Safety method and apparatus for a perforating gun

Information

  • Patent Grant
  • 6298924
  • Patent Number
    6,298,924
  • Date Filed
    Friday, August 18, 2000
    23 years ago
  • Date Issued
    Tuesday, October 9, 2001
    22 years ago
Abstract
An apparatus for use in a subterranean well includes a downhole energy source, a first switch, a second switch, a detonator, a first controller and a second controller. The first switch has a first predetermined state to transfer energy from the energy source, and the second switch has a second predetermined state to transfer the energy from the energy source. A detonator receives the energy from the energy source when the first switch and second switches are concurrently in the first and second predetermined states. A first controller independently detects a predetermined stimulus that is transmitted from the surface of the well and causes the first switch to enter to first predetermined state based on the detection by the first controller. A second controller independently detects the predetermined stimulus transmitted from the surface of the well and causes the second switch to enter the second predetermined state based on the detection by the second controller.
Description




BACKGROUND




The invention relates to a safety method and apparatus for a perforating gun.




Referring to

FIG. 1

, a typical perforating gun string


10


may have several perforating guns


12


. Each perforating gun


12


may have phased shaped charges


14


that are used to penetrate a casing of a subterranean well and form fractures in surrounding formations to enhance the production of well fluids from these formations. Because the shaped charges


14


may potentially inflict harm if the charges


14


prematurely detonate, several safety mechanisms typically are used to prevent accidental detonation of the shaped charges


14


.




For example, the shaped charges


14


may be secondary explosives that, as compared to primary explosives, are very difficult to detonate. To detonate these secondary explosives, the perforating gun string


10


may have a firing head


11


that is associated with each perforating gun


12


. In this manner, the firing head


11


may include a detonator


15


that, when activated, detonates a primary explosive to initiate a shockwave on a detonating cord


17


that extends to the shaped charges


14


. The shockwave, in turn, propagates down the detonating cord


17


and detonates the shaped charges


14


. Because the primary explosive is capable of being detonated by naturally occurring phenomena, extreme care must be exercised to ensure that the primary explosive does not prematurely detonate.




The detonation of the perforating gun


12


may be remotely controlled from the surface of the well. To accomplish this, stimuli may be transmitted downhole to the firing head


11


to cause the detonator


15


to initiate the shockwave on the detonating cord


17


. As examples of techniques that are used to transmit the stimuli, an internal passageway of the string


10


, an annulus that surrounds the string


10


, a tubing of the string


10


, or a line (a slickline or a wireline, as examples) extending downhole may all be used. Other techniques may also be used to transmit command stimuli downhole.




Detonation of the primary explosive typically requires energy from an energy source, a source that may either be located at the surface of the well or downhole in the perforating gun string


10


. If the energy source is at the surface of the well, then an operator may disconnect the energy source until firing of the perforating guns


12


is desired. However, unfortunately for the other case, connection/disconnection of a downhole energy source may present difficulties, as circuitry (not shown) of the firing head


11


must connect/disconnect the energy source. For example, a battery


16


of the string


10


may provide the energy needed to cause the detonator


15


to initiate a shockwave on the detonating cord


17


. However, a problem with this arrangement is that the battery


16


is located downhole with the detonator


15


. Thus, if the circuitry that couples the battery


16


to the detonator


15


should fail, the shaped charges


14


may be inadvertently detonated.




Thus, there is a continuing need for a downhole safety system to reliably prevent accidental detonation of a perforating gun when an energy source to detonate the gun is located downhole with the gun.




SUMMARY




Generally, in one embodiment, an apparatus for use in a subterranean well includes a downhole energy source, a first switch, a second switch, a detonator, a first controller and a second controller. The first switch has a first predetermined state to transfer energy from the energy source, and the second switch has a second predetermined state to transfer the energy from the energy source. A detonator receives the energy from the energy source when the first switch and second switches are concurrently in the first and second predetermined states. A first controller independently detects a predetermined stimulus that is transmitted from the surface of the well and causes the first switch to enter to first predetermined state based on the detection by the first controller. A second controller independently detects the predetermined stimulus transmitted from the surface of the well and causes the second switch to enter the second predetermined state based on the detection by the second controller.




Generally, in another embodiment, a method for use in a subterranean well includes furnishing a predetermined stimulus downhole and using at least two controllers downhole to independently detect the predetermined stimulus. A downhole energy source is coupled to a detonator based on the detection of the stimulus by all of the at least two controllers.




Other embodiments will become apparent from the following description, from the drawing and from the claims.











BRIEF DESCRIPTION OF THE DRAWING





FIG. 1

is a schematic view of a perforating gun string of the prior art.





FIG. 2

is a view of a perforating gun string according to an embodiment of the invention.





FIG. 3

is a view of a perforating gun tool according to an embodiment of the invention.





FIG. 4

is an electrical schematic diagram of the perforating gun string of FIG.


2


.





FIGS. 5

,


6


and


7


are charts illustrating information communicated between a fire control circuit and detonators of FIG.


4


.





FIG. 8

is a waveform of a signal illustrating a communication protocol between the fire control circuit and the detonators.





FIG. 9

is an electrical schematic diagram of the fire control circuit of FIG.


4


.





FIGS. 10

,


11


and


12


are timing diagrams illustrating signals generated by the fire control circuit.





FIGS. 13 and 14

are alternative electrical schematic diagrams of a switch of FIG.


9


.





FIG. 15

is an electrical schematic diagram of the initiation control circuit of FIG.


4


.





FIG. 16

is a more detailed electrical schematic diagram of the initiation control circuit of FIG.


15


.











DETAILED DESCRIPTION




Referring to

FIG. 2

, in a subterranean well, an embodiment


50


of a perforating gun string in accordance with the invention uses energy from a battery


52


of the perforating gun string


50


to detonate, or fire, multiple perforating guns


59


. Although each perforating gun


59


is fired by an associated electrical detonator


56


, the battery


52


remains electrically isolated from the detonators


56


until a unique detonation command (i.e., a command used for no other purpose than detonation) is sent from the surface of the well to begin a firing sequence for the guns


59


. To accomplish this, the perforating gun string


50


has a fire control circuit


54


which controls the connection of the battery


52


to the detonators


56


. The fire control circuit


54


has redundant circuits (described below) which independently verify the reception of the detonation command before the detonators


56


are connected to the battery


52


.




In some embodiments, the perforating gun string


50


may include multiple perforating gun assemblies


60


. In this manner, each assembly


60


may have one detonator


56


and one perforating gun


59


. Referring also to

FIG. 4

, after reception of the detonation command is verified, the fire control circuit


54


selectively transmits commands (described below) to the detonators


56


. In response, an initiation control circuit


61


of a selected detonator


56


fires the associated gun


59


by activating an exploding foil initiator (EFI)


58


of the detonator


56


. When activated, the EFI


58


initiates a shockwave on an associated detonating cord


51


that extends to shape charges of the associated gun


59


. The shockwave from the detonator cord


51


fires the shape charges, and thus, fires the gun


59


.




In some embodiments, remote control is used, as the commands are transmitted to the fire control circuit


54


via stimuli that are transmitted downhole, such as via pressure pulses applied to hydrostatic fluid present in an annulus


46


(see

FIG. 2

) of the well. The annulus


46


is the annular space accessible from the surface of the well that is between the outside of the string


10


and the interior of a casing


48


of the well. In some embodiments, a duration of the pressure pulse, a pressure of the pressure pulse, and the number of pressure pulses in succession form a signature that uniquely identifies each command. The fire control circuit


54


uses at least one pressure sensor


53


in contact with the hydrostatic fluid in the annulus


46


to receive the commands.




Alternatively, in other embodiments, the commands may be transmitted downhole via other types of stimuli. In this manner, stimuli may be transmitted downhole via a passageway of the tubing of the string


10


, via a casing of the string


10


, or via a downhole line, as a few examples. For the case of the downhole line, a wireline or a slickline, for example, may be used to lower perforating gun assemblies


60


downhole when the assemblies


60


are part of a perforating tool


70


(see FIG.


3


). In this manner, the line may impart a predetermined movement (a velocity or an acceleration) on the tool


70


. This predetermined movement, in turn, indicates downhole commands, such as the detonation command, that are decoded by a motion sensor (not shown) of the tool


70


. Similar to the perforating gun string


50


, the tool


70


may have one or more perforating gun assemblies


60


, the fire control circuit


54


, and the battery


52


. The perforating gun tool


70


may be alternatively attached to a coiled tubing which may be used in the ways described above to send stimuli downhole.




Referring back to

FIG. 4

, the fire control circuit


54


is configured to receive the stimuli transmitted downhole and selectively connect the battery


52


to the detonators


56


only if several conditions are met, as described below. Otherwise, the battery


52


remains isolated from the detonators


56


, and the perforating guns


59


cannot be fired. To accomplish this, the fire control circuit


54


is coupled between the battery


52


and a power line


82


extending to the detonators


56


. A power line


81


extends between the battery


52


and the fire control circuit


54


. If the fire control circuit


54


detects an external fault condition (e.g., the presence of water near circuitry of the tool) or the partial failure of the fire control circuit


54


itself, the fire control circuit


54


shorts the battery


52


to ground which blows a fuse


80


that is serially coupled between the battery


52


and ground. Once the fuse


80


is blown, power from the battery


52


cannot be furnished to the detonators


56


which allows the tool


50


to be safely extracted from the well and serviced.




If no fault conditions exist and the fire control circuit


54


is operating properly, then the fire control circuit


54


monitors for transmitted downhole stimuli to detect a detonation command. In some embodiments, the detonation command is a partial key. When the fire control circuit


54


detects a valid (discussed below) detonation command key, the fire control circuit


54


must generate at least three fire control keys. The fire control circuit


54


does not contain within a complete fire key, but only a partial key. In this manner, the partial detonation command key received from the surface must be combined with the internal partial key to form the fire control keys. The importance of this sequence is to prevent the fire control circuit from accidentally jumping to a subroutine and generating a firing sequence without a valid command.




Referring also to

FIG. 9

, after at least three fire control keys are generated, the fire control circuit


54


starts a sequence of events to connect the battery


52


to the power line


82


. When a primary processor


120


and a secondary processor


126


have generated at least three keys that may or may not be valid keys, the processors each send out the first key each to start associated synchronous timers,


122


and


129


, respectively. Immediately thereafter, the processors


120


and


126


each start firmware timers. If the key was invalid, the hardware will terminate the sequence by blowing the fuse


80


between the battery


52


and fire control circuit


54


. If the key was valid, a certain time later, for example


32


seconds, the processors


120


and


126


send out the second key each. If the key is invalid, the hardware will terminate the sequence by blowing the fuse


80


between the battery


52


and fire control circuit


54


. If the key is valid, the key will open (unlock) shunt switch(es)


110


and


112


and a certain time later (10 milliseconds (ms), for example), the processors


120


and


126


each send out a third key. If the key is invalid, the hardware will terminate the sequence by blowing the fuse


80


between the battery


52


and fire control circuit


54


. If the key is valid, the key will close series switches


106


and


108


. The battery


52


is now connected to one of the detonators


56


, as described below.




Once the battery


52


is connected, the fire control circuit


54


selectively and serially communicates with the detonators


56


(via the power line


82


) to fire the guns


59


. Besides selectively instructing the detonators


56


to fire the guns


59


, the fire control circuit


54


may also selectively request and receive status information from the detonators


56


. In some embodiments, the guns


59


may be sequentially fired, beginning with the gun


59


farthest from the surface of the well and ending with the gun


59


closest to the surface of the well. In some embodiments, if the closest gun


59


to the fire control circuit


54


is otherwise fired first, the detonation of the detonation cord and shape charges will cut the power line


82


, and thus, no other gun can be fired. Each detonator


56


has a mechanism to electrically disconnect the power line


82


from the next gun


59


below.




Although other addressing schemes may be used, in some embodiments, the fire control circuit


54


may communicate with the initiation control circuit


61


of each detonator


56


, one at a time, beginning with the initiation control circuit


61


nearest from the fire control circuit


54


. Each initiation control circuit


61


has a switch


57




a


which serially couples the terminals of each initiation control circuit


61


to adjacent detonators


56


and a switch


57




b


to connect the power line


82


to circuitry of the initiation control circuit


61


. The switches


57




a


and


57




b


closest to the fire control circuit


54


are connected to the power line


82


. Initially, all of the switches


57




a


are open which permits the fire control circuit


54


to connect the battery


52


(via the appropriate switch


57




b


) to communicate with the nearest detonator


56


first.




In communicating with one of the detonators


56


, the fire control circuit


54


either fires the perforating gun


59


associated with the detonator


56


or selects the next detonator


56


. When the next gun is selected, the switch


57




a


of the currently selected detonator


56


closes, and the switch


57




b


of the currently selected detonator


56


opens. In some embodiments, the above-described process may be used to find the bottom gun


59


and fire this gun


59


first.




Referring to

FIG. 5

, in some embodiments, the initiation control circuit


61


may perform many operations in response to many different types of commands, which include, as examples, control commands and test commands. Control commands such as ID, NEXT_GUN, and FIRE_GUN, in some embodiments, control primary downhole functions.




The fire control circuit


54


sends either the FIRE_GUN command to actuate the initiation control circuit


61


or the NEXT_GUN command to deselect the initiation control circuit


61


that is currently coupled to the fire control circuit


54


. Next, the fire control circuit


54


selects the next farther away (as measured from the fire control circuit


54


) initiation control circuit


61


from the deselected initiation control circuit


61


. After the bottom gun


59


is found, the fire control circuit


54


transmits the FIRE_GUN command. After the selected initiation control circuit


61


fires the associated perforating gun


59


, a new detonation command must be received by the fire control circuit


54


and processed using the above-described technique before firing the next available perforating gun


59


.




Referring to

FIGS. 6 and 7

, the initiation control circuit


61


may, in communications with the fire control circuit


54


, communicate status information. After the fire control circuit


54


has detected a valid detonation command and the battery


52


is connected to one of the detonators


56


, the initiation control circuit


61


, when selected, commnunicates a PRESENCE status to the fire control circuit


54


acknowledging presence and readiness for a command. The detonator


56


closest to the fire control circuit


54


is selected by default while all others are selected by command. Each command issued by the fire control circuit


54


is answered by the initiation control circuit


61


with an appropriate STATUS or an ERROR STATUS. The primary downhole command acknowledge responses are for ID, NEXT_GUN, FIRE_GUN, and for initiation control circuit error. All other acknowledge responses are for function testing. The ID command initiates an identification (ID) status which causes the initiation control circuit


61


to transmit an acknowledge response, a year and week that the module was manufactured, an indication of a serial number, an indication of a version of the firmware, and a checksum for correct transmission detection.




The NEXT command initiates a bypass of the initiation control circuit


61


, and as a result, the next detonator


56


further form the fire control circuit


54


is selected. The FIRE_GUN command initiates the firing of the associated perforating gun


59


. A status is always sent to acknowledge the reception of a command before the initiation control circuit


61


executes the command. A time delay is incorporated between the status acknowledging the reception of a command and the execution of the command by the initiation control circuit


61


which permits the fire control circuit


54


to terminate the execution of the command if the command is incorrect. If the initiation control circuit


61


receives an invalid command, the initiation control circuit


61


returns an ERROR status.




Referring to

FIG. 8

, for communication purposes, a voltage level V


LINE


of the power line


82


is biased at a threshold voltage level V


TH


(e.g., nine volts). A logic zero corresponds to the voltage level V


LINE


being below the voltage level V


TH


(e.g., eight volts), and a logic one corresponds to the voltage V


LINE


being above the voltage V


TH


(e.g., ten volts). Besides the logical voltage levels, several other measures are in place to maximize the accuracy of serial communications with the detonators


56


. For example, the duration of a logic zero pulse


150


is one third the duration of a logic one pulse


152


. All pulses (i.e., logic one or logic zero pulses) are separated by a separation pulse (a pulse having a logic one voltage level) that has a duration equal to sum of the durations of the logic zero


150


and logic one


152


pulses. The voltage level V


LINE


is normally at the logical one level if the line


82


is not negated (i.e., pulled to the logic zero voltage level) by one of the detonators


56


or the fire control circuit


54


. To indicate the beginning of a serial transmission, the line


82


is negated for a start pulse


154


that is twice the duration of the logic zero pulse


150


.




Referring to

FIG. 9

, to minimize the possibility of connection of the battery


52


to the detonators


56


due to partial or total failure of the fire control circuit


54


, the fire control circuit


54


has two circuits


100


and


102


which must both independently verify reception of the detonation command before the battery


52


is connected to the detonators


56


. In this manner, no perforating guns


59


may be fired if one of the circuits


100


or


102


fails and incorrectly verifies reception of the detonation command. To accomplish this, the circuit


100


controls a switch


108


that is coupled in series with the battery


52


(and line


82


) and a switch


112


that is coupled in parallel with the battery


52


. Similarly, the circuit


102


controls a switch


106


that is coupled in series with the battery


52


(and line


82


) and a switch


110


that is coupled in parallel with the battery


52


. Thus, to connect the battery


52


to the detonators


56


, the parallel switches


110


and


112


must be opened, and subsequently, the series switches


106


and


108


must be closed.




After initial power-up of the circuitry of the tool, the circuits


100


and


102


enter a safe state (the state of the fire control circuit


54


before the tool is lowered downhole) in which the circuits


100


and


102


ensure that the series switches


106


and


108


are open and the shunt switches


110


and


112


are closed. The circuits


100


and


102


remain in the safe state (assuming no malfinction in the fire control circuit


54


occurs) until the circuits


100


and


102


open the parallel switches


110


and


112


and close the series switches


106


and


108


. If both circuits


100


and


102


do not enter the safe state after reset, fault detection logic


130


closes another switch


112


(normally open) that is in parallel with the battery


52


to blow the fuse


80


(see FIG.


4


).




The circuit


100


has the processor


120


(an eight bit microcontroller, for example) that interacts with the sensor(s)


53


to detect the stimuli transmitted downhole. Based on the detected stimuli, the processor


120


extracts the command(s) transmitted from the surface of the well and thus, eventually extracts the detonation command.




Referring also to

FIGS. 10

,


11


and


12


, to ensure that the processor


120


is not malfunctioning, the circuit


100


has a timer


122


that is used to establish a time interval window


140


(as indicated by an output signal of the timer


122


called EN


1


) of a predetermined duration (e.g., sixty-four seconds) in which the battery


52


is to be connected to the detonators


56


(i.e., switch


108


is closed and switch


112


is opened) and in which the perforating guns


59


are to be fired. When the processor


120


detects the detonation command, the processor


120


enables the timer


122


to measure a time interval T1 of a predetermined duration (e.g., sixty-four seconds). The window


140


begins (as indicated by the assertion of the EN


1


signal) when the time interval T1 elapses.




While the timer


122


is measuring the time interval T1, the processor


120


is internally and independently measuring another time interval T2 of a predetermined duration (e.g., sixty-five seconds) that is slightly longer in duration (e.g., one second longer) than the time interval T1. At the end of the time interval T2, the processor


120


attempts to open the parallel switch


112


. If the window


140


exists, switch logic


124


allows the processor


120


to open the parallel switch


112


. Otherwise, the switch logic


124


keeps the parallel switch closed


112


.




After the time interval T2 elapses, the processor


120


measures another successive time interval T3 of a predetermined duration sufficient to allow the parallel switch


112


to open (e.g., 10 μs) before attempting to close the series switch


108


. If the window


140


exists, the switch logic


124


allows the processor


120


to close the series switch


108


. Otherwise, the switch logic


124


keeps the series switch


108


open.




After the time interval T3 elapses, the processor


120


measures another successive time interval T4 of a predetermined duration (e.g., thirty-one seconds) which is equivalent to the time left in the window


140


. Just before (e.g., 10 μs before) the time interval T4 elapses, the processor


120


opens the series switch


108


(if not already open). When the time interval T4 expires, the processor


120


closes the parallel


112


(if not already closed) which returns the circuit


100


to the safe state.




The circuit


102


has a processor


126


, switch logic


128


, and a timer


129


that behave similarly to the processor


120


, switch logic


124


, and timer


122


, respectively, to control the series switch


106


and the parallel switch


110


. Instead of monitoring the output of the sensor


53


directly, the processor


126


receives an indication of the output of the sensor


53


from the processor


120


and independently verifies the signature of the pulses present in the hydrostatic fluid in the annulus


46


to extract commands sent from the surface of the well.




To verify that both circuits


100


and


102


come up in the safe state after power up of the fire control circuit


54


, the fault detection logic


130


monitors the outputs (CMD1[15:0] and CMD2[15:0]) of the processors


120


and


126


to ensure these outputs indicate the processors


120


and


126


are in the safe state (e.g., “10100101b,” wherein the suffix “b” denotes a binary representation). The fault detection logic


130


also monitors the output of an oscillator


115


which is used to clock the counters


122


and


129


and the processors


120


and


126


. In this manner, if the fault detection logic


130


detects failure of the oscillator


115


, the fault detection logic


130


closes the parallel switch


112


which blows the fuse


80


. As a result, if the oscillator


115


temporarily fails while the tool


50


is downhole and the fire control circuit


54


is not in the safe state, the battery


52


does remain connected to any of the detonators


56


should the oscillator


115


revive after the tool


50


is brought to the surface. The fault detection logic


130


also receives the outputs of several water sensors


131


selectively placed around the circuitry of the tool


50


. In this manner, if water is detected in the presence of the circuitry of the tool


50


, the fault detection logic


130


closes the parallel switch


112


and blows the fuse


80


. The fault detection logic


130


also monitors the terminal voltage of the battery


52


(as indicated by a signal called V


BAT


) and closes the switch


112


should the terminal voltage exceed predetermined limits.




The fire control circuit


54


has a transmitter


116


and a receiver


118


which the processor


120


uses to serially communicate over the line


82


with the initiation control circuits


61


of the detonators


56


. The input of the receiver


118


and the output of the transmitter


116


are connected to the output side of a current limiter


114


that is serially coupled between switch


108


and line


82


. When fire control circuit


54


has completed the communication protocol, fire control circuit


54


applies full battery


52


power to initiation control circuits


61


by closing a bypass switch


115


to fire the associated perforating gun


59


.




Referring to

FIG. 13

, as an example of the structure of the switches, the switch


106


may have a driver circuit


183


that has output terminals that are coupled to the gate and source of an n-channel metal oxide field-effect (NMOS) transistor


184


. The current path of the transistor


184


is coupled between the line


81


and the current path of switch


108


. The input of the drive circuit is connected to the switch logic


128


.




Alternatively, as another example, the switch


106


may include an NMOS transistor


300


that has its drain-source path coupled between the line


81


and the switch


108


. The gate-source voltage across the transistor


300


may be established by a resistor


302


that has one terminal coupled to the gate and one terminal coupled to the source of the transistor


300


. Another NMOS transistor


304


of the switch


106


may have its drain-source path coupled between the gate of the transistor


300


and ground. The gate of the transistor


304


may be coupled to the switch logic


128


.




The other switches


108


,


110


and


112


may be constructed in a similar manner to the switch


106


. Each switch


106


,


108


,


110


,


112


has two states: an open state (in which the switch does not conduct) and a closed state (in which the switch conducts). The connection (i.e., a serial connection or a parallel connection) of the switch


106


,


108


,


110


,


112


governs which state of a particular switch permits energy to flow from the battery


52


to the detonator


56


.




Referring to

FIG. 15

, in some embodiments, each initiation control circuit


61


may have a processor


172


that controls a switch circuit


57


(including the switches


57




a


and


57




b


) as well as operations of a fly-back, switching converter


170


(used to boost the voltage of the battery


52


) and communications with the fire control circuit


54


. The communications of the initiation control circuit


61


are accomplished via a receiver


176


and a transmitter


178


which are coupled to the line


82


and the processor


172


.




When power is applied to initiation control circuits


61


, the default setting of switch


57




a


is open to disconnect the initiation control circuit


61


from the other detonators


56


, and the switch


57




b


is closed to power the immediate initiation control circuits


61


when instructed to do so by the fire control circuit


54


. When the switch circuit


57


opens the switch


57




a


, the switch circuit


57


also closes the switch


57




b


which connects the battery


52


to the converter


170


. Upon this occurrence, the processor


172


interacts with the converter


170


to boost the terminal voltage level of the battery


52


to a higher voltage level which is present at the output of the converter


170


. A discharge circuit


174


(a gas discharge tube, for example) discharges an output capacitor


171


of the converter


170


when the output voltage of the converter


170


reaches a predetermined level (three thousand volts, for example). In this manner, the discharge circuit


174


transfers energy from the capacitor


171


to activate the EFI


58


. Once activated, the EFI


58


initiates a shockwave in the detonator cord


51


.




To minimize unpredictable behavior of the initiation control circuit


61


, the initiation control circuit


61


, in some embodiments, includes six low pass filters


10


,


191


,


192


,


193


,


194


and


195


that are selectively placed around the circuitry of the initiation control circuit


61


to reduce the level of any stray radio frequency (RF) signals. The initiation control circuit


61


also has an in-line fuse


182


coupled in series with the battery


52


and a Zener diode


180


shunted to ground to guard against such possibilities as the polarity or voltage level of the battery


52


being incorrect.




Referring to

FIG. 16

, the processor


172


may control the fly-back converter


170


by using two switches


214


and


216


to switch current through a primary winding


218




a


of a transformer


218


of the converter


170


. The switch


214


may be a simple redundant (backup safety switch) that is switched on and off by the processor


172


.




The processor


172


closes the switch


216


(i.e., turns on current in the primary winding


218




a


) at a predetermined rate by a clocking latch


224




b


. A sensing resistor


228


is coupled to the input of a comparator


224




a


which provides a reset to a latch


224




b


when the current in the primary winding


218




a


exceeds a predetermined threshold level. Upon this occurrence, the latch


224




b


opens the switch


216


which turns off current in the primary winding


218




a


. Subsequently, after waiting a predetermined duration, the processor


172


closes the switch


216


and repeats the above-described control process.




When current in the primary winding


218




a


is disrupted (i.e., by the opening of the switch


216


), the energy stored in the transformer


218


is transferred to a secondary circuit


222


(having the capacitor


171


) that is coupled to a secondary winding


218




b


of the transformer


218


. On each power cycle of the converter


170


, additional energy (corresponding to a step up in the voltage level of the capacitor


171


) is transferred to the capacitor


171


. When the voltage level of the capacitor


171


is large enough to activate the discharge circuit


174


, the EFI


58


is activated which sends a shockwave down the detonator cord


51


.




The switch circuit


57


has a two NAND gate latch


202


which controls the switches


57




a


and


57




b


. On power up, switch


57




a


is closed and switch


57




b


is open by default. In some embodiments, the processor


172


can only change the state of latch


202


to open switch


57




a


and close


57




b


. Only a new power up cycle can reset the latch


202


. Once the switch


57




a


is open, no power is available for processor


172


to control anything.




The initiation control circuit


61


also has an RC ring-type oscillator


212


which provides a clock signal used by the circuitry of the initiation control circuit


61


. A reset circuit


210


momentarily places the processor


172


in reset after power up of the initiation control circuit


61


. The initiation control circuit


61


has a voltage regulator


200


to furnish direct current (DC) voltage for the logic of the initiation control circuit


61


.




Other embodiments are within the scope of the following claims. For example, the initiation control circuit


61


may fire downhole devices other than the associated perforating gun


59


, such as a single shot device (a packer, for example).




While the invention has been disclosed with respect to a limited number of embodiments, those skilled in the art, having the benefit of this disclosure, will appreciate numerous modifications and variations therefrom. It is intended that the appended claims cover all such modifications and variations as fall within the true spirit and scope of the invention.



Claims
  • 1. An apparatus for use in a subterranean well, comprising:a downhole energy source; at least two controllers, each controller independently detecting a predetermined stimulus transmitted from the surface of the well; and a detonator to receive the energy from the energy source when each of the at least two controllers detects the predetermined stimulus.
  • 2. The apparatus of claim 1, wherein the energy source comprises a battery.
  • 3. The apparatus of claim 1, wherein the controllers are adapted to prevent the transfer of energy from the energy source to the detonator if all of the controllers do not indicate detection of the predetermined stimulus within a predetermined window of time.
  • 4. The apparatus of claim 1, further comprising:switches coupled between the detonator and the energy source in series, wherein each of the controllers operates a different one of the switches based on the detection of the predetermined stimulus by said each of the controllers.
  • 5. The apparatus of claim 1, further comprising:an explosive charge; and a detonator cord for transmitting a shockwave to the explosive charge, wherein the detonator initiates the shockwave after receiving energy from the energy source.
  • 6. The apparatus of claim 1, wherein at least one of the controllers comprises:a processor to: detect the predetermined stimulus, and measure a first predetermined time interval from when said at least one of the controllers detects the predetermined stimulus; a timer to measure a second predetermined time interval from when the stimulus is first detected; and logic connected to indicate detection of the predetermined stimulus in response to the measurement of the first and second predetermined time intervals.
  • 7. The apparatus of claim 6, further comprising:a switch coupled between the energy source and the detonator and being adapted to operate in response to the indication from the logic.
  • 8. The apparatus of claim 6, wherein the logic is further adapted to indicate detection of the predetermined stimulus only if completion of the measurement of both the first and second time intervals occur within a predetermined window of time.
  • 9. The apparatus of claim 1, wherein the well includes an annulus having a fluid, and wherein the predetermined stimulus comprises at least one pressure pulse in the fluid.
  • 10. An apparatus usable in a subterranean well, comprising:a downhole energy source; a detonator; and a circuit to couple the detonator to the downhole energy source in response to different subcircuits of the circuit independently detecting the presence of a predetermined stimulus communicated from a surface of the well.
  • 11. The apparatus of claim 10, wherein at least one of the subcircuits comprises a controller to detect the stimulus.
  • 12. The apparatus of claim 10, wherein the circuit comprises:at least one switch to couple the detonator to the downhole energy source in response to the detection of the presence of the predetermined stimulus by the subcircuits.
  • 13. The apparatus of claim 12, wherein said at least one switch comprises:a first switch coupled between the downhole energy source and the detonator to transition to a first state to permit coupling of the downhole energy source to the detonator in response to the detection of the presence of the predetermined stimulus by one of the subcircuits; and a second switch coupled between the first switch and the detonator to transition to a second state to permit coupling of the downhole energy source to the detonator in response to the detection of the presence of the predetermined stimulus by one of the subcircuits.
  • 14. The apparatus of claims 10, wherein the circuit is adapted to couple the detonator to the downhole energy source only if all of the different subcircuits indicate detection of the predetermined stimulus within a predetermined window of time.
  • 15. An assembly, comprising:a downhole energy source; a detonator; a tool to respond to detonation of the detonator; and a circuit to couple the detonator to the downhole energy source in response to different subcircuits of the circuit independently detecting the presence of a predetermined stimulus communicated from a surface of the well.
  • 16. The assembly of claim 15, wherein the tool comprises a perforating gun.
  • 17. The assembly of claim 15, wherein at least one of the subcircuits comprises a controller to detect the stimulus.
  • 18. The assembly of claim 15, wherein the circuit comprises:at least one switch to couple the detonator to the downhole energy source in response to the detection of the presence of the predetermined stimulus by the subcircuits.
  • 19. The assembly of claim 18, wherein said at least one switch comprises:a first switch coupled between the downhole energy source and the detonator to transition to a first state to permit coupling of the downhole energy source to the detonator in response to the detection of the presence of the predetermined stimulus by one of the subcircuits; and a second switch coupled between the first switch and the detonator to transition to a second state to permit coupling of the downhole energy source to the detonator in response to the detection of the presence of the predetermined stimulus by one of the subcircuits.
  • 20. The assembly of claim 15, wherein the circuit is adapted to couple the detonator to the downhole energy source only if all of the different subcircuits indicate detection of the predetermined stimulus within a predetermined window of time.
  • 21. An apparatus for use in a subterranean well, comprising:a downhole energy source; at least two controllers, each controller independently detecting a predetermined stimulus transmitted from the surface of the well; a detonator to receive the energy from the energy source when each of the at least two controllers detects the predetermined stimulus; and a switch coupled between the detonator and the energy source, wherein one of the controllers is adapted to cause the switch to remain in a state to couple the detonator to the energy source for a first predetermined duration of time after detection of the predetermined stimulus by said one of the controllers.
  • 22. The apparatus of claim 21, wherein the controllers are adapted to prevent the transfer of energy from the energy source to the detonator if all of the controllers do not indicate detection of the predetermined stimulus within a predetermined window of time.
  • 23. The apparatus of claim 21, further comprising:switches coupled between the detonator and the energy source in series, wherein each of the controllers operates a different one of the switches based on the detection of the predetermined stimulus by said each of the controllers.
  • 24. The apparatus of claim 21, further comprising:an explosive charge; and a detonator cord for transmitting a shockwave to the explosive charge, wherein the detonator initiates the shockwave after receiving energy from the energy source.
  • 25. The apparatus of claim 21, wherein at least one of the controllers comprises:a processor to: detect the predetermined stimulus, and measure a first predetermined time interval from when said at least one of the controllers detects the predetermined stimulus; a timer to measure a second predetermined time interval from when the stimulus is first detected; and logic connected to indicate detection of the predetermined stimulus in response to the measurement of the first and second predetermined time intervals.
  • 26. The apparatus of claim 25, further comprising:a switch coupled between the energy source and the detonator and being adapted to operate in response to the indication from the logic.
  • 27. The apparatus of claim 25, wherein the logic is further adapted to indicate detection of the predetermined stimulus only if completion of the measurement of both the first and second time intervals occur within a predetermined window of time.
  • 28. The apparatus of claim 21, wherein the well includes an annulus having a fluid, and wherein the predetermined stimulus comprises at least one pressure pulse in the fluid.
  • 29. The apparatus of claim 21, wherein the energy source comprises a battery.
Parent Case Info

This application claims priority and is a continuation of U.S. application Ser. No. 09/121,192 filed on Jul. 22, 1998 by Vaynshteyn and Spring, now U.S. Pat. No. 6,105,688.

US Referenced Citations (6)
Number Name Date Kind
4478294 Sumner Oct 1984
4660638 Yates, Jr. Apr 1987
4867266 Martin Sep 1989
4895218 Chen et al. Jan 1990
4928783 Crook May 1990
5278359 Miller et al. Jan 1994
Continuations (1)
Number Date Country
Parent 09/121192 Jul 1998 US
Child 09/641828 US