One concern relating to use of rotary, impact, or percussive drilling methods when forming a wellbore is well control. A weighted or pressurized drilling fluid, such as drilling mud, may be used to provide pressure control against pressures encountered in a geological formation. Drilling mud is typically pumped toward the bottom of a wellbore using a single tubular string, then returned to the surface via the outer annulus between the tubular string and the walls of the wellbore.
Certain implementations and embodiments will now be described more fully below with reference to the accompanying figures, in which various aspects are shown. However, various aspects may be implemented in many different forms and should not be construed as limited to the implementations set forth herein. The figures are not necessarily to scale, and the relative proportions of the indicated objects may have been modified for ease of illustration and not by way of limitation. Like numbers refer to like elements throughout.
While implementations are described in this disclosure by way of example, those skilled in the art will recognize that the implementations are not limited to the examples or figures described. It should be understood that the figures and detailed description thereto are not intended to limit implementations to the particular form disclosed but, on the contrary, the intention is to cover all modifications, equivalents, and alternatives falling within the spirit and scope as defined by the appended claims. The headings used in this disclosure are for organizational purposes only and are not meant to be used to limit the scope of the description or the claims. As used throughout this application, the word “may” is used in a permissive sense (i.e., meaning having the potential to) rather than the mandatory sense (i.e., meaning must). Similarly, the words “include”, “including”, and “includes” mean “including, but not limited to”.
Some conventional drilling techniques for forming a wellbore include rotary, impact, or percussive drilling methods. Resources, such as water, gas, oil, and so forth, may be present in a geologic formation, such as rock. The resources in the geologic formation may be under pressure. To provide pressure control against the pressures within the formation, a weighted or pressurized drilling fluid, such as drilling mud, may be pumped into the wellbore. Drilling muds may be water-based, carbon dioxide-based, petroleum-based, oil-based, or may include other liquids, gasses, or fluids. Typically, a wellbore is formed using a single tubular string, through which drilling mud may be pumped to the bottom of the hole, where drilling operations occur. The drilling mud then flows from the bottom of the hole toward the surface through the outer annulus surrounding the tubular string. In addition to resisting the formation pressures within the wellbore, drilling fluids may also stabilize the wellbore, reduce friction during the drilling operation, and remove cuttings or other debris from the wellbore.
This disclosure relates to techniques for drilling, in a downhole environment, using explosive perforating charges in conjunction with a tubular string. The perforating charges may include detonable (e.g., explosive) material. In some cases, the tubular string may include elements associated with a drilling system, which may be operated in series or in parallel with the use of the perforating charges. For example, an existing tubular string used during conventional drilling techniques may be equipped with a specialized drill bit that may be used in conjunction with perforating charges. An at-surface or above-ground loading mechanism and pump mechanism may be used to move perforating charges, which may be more dense than the drilling mud, through the tubular string. The fluid motion of the drilling mud or other materials and the weight of the charges may facilitate movement of the charges through the tubular string, while the pressure of the drilling mud and the weight of the charges may maintain pressure control of the wellbore.
A charge unit, which in some implementations may be formed from metallic and explosive components, may be flowed through a portion of the tubular string to impact the bottom of the hole, eroding both a portion of the geologic formation and the charge unit itself. In some cases, the charge unit may be accelerated to a high speed, such as through use of a mass and shock driving mechanism. In other cases, the charge unit may be moved through the tubular string using the flow of drilling fluid or other materials. The particles resulting from the interaction between the charge unit and the geologic material may be returned to the surface using the flow of the drilling mud, in the manner associated with typical transport of cuttings. In some implementations, the perforating charges may be accelerated using chemical energy. However, in other implementations, perforating charges may be accelerated using components of a hypersonic-augmented drilling system, impact (e.g., using pneumatic or mechanical force), or rotational energy. In some implementations, a charge unit may include multiple parts which may be separable or integral. For example, a charge unit may include a penetrator section configured to penetrate or erode the geological material. In one implementation, the penetrator section may include a shape similar to that of a drill bit. The charge unit may also include one or more separation stages that create barriers between different portions thereof. Additionally, a charge unit may include one or more propellant generating materials. Propellant generating materials may include a solid, liquid, or gas that under specific conditions (e.g., mechanical, electrical, or pressure-based conditions) may provide a force to the charge unit, such as a mass-based force, a pressure, a shock wave, and so forth. For example, actuation of a propellant generating material may cause generation of gas or another fluid, which may accelerate the perforating charge to penetrate through geologic material. In some implementations, generated propellant materials may also act as diluents.
In one implementation, the tubular string may be provided with a heavy, steel bottom hole assembly, such as a bottom hole assembly having a length of 50 feet. Perforating charges may be provided with a shape that facilitates transport and embedding of the charges, such as the shape of a chip or puck. For example, the charges may be shaped in a manner that facilitates nesting or stacking of the charges on top of one another, or transporting through the tubular string, one after the other. Individual perforating charges, or stacks thereof, may be released through an opening, such as a port accessible using a ball valve or other closure element, to position the charges in the drilling mud, between a surface of the wellbore and the bottom hole assembly. In some cases, the perforating charges may be passed through an opening without use of a closure element. The charges may then be detonated, which in some implementations, may create a Monroe jet or similar movement of explosive gas, shock waves, and particles of metal or other materials that may penetrate and erode the geologic formation and the charge itself. The perforating charges may be configured to direct the energy from detonation thereof as a shock wave, causing very little bulk gas movement. In some cases, materials generated through combustion or erosion of the charge or geologic material may be condensed or suspended within the drilling mud. The drilling mud may provide a barrier between the formation and the ball valve or other closure or separator mechanism in the bottom hole assembly through which the charges may be accelerated. In some implementations, the closure mechanism may include a floating ball or endcap. In other implementations, the pressure of the drilling mud may function to restrict backflow or ingress of material in place of or in addition to an endcap or other closure mechanism. Additionally, the drilling mud may function as a recoil mechanism against which the force from the perforating charge may push against to direct the charge toward the geologic material at the bottom of the hole.
The perforating charges may be used continuously, or semi-continuously, to bore through geologic material using the perforating charges, in the manner of a percussive perforation gun, that may be operated nearly entirely below the surface (e.g., in a downhole environment near the working face of a wellbore). Use of a single column in conjunction with fluid and charge units may facilitate well pressure control and limit the energy losses associated with long transits through tubular strings. In some implementations, in situ propellant materials may be used to accelerate the perforating charges. Propellant materials may include pressurized or combustible gasses, diesel, or similar components that may be used to impart a force to a perforating charge. For example, structures containing propellant materials may be pumped into a tubular string. As another example, propellant materials, such as gasses, may be entrained within the drilling mud, which may enable the materials to be transported toward the bottom of the hole without use of additional fluid connections. Propellant materials may be encapsulated in small pellets or dissolved or suspended into the drilling mud. In some implementations, the drilling mud may also contain one or more of fuel or oxidizer for use accelerating perforating charges, such as through use of a portion of the tubular string or bottom hole assembly as a ram accelerator or gas gun. Components entrained or suspended in the drilling mud may be separated from the drilling mud using a downhole mechanism. In some cases, the acceleration or impact of a perforating charge may initiate a mechanism for the release and capture of fluids or gasses used for the acceleration process. As yet another example, material within the charge unit, itself, may include a propellant material or a material that can be used to generate propellant material in the downhole environment. Use of in situ propellant materials may enable movement of surface components, such as the rotation of a drilling rod that provides energy to a downhole assembly, to be converted into chemical energy, which may then be used to provide energy to the perforating charges by providing linear velocity thereto.
In some implementations, radio frequency identification (RFID) chips, microchips, or similar communication components, materials, or devices may be suspended within the drilling fluid. The detectable materials may be used to communicate, via communication signals, with components of the downhole assembly, such as downhole logging equipment. Communication between devices, such as chips, within the drilling fluid may be used to provide data to computing devices at the surface or to communicate with downhole components. Such devices may also receive data from surface devices and transport the data to one or more downhole components.
As illustrated at the second time T2, the flow of drilling fluid 110 or other materials, such as propellant materials or other substances entrained in the drilling fluid 110, may urge at least one perforating charge 104 into the inner bore of the bottom hole assembly 108. For example, a closure element 114 may be opened to permit passage of the perforating charge 104 into the bottom hole assembly 108. Within the bottom hole assembly 108, the perforating charge 104 may be accelerated toward the bottom of the wellbore 102, such as through actuation of one or more propellant materials. In some implementations, a closure element 114 at the lower end of the bottom hole assembly 108 may be opened to permit passage of the perforating charge 104. The perforating charge 104 may at least partially penetrate, erode, or otherwise interact with geologic material at the bottom of the wellbore 102, and detonation 116 of the perforating charge 104 may further erode or displace geologic material, creating a region of eroded formation 118 at the bottom of the wellbore 102. Creation of the region of eroded formation 118 may extend at least one dimension of the wellbore 102, such as by increasing the length (e.g., depth) thereof.
The process illustrated at the first time T1 and second time T2 may be repeated using successive perforating charges 104. For example, at the third time T3, a subsequent perforating charge 104 may be urged into the bottom hole assembly 108, such as by the flow of the drilling fluid 110. At the fourth time T4, the perforating charge 104 may be accelerated to contact the bottom of the region of eroded formation 118, where a subsequent detonation 116 may further erode or displace geologic material from the wellbore 102.
In some implementations, use of perforating charges 104 to generate a wellbore 102 may eliminate the need for a separate circulating tube, which may increase the circulating area for drilling fluid 110 and other materials in the annulus 112, improving the removal of cuttings. For example, in one implementation, a generated wellbore 102 may have a diameter that is 2.75 times as large as that of the tubular string 106 used to provide the perforating charges 104 to the bottom of the wellbore 102. Use of a single tubular string 106 and movement of drilling fluid 110 to provide components into and from the wellbore 102 may improve well pressure control, efficiency, depth, lateral reach, and steering capability when compared to conventional drilling techniques. Additionally, use of the tubular string 106 and drilling fluid 110 may eliminate the need for separate lines or other conduits for providing materials to or removing materials from the wellbore 102.
The bottom hole assembly 108 may be engaged with the lower end of the tubular string 106. The bottom hole assembly 108 may include a launch tube 206 through which perforating charges 104 may be passed, and one or more closure elements 114, such as ball valves, that separate particular portions of the bottom hole assembly 108 from other portions. As described with regard to
In some implementations, the lower portion of the bottom hole assembly 108 may include a ram accelerator for accelerating the perforating charges 104 toward the bottom of the wellbore 102. The ram accelerator may include internal baffles or rails, dampers for affecting the movement of the perforating charges 104, and may include single or multiple stages. In some cases, the drilling fluid 110 or other substances proximate to the lower end of the bottom hole assembly 108 may prevent ingress of materials into the bottom hole assembly 108 from the lower end thereof. For example, the ram accelerator may be pressurized to a pressure equal to or greater than that of the wellbore 102 to provide well control. In other implementations, the bottom hole assembly 108 may include or be engaged with measurement while drilling equipment, a rotatable reamer or drill bit, such as a polycrystalline diamond compact or tri cone drill bit, or other equipment.
At the second time T2,
At the fifth time T5,
Energy for the detonation 116 of the perforating charge 104 may be obtained using one or more explosive compounds, such as Research and Development Formula X (RDX), octogen (e.g., cyclotetramethylene-tetranitramine, known as HMX), PYX explosive (e.g., 2,6-Bis(picrylamino)-3,5-dinitropyridine), hexanitrostilbene (HNS or JD-X), and so forth. In some implementations, hydrocarbons or other sources of energy, such as gelled diesel fuel or fertilizer, may be provided into a downhole environment by encapsulating such materials within drilling fluid 110. In some implementations, materials provided into the downhole environment may be mixed in situ (e.g., into a cake layer) and detonated.
Block 904 provides fluid, such as drilling fluid 110, into the tubular string 106 to move the perforating charge 104 through the tubular string 106 into a portion of a bottom hole assembly 108. As described with regard to
Block 906 isolates the portion of the bottom hole assembly 108 containing the perforating charge 104 from the tubular string 106 and the hole. For example, one or more seals 404, such as cup-type seals 404, closure elements 114, such as ball valves or end caps, or other types of separation mechanisms may be used to at least partially enclose the portion of the bottom hole assembly 108. Continuing the example, the bottom hole assembly 108 may include a ram acceleration assembly 402 that may be sealed to enable pressurization of one or more propellant materials 802, such as gasses, contained therein.
Block 908 actuates a propellant material 802 within one or more of the fluid, the perforating charge 104, or the bottom hole assembly 108 to move the perforating charge 104 through the bottom hole assembly 108. In some implementations, propellant material 802 may be entrained within the fluid and provided into the portion of the bottom hole assembly 108 concurrent with the perforating charge 104. In other implementations, the perforating charge 104 may include propellant material 802 in the body thereof. In still other implementations, propellant material 802 may be generated in situ within the bottom hole assembly 108 or another portion of the tubular string 106, such as through use of gas or fluid generating components contained in the perforating charge 104, fluid, or bottom hole assembly 108. In yet another implementation, propellant material 802 may be positioned in the bottom hole assembly 108 prior to entry of the perforating charge 104 or may be separately flowed to the bottom hole assembly 108 using one or more fluid conduits. Actuation of the propellant material 802 may include pressurization or combustion of the propellant material 802. In some implementations, interactions between the perforating charge 104, the propellant material 802, and the interior of a ram acceleration assembly 402 may generate a ram effect that accelerates the perforating charge 104 through the bottom hole assembly 108.
Block 910 permits the perforating charge 104 to exit the bottom hole assembly 108 and move into association with a surface of the hole. For example, a closure element 114, such as a ball valve, may be opened to permit the perforating charge 104 to pass through a lower orifice of the bottom hole assembly 108. In other implementations, the closure element 114 may include an endcap or floating ball. In still other implementations, pressure within the bottom hole assembly 108 may prevent the ingress of material from the hole into the bottom hole assembly 108, and use of a closure element 114 may be omitted. In some implementations, the perforating charge 104 may include a front endcap 502 or other structure shaped to at least partially penetrate into the surface of the hole.
Block 912 detonates the detonable material in the perforating charge 104 to displace, stress, or fracture material in the hole. For example, the perforating charge 104 may include an explosive material that detonates upon impact with the surface of the hole, or upon a separate triggering event. In some implementations, detonation of the perforating charge may extend at least one dimension of the hole.
Block 914 removes detonated material from the hole using movement of the fluid. For example, detonation of the perforating charge 104 may fill at least a portion of the hole with material removed from the surface of the hole and portions of the detonated perforating charge 104. Movement of the fluid in an uphole direction may move such materials away from the surface of the hole. For example, circulation of drilling fluid 110 in a downhole direction through a tubular string 106, then in an uphole direction through an annulus 112 may remove the detonated material from a wellbore 102.
The following clauses provide additional description of various embodiments and structures:
1. A method comprising:
providing a detonable material into a tubular string positioned within a wellbore;
moving the detonable material through the tubular string and into association with a surface of the wellbore; and
detonating the detonable material to one or more of displace, stress, or fracture geologic material of the surface of the wellbore.
2. The method of clause 1, wherein the detonable material is contained within a charge assembly including:
a first end;
a second end opposite the first end;
an endcap at the first end having a shape configured to at least partially penetrate into the surface of the wellbore; and
an obturator at the second end having a shape configured to receive a force from at least one material within the tubular string to accelerate the charge assembly.
3. The method of one or more of clauses 1 or 2, further comprising providing a drilling fluid into the tubular string, wherein the drilling fluid moves the detonable material through the tubular string.
4. The method of clause 3, further comprising moving displaced geologic material and detonated detonable material away from the surface of the wellbore using movement of the drilling fluid.
5. The method of clause one or more of clauses 3 or 4, further comprising:
providing a plurality of communication components into the drilling fluid; and
providing one or more communication signals from a first device associated with the tubular string to a second device associated with the tubular string, wherein the one or more communication signals are transmitted via the plurality of communication components.
6. The method of one or more of clauses 1 through 5, further comprising:
moving the detonable material through the tubular string to an interior of a bottom hole assembly;
isolating the bottom hole assembly from the tubular string; and
actuating one or more propellant materials in the bottom hole assembly to move the detonable material through the bottom hole assembly and into association with the surface of the wellbore.
7. The method of clause 6, further comprising:
entraining at least a portion of the one or more propellant materials within drilling fluid; and
providing the drilling fluid to the bottom hole assembly through the tubular string.
8. The method of one or more of clauses 1 through 7, further comprising:
providing a drilling fluid into the tubular string, wherein the drilling fluid moves the detonable material through the tubular string;
moving the detonable material through the tubular string to an interior of a bottom hole assembly;
isolating the bottom hole assembly from the tubular string; and
diverting at least a portion of the drilling fluid through a fluid path in the bottom hole assembly, wherein the fluid path is located outside of the interior.
9. The method of one or more of clauses 1 through 8, further comprising moving the detonable material past an electrical generator associated with a wall of the wellbore, wherein the moving of the detonable material causes the electrical generator to generate power.
10. A system comprising:
a tubular string positioned within a hole, the tubular string having a first end and a second end opposite the first end;
a bottom hole assembly engaged with the second end;
a fluid source configured to move fluid through the tubular string toward the second end;
a perforating charge moved by the fluid through the tubular string toward the second end, wherein the fluid moves the perforating charge into the bottom hole assembly; and
a propellant material, wherein actuation of the propellant material moves the perforating charge through the bottom hole assembly into association with a surface of the hole.
11. The system of clause 10, wherein the propellant material is contained within the perforating charge.
12. The system of one or more of clauses 10 or 11, wherein the propellant material is entrained within the fluid in the tubular string.
13. The system of one or more of clauses 10 through 12, wherein the perforating charge includes:
an endcap at a first end, the endcap shaped to at least partially penetrate the surface of the hole; and
an obturator at a second end opposite the first end, the obturator shaped to receive a force from one or more of the fluid or the propellant material.
14. The system of one or more of clauses 10 through 13, wherein the bottom hole assembly includes a ram acceleration assembly having an interior with one or more of a plurality of baffles or a plurality of rails, wherein an interaction between the perforating charge, the propellant material, and the one or more of the plurality of baffles or the plurality of rails accelerates the perforating charge through the bottom hole assembly.
15. The system of clause 14, wherein the bottom hole assembly further includes a tubular member having an inner bore in communication with the ram acceleration assembly and a plurality of closure elements for controlling access to one or more of the inner bore or the ram acceleration assembly.
16. The system of one or more of clauses 14 or 15, wherein the ram acceleration assembly further comprises a first seal proximate to a first end and a second seal proximate to a second end, the first seal and the second seal configured to isolate the ram acceleration assembly from the tubular string for pressurizing of the propellant material.
17. A method comprising:
providing a perforating charge into a tubular string, wherein the tubular string is positioned within a hole;
providing a fluid into the tubular string to move the perforating charge through the tubular string into a portion of a bottom hole assembly; and
actuating a propellant material to move the perforating charge through the bottom hole assembly and into association with a surface of the hole.
18. The method of clause 17, wherein the portion of the bottom hole assembly includes a ram acceleration assembly, the method further comprising pressurizing the propellant material within the ram acceleration assembly, wherein an interaction between the perforating charge, the propellant material, and the ram acceleration assembly accelerates the perforating charge through the bottom hole assembly.
19. The method of one or more of clauses 17 or 18, further comprising:
providing a plurality of communication components into the fluid; and
communicating one or more signals between a first device proximate to a first end of the tubular string and a second device proximate to a second end of the tubular string by transmitting the one or more signals via the plurality of communication components.
20. The method of one or more of clauses 17 through 19, further comprising:
providing the propellant material into the fluid; and
transporting the propellant material to the bottom hole assembly using movement of the fluid.
Those having ordinary skill in the art will readily recognize that certain steps or operations illustrated in the figures above can be eliminated, combined, subdivided, executed in parallel, or taken in an alternate order. Moreover, the methods described above may be implemented using one or more software programs for a computer system and are encoded in a computer-readable storage medium as instructions executable on one or more hardware processors. Separate instances of these programs can be executed on or distributed across separate computer systems.
Although certain steps have been described as being performed by certain devices, processes, or entities, this need not be the case, and a variety of alternative implementations will be understood by those having ordinary skill in the art.
Additionally, those having ordinary skill in the art readily recognize that the techniques described above can be utilized in a variety of devices, environments, and situations. Although the present disclosure is written with respect to specific embodiments and implementations, various changes and modifications may be suggested to one skilled in the art, and it is intended that the present disclosure encompass such changes and modifications that fall within the scope of the appended claims.
This patent application claims priority to the U.S. provisional application for patent, having application Ser. No. 62/255,161, filed on Nov. 13, 2015, entitled “Down-Hole Hyperdrill”. Application 62/255,161 is incorporated by reference herein in its entirety. In addition to Application 62/255,161, which is incorporated by reference in its entirety above, the following are incorporated by reference for all that they contain: U.S. provisional patent application 62/253,228, filed on Nov. 10, 2015, entitled “Pressurized Ram Accelerator System”. U.S. patent application Ser. No. 15/340,753, filed on Nov. 1, 2016, entitled “Projectile Drilling System”. U.S. patent application Ser. No. 13/841,236, filed on Mar. 15, 2013, entitled “Ram Accelerator System”. U.S. patent application Ser. No. 15/292,011, filed on Oct. 12, 2016, entitled “Ram Accelerator System”. U.S. provisional patent application 61/992,830, filed on May 13, 2014, entitled “Ram Accelerator System with Endcap”. U.S. patent application Ser. No. 14/708,932, now U.S. Pat. No. 9,458,670, filed on May 11, 2015, entitled “Ram Accelerator System with Endcap”. U.S. patent application Ser. No. 15/246,414, filed on Aug. 24, 2016, entitled “Ram Accelerator System with Endcap”. U.S. provisional patent application 62/067,923, filed on Oct. 23, 2014, entitled “Ram Accelerator System with Rail Tube”. U.S. patent application Ser. No. 14/919,657, filed on Oct. 21, 2015, entitled “Ram Accelerator System with Rail Tube”. U.S. provisional patent application 62/150,836, filed on Apr. 21, 2015, entitled “Ram Accelerator System with Baffles”. U.S. patent application Ser. No. 15/135,452, filed on Apr. 21, 2016, entitled “Ram Accelerator System with Baffles”. U.S. provisional patent application 393,631, filed on Sep. 12, 2016, entitled “Augmented Drilling System Using Ram Accelerator Assembly”.
Number | Name | Date | Kind |
---|---|---|---|
2544573 | Vincent | Mar 1951 | A |
2621732 | Ahlgren | Dec 1952 | A |
2913959 | Mohaupt | Nov 1959 | A |
3075463 | Eilers et al. | Jan 1963 | A |
3185224 | Robinson, Jr. | May 1965 | A |
3244232 | Myers | Apr 1966 | A |
3253511 | Zwicky | May 1966 | A |
3441095 | Youmans | Apr 1969 | A |
3695715 | Godfrey | Oct 1972 | A |
3863723 | Godfrey | Feb 1975 | A |
3867867 | Duff | Feb 1975 | A |
4030557 | Alvis et al. | Jun 1977 | A |
4063486 | Ashley | Dec 1977 | A |
4123975 | Mohaupt | Nov 1978 | A |
4467878 | Ibsen | Aug 1984 | A |
4582147 | Dardick | Apr 1986 | A |
4638712 | Chawla et al. | Jan 1987 | A |
4679637 | Cherrington et al. | Jul 1987 | A |
4722261 | Titus | Feb 1988 | A |
4791850 | Minovitch | Dec 1988 | A |
4907488 | Seberger | Mar 1990 | A |
4932306 | Rom | Jun 1990 | A |
4982647 | Hertzberg et al. | Jan 1991 | A |
5063826 | Bulman | Nov 1991 | A |
5097743 | Hertzberg et al. | Mar 1992 | A |
5098163 | Young, III | Mar 1992 | A |
5421237 | Naumann | Jun 1995 | A |
5487405 | Skoglund | Jan 1996 | A |
5574244 | Powell et al. | Nov 1996 | A |
5578783 | Brandeis | Nov 1996 | A |
5768940 | Kawaguchi et al. | Jun 1998 | A |
5833003 | Longbottom et al. | Nov 1998 | A |
5996709 | Norris | Dec 1999 | A |
6000479 | Ambs | Dec 1999 | A |
6035784 | Watson | Mar 2000 | A |
6457417 | Beal | Oct 2002 | B1 |
6467387 | Espinosa et al. | Oct 2002 | B1 |
6591731 | Goldstein | Jul 2003 | B2 |
7069862 | Bassett | Jul 2006 | B2 |
7681352 | Fu et al. | Mar 2010 | B2 |
7775148 | McDermott | Aug 2010 | B1 |
7942481 | Leppanen | May 2011 | B2 |
8181561 | Riggs et al. | May 2012 | B2 |
8302584 | Lu | Nov 2012 | B1 |
8943970 | Greeley et al. | Feb 2015 | B2 |
9103618 | Daniel et al. | Aug 2015 | B2 |
9169695 | Calvert | Oct 2015 | B1 |
9540895 | Mackenzie | Jan 2017 | B2 |
10132578 | Knowlen et al. | Nov 2018 | B2 |
20020100361 | Russell | Aug 2002 | A1 |
20050034896 | Youan | Feb 2005 | A1 |
20070044963 | MacDougall | Mar 2007 | A1 |
20070256826 | Ceccarelli et al. | Nov 2007 | A1 |
20080205191 | Coste et al. | Aug 2008 | A1 |
20090322185 | Barnard et al. | Dec 2009 | A1 |
20100032206 | Becker et al. | Feb 2010 | A1 |
20100133006 | Shakra et al. | Jun 2010 | A1 |
20110114388 | Lee et al. | May 2011 | A1 |
20110186377 | Kline et al. | Aug 2011 | A1 |
20130032337 | Rytlewski et al. | Feb 2013 | A1 |
20140158356 | Andrzejak et al. | Jun 2014 | A1 |
20140260930 | Russell | Sep 2014 | A1 |
20150021023 | Roberts et al. | Jan 2015 | A1 |
Number | Date | Country |
---|---|---|
101017076 | Aug 2007 | CN |
101099024 | Jan 2008 | CN |
102322216 | Jan 2012 | CN |
102667047 | Sep 2012 | CN |
102822442 | Dec 2012 | CN |
202596572 | Dec 2012 | CN |
2420035 | Mar 1976 | DE |
0663582 | Nov 1995 | EP |
1999037878 | Jul 1999 | WO |
2014149173 | Sep 2014 | WO |
2015030730 | Mar 2015 | WO |
Entry |
---|
Thomas, Shane, “Patent Cooperation Treaty International Search Report and Written Opinion dated Feb. 2, 2017”, Patent Cooperation Treaty Application No. PCT/US16/61660, Patent Cooperation Treaty, Feb. 2, 2017. |
Becamel, Philippe, “Patent Cooperation Treaty International Preliminary Report on Patentabililty dated Sep. 15, 2015”, Patent Cooperation Treaty Application PCT/US2014/012317, Patent Cooperation Treaty, Sep. 15, 2015. |
Committee on Advanced Drilling Technologies, “Drilling and Excavation Technologies for the Future”, National Research Council, ISBN: 0-309-57320-3, <<Retrieved from http://www.nap.edu/catalog/2349.html>>, 1994, 176 pages. |
Copenheaver, Blaine R., “Patent Cooperation Treaty International Search Report and Written Opinion dated Aug. 10, 2015”, Patent Cooperation Treaty Application No. PCT/US2015/030320, Patent Cooperation Treaty, Aug. 10, 2015. |
Fang, et al., “Hypersonic wave drag reduction performance of cylinders with repetitive laser energy depositions”, 3rd Int'l Photonics & OptoElectronics Meetings (POEM 2010), Journal of Physics: Conference Series 276 (2011) 012021, [retrieved on Oct. 20, 2015]. Retrieved from <<http://iopscience.iop.org/article/10.1088/1742-596/276/1/012021/pdf>> 8 pages. |
Gold, et al., “Concrete Penetration by Eroding Projectiles Experiments and Analysis”, Journal of Engineering Mechanics, v122, pp. 145-152 <<Retrieved from ascelibrary.org on Feb. 17, 2013>>, Feb. 1996, 145-152. |
Gold, et al., “Constitutive Models for Concrete Penetration Analysis”, Journal of Engineering Mechanics v122 <<Retrieved from ascelibrary.org on Feb. 17, 2013 >>, Mar. 1996, pp. 230-238. |
Jingna, Xie, “First Office Action dated Jun. 2, 2016”, CN Patent Application No. 201480016227.3, The Chinese Intellectual Property Office, Jun. 2, 2016. |
Lundquist, Robert G., “Underground Tests of the Ream Method of Rock Fragmentation for High-Speed Tunneling”, Rapid Excavation and Tunneling Conference Proceedings, Ch. 56, <<Retrieved from http://www.onemine.org/view/?d=689528D8459E7257609C73381053FBF203FD5CC5A9FC7839952A414670F0591638551, Mar. 13, 2013>>, Jan. 1974, pp. 825-840. |
Semick, Joshua T., “Notice of Allowance dated May 25, 2016”, U.S. Appl. No. 14/708,932, The United States Patent and Trademark Office, May 25, 2016. |
Weber, Jonathan C., “Non-final Office Action dated Dec. 20, 2016”, U.S. Appl. No. 15/292,011, The United States Patent and Trademark Office, Dec. 20, 2016. |
Weber, Jonathan C., “Non-Final Office Action dated Jun. 1, 2015”, U.S. Appl. No. 13/841/236, The United States Patent and Trademark Office, Jun. 1, 2015. |
Weber, Jonathan C., “Notice of Allowance dated Jul. 14, 2016”, U.S. Appl. No. 13/841,236, The United States Patent and Trademark Office, Jul. 14, 2016. |
Young, Lee W., “Patent Cooperation Treaty International Search Report and Written Opinion dated Jan. 8, 2016”, Patent Cooperation Treaty Application No. PCT/US2015/056947, Patent Cooperation Treaty, Jan. 8, 2016. |
Young, Lee W., “Patent Cooperation Treaty International Search Report and Written Opinion dated Jul. 28, 2016”, Patent Cooperation Treaty Application No. PCT/US2016/028704, Patent Cooperation Treaty, Jul. 28, 2016. |
Young, Lee W., “Patent Cooperation Treaty International Search Report and Written Opinion dated May 16, 2014”, Patent Cooperation Treaty Application No. PCT/US2014/012317, Patent Cooperation Treaty, May 16, 2014. |
Semick, Joshua T., “Non-final Office Action dated Jul. 18, 2017”, U.S. Appl. No. 15/246,414, The United States Patent and Trademark Office, Jul. 18, 2017. |
Sayre, James G., “Non-Final Office Action dated Aug. 24, 2017”, U.S. Appl. No. 14/919,657, The United States Patent and Trademark Office, Aug. 24, 2017. |
Weber, Jonathan C., “Final Office Action dated Jun. 15, 2017”, U.S. Appl. No. 15/292,011, The United States Patent and Trademark Office, Jun. 15, 2017. |
Kasten, Klaus, “European Search Report dated Jan. 23, 2017”, European Application No. 14770528.9, European Patent Office, Jan. 23, 2017. |
Young, Lee W., “Patent Cooperation Treaty International Search Report and Written Opinion dated Jan. 19, 2017”, Patent Cooperation Treaty Application No. PCT/US16/60129, Patent Cooperation Treaty, Jan. 19, 2017. |
Bogdanoff, David W., “New Tube End Closure System for the Ram Accelerator,” Journal of Propulsion and Power., vol. 10, No. 4, Jul. 1-Aug. 1994, pp. 518-521. |
Hansen, Viggo, “Ram Accelerator Animation”, YouTube, Science & Technology, Uploaded on May 2, 2011. Retrieved from the Internet: https://www.youtube.com/watch?v=iFQfOKVi98l. |
Van Berlo, Andre, “European Search Report dated Sep. 7, 2017”, European Patent Application No. 15791990.3, European Patent Office, Sep. 7, 2017. |
Wittmann-Regis, Agnes, “PCT International Preliminary Report on Patentability dated May 24, 2018”, Patent Cooperation Treaty Application No. PCT/US16/60129, Patent Cooperation Treaty, May 24, 2018. |
Runyan, Ronald R., “Final Office Action dated Jan. 28, 2019”, U.S. Appl. No. 15/135,452, The United States Patent and Trademark Office, Jan. 28, 2019. |
Number | Date | Country | |
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20170138128 A1 | May 2017 | US |
Number | Date | Country | |
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62255161 | Nov 2015 | US |