103 further than the upper protruding portion 107 protrudes away from the upper face 102. In other words, the relative height of the lower protruding portion 108 is taller than the relative height of the upper protruding portion 107.
Turning now to
As best shown in
Because the upper protruding portion 107 and lower protruding portion 108 are elastic and located above or below the groove 106, the upper protruding portion 107 and lower protruding portion 108 may compress and deform to form a bubble tight seal when torque and compressive load are applied to screw the fitting 120 into the port 130. Additionally, only standard industry torque and compressive load values need be applied to create higher contact stresses (i.e., sealing forces). Thus, under standard industry torque and compressive load values, the seal of the instant application is capable of creating higher contact stresses (i.e., sealing forces) than conventional seals and a bubble tight seal. Additionally, due to the orientation and size of the lower protruding portion 108, the sealing forces are localized on the conical surface of the port 130, which allows for tighter control of leakage.
In order to provide additional deformation and effect a tighter seal between the fitting 120 and port 130, the seal 100 may be plated with a ductile plating. The plating will plastically deform into features or imperfections on the surfaces of the fitting or port. The plating may be any suitable ductile plating, such as gold, nickel or silver. The plating may be located on every surface of the seal or, in an alternate configuration, on just the upper protruding portion 107 and lower protruding portion 108. The thickness of the plating layer, whether all over the seal or on only the upper protruding portion and lower protruding portion, may be any suitable thickness for the application in which the seal is used. In one aspect of the embodiment, the thickness of the plating is between about 0.0001 and 0.0010 inches. The plating thickness may also vary at different points on the same seal. In one aspect of the embodiment described herein, the seal may include a first plating layer and a second plating layer, the first and second plating layers being different ductile materials.
In order to withstand high temperature and high pressure operations, the seal comprises high-strength, heat resistant alloy. The alloy may be a steel alloy, nickel alloy or any other suitable metallic or non-metallic material.
The seal may be formed from one integral piece of material. That is to say, all parts of the seal are machined from a single piece of material without the need to attach portions of the seal (such as the lower protruding portion) via welding, soldering or other means of attachment.
In one aspect of the embodiment, the groove 106 of the seal 100 is adapted such that the groove 106 receives a thread of the fitting 120. In other words, the fitting 120 is screwed into the port 130 such that a thread of the fitting 120 resides in the groove 106 of the seal 100. The thread of the fitting 120 and groove 106 may have corresponding shapes, such as a V-shaped groove 106 and a V-shaped thread of the fitting 120. In this aspect, the lower protruding 108 portion will be flattened between a thread of the port 130 and a thread of the fitting 120 located below the thread of the fitting 120 residing in the groove 106. The ductility of the lower protruding portion 108 as described above allows for the deformation and flattening of the lower protruding portion 108 between the threads. In a specific aspect, an upper thread or the most uppermost thread of the fitting 120 resides in the groove such that the majority of the fitting 120 may be screwed into the port 130. Such a configuration further assists in effecting a seal between the port 130 and the fitting 120.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
This application claims the benefit of priority to U.S. Provisional Application No. 60/909,196, filed Mar. 30, 2007, the entirety of which is herein incorporated by reference.
| Number | Date | Country | |
|---|---|---|---|
| 60909196 | Mar 2007 | US |