A high-power millimeter-wave beam produced by a gyrotron can make a borehole in rock by melting and/or vaporizing the rock. This borehole opening process operates at temperatures greater than the melting and vaporization temperatures of rock of 1000° C. and 3000° C., respectively. Conventional sensors used for monitoring mechanically drilled boreholes require physical contact with the bottom of the borehole and cannot survive at these temperatures.
The present technology can be used to form deep boreholes in rock with a high-power millimeter-wave beam and to monitor the bottom of the borehole. The monitoring equipment can remain on the ground surface, at ambient temperature and pressure, regardless of the borehole depth or temperature.
The present technology includes a method of measuring a depth and/or a rate of penetration of a borehole drilled with a millimeter-wave drilling beam guided by a transmission line to the bottom of the borehole. This method includes coupling a probe signal into the transmission line. The transmission guides the probe signal to the bottom of the borehole, and at least a portion of the probe signal reflects and/or scatters from the bottom of the borehole as a return beam. The transmission line guides the return beam from the bottom of the borehole. The return beam is coupled out of the transmission line and mixed with a local oscillator to produce an intermediate frequency beam whose amplitude and/or frequency are used to determine the depth and/or the rate of penetration of the borehole.
In some cases, the amplitude of the probe signal is modulated, in which case the depth and/or the rate of penetration of the borehole can be based on the amplitude of the intermediate frequency beam. In other cases, the frequency of the probe signal is modulated, in which case the depth and/or the rate of penetration of the borehole is based on the frequency of the intermediate frequency beam. And in yet other cases, the probe signal comprises a pulse and the depth and/or the rate of penetration of the borehole is based a time of flight of the pulse.
The probe signal can be generated at a frequency different than a frequency of the millimeter-wave drilling beam or can be picked off from the millimeter-wave drilling beam.
If desired, a temperature signal at a temperature signal frequency different than the frequency of the millimeter-wave drilling beam (and different than the probe frequency) can be coupled into the transmission line with the probe signal for determining the temperature at the bottom of the borehole.
Other embodiments of the present technology include a system for drilling a borehole with a source, transmission line, depth/rate-of-penetration monitor, and beam combiner. In operation, the source generates a millimeter-wave drilling beam. The transmission line, which is coupled to the source, guides the millimeter-wave drilling beam to the bottom of the borehole. The depth/rate-of-penetration monitor, which is also coupled to the transmission line, monitors a depth and/or a rate-of-penetration of the borehole. And the beam combiner, which is coupled to the transmission line and the depth/rate-of-penetration monitor, couples a probe signal into the transmission line for transmission to the bottom of the borehole and couples a return beam generated by reflection and/or scattering of the probe signal from the bottom of the borehole from the transmission line to the depth/rate-of-penetration monitor.
The depth/rate-of-penetration monitor can be configured to operate as a reflectometer, frequency-modulated radar, or pulse-modulated time of flight radar. The depth/rate-of-penetration monitor can generate the probe signal at a frequency different than a frequency of the millimeter-wave drilling beam. In other cases, the beam combiner directs a portion of the millimeter-wave drilling beam returned from the bottom of the borehole to the depth/rate-of-penetration monitor as the return beam.
The beam combiner may comprise a miter mirror to reflect the millimeter-wave drilling beam around a bend of the transmission line. There can be a hole in the miter mirror to pass radiation at the probe frequency and to reject radiation at the frequency of the millimeter-wave drilling beam.
The system may also include a temperature monitor to receive a temperature signal for monitoring a temperature of the borehole at a temperature signal frequency different than the frequency of the millimeter-wave drilling beam and different than the probe frequency. And it can include a small-signal beam combiner, coupled to the depth/rate-of-penetration monitor, the temperature monitor, and the beam combiner, to couple the temperature signal with the probe signal.
All combinations of the foregoing concepts and additional concepts discussed in greater detail below (provided such concepts are not mutually inconsistent) are contemplated as being part of the inventive subject matter disclosed herein. In particular, all combinations of claimed subject matter appearing at the end of this disclosure are contemplated as being part of the inventive subject matter disclosed herein. Terminology explicitly employed herein that also may appear in any disclosure incorporated by reference should be accorded a meaning most consistent with the particular concepts disclosed herein.
The drawings are primarily for illustrative purposes and are not intended to limit the scope of the inventive subject matter. The drawings are not necessarily to scale; in some instances, various aspects of the inventive subject matter disclosed herein may be shown exaggerated or enlarged in the drawings to facilitate an understanding of different features. In the drawings, like reference characters generally refer to like features (e.g., functionally similar and/or structurally similar elements).
High-power MMW radiation 103 from the high-power source 120 can be coupled into high-power transmission lines 130 (which may be implemented as waveguides) and delivered to the bottom of the borehole 110. At the bottom of the borehole, the high-power MMW radiation 103 can exit the distal end 138 of the transmission line 130 and form the drilling beam 105 that interacts with material in its path. According to some embodiments, the drilling beam 105 has sufficient power to melt granite, for example. A high-power source 120, such as a gyrotron, can generate the MMW radiation 103 at a frequency in a range from approximately or exactly 30 GHz to approximately or exactly 300 GHz with an average power in a range from approximately or exactly 100,000 Watts to approximately or exactly 2,000,000 Watts. The MMW radiation 103 can be continuous wave at these power levels or can be pulsed to produce higher instantaneous power levels.
The power and frequency of MMW radiation 103 from the high-power source 120 can be constant with time when the system 100 is drilling the borehole 110. For example, the power and frequency may remain constant for seconds, minutes, tens of minutes, or even over an hour as the borehole is drilled. In some cases, one or both of the power and frequency of MMW radiation 103 from the high-power source 120 can vary within the frequency range and power range described above when the system 100 is drilling the borehole 110. For example, the frequency and/or power may change when encountering different materials to improve energy coupling to and heating of the different materials.
Probe signals 108, 109 from the monitors 160, 170 can be radiatively coupled into and from the high-power transmission line 130 with one or more combiners 140, 142. The probe signal(s) 108, 109 can be at one or more different frequencies from a frequency of the high-power drilling beam 105 to sense condition(s) at the bottom of the borehole 110. Further, the probe signal 108 from the ROP/depth monitor 160 can be at a different frequency than a frequency or frequencies used for the ancillary monitor(s) 170. For example, the frequency used for the ROP/depth monitor can be in a range from 10 GHz to 300 GHz. In some cases, the frequency used for the ROP/depth monitor can be in a range from 10 GHz to 1 THz. The frequency used for the ancillary monitor(s) can also be in a range from 10 GHz to 300 GHz. In some cases, the frequency used for the ancillary monitor(s) can be in a range from 10 GHz to 1 THz. The power level of probe signals can be in a range from 0.1 Watt to 100 Wats, or even higher power levels in some cases. When detecting thermal emission from the bottom of the borehole 110, the power level of a received probe signal 109 can be less than 0.1 Watt. The phrase “probe signal” is used herein to refer to a signal that is launched into the borehole by the ROP/depth monitor 160 or an ancillary monitor 170 and used for measuring a characteristic of the borehole 110. In some cases, an ancillary monitor (such as a temperature radiometer) may not launch a probe signal and instead receive and monitor radiative emissions (e.g., black body radiation) from the borehole. Conditions that can be sensed by the ROP/depth monitor 160 and ancillary monitor(s) include but are not limited to: the rate of penetration of the borehole 110 as it is being drilled, the depth of the borehole 110, surface emissivity ε of the earthen material, and a temperature of earthen material 150 as the borehole 110 is being drilled. The depth of the borehole 110 may or may not be measured while the borehole is actively being drilled.
The high-power transmission line 130 guides the high-power MMW radiation 103 from the high-power source 120 to the bottom of the borehole, where the drilling beam 105 can vaporize rock and other material. The high-power transmission line 130 is typically hollow and of a size that is more than one wavelength in diameter (overmoded) so it can handle high power. It is constructed to reduce or minimize mode conversion so that the most efficient fundamental mode can propagate with minimum losses. There can be some purposeful mode conversion for special applications at launch from the distal end 138 or to negotiate a bend more efficiently, but largely the MMW radiation 103 propagates through the high-power transmission line 130 in a single mode for efficient long-distance transmission. The linearly polarized HE11 mode is the most efficient mode in a circular high-power transmission line 130 that is internally corrugated having a good conductor metal surface, such as copper. Other suitable modes include the azimuthally polarized TE01 mode in a smooth-walled metal waveguide. This has 69% of the efficiency of the HE11 mode in an internally corrugated circular waveguide. The HE11 mode can also be guided by the borehole 110, which acts like a dielectric waveguide, such as a hollow fiber optic cable. For example, the drilling beam 105 can vitrify walls of the borehole 110 as it advances forming a hollow, circular dielectric waveguide.
The MMW drilling system 100 can include a ROP/depth monitor 160 that is radiatively coupled to the high-power transmission line 130. The ROP/depth monitor 160 generates a small-signal probe signal, also called a probe signal 108 or probe beam, which can be at a different frequency than the drilling beam 105 for sensing the ROP and/or depth of the borehole. For example, the probe signal 108 may be centered at a probe frequency in a frequency range from 30GHz to 1 THz range with a bandwidth up to 5 GHz. In some cases, the frequency of the probe signal 108 can vary over frequencies within this range of frequencies when making measurements. Preferably, the probe signal 108 can be guided by the same high-power transmission line 130 that guides the drilling beam 105. The average probe signal power can be in a range from 0.01 Watt to 10 Watts and may be constant or vary over a range of power levels within this range when making a measurement.
One or more ancillary monitors 170 may generate and/or receive one or more other small-signal probe signals 109 at other frequencies for probing or monitoring other parameters associated with drilling the borehole 110 and the MMW drilling system 100. In some cases, an ancillary monitor 170 receives radiative emissions from the borehole for analysis. For instance, the ancillary monitor 170 may monitor the borehole temperature by radiometry and/or the waveguide/borehole fill composition by millimeter-wave or terahertz spectroscopy, respectively. In some implementations, the temperature can be monitored by millimeter-wave thermal emission from the bottom of the borehole 110 that couples into the transmission line 130 and propagates back to the ancillary monitor 170. The radiometer antenna pattern defined by the high-power transmission line 130 and 138 selects the viewed spot size that forms the returned temperature signal. (Thermal emission occurs in all modes, with the receiver antenna pattern selecting the mode(s) that will propagate along the high-power transmission line 130 and be detected by the ancillary monitor 170. Therefore, the returned thermal signal 109 has properties that are defined at least in part by the radiometer field of view.) In some cases, the fill composition can be monitored by millimeter-wave or terahertz spectroscopic emission or absorption. Spectroscopy performed by an ancillary monitor 170 can be either passive using the thermal blackbody emission background or local plasma excited emission, or active with a frequency-swept probe signal. For passive spectroscopy, the receiving antenna (essentially the high-power transmission line 130) essentially defines the return signal, as is the case for the return temperature signal. For active probing, the high-power waveguide defines and guides the probe signal. These ancillary probe signals may have average power levels in a range from 0.1 Watt to 100 Watts and may operate at one or more frequencies in a range from 30 GHz to 1 THz.
In some implementations, temperature monitoring can include launching a temperature probe signal by an ancillary monitor 170 into the borehole 110. The temperature probe signal can be used to determine surface emissivity ε at the bottom of the borehole. Generally, the radiative emission from the bottom of the borehole (and detected by a temperature radiometer) is the product of surface emissivity and temperature (εT). The emissivity can have a value in a range from 0 to 1. Knowing the surface emissivity can provide a more accurate determination of temperature of earthen material 150 at the bottom of the borehole 110. Emissivity can be measured by measuring the reflectivity of the surface with the temperature probe signal. For an opaque surface the emissivity can be found from the expression, ε=1−r, where r is the surface reflection.
Temperature monitoring can be useful for two reasons. First, the temperature of the earthen material can be monitored while drilling to improve removal efficiency. For example, a certain temperature may be maintained while drilling (e.g., using a feedback loop that receives a signal from the drilling area indicative of temperature and adjusts delivered power accordingly). The maintained temperature may be one that vaporizes the earthen material or ablates it into predominantly micro-particles that can be ejected from the borehole using high-pressure gas. The pressurized gas can be pumped down the transmission line 130 and pressurized by energy from the drilling beam 105 which increases the temperature of material in the confined borehole volume as described by the ideal and real gas laws while vapors and/or micro-particles are ejected upward outside the transmission line.
Second, for geothermal heat access, temperature monitoring is also useful when drilling has ceased, and the earthen material allowed to cool to a lower temperature or its steady-state temperature. In this case, the temperature monitoring can determine when a sufficient depth is reached to access the geothermal heat. For example, the temperature may fall to its steady-state temperature, which can be measured by a temperature monitor. Alternatively, at least one lower temperature can be measured as the temperature falls to its steady-state temperature. A steady-state temperature (at which geothermal energy can be harnessed and further drilling is not needed) can be in a range from 50° C. to 500° C. An exponential or functional fit to the falling temperature may be used to determine an ultimate steady-state temperature at the bottom of the borehole.
The ancillary probe signal(s) 109 from the ancillary monitor(s) 170 can be combined with the probe signal 108 from the ROP/depth monitor 160 by a small-signal combiner 142 onto a common small-signal transmission line 133 that carries the probe signals 108, 109 to and from a power combiner 140, as depicted in
The small-signal probe signals 108, 109 can return from the bottom of the borehole 110 and can be guided by the high-power transmission line 130 back to the power combiner 140, which couples the returned small-signal probe signals 108, 109 to the small-signal combiner 142 via the small-signal transmission line 133. The small-signal combiner 142 directs the different small-signal probe signals 108, 109 and/or radiative emissions to the respective monitors 160, 170. The return signals can be divided and sent to the respective monitors using frequency, polarization, or time to demultiplex the signals at the small-signal combiner 142. The monitors 160, 170 measure the amplitude, frequency, and/or phase of their corresponding received probe signal to derive some information about conditions at the bottom of the borehole 110, such as the drilling beam's rate of penetration, the borehole depth, surface emissivity, melt turbulence, and/or temperature among other characteristics. Because the monitors 160, 170 derive information from the returned probe signals 108, 109 and/or radiative emissions, they can remain on the ground surface, far from the bottom of the borehole 110 which is heated to extreme temperatures. As a result, the monitors do not have to be as rugged as the downhole monitors used to monitor mechanical drills, for example. They can also monitor conditions at the bottom of the borehole 110 that are more extreme (e.g., hotter) than those at bottom of boreholes made with mechanical drills.
Evaluating melt turbulence can be beneficial for drilling deep boreholes. Melt turbulence can indicate a level of viscosity of the molten earthen material 150. For some drilling applications, once a suitable viscosity is reached, the molten earthen material 150 can be displaced to the wall of the borehole where it will cool to form a solid casing that lines the borehole 110. This self-casing can stabilize the borehole 110 and may be sufficiently strong in some cases to prevent collapse of the borehole.
In the second ROP/depth monitor 162, the reflected signal from the polarizing grill mixes coherently with the portion of the forward-traveling high-power MMW radiation 103 coupled to the ROP/depth monitor 162 for use as a local oscillator. The ROP/depth monitor 160 can have its own frequency source that provides the local oscillator signal for that monitor, which can be at a frequency different than the frequency of the MMW radiation 103. The ROP/depth monitors 160, 162 detect their beat or intermediate frequency caused by mixing their respective local oscillator signals with received reflected signals from the borehole 110 and they process their respective detected beat signals to determine ROP or depth of the borehole 110. If the MMW radiation 103 and drilling beam 105 are at a constant frequency, the rate-of-penetration/depth monitor 162 acts a reflectometer, with the number of amplitude maxima and minima representing the depth of the borehole as described below. If the frequency of the MMW radiation 103 and drilling beam 105 are chirped or swept, the rate-of-penetration/depth monitor 162 acts as a frequency-modulated (FM) radar, with the phase or frequency of the beat representing the depth of the borehole as described below. Similarly, the frequency source of the ROP/depth monitor 160 can be fixed or swept to operate the ROP/depth monitor as a reflectometer or FM radar, respectively.
In some examples, the high-power MMW radiation 103, small-signal probe signals 108, 109, and radiative emissions of interest from the bottom of the borehole 110 are at different frequencies so that they can be frequency multiplexed and demultiplexed using the small-signal combiner 142 and power combiner 140. The small-signal monitors 160, 170 can be radiatively coupled to the high-power transmission line 130 by using fundamental mode microwave/millimeter-wave waveguide components, such as signal dividers, directional couplers, or frequency multiplexers. (A waveguide that supports only a fundamental mode has a cross section less than one wavelength or on the order of one-half wavelength of the radiation used by a small-signal monitor 160 or 170.) The monitors' probe signals 108, 109 can be coupled to the high-power transmission line 130 using configurations described in connection with
In the beam combiner of
In the power combiner 140b of
A transition region comprising a section of tapered waveguide 230 can be located between the small-signal transmission line 133 and the high-power transmission line 130 and may be located near the dichroic or polarization-dependent filter 220 (e.g., within 10 cm of the mirror). The tapered waveguide 230 can transform the transverse mode from the small-signal transmission line 133 to better match to a mode supported by the high-power transmission line 130 and vice versa so as to reduce mode coupling losses between the two transmission lines. In some cases, even though the wavelength(s) of the probe signal(s) can be longer than the wavelengths of the high-power MMW radiation 103, the diameter of the small-signal transmission line 133 can be much smaller than the diameter of the high-power transmission line 130. The tapered waveguide 230 aides in coupling the probe signals 108, 109, which propagate in the small-signal transmission line 133, to and from the larger high-power transmission line 130. The taper of the tapered waveguide 230 can be linear or parabolic and should be long enough to reduce or minimize mode conversion losses (e.g., below 10 dB). Parabolic tapers are generally shorter than linear tapers. The internal surface of the tapered waveguide 230 preferably matches the internal surfaces of the transmission lines to which the tapered waveguide 230 connects. For example, the tapered waveguide 230 may have a corrugated internal surface to transmit the HE11 mode efficiently when the transmission lines 130, 133 to which it connects are implemented as waveguides having corrugated internal surfaces. The end widths (diameters) of the tapered waveguide 230 are sized to match the widths (diameters) of the transmission lines to which the ends connect. A high-power gyrotron frequency notch filter may also be added to the small signal monitoring waveguide to further reject any stray or scattered high-power gyrotron electromagnetic radiation.
One example of a high-power dielectric component that can be used in a power combiner 140b is a diamond plate oriented at Brewster's angle, which is 67 degrees for diamond in air at one atmosphere pressure. The diamond plate combines and separates beams with orthogonal linear polarizations. At Brewster's angle, the polarization in the plane-of-incidence (plane containing the incident and reflected beam vectors and the normal to the plate) is transmitted with no loss (except for very minor plate absorption) and the beam with perpendicular polarization to the plane-of-incidence is highly reflected. The transmitted beam would be the high-power MMW radiation 103 propagating along the high-power transmission line 130 and the reflected beam would be the probe signal 108 and/or probe signal 109.
Continuing up from the miter mirror 210 in the example system of
The ROP/depth monitor 160 can operate as either a reflectometer (reflection interferometer), a frequency-modulated (FM) radar, or a pulsed time-of-flight radar. In the reflectometer configuration, the frequency of the small-signal ROP/depth probe signal 108, also called the probe frequency, is fixed. The returned probe signal 108 is mixed with an un-transmitted part of itself to produce a DC signal whose amplitude depends on the round-trip return phase of the returned probe signal 108 relative to what it was before transmission. For a change in depth equal to a quarter of a wavelength at the probe frequency, the detected signal amplitude should vary from a maximum to a minimum or vice versa. Put differently, in the reflectometer configuration, the ROP/depth monitor 160 has a depth resolution, Δz, that can be written as:
where λ is the wavelength at the probe frequency. The ROP is determined by measuring the rate at which the signal changes from maximum to minimum and the depth is determined by counting the number maximum-to-minimum changes from a starting or reference phase of the probe transmission as a function of time.
In the FM radar configuration, the probe frequency is swept over a bandwidth of Δf at some modulation frequency rate fm. The phase shift of the round-trip reflection when detected in a mixer with an un-transmitted copy of the ROP/depth probe signal 108 generates a tone at an intermediate beat frequency, fB, that is proportional to the depth, Z. The depth is given by:
where c is the speed of the MMW propagation in the high-pressure fill of the high-power MMW transmission line 130. In some implementations, a gas may be forced down the transmission line 130 to aid in removal of vaporized and/or particulate material from the bottom of the borehole 110 to deepen the borehole. The resolution of the depth depends on the bandwidth of the frequency sweep:
The relative merits of the reflectometer and FM radar configurations can be appreciated by considering an example frequency. At 94 GHz (λ=3.19 mm) and tuning bandwidth of 1 GHz typically available for a commercial Gunn oscillator, the depth resolution for the reflectometer would be 0.8 mm (Eq. 1) and 150 mm for the FM radar (Eq. 3). The reflectometer is better suited for shallow boreholes (e.g., laboratory boreholes) that are less than a few times deeper than the FM radar resolution, while the FM radar is better suited for deep boreholes in the field. Also, the measurement of a frequency is more reliable for a deep borehole than an amplitude change that could vary for reasons other than a phase change.
In the time-of-flight configuration, a short electromagnetic pulse (having a full-width-half-maximum pulse duration of τ) is transmitted toward the bottom of the borehole. The round-trip time delay for the pulse's return to the surface electronics can be used to determines the distance to the bottom of the hole. The relation is given by:
where c is the speed of the transmitted pulse and Δt is the round-trip delay time. The spatial resolution depends on the pulse length, τ, and the speed of the transmitted pulse:
In air at atmospheric pressure, the speed of propagation is the speed of light. For a 1 ns pulse, which corresponds to available 1 GHz electronics, the resolution would be 300 mm.
The peak pulse power level could be as high at 100 kW in pulsed operation. The high-power and lower spatial resolution with a time-of-flight configuration would be suitable for the deepest boreholes that are drilled.
The circuitry of
Apparatus for measuring the depth or rate of penetration of a borehole drilled with a millimeter-wave directed-energy drilling beam can be implemented and/or included in drilling systems in various configurations. Example configurations are listed below. Corresponding methods of measuring depth or rate of penetration can also be implemented.
All parameters, dimensions, materials, and configurations described herein are meant to be exemplary and the actual parameters, dimensions, materials, and/or configurations will depend upon the specific application or applications for which the inventive teachings is/are used. It is to be understood that the foregoing embodiments are presented primarily by way of example and that, within the scope of the appended claims and equivalents thereto, inventive embodiments may be practiced otherwise than as specifically described and claimed. Inventive embodiments of the present disclosure are directed to each individual feature, system, article, material, kit, and/or method described herein. In addition, any combination of two or more such features, systems, articles, materials, kits, and/or methods, if such features, systems, articles, materials, kits, and/or methods are not mutually inconsistent, is included within the inventive scope of the present disclosure.
Also, various inventive concepts may be embodied as one or more methods, of which at least one example has been provided. The acts performed as part of the method may in some instances be ordered in different ways. Accordingly, in some inventive implementations, respective acts of a given method may be performed in an order different than specifically illustrated, which may include performing some acts simultaneously (even if such acts are shown as sequential acts in illustrative embodiments).
All publications, patent applications, patents, and other references mentioned herein are incorporated by reference in their entirety.
All definitions, as defined and used herein, should be understood to control over dictionary definitions, definitions in documents incorporated by reference, and/or ordinary meanings of the defined terms.
The indefinite articles “a” and “an,” as used herein in the specification and in the claims, unless clearly indicated to the contrary, should be understood to mean “at least one.”
The phrase “and/or,” as used herein in the specification and in the claims, should be understood to mean “either or both” of the elements so conjoined, i.e., elements that are conjunctively present in some cases and disjunctively present in other cases. Multiple elements listed with “and/or” should be construed in the same fashion, i.e., “one or more” of the elements so conjoined. Other elements may optionally be present other than the elements specifically identified by the “and/or” clause, whether related or unrelated to those elements specifically identified. Thus, as a non-limiting example, a reference to “A and/or B”, when used in conjunction with open-ended language such as “comprising” can refer, in one embodiment, to A only (optionally including elements other than B); in another embodiment, to B only (optionally including elements other than A); in yet another embodiment, to both A and B (optionally including other elements); etc.
As used herein in the specification and in the claims, “or” should be understood to have the same meaning as “and/or” as defined above. For example, when separating items in a list, “or” or “and/or” shall be interpreted as being inclusive, i.e., the inclusion of at least one, but also including more than one, of a number or list of elements, and, optionally, additional unlisted items. Only terms clearly indicated to the contrary, such as “only one of” or “exactly one of,” or, when used in the claims, “consisting of,” will refer to the inclusion of exactly one element of a number or list of elements. In general, the term “or” as used herein shall only be interpreted as indicating exclusive alternatives (i.e., “one or the other but not both”) when preceded by terms of exclusivity, such as “either,” “one of,” “only one of,” or “exactly one of.” “Consisting essentially of,” when used in the claims, shall have its ordinary meaning as used in the field of patent law.
As used herein in the specification and in the claims, the phrase “at least one,” in reference to a list of one or more elements, should be understood to mean at least one element selected from any one or more of the elements in the list of elements, but not necessarily including at least one of each and every element specifically listed within the list of elements and not excluding any combinations of elements in the list of elements. This definition also allows that elements may optionally be present other than the elements specifically identified within the list of elements to which the phrase “at least one” refers, whether related or unrelated to those elements specifically identified. Thus, as a non-limiting example, “at least one of A and B” (or, equivalently, “at least one of A or B,” or, equivalently “at least one of A and/or B”) can refer, in one embodiment, to at least one, optionally including more than one, A, with no B present (and optionally including elements other than B); in another embodiment, to at least one, optionally including more than one, B, with no A present (and optionally including elements other than A); in yet another embodiment, to at least one, optionally including more than one, A, and at least one, optionally including more than one, B (and optionally including other elements); etc.
In the claims, as well as in the specification above, all transitional phrases such as “comprising,” “including,” “carrying,” “having,” “containing,” “involving,” “holding,” “composed of,” and the like are to be understood to be open-ended, i.e., to mean including but not limited to. Only the transitional phrases “consisting of” and “consisting essentially of” shall be closed or semi-closed transitional phrases, respectively, as set forth in the United States Patent Office Manual of Patent Examining Procedures, Section 2111.03.
The present application claims a priority benefit, under 35 U.S.C. § 119(e), to U.S. Application No. 63/291,731 filed on Dec. 20, 2021, titled “Rate of Penetration/Depth Monitor for a Millimeter-Wave Beam Made Hole,” which application is incorporated herein by reference in its entirety.
This invention was made with Government support under Grant No. DE-AR0001051 awarded by the Department of Energy. The Government has certain rights in the invention.
Filing Document | Filing Date | Country | Kind |
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PCT/US2022/078255 | 10/18/2022 | WO |
Number | Date | Country | |
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63291731 | Dec 2021 | US |