Abstract
In a blowout preventer central bore and a central bore axis with an oval ram cavity having a ram cavity axis having one or more horizontal interface portions between the ram cavity and an actuator body, a method of connecting the actuator body to the ram cavity comprising providing one or more locking bar receptacles passing through one or more of the planes of the one or more horizontal interface portions of the ram cavity, providing one or more locking bar receptacles passing through one or more of the planes of the one or more horizontal interface portions of the actuator body, and providing one or more locking bars in one or more of the one or more locking bar receptacles in both the ram cavity and the actuator body.
Claims
1. In a blowout preventer central bore and a central bore axis with an oval ram cavity having a ram cavity axis having one or more horizontal interface portions between the ram cavity and an actuator body, a method of connecting the actuator body to the ram cavity comprising providing one or more locking bar receptacles passing through one or more of the planes of the one or more horizontal interface portions of the ram cavity, providing one or more locking bar receptacles passing through one or more of the planes of the one or more horizontal interface portions of the actuator body, and providing one or more locking bars in one or more of the one or more locking bar receptacles in both the ram cavity and the actuator body.
2. The method of claim 1 further comprising the locking bar receptacles are round.
3. The method of claim 1 further comprising the locking bar receptacles are rectangular.
4. The method of claim 1 further comprising the locking bar receptacles are hexagon shaped.
5. The method of claim 1 further comprising the locking bar receptacles are flat on the top and bottom and sloping inwardly on at least one side proximate the top corner and proximate the bottom corner to an intersection proximate the middle.
6. The method of claim 1 further comprising the locking bar is are flat on the top and bottom and sloping inwardly on at least one side proximate the top corner and proximate the bottom corner to an intersection proximate the middle.
7. The method of claim 1 further comprising two locking bar opposing sides approximate the shape of an “X”.
8. The method of claim 1 further providing the locking bar having a locking bar axis and an inner locking bar segment and an outer locking bar segment which have an interface between them which is in a plane at a first angle about a first axis parallel to the central bore axis which passes through the locking bar axis and the ram cavity axis to a plane defined by the first axis and the locking bar axis.
9. The method of claim 8 further providing moving the inner locking bar segment relative to the outer locking bar segment to preload the actuator body with the ram cavity.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0016] FIG. 1 is a view of a contemporary deep-water riser system.
[0017] FIG. 2 is a perspective view of a blowout preventer stack utilizing the features of this invention.
[0018] FIG. 3 is a perspective view of a subsea wellhead housing which the blowout preventer stack of this invention would land on.
[0019] FIG. 4 is a perspective view of the lower portion of the blowout preventer stack of FIG. 2, generally called the lower BOP stack.
[0020] FIG. 5 is a perspective view of the upper portion of the blowout preventer stack of FIG. 2, generally called the lower marine riser package or LMRP.
[0021] FIG. 6 is a perspective view of a section of the drilling riser which will be used to lower the blowout preventer stack.
[0022] FIG. 7 is a view of the blowout preventer stack of FIG. 2, taken along lines “7-7.
[0023] FIG. 8 is a view of the blowout preventer stack of FIG. 2, taken along lines “8-8.
[0024] FIG. 9 is a top view of FIG. 8.
[0025] FIG. 10 is a perspective view of a locking bar.
[0026] FIG. 11 is a perspective view of a blowout preventer body similar to item 130 if FIGS. 7 and 8 with an actuator partially exploded.
[0027] FIG. 12 is a cross section of a portion of the blowout preventer taken along lines “12-12”.
[0028] FIG. 13 is an end view of an actuator taken along lines “13-13” of FIG. 12.
[0029] FIG. 14 is a cross section of FIG. 13 taken along lines “14-14” of FIG. 13 showing loadings imparted to the actuator bar.
[0030] FIG. 15 a top view of an locking bar taken along lines “15-15” of FIG.
[0031] 13.
[0032] FIG. 16 is a cross section of the locking bar of FIG. 15 taken along lines “16-16”.
[0033] FIG. 17 is a perspective view of two locking bars defining the plane separating to parts of a locking bar.
DETAILED DESCRIPTION OF THE INVENTION
[0034] Referring now to FIG. 1, a view of a system 20 which might use the present invention is shown. It shows a floating vessel 22 on a body of water 24 and having a derrick 26. Drill pipe 28, drilling mud system 30, control reel 32, and control cable 34 are shown. A riser system 40 including a flex joint 42 is shown. During drilling the drilling mud circulated from the drilling mud system 30, up the standpipe 44, down the drill pipe 28, through the drill bit 46, back up through the casing strings 48 and 50, through the blowout preventer stack 60, up thru the riser system 40, and out the bell nipple at 62 back into the mud system 30.
[0035] Blowout preventer stack 60 is landed on a subsea wellhead system 64 landed on the seafloor 66. The blowout preventer stack 60 includes pressurized accumulators 68, kill valves 70, choke valves 72, choke and kill lines 74, choke and kill connectors 76, choke and kill flex means 78, and control pods 80.
[0036] Referring now to FIG. 2, the seafloor drilling system 100 comprises a lower blowout preventer stack 102, a lower marine riser package 104, a drilling riser joint 106, and control cables 108.
[0037] Referring now to FIG. 3, a subsea wellhead is shown which the seafloor drilling system lands on. It is the unseen upper portion of the subsea wellhead system 64 shown in FIG. 1.
[0038] Referring now to FIG. 4, the lower blowout preventer stack 102 comprises a lower structural section 120, vertical support bottle 122, and upper structural section 124, accumulators 126, choke and kill valves 128, blowout preventers 130 and an upper mandrel 132 which will be the connection point for the lower marine riser package.
[0039] Referring now to FIG. 5 the lower marine riser package 104 is shown comprising a lower marine riser package structure 140, an interface 142 for a remotely controlled vehicle (ROV), annular blowout preventers 146, choke and kill flex loops 148, a flexible passageway 150, a riser connector 152, and an upper half of a riser connector 154.
[0040] Referring now to FIG. 6, a drilling riser joint 106 is shown having a lower half of a riser connector 160, a upper half of a riser connector 154, and buoyancy sections 162.
[0041] Referring now to FIG. 7, is a view of seafloor drilling system 100 taken along lines “7-7” of FIG. 1 showing wellhead connector 170, lower marine riser connector 172, a man 174 for size perspective, and choke and kill valves 176.
[0042] Referring now to FIG. 8, is a view of seafloor drilling system 100 taken along lines “8-8” of FIG. 1.
[0043] Referring now to FIG. 9, is a top view of seafloor drilling system 100.
[0044] Referring now to FIG. 10 a much simpler bonnet retention means is shown in perspective as locking bar 200. It can be utilized in a square, rectangular, hexagon, round, “X” or other shape, with the “X” shape being described herein. Locking bar 200 provides tapered ends 202 for easy insertion and has a hole 204 on each end for retaining in place. The locking bar 200 shape can be straight for easy insertion, tapered for a snug fit, or made of multiple tapered parts for easy insertion and then expansion to a snug fit once inserted.
[0045] Referring now to FIG. 11, a first locking bar 200 is shown being inserted into a similarly shaped receptacle in blowout preventer body 210 and a second locking bar 200 is shown completely installed. Similarly a first locking bar 212 is shown being inserted into a similarly shaped receptacle in actuator body 214 and a second locking bar 212 is shown completely installed. It can readily seen that both the locking bar 200 and the locking bar 212 provide large areas in shear to retain the bonnet 214 and the bonnet end cap 216 rather than the limited circular diameter of bolting which might be utilized otherwise.
[0046] Referring back to FIGS. 7 and 8 it can be noted that by utilizing this bonnet connection method, the actuators can be placed right next to each other rather than requiring both added vertical and horizontal spacing to allow for the makeup of bolting. As every inch of height and length provide actual cost, weight addition, and extra handling cost on this type equipment.
[0047] Referring now to FIG. 12, a cross section generally taken along lines “12-12” of FIG. 11 (unexploded) is shown with the piston rod 220, piston 222, profile on the end of the piston rod 224 for engaging the rams.
[0048] Referring now to FIG. 13 which is generally taken along lines “13-13” of FIG. 12 showing the end of the actuator body 214 and the bonnet end cap 216 with the locking bar 212 approaching. It will be noted that both the piston 222, the bonnet end cap 216 and the actuator body 214 are in the form of a “race track” oval, as the ram cavities are. This is to gain a greater piston area than would be available in the spacing using a simple circular piston. It will be noted that at the pressures required to operate these blowout preventers, the center of the “race track” oval actuator body 214 will tend to be deflect and produce a gap 230 with the piston 222 and the bonnet end cap 216.
[0049] Referring now to FIG. 14 which is a cross section of locking bar 212 taken along lines “14-14” of FIG. 13 showing that the pressure force 250 of the pressurized fluids in the system will be restrained by a mechanical force 252, generally causing a shear stress in the shear plane 254. The length of shear plane 254 can be made as long as required to reduce the shear stresses to an acceptable level. It can also be noted that due to the angle 256 which is shown to be 30° forces 250 and 252 generate forces 258-264 which restrain the deflection in the actuator body 214 which produced the gap 230 therefore making the seals sealing within the actuator body 214 more reliable. The same will be true of the locking bar 200 and the blowout preventer body 210. In this case the wall thicknesses are much thicker to minimize deflection, but the pressures sustained to cause deflection are also considerably higher. Typically the actuator body will see pressures in the range of 3,000 to 5,000 p.s.i. and the blowout preventer bodies will see pressures in the range of 5,000 to 20,000 p.s.i.
[0050] Referring now to FIG. 15 which is taken along lines “15-15” of FIG. 13, a top view of a locking bar 270 is shown being made of two pieces 272 and 274 with an angled interface at 276. Each of these pieces are tapered such that after being pushed into a mating profile, they can be move one relative to the other to expand their width and remove all “play” or movement within the mating profile. If pressed hard enough they can be fully preloaded to any force expected to be experienced.
[0051] Referring now to FIG. 16 which is taken along lines “16-16” of FIG. 15, it can be seen that the profile is similar to the profile in FIG. 14 and that the length of the load supporting shear plane has not been reduced. In fact the length of the shear plane has been slightly increased as there is no gap between locking bar 270 and the mating profile.
[0052] Referring now to FIG. 17 rotational axis 280 is parallel to central bore axis 282 and passes through both ram cavity axis 284 and locking bar axis 286. Plane 290 is defined by rotational axis 280 and locking bar axis 286. Plane 292 shown in dashed lines is rotated from plane 290 about rotational axis 280 at angle 294. Interface 276 is in plane 292.
[0053] The particular embodiments disclosed above are illustrative only, as the invention may be modified and practiced in different but equivalent manners apparent to those skilled in the art having the benefit of the teachings herein. Furthermore, no limitations are intended to the details of construction or design herein shown, other than as described in the claims below. It is therefore evident that the particular embodiments disclosed above may be altered or modified and all such variations are considered within the scope and spirit of the invention. Accordingly, the protection sought herein is as set forth in the claims below.
