Liner hanger

Information

  • Patent Grant
  • 6431277
  • Patent Number
    6,431,277
  • Date Filed
    Wednesday, September 27, 2000
    23 years ago
  • Date Issued
    Tuesday, August 13, 2002
    21 years ago
Abstract
A liner hanger assembly has a slip actuation system which is locked for run-in. A piston assembly bolts onto the mandrel in a sealable manner to actuate a mechanical lock. Upon release of the lock, a plurality of springs actuate a sleeve which is in turn attached to the slips to move them relative to their slip seats. The slip seats are preferably mounted to the mandrel without welding and have longitudinal spaces for mud or cement flow therebetween. Load is distributed from each slip through its slip seat into the mandrel without interaction from an adjacent slip or slip seat. A rupture disk ensures that a predetermined pressure is built up before the piston can actuate to defeat the lock. The lock can come in a variety of configurations. One of which is a sliding sleeve over a dog and another is a yoke over a split ring which, when shifted, allows the split ring to expand, thus unlocking the parts. The slips can also be configured to allow flow of mud or cement behind them, thus reducing the resistance to flow of such materials.
Description




FIELD OF THE INVENTION




The field of this invention relates to liner hangers, and, more particularly, to the techniques for securing liner hangers in well bores.




BACKGROUND OF THE INVENTION




Liner hangers are secured in the well bores by slips. Actuation systems for such slips in the past brave employed full circumference hydraulically actuated pistons to move the slips. These designs presented a pressure rating problem in that the full circumference piston frequently had a maximum working pressure significantly lower than the mandrel which it surrounded. Thus, this type of design limited the maximum working pressure in the string to the rating of the cylindrical piston housing assembly. For example, it was not unusual in prior designs to have mandrels rated for 12,000 PSI while the surrounding cylinder housing for the cylindrical piston to only have a rating of approximately 3,000 PSI. In an effort to improve the shortcoming of this design, another design illustrated in U.S. Pat. No. 5,417,288 was developed. In this design the mandrel body received a pair of bores straddling each of the slips. A piston assembly was mounted in each of the bores with all of the necessary seals. The application of hydraulic pressure in the mandrel into all the piston bores actuated the pistons on either side of each slip through a common sleeve to which all the slips were attached. This design, however, was expensive to manufacture and had many potential leak paths in the form of the ring seals on each of the pistons wherein each slip required two pistons. This design, however, did provide for a higher pressure rating for the liner hanger body. It also used the hydraulic pressure directly to actuate the slips. Necessarily it did not include a locking feature against premature slip movements due to inadvertently applied pressures. The design in the U.S. Pat. No. 5,417,288 also did not provide for flexibility for changed conditions down-hole which could require additional force to set the slips. In essence, each application was designed for a pre-existing set of conditions with field variability not included as a feature of that prior art design.




Slip assemblies in the past have been configured in a variety of ways. In one configuration, when the slips are actuated, the load is passed through the slips circumferentially through their guides or retainers and transmission of the load to the underlying mandrel is avoided. In other more traditional designs, the slips are driven along tapered surfaces of a supporting cone and the loading is placed on the supporting mandrel is in a radial direction toward its center, thus tending to deform the mandrel when setting the slips. Typical of such applications are U.S. Pat. Nos. 4,762,177, 4,711,326 and 5,086,845.




The design of the liner hanger needs to accommodate circulation of mud and cement. The prior designs, particularly those using a cylindrical piston, obstructed the passages that could have been used for circulating cement and mud.




The apparatus of the present invention has many objectives. A versatile actuation system for a locking system is provided. The apparatus uses a combination of hydraulic pressure to defeat a locking mechanism which in turn allows mechanical actuation of the slips. The slips are configured to pass the loading into the slip seat and then into the mandrel in a manner so as not to deform the mandrel. The slips act independently of each other and transfer their load through the surrounding slip seat directly to the mandrel. The slip seats are attached to the mandrel without welding because standard setting organizations and well operators have restrictions against connecting parts made of certain materials by welding or against welding altogether in down-hole tools. The slip seats are spaced from each other to provide flow channels along the exterior of the liner hanger to facilitate the movement of cement or mud. Those passages are continued for the length of the tool. The actuating piston assembly to defeat the lock mechanism is a bolt-on arrangement which can be readily interchanged in the field to react to changing down-hole conditions. The actuating piston is fully compensated for thermal effects and a system is provided to vent any gases from the piston actuation system which is used to defeat the lock. The lock can be in a number of alternative styles. One of which involves using a dog to hold the parts together for run in and liberating the dog from its groove to allow setting of the slips, which is preferably done by a plurality of springs. The parts are also disposed in a preferred spacing to make maximum use of the limited force available from the piston assembly for releasing the lock. The lock configuration can also be in the form of a split ring held together by a yoke which allows relative movement when the yoke is shifted, allowing the split ring to expand. These and other objectives of the present invention will become more apparent to those skilled in the art from a review of the preferred and alternative embodiments described below.




SUMMARY OF THE INVENTION




A liner hanger assembly has a slip actuation system which is locked for run-in. A piston assembly bolts onto the mandrel in a sealable manner to actuate a mechanical lock. Upon release of the lock, a plurality of springs actuate a sleeve which is in turn attached to the slips to move them relative to their slip seats. In an alternative embodiment, a plurality of springs can directly move the slips relative to their slip seats, when the springs are released. The slip seats are preferably mounted to the mandrel without welding and have longitudinal spaces for mud or cement flow therebetween. Load is distributed from each slip through its slip seat into the mandrel without interaction from an adjacent slip or slip seat. A rupture disk ensures that a predetermined pressure is built up before the piston can actuate to defeat the lock. The lock can come in a variety of configurations. One of which is a sliding sleeve over a dog and another is a yoke over a split ring which, when shifted, allows the split ring to expand, thus unlocking the parts. Yet another variant is a yoke restraining a split ring. The slips can also be configured to allow flow of mud or cement behind them, thus reducing the resistance to flow of such materials.











DETAILED DESCRIPTION OF THE DRAWINGS





FIGS. 1A through C

are a plan view of the apparatus looking down on the spring housing;





FIG. 2

is a rotated view from the view of

FIGS. 1A and B

showing a plan view of the lock housing;





FIG. 3

is a section view through lines


3





3


of

FIG. 2

;





FIG. 4

is a section of lines


4





4


of

FIG. 2

;





FIG. 5

is a section through lines


5





5


of

FIG. 2

;





FIG. 6

is a section through lines


6





6


of

FIG. 2

;





FIGS. 7A through C

are a section view through the lock housing during the run-in position;





FIG. 8

is the section view through the piston housing in the set position when the lock has been defeated.;





FIG. 9

illustrates the connection between the spring housing and the gage ring;





FIG. 10

illustrates the springs used to set the slips and the guide for each spring in section through either the spring housing or the lock housing.





FIG. 11

is a top view showing the longitudinal passages that facilitate the flow of cement or mud;





FIG. 12

is a section view through the piston housing retainer bolt showing the passages therethrough;





FIG. 13

is a section view through the piston housing showing the passages from the retainer bolt to the rupture disk location;





FIG. 14

is a plan view of one of the slips;





FIG. 15

is a perspective view of the same slip shown in

FIG. 14

, showing the slip in perspective and the sloping end surfaces;





FIG. 16

is a plan view of the lock dog retainer;





FIG. 17

is a section view through lines


17





17


in

FIG. 16

;





FIG. 18

is a section view of the lock dog;





FIG. 19

is a plan view of the lock dog release;





FIG. 20

is a section view through lines


20





20


of

FIG. 19

;





FIG. 21

is a partial section through the longitudinal interior passage in the lock housing which in part holds the locking dog;





FIG. 22

is a plan view of the lock housing;





FIG. 23

is a plan view of the slip seat;





FIG. 24

is a section view through lines


24





24


of

FIG. 23

;





FIG. 25

is a section view through lines


25





25


of

FIG. 24

;





FIG. 26

is a section through the slip seat retainer;





FIG. 27

is a plan view of the mandrel;





FIG. 28

is a more detailed plan view of the mandrel;





FIG. 29

is a section through lines


2929


of

FIG. 28

;





FIG. 30

is a section view of an alternative embodiment taken through one of the slips;





FIG. 31

is a plan view of the slip shown in

FIG. 30

taken along line


31





31


of FIG.


30


.





FIGS. 32A and B

are the view of

FIGS. 30

A through C rotated to show the spring housings;





FIGS. 33A and B

are the view of

FIGS. 30

A through C rotated to show the spring housings;





FIGS. 33A and B

are the view of

FIGS. 30

A through C further rotated to show the locking feature;





FIG. 34

is an elevation view of the snap ring;





FIG. 35

is an isometric view of the internal key;





FIG. 36

is a view taken along lines


36





36


of FIG.


31


.





FIG. 36



a


illustrates a longitudinal cross section of the tool through the piston assembly, lock mechanism, slip and slip seat.





FIG. 37

is a plan view of the tool in the set position.





FIG. 38

is a plan view of the tool in the run-in position.





FIG. 39

is a section view of the piston assembly and lock mechanism in the run-in position.





FIG. 40

is a section view of the piston assembly and lock mechanism in the set position.





FIG. 41

is a section view through

FIG. 39

, of the piston assembly bolted to the mandrel.





FIG. 42

is an end view of the lock.





FIG. 43

is an end view of the snap ring.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring to

FIGS. 1 through 11

, the major components of the apparatus in A will now be described. Apparatus A has a mandrel


10


which has a lower end


12


. Lower end


12


is shown schematically and those skilled in the art will appreciate that the liner string is connected at lower end


12


. The mandrel


10


has an upper end


14


to which those skilled in the art will appreciate is attached a running string for proper positioning of securing assembly S shown in

FIGS. 1A through C

. The mandrel


10


has a shoulder


16


which defines a reduced diameter segment


18


.




A gage ring


20


is shown in FIGS.


1


A and in section in FIG.


3


. The gage ring


20


has a split


22


(see

FIG. 3

) and a draw bolt


24


so as to bring the components of the gage ring


20


together at split


22


once the gage ring


20


has been advanced beyond the shoulder


16


and onto the reduced diameter segment


18


. Gage ring


20


has several flats, one of which


26


is shown in interrupted form in FIG.


9


.

FIG. 9

is a section view through the gage ring


20


showing the spring housing


28


mounted to it.




By comparing

FIGS. 1A and 9

, it can be seen that the spring housing


28


has a tab


30


which extends into a window


32


in flat


26


of gage ring


20


. In that manner as shown in

FIG. 9

, the position of the spring housing


28


is initially fixed to the gage ring


20


and that engagement is secured by bolts


34


.





FIG. 2

shows a rotated view from

FIGS. 1A and B

, indicating that the gage ring


20


also supports the lock housing


36


. The number of spring housings


28


can vary without departing from the spirit of the invention. In the preferred embodiment disclosed, there are three spring housings


28


and one lock housing


36


, generally at 90 degree spacings, thus defining elongated passages


38


therebetween (see FIG.


11


), these passages


38


shown schematically in

FIG. 1B

allow mud or cement to pass relatively unimpeded.




Referring again to

FIG. 2

, the lock housing


36


is secured to the gage ring


20


by bolts


34


.




Referring to

FIG. 22

, a top view of the lock housing


36


is illustrated. It has a top end


40


adjacent to which are the openings


42


through which the bolts


34


are inserted. Also shown in hidden lines is a downwardly oriented tab


44


which is placed through a corresponding opening or window in the gage ring


20


, similar to the method of attachment shown in FIG.


1


A. The lock housing


36


also has an extending arm


46


which is rectangular in cross-section and includes a receptacle


48


for engagement of a slip


50


(see FIG.


1


B). It should be noted that

FIG. 1B

illustrates in dashed lines the movement of receptacle


48


into a second position which reflects the setting of the slip


50


. Arm


46


, shown in

FIG. 22

also has an oblong undercut


52


which fits into slot


54


of slip seat retainer


56


(see FIGS.


26


and


1


B). In that manner the slot


54


acts as a guide to the longitudinal motion of lock housing


36


. It also holds arm


46


against centrifugal force created by rotation of the apparatus A at speeds as high as about 250 RPM. The same configuration is found in the spring housing


28


shown in

FIGS. 1A through C

employing the identical undercut


52


with the same slip seat retainer


56


providing a slot


54


to guide an arm


46


which in turn through receptacle


48


secures yet another slip


50


. It should be noted that

FIG. 2

is a partial view of the lock housing


36


shown in a rotated position from the view of

FIG. 22

, and therefore, it does not show the arm


46


or receptacle


48


at the end of it which is used to connect to a slip


50


. Referring again to

FIG. 22

, the lock housing


36


has a series of blind bores


58


, two of which are shown in

FIG. 22

in hidden lines. A section through one of the blind bores


58


is seen in FIG.


10


. There, a spring


60


surrounds a spring retainer


62


. In the run-in position, the spring


60


is compressed so that when the lock mechanism L is released, the energy stored in spring


60


is also released allowing upward movement of the gage ring


20


as shown by comparing

FIGS. 7 and 8

. Initially, however, each of the spring housings


28


has a plurality of blind bores


58


(see FIG.


1


B), each of which has a spring


60


and a retainer


62


mounted therein. The number of springs and the size of the spring


60


can vary without departing from the spirit of the invention. Those skilled in the art will appreciate that the number of available spring


60


and their size will dictate the amount of upward force that can be exerted on gage ring


20


which pulls up with it the spring housing


28


and the lock housing


36


, which in turn pull slips


50


relative to slip seat


64


, securing assembly S to a tubular in the well bore.




One version of the lock mechanism L will now be described. The lock housing


36


has a multi-dimensional longitudinal opening


66


(see FIG.


22


). As shown in

FIG. 22

, the opening


66


extends for a significant length of the piece and then continues as a bore


68


which has a generally rectangular cross-section with a downwardly depending opening


70


, shown in hidden lines in

FIG. 22 and a

subsequent upwardly depending opening


72


. These features can be better seen in the section view of the lock housing


36


illustrated in FIG.


21


. In

FIG. 21

, bore


68


is illustrated with an opening


74


for insertion of a breakable pin


76


(see FIG.


7


B). Further down bore


68


is another opening


78


for the insertion of a guide pin


80


(see FIG.


7


A). Finally, the downwardly oriented opening


70


and upwardly oriented opening


72


are illustrated as well as one opening


42


for attachment to the gage ring


20


. The downwardly oriented opening


70


accepts a dog


82


. Its tapered up-hole and down-hole surfaces


84


and


86


(see

FIG. 18

) are illustrated to be disposed at preferably an 80 degree angle measured from the lower end


88


of dog


82


. Dog


82


sits in notch


90


on the mandrel


10


as shown in FIG.


7


A. Notch


90


has tapered surfaces conforming to the tapered surfaces


84


and


86


of dog


82


. While 80 degrees is preferred, other angles can be used without departing from the spirit of the invention. The matching taper angles between the dog


82


and the receptacle


90


facilitate in driving the dog


82


out of receptacle


90


. In the run-in position shown in

FIG. 7A

, the dog


82


is retained by lock dog retainer


92


. As show in

FIGS. 7A and B

, the lock dog retainer


92


overlays the dog


82


holding it in the notch


90


on mandrel


10


. Referring to

FIG. 16

which is a top view of the lock dog retainer


92


, an elongated slot


94


accepts the guide pin


80


which extends through the lock housing


36


. In that manner, the guide pin


80


limits the down-hole movement of lock dog retainer


92


. This concept is illustrated in

FIG. 16

by placement of guide pin


80


in the slot


94


to illustrate that only movement up-hole or to the left in

FIG. 16

is possible for lock dog retainer


92


. Lock dog retainer


92


has a receptacle


96


shown in FIG.


16


. As shown in

FIGS. 19 and 20

, receptacle


96


accommodates tab


98


of lock dog release


100


. In an important feature, the width of tab


98


is shorter than the length of receptacle


96


, thus allowing for the possibility of relative motion therebetween. For the run-in position, the lock dog release


100


has a receptacle


102


(see

FIGS. 19 and 20

) which accepts pin


76


, which in turn extends through the lock housing


36


. Thus, for run-in, the lock dog release


100


is pinned to the lock housing


36


and has a tab


98


inserted into receptacle


96


of lock dog retainer


92


.

FIG. 16

shows the maximum down-hole position of lock dog retainer


92


due to the travel limitation of guide pin


80


extending into slot


94


. In the position shown in

FIG. 16

, the tab


98


of lock dog release


100


is so positioned in receptacle


96


so as to be able to move up-hole, i.e. toward pin


80


for a limited distance before tandem movement of lock dog release


100


and lock dog retainer


92


occurs. The significance of the relative movement will be explained later.




Referring to the section view of the lock dog retainer


92


(FIG.


17


), it can also be seen that it has an undercut


104


which is offset from dog


82


in

FIGS. 7A and B

, and shifted to coincide with dog


82


in FIG.


8


. Those skilled in the art will appreciate that when the undercut


104


moves over the dog


82


the dog can be pushed out of notch


90


, thus allowing an unlocking of the lock housing


36


from the mandrel


10


. As previously explained, when such unlocking of the lock mechanism L occurs, the various springs


60


bearing on their respective retainers


62


collectively expand up hole, moving the spring housings


28


and the lock housing


36


, along with gage ring


20


to which housings


28


and


36


are connected, which has the ultimate effect of pulling the slips


50


to set them.




In order to actuate the lock mechanism L to unlock and permit setting of the slips


50


a release device is required. In this instance, the release device comprises a piston housing


106


which has internal passages which are best seen in FIG.


13


. Passage


108


accepts a bolt


110


whose details are best shown in FIG.


12


. Bolt


110


is placed over an opening


112


in the mandrel


10


. The piston housing


106


has a circular groove


114


which accepts a sealing member, such as an O-ring


116


(see FIG.


7


B). With bolt


110


securing the piston housing


106


about the opening


112


, there is a sealed passage from inside the mandrel


10


through the bolt


110


, through its passage


118


(see FIG.


12


). Passage


118


in bolt


110


is sealingly aligned to passage


120


in piston housing


106


. Passage


120


leads to passage


122


within which are mounted a rupture disk


124


and a piston assembly


126


(see FIG.


7


B).





FIG. 7B

shows the rupture disk


124


adjacent the piston assembly


126


all within the passage


122


of the piston housing


106


. The purpose of the rupture disk


124


is to insure that a certain minimum pressure is achieved in the mandrel


10


before internal pressure in mandrel


10


is communicated to the piston assembly


126


. The piston assembly


126


has a central passage


128


which can be sealed by a cap


130


in combination with a seal


132


. Externally, the piston assembly


126


has a seal


134


to seal it in passage


122


for reciprocal movement therein. The cap


130


allows proper displacement of air or other gases from passage


122


as the piston assembly


126


is inserted into the passage


122


. Upon insertion to the position shown in

FIG. 7B

, the trapped fluids are displaced through passage


128


until the desired position of the piston assembly


126


is reached. At that time, the cap


130


is screwed on, sealing off the piston assembly


126


in passage


122


. Prior to installing the piston assembly


126


, the rupture disk


124


is inserted. The piston assembly


126


is thus free to move in opposed directions to compensate for thermal effects or other effects. As shown in

FIG. 7B

, there is a space between the piston assembly


126


extending out of the piston housing


106


and the lock dog release


100


. This space can also be easily seen in FIG.


2


. Those skilled in the art will appreciate that the piston housing


106


as well as the piston assembly


126


which is in it, can be easily replaced with a different sized unit to accommodate these specific down hole conditions as they occur. Such replacements can be done in the field without having to send the tool back to the shop. What is simply done is that the bolt


110


is loosened and a different piston housing


106


, having a bigger or smaller piston, or with a rupture disk


124


set to break at a different value is easily insertible as a unit in replacement of the original equipment. Thus the bolt-on feature of the piston housing


106


holding the piston assembly


126


adds versatility to the apparatus A of the present invention and allows for field changes to meet last minute changes in well operating conditions where the apparatus A is to be set. It also facilitates the presence of passages


38


.




In order to set the slips


50


, pressure must be built up sufficiently within the mandrel


10


to break the rupture disk


124


. When the rupture disk


124


breaks, pressure is then applied to the piston assembly


126


, moving the piston to the left as seen by comparing

FIGS. 7B and 8B

. The piston assembly


126


first impacts the lock-dog release


100


, pushing it up hole. As seen in

FIG. 2

, the lock-dog release


100


has a downwardly oriented tab


136


adjacent to an opening


138


. As shown in

FIGS. 7A & B

, the lock-dog release


100


is initially retained by a shear pin


76


or similar retaining device. The impact of the piston assembly


126


on the lock-dog release


100


breaks the shear pin


76


and starts the lock-dog release


100


moving up hole. It should be noted that at this time there is no movement of the lock-dog retainer


92


. As previously explained, the receptacle


96


of the lock-dog retainer


92


(see

FIG. 16

) is longer than the width of the tab


98


on lock-dog release


100


. As a result, the energy imparted into the piston assembly


126


is initially expended solely to break the shear pin


76


without also, at the same time, having a need to overcome the frictional resistance between the lock-dog retainer


92


and the dog


82


, which it squeezes into notch


90


. Those skilled in the art will appreciate that these movements occur almost instantaneously so that after the shear pin


76


is broken and the piston assembly


126


is moving in tandem with lock-dog release


100


, the lock-dog retainer


92


is eventually driven up hole as shown in FIG.


8


A. This places the undercut


104


(see

FIG. 17

) in alignment with dog


82


. Further movement of lock-dog retainer


92


allows springs


60


to push lock housing


36


which in turn forces tapered surface


84


of dog


82


along its parallel surface in notch


90


so that the dog


82


comes out of notch


90


to the final position shown in FIG.


8


A. It should be noted that as these movements are occurring, the tab


136


pushes any mud out through opening


138


in lock-dog release


100


. Similarly, the uphole movement of lock-dog retainer


92


forces any adjacent mud through the upwardly oriented opening


72


in the lock housing


36


.




With the dog


82


out of notch


90


, the spring housings


28


and lock housing


36


are no longer held to the mandrel


10


. At that point, the springs


60


in the various spring housings


28


and the lock housing


36


can push off against their respective retainers


62


, thus moving uphole all of the spring housings


28


and lock housing


36


along with gauge ring


20


. This upward movement shown by a comparison of

FIGS. 7 & 8

results in a pull upward on all of the slips


50


which drives the slips


50


outwardly into a gripping engagement with the tubular in the well bore to set the apparatus A.




The method of securing the slips


50


to the respective slips seat


64


will now be described. Each of the slip seats


64


can be attached to the reduced diameter segment


18


of the mandrel


10


without welding. This is a distinct advantage to well operators whose requirements preclude welding as well as when certain materials are used allowing the affixation of the slip seat


64


to the mandrel in conformance with regulations that prohibit welding, such as those promulgated by the National Association of Corrosion Engineers (NACE). The mandrel


10


is shown in more detain in

FIGS. 27 through 29

. As seen in

FIG. 27

, each slip seat


64


is attachable to the mandrel


10


through a series of rows of longitudinal slots


140


. Each individual slot


140


is shown in greater detail in FIG.


28


. At least one opposed pair of slots, shown in

FIG. 28

, has a lateral opening


142


, which is designed to accept a tab


144


(see

FIG. 25

) on the underside of the slip seat


64


. The various tabs on the underside of the slip seat


64


are aligned with the longitudinal slots


140


and more particularly, the lateral openings


142


. The slots


140


have elongated undercuts


146


such that the tab


144


on the underside of the slip seat


64


can be first inserted into the lateral opening


142


as shown in FIG.


28


and then the slip seat


64


can be moved longitudinally with respect to mandrel


10


to put the tabs


144


in an offset position from lateral opening


142


. This position is shown in FIG.


27


. Also shown in

FIG. 27

is an opening


148


in the mandrel


10


. Opening


148


is in fact a depression in the outer surface of mandrel


10


. Referring to

FIG. 24

, the slip seat


64


has a transverse lug


150


which fits into the opening


148


and mandrel


10


. Opening


148


is necessarily larger than the lug


150


so that upon insertion of tabs


144


and lug


150


into respective openings


140


and


148


and translation of the slip seat


64


with respect to the mandrel


10


, any load transmitted to the slip seat


64


goes into the mandrel


10


via transverse lug


150


and aligned lugs


144


. In essence, lugs


144


take a hanging load on upper ends of slots


140


and take up a radial load on the sides of slots


140


while transverse lug


150


bears on the upper end of opening


148


. To finally fix the slip seat


64


to the mandrel


10


, a slip seat retainer


56


is inserted through an opening


152


in the slip seat


64


and further into a notch


154


in the mandrel


10


(see FIGS.


23


&


27


). Each of the slip seat


64


are attached to the mandrel


10


which does not deform the mandrel


10


in the identical manner. While a specific non-welding mode of attachment of slip seat


64


to mandrel


10


is disclosed, those skilled in the art will appreciate that other techniques for so joining those two components can be utilized without departing from the spirit of the invention.




Another feature of the apparatus A of the present invention is the manner in which the loading is transferred from the slip


50


to the slip seat


64


and into the mandrel


10


. Each individual slip


50


transfers loading to the slip seat


64


which surrounds it, whereupon the loading through the shape of the slip


50


is transferred into the wall of the mandrel


10


. There is no interaction between one slip


50


and its slip seat


64


and any other slip seat


64


. The loading is transferred from each slip


50


into the wall of mandrel


10


through slip seat


64


rather than radially toward the center of mandrel


10


, which would be a force that would tend to deform or crush the mandrel


10


. Referring specifically to

FIGS. 23 and 14

and


15


, it can be seen that the edges


156


and


158


are preferably beveled with respect to the plane of the paper and there is a matching slope on surfaces


160


&


162


of the slip seat


64


. Thus, taking into consideration the strength of the slip seat


64


, the edge configuration of each slip


50


along surfaces


158


&


156


and the conforming surfaces on the slip seat


64


surfaces


160


&


162


are such that the resultant force from loading a slip


50


is a force that is merely close to tangential to the wall which comprises the mandrel


10


. In the preferred embodiment, the angle is approximately 80 degrees, putting the greatest component of force closer to the tangential direction into the wall which comprises the mandrel


10


with a smaller component directed radially toward the central of the mandrel


10


. Such angles can be placed in the slip


50


by repositioning it during the machining process. As can be seen in looking at

FIG. 23

, when the upward pull comes to each of the slips


50


, they are guided by surfaces


160


&


162


to move radially outwardly to lock the apparatus A downhole, while at the same time, independently transferring load from each slip to its respective slip seat


64


through surfaces


160


&


162


which are preferably at a slope of about 80 degrees resulting in the largest component of force being transferred into the mandrel


10


in a near tangential manner.




Those skilled in the art will now appreciate that the above-described preferred embodiment has numerous advantageous over tools in the prior art. The apparatus A employs a mechanical lock which prevents premature settings. It uses a bolt-on piston housing


106


which allows for field replacements to obtain different forces for disabling the mechanical lock. The rupture disk


124


requires a pre-determined pressure be applied before the lock mechanism L can release. The use of a bolt-on piston housing


106


also helps reduce the profile of the lock mechanism L and enables the provision of longitudinal passages


38


for the passage of mud and cement. The slips


50


are secured to slip seat


64


which are, in turn, connected to the mandrel


10


without welding. Each slip


50


is configured to direct applied loads into the mandrel


10


in a direction nearly approximating the tangential or into the wall of the mandrel


10


. Thus there is less of a tendency to deform the mandrel as with designs of the prior art which simply move slips up cones. Additionally, as distinguished from other slip designs of the prior art, there is no interaction in sharing the load among the slips


50


. Each slip individually distributes the load applied to it to the mandrel


10


through the slip seat


64


. The piston assembly


126


through the use of cap


130


allows venting of fluids from passage


122


in the piston housing


106


. The piston assembly


126


is free to move in both directions to react to thermal and other effects. The rupture disk


124


can be configured so that it ruptures at significantly higher pressures upon an excess of pressure in passage


122


as opposed to its normal operation where an increase in pressure from the mandrel


10


results in breaking of the rupture disk


124


. Maximum use is made of the force generated by the piston assembly


126


through the lost motion between the lock dog release


100


and the lock dog retainer


92


. Since rotation of the apparatus A is possible, provisions have been made to retain the arms


46


which are attached to the slips


50


against centrifugal force from such rotation. The slip seat retainer


56


accomplishes this function. Yet another new feature is the drop-in arrangement for the slip seat


64


into the slots


140


and opening


148


. The dove-tail arrangement also helps to secure the slip seat


64


to the mandrel


10


. The edge slopes on the slips


50


are designed to avoid over-stressing the slip seat


64


while at the same time efficiently communicating loads on each slip


50


into the wall which defines the mandrel


10


.




Referring now through

FIGS. 30 through 36

, an alternative embodiment is described. As shown in

FIGS. 30A through C

, a mandrel


160


has a series of slips


162


retained in a similar manner as previously described for the slips


50


. What is different in the alternative embodiment can be seen in

FIG. 33A

where a passage


164


leads from internally of the mandrel


160


to a rupture disk


166


. On the other side of the rupture disk


166


is a piston assembly


168


. These components operate in the identical manner as described for the comparable structure in the preferred embodiment. Looking at

FIG. 32B

, a spring housing


170


is locked to the mandrel


160


by virtue of the fact that a split ring


172


extends into a groove


174


in the mandrel


160


. The split ring


172


also extends into a recess


176


in spring housing


170


. A spring


178


is shown in FIG.


32


B. Those skilled in the art will appreciate it as one of many springs


178


, each of which is guided by a guide


180


. Referring to

FIG. 31

, the lower end


182


of the spring housing


170


has a recess


184


which accepts a tab


186


which is part of the structure of the slip


162


. Accordingly, the spring housing


170


is operably connected to all the slips


162


and has numerous springs


178


which will drive all the slips


162


upward as the spring housing


170


moves upwardly once the split ring


172


is moved out of the way. This occurs when the split ring


172


is allowed to expand effectively out of groove


174


thereby no longer restraining the spring housing


170


and thus allowing the force of all the springs


178


to move the slips


162


upwardly, thus distributing the load on each of the slips


162


in the manner previously described for the preferred embodiment. The split ring


172


is shown in FIG.


34


. It has a pair of opposed shoulders


188


&


190


which are tightly squeezed together by a yoke


192


(shown in FIG.


35


). Yolk


192


has a pair of opposed surfaces


194


&


196


which engage surfaces


190


&


188


respectively to hold the position of the split ring


172


to a diameter sufficiently small so that it can effectively serve as an anchor when fixed in groove


174


. The release simply occurs by a pressure buildup in the mandrel


160


which is communicated through passage


164


to break rupture disk


166


which in turn actuates the piston assembly


168


. The piston assembly


168


engages a connecting rod


198


which is fixedly secured to the yoke


192


. When the surfaces


194


&


196


on yoke


192


are displaced from the surfaces


190


&


188


on split ring


172


, the split ring


172


can expand radially outwardly, thus defeating the lock of the spring housing


170


to the mandrel


160


. When this occurs, the springs


178


can bias the spring housing


170


upwardly, thus taking up all the slips


162


and securing the apparatus A while distributing the load into the mandrel


160


in the manner previously described.




Yet another feature of the alternative embodiment can be seen from

FIGS. 31 & 36

. As shown in

FIG. 36

, a flow channel


200


on the back side of each slip


162


allows mud or cement flow underneath to permit circulation of such materials during the normal operation of the apparatus A. This is significant in this particular design because it does not have the feature of the longitudinal passages


38


as in the preferred embodiment. However, in common with the preferred embodiment, pressure in the mandrel


160


results in defeat of a lock mechanism (in this embodiment the split ring


172


). The slips


162


are independently set with the spring force from springs


178


. This mode of operation is to be contrasted with that revealed in U.S. Pat. No. 5,417,288 where the pistons actuate a ring which is directly connected to the slips. Thus, in that design the hydraulic pressure actually moves the slips whereas in this alternative embodiment, as well as in the preferred embodiment, the applied hydraulic pressure, without breaking any components other than a rupture disk such as


124


and shear pin


76


, results in the release of a mechanical lock which allows the independent operation of the setting of the slips


50


. Again, comparing to the previous technique of U.S. Pat. No. 5,417,288, numerous passages have to be drilled in the mandrel. More specifically, two passages were needed for each slip to operate it. Here, a single passage is presented through the mandrel


160


to operate the connecting rod


198


so as to release the split ring


172


from the groove


174


thus allowing independent mechanical actuation using spring force to set the slips


162


.




Referring to

FIG. 36



a


, one alternative embodiment of the liner hanger is composed of a mandrel


201


which has a lower end


217


. The lower end is shown schematically and those skilled in the art will appreciate that the liner string is connected at the lower end


217


. The mandrel


201


has an upper end


216


which, to those skilled in the art will appreciate, is attached to a running tool for proper positioning and securing of assembly S shown in

FIGS. 36



a


through


38


.




Referring to

FIG. 36



a


, a piston assembly


202


is secured to the mandrel


201


using a bolt


110


previously described. Secured loosely by the piston assembly


202


, is a lock bar


203


, which connects to the snap ring


204


, which extends into a recess


205


(

FIGS. 39 and 40

) on the mandrel


201


, and is retained in place by a breakable pin


206


. The pusher sleeve


207


is biased against the snap ring


205


through the t-slot segment


212


, which is biased by the slip


50


, which is biased by the spring


60


through the spring guide


62


.




One alternative embodiment of the piston housing


223


can best be seen in

FIG. 39

in the run-in and

FIG. 40

in the set position, where the end of the piston housing


223


has been extended to present a cover


218


over the lock bar


203


to prevent shifting of the lock bar


203


by means other that the piston


126


. The lock bar


203


is similar to the yoke


192


in that it combines the yoke


192


and the connecting rod


198


from the previous description. The lock bar


203


has a pair of opposed surfaces


219


&


220


(

FIG. 42

) which hold the opposed shoulders


212


&


222


(

FIG. 43

) respectively of the snap ring


204


and secure the snap ring


204


in the recess


205


in the mandrel


201


. This method demonstrates that the snap ring


204


can be restrained from the top or the bottom without departing from the spirit of the invention.




Another alternative embodiment of the piston housing


223


is that it can be mounted on a milled flat

FIG. 41

on the mandrel, verses mounting on a curved surface

FIG. 6

of the mandrel


201


&


10


without departing from the spirit of the invention.




The alternative embodiment of the slip seat


209


, where the springs


60


are contained in the slip seat


209


and bias the slips from the bottom, indirectly through a collection of parts, against the snap ring


205


and lock bar


203


, also demonstrates that the slips


50


, can be pushed versus pulled, to set the slips


50


without departing from the spirit of the invention.




Further modifications to the equipment and to the techniques described herein should be apparent from the above description of these preferred embodiments. Although the invention has thus been described in detail for a preferred embodiment, it should be understood that this explanation is for illustration, and that the invention is not limited to the described embodiments. Alternative equipment and operating techniques will thus be apparent to those skilled in the art in view of this disclosure. Modifications are thus contemplated and may be made without departing from the spirit of the invention, which is defined by the claims.



Claims
  • 1. A liner hanger comprising:a body; a plurality of slips mounted to individual seats on said body, said individual seats substantially surrounding a respective slip such that upon actuation of said slips load is transferred to said body from each slip substantially peripherally through its individual seat.
  • 2. The hanger of claim 1, wherein:said seats transfer load applied through each slip, when set, in a substantially tangent direction to said body.
  • 3. The hanger of claim 1, wherein:said slips and their respective seats make contact along matting edge surfaces which transmit a majority of the force applied to the slip into said body tangentially.
  • 4. A liner hanger comprising:a body; a plurality of slips mounted to individual seats on said body such that upon actuation of said slips load is transferred to said body from each slip through its individual seat; said seats are attached to said body without welding.
  • 5. A liner hanger comprising:a body; a plurality of slips mounted to individual seats on said body such that upon actuation of said slips load is transferred to said body from each slip through its individual seat said seats are circumferentially spaced from each other creating longitudinal passages outside said body where wellbore fluids can flow.
  • 6. A liner hanger comprising:a body; a plurality of slips mounted to individual seats on said body such that upon actuation of said slips load is transferred to; said body from each slip through its individual seat; a lock to retain said slips in a retracted position for run in; a release mechanism removably mounted to an exterior surface of said body for selective contact with said lock to allow said slips to set.
  • 7. The hanger of claim 6, further comprising:an actuation assembly on said body which selectively applies a force to set said slips after said lock has been defeated by movement of said release mechanism.
  • 8. The hanger of claim 7, wherein:said release mechanism comprises a housing having a passage which communicates with an opening in said body and a movable piston in said housing; whereupon, pressure from said body into said housing moves said piston against said lock to allow said actuation assembly to set said slips.
  • 9. The hanger of claim 8, wherein:said housing is retained by a fastener which is inserted into the opening in said body and has a passage therethrough to allow fluid communication to said piston.
  • 10. The hanger of claim 8, wherein:said piston is free to move in said housing to compensate for thermal effects from surrounding wellbore fluids.
  • 11. The hanger of claim 8, further comprising:a removable member in said housing which is responsive to applied pressure from said body to insure pressure buildup to a predetermined level prior to communicating said pressure to said piston.
  • 12. The hanger of claim 6, wherein:said lock comprises at least one dog retained to said body by a biased sliding sleeve assembly, said sliding sleeve assembly comprises a plurality of components connected to each other to provide for initial relative movement followed by tandem movement when contacted by said release mechanism to release said dog from said body.
  • 13. The hanger of claim 12, wherein:a first component of said sliding sleeve assembly which is initially contacted by said release mechanism is initially secured to said body; whereupon contact of said first component by said release mechanism said secured connection to said body is disconnected while leaving a second component of said sliding sleeve assembly initially undisturbed.
  • 14. The hanger of claim 13, wherein:said body comprises a plurality of openings and each seat comprises tabs to enter respective openings whereupon relative longitudinal movement between said seat and said body moves said seat to a secure position where said seat can't move away from said body.
  • 15. The hanger of claim 6, wherein:said lock comprises a biased sleeve held to said body by a split ring held together by a yoke, whereupon when said yoke is displaced by said release mechanism said split ring expands to release said sleeve to be biased which in turn moves said slips to a set position.
  • 16. The hanger of claim 6, wherein:said lock comprises a split ring which is held by a yoke to said body, to retain said slips against a bias force, said release mechanism moving said yoke to allow said bias force to set said slips.
  • 17. A liner hanger comprising:a body; a plurality of slips mounted to individual seats on said body such that upon actuation of said slips load is transferred to said body from each slip through its individual seat; a retainer for at least one slip to counteract a separation force from rotation of said body.
  • 18. A liner hanger, comprising:a body; a plurality of slips, said slips actuable by a bias force stored in said body and applied to a connected sliding sleeve; a lock selectively retaining said sleeve to said body; a pressure operated release mechanism on said body to selectively move said lock to allow said sliding sleeve to be biased by said stored force to move said slips to a set position.
  • 19. A liner hanger, comprising:a body; a plurality of slips, Said slips actuable by a bias force applied to a connected sliding sleeve; a lock selectively retaining said sleeve to said body; a release mechanism on said body to allow said biased sliding sleeve to move said slips to a set position: said release mechanism is removably secured to said body by a fastener to allow different release mechanisms to be used on the same body.
  • 20. The hanger of claim 19, whereinsaid release mechanism comprises a housing having a piston in a chamber therein, said body having an opening and said fastener providing communication through itself from said opening in said body to said piston in said chamber.
  • 21. A liner hanger, comprising:a body; a plurality of slips, said slips actuable by a bias force applied to a connected sliding sleeve; a lock selectively retaining said sleeve to said body; a release mechanism on said body to allow said biased sliding sleeve move said slips to a set position; said slips are individually supported by seats which are circumferentially spaced and secured to said body without welding whereupon loads transferred from said slips to their respective seats are principally tangentially transferred into said body.
Parent Case Info

The application claims the benefit of U.S. Provisional Application No. 60/156,831, filed on Sep. 30, 1999.

US Referenced Citations (21)
Number Name Date Kind
3608634 Cochran Sep 1971 A
3871447 Crowe Mar 1975 A
3999605 Braddick Dec 1976 A
4060131 Kenneday et al. Nov 1977 A
4096913 Kenneday et al. Jun 1978 A
4311194 White Jan 1982 A
4497368 Baugh Feb 1985 A
RE31881 Lindsey, Jr. May 1985 E
4640354 Boisson Feb 1987 A
4711316 Baugh et al. Dec 1987 A
4712614 Allwin et al. Dec 1987 A
4712615 Dockins, Jr. et al. Dec 1987 A
4762177 Smith, Jr. Aug 1988 A
4898245 Braddick Feb 1990 A
4942924 Duncan Jul 1990 A
5086845 Baugh Feb 1992 A
5318131 Baker Jun 1994 A
5417288 Melenyzer et al. May 1995 A
5560426 Trahan et al. Oct 1996 A
5799730 Lam et al. Sep 1998 A
5829531 Herbert et al. Nov 1998 A
Foreign Referenced Citations (4)
Number Date Country
2165282 Apr 1986 GB
2165282 Apr 1986 GB
PCTUS9202497 Apr 1992 WO
WO9320329 Nov 1993 WO
Provisional Applications (1)
Number Date Country
60/156831 Sep 1999 US