This invention relates in general to oil and gas equipment, and in particular to variable ram packers for use in blowout preventers.
During oil and gas well drilling and workover operations, precautions must be taken to prevent high pressure from the earth formations from escaping. Blowout preventer assemblies often include pipe rams, each having a packer element within. When the rams are brought together, the force causes the elastomer in the packers to seal around the pipe.
Some rams are configured to seal around a particular diameter of pipe. Others are variable in inner diameter in order to seal around a range of pipe diameter sizes. A typical variable ram packer has a central elastomeric body with a semi-cylindrical recess for receiving a pipe. Wings may extend radially outward from the central body. Each wing has a flat face that abuts against the flat face of one of the wings of the packer in the other ram.
Metal inserts embedded in the elastomer extend around the cylindrical recess. Each insert typically has upper and lower plates joined by a web. Metal wing top plates bond to the upper side of each wing, and metal wing bottom plates bond to the lower side of each wing. In the prior art, the portion of each top and bottom wing plate in contact with the elastomer of the wing bonds to the elastomer. The bonding is caused by applying adhesive coatings to these surfaces before placing the top and bottom wing plates in the mold.
As the packers seal around a pipe, the elastomer deforms and the inserts move. The bonding of the top and bottom wing plates can cause considerable strain in the elastomer as the bonded portions are not free to move relative to the top and bottom wing plates.
Also, strain occurs to the wing faces after sealing engagement. The high pressure differential of the well bore fluid being sealed can tend to break down the elastomer at the wing faces. High temperatures can increase the break down. The well bore fluid being sealed tends to flow upward from the lower to the upper side of the packers if the pressure is higher below.
A variable ram packer has a body formed of an elastomer and having a central portion with an upper surface, a lower surface, and a central semi-cylindrical recess for sealing around a pipe. Wings extend from opposite lateral sides of the recess. Each of the wings has an upper surface and a lower surface with a face extending between. Multiple inserts are embedded within the central portion of the body and positioned around the recess. Each of the inserts has an upper plate at the upper surface of the central portion of the body, a lower plate at the lower surface of the central portion of the body and a web joining the upper and lower plates. An upper wing plate is on the upper surface of each of the wings, and a lower wing plate is on the lower surface of each of the wings. Each of the upper and lower wing plates has an inner edge overlapping one of the inserts and an outer edge. Each of the wing plates has an abutting surface extending inward from the outer edge and in abutment with a portion of the elastomer of the body extending outward from one of the plates of one of the inserts. An adhesive layer on an outer portion of each of the abutting surfaces bonds each of the upper and lower wing plates to the elastomer of the body. Each of the abutting surfaces has an inner portion free of the adhesive layer.
The adhesive layer on each of the abutting surfaces of the upper and lower wing plates has a radial length less than one-half a radial length of each of the upper and lower wing plates from the outer edge to the inner edge.
In one embodiment, each of the wings has an inner portion that joins the central portion of the body and an inclined section extending outward and upward from the inner portion. The outer edge of the abutting surface of each of the upper and lower wing plates is at an angle relative to the inner portion of each of the abutting surfaces. The outer portion that contains the adhesive layer is located only at the outer edge of each of the upper and lower wing plates.
In one embodiment, an upper inclined section plate is on an upper surface of each of the inclined sections, and a lower inclined section plate is on a lower surface of each of the inclined sections. An inner edge of each of the upper inclined section plates and the outer edge of one of the upper wing plates has a notch and tab engaging arrangement. An inner edge of each of the lower inclined section plates and the outer edge of one of the lower wing plates has a notch and tab engaging arrangement. Each of the adhesive layers is located at the notch and tab engaging arrangement of the upper and lower wing plates.
The inserts include a wing insert located at each junction of the curved recess with one of the wings. In one embodiment, a barrier plate joins the web of each of the wing inserts between and parallel with the upper and lower plates of each of the wing inserts. Each of the barrier plates has a face edge that is substantially flush with the face of one of the wings. Each of the barrier plates has a back edge spaced farther from the face of the wing than any back portion of either of the plates of the wing insert. Each of the barrier plates has an outer edge spaced farther from the recess than any portion of either of the wing inserts.
So that the manner in which the features, advantages and objects of the disclosure, as well as others which will become apparent, are attained and can be understood in more detail, more particular description of the disclosure briefly summarized above may be had by reference to the embodiment thereof which is illustrated in the appended drawings, which drawings form a part of this specification. It is to be noted, however, that the drawings illustrate only a preferred embodiment of the disclosure and is therefore not to be considered limiting of its scope as the disclosure may admit to other equally effective embodiments.
The methods and systems of the present disclosure will now be described more fully hereinafter with reference to the accompanying drawings in which embodiments are shown. The methods and systems of the present disclosure may be in many different forms and should not be construed as limited to the illustrated embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey its scope to those skilled in the art. Like numbers refer to like elements throughout.
Referring to
Elastomeric body 13 has a pair of wings 19, each joining central portion 14 extending laterally outward relative to axis 17. Both the left-hand and right-hand wings 19 are referred to by the same numeral. Each wing 19 has a flat wing face 21 that are located in an axial radial plane. Wing faces 21 join recess 15 and are located in a common plane. Each wing 19 has a back side 23 that may be parallel with wing faces 21.
Inserts 25 are embedded in the elastomeric material of elastomeric body 13 around recess 15. Inserts 25 are identical to each other and are formed of a rigid material, such as a metal. As shown in
Two of the inserts 25 are located at the junction with each wing face 21 and recess 15. These two inserts 25, referred to herein as wing inserts 33, are identical to the other inserts 25, except that each may have a barrier plate 35. As described in more detail below, each barrier plate 35 is in a plane parallel with planes of insert upper plates 27 and lower plates 29. Each barrier plate 35 is located approximately equidistant between upper and lower plates 27,29. Barrier plates 35 are mounted to only the wing inserts 33, not the other inserts 25.
Referring still to
Each wing top plate 39 has an outer edge 45 at the inner edge of wing inclined section 37. Wing top plate outer edge 45 abuts the inner edge of wing top inclined plate 41. Referring again to
Referring again to
Adhesive coating 53 will cause wing top plate 39 to adhere to the elastomer in only a small part of the upper portion of wing 19 outward from wing insert upper plate 27 (
In this embodiment, a notch 55 (
Referring to
During manufacturing, adhesive coatings are conventionally applied to portions of the inserts 25, 33 and wing inclined plates 41, 51. Adhesive coatings 53, 57 are applied to wing plates 39, 49 as described. The various inserts 25, 33 and wing plates 39, 41, 49 and 51 are placed in a mold and an elastomer is injected under high pressure. Packer 11 is removed from the mold after curing.
When packers 11 are installed in rams, and the rams are moved together to seal around a pipe, the elastomer stretches and deforms to meet the faces of the pipe. The large area of elastomer of body 13 that is located behind wing inserts 33 stretches the most. The small adhesive strips 53, 57 at the outer edges of wing plates 39, 49 allow more of the elastomer in this area to expand freely and not become overstrained. This adhesive configuration for the packer 11 allows the packer to seal at higher temperatures for a longer period of time. This means that the packer 11 has a longer life and is capable of longer periods of operation.
Barrier plate 35 (
Each barrier plate 35 is rigid and may be formed of metal. The left-hand barrier plate 35 (
In operation, rams (not shown) are brought together, with wing faces 21 abutting and the rubber of body 13 at recess 15 sealing around a pipe. The sealing engagement blocks well bore fluid from below the mating packers 11 from fluid above. The barrier plates 35 create a tortuous path for any fluid that has broken down the elastomer of packer body 13 at wing faces 21 trying to move from below to above, or vice-versa. The face edges 65 of the barrier plates 35 in each packer 11 mate, forming a solid barrier for any well bore fluid that has successfully broken down the rubber at wing faces 21. As the well bore fluid encounters this solid barrier, it is forced to migrate back into the packer 11 and thus has a much longer path through the rubber body 13 before it can escape the seal created by the packers 11. Since it lakes time for the rubber to break down during exposure to well bore fluid, barrier plates 35 create a longer packer life. Barrier plates 35 also assist in maintaining the life of the packers under elevated temperatures.
It is to be understood that the scope of the present disclosure is not limited to the exact details of construction, operation, exact materials, or embodiments shown and described, as modifications and equivalents will be apparent to one skilled in the art. In the drawings and specification, there have been disclosed illustrative embodiments and, although specific terms are employed, they are used in a generic and descriptive sense only and not for the purpose of limitation.
This application claims priority to provisional patent application Ser. No. 62/089,642, filed Dec. 9, 2014.
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