Patent Application
20200027571
Inertial Confinement Fusion (“ICF”) is a process by which energy is produced by nuclear fusion reactions. The fuel pellet, generally called the target, is conventionally a spherical device which contains fuel for the fusion process. Various ways of driving and imploding the target have been utilized and considered (lasers, ion beams, etc.). These drives transfer energy to the target which then implodes and ignites the fuel. If the fuel is sufficiently heated and compressed, a self-sustaining fusion reaction occurs, wherein the fuel self-heats and produces energy from the fusion reaction.
If the target is to be useful for energy production, it must output more energy than the amount of energy needed to drive the implosion. The amount of energy needed to drive the target may be quite high, as very high temperatures and densities are required to initiate fusion reactions. Also, the amount of energy needed to drive the target must be physically and economically achievable.
The conventional approach to ICF target design is exemplified by the Department of Energy's program, NIF (National Ignition Facility). NIF target designs, as described in Lindl, “The Physics Basis for Ignition Using Indirect Drive Targets on the National Ignition Facility”, consists of a mostly plastic or beryllium ablator region which surrounds a cryogenic DT ice, and a central void which is filled with very low density DT gas. The target is then placed in a cylindrical hohlraum. The entire target assembly (hohlraum and target) are then placed in the target chamber, where a 192 beamline laser delivers up to 1.8 MJ of energy to the hohlraum. The hohlraum converts the energy to x-rays which then ablate the ablator region, and by the reactive force drives the DT shell inward. This ablation process may take a very long time in comparison to the hydrodynamic motion of the target material. Due to this long time-scale, NIF hohlraums must have very large laser entrance holes. As the temperature of the hohlraum rises, the hohlraum material will be ablated and thereby begin to close these holes. If the holes close or become too small, the laser light will not be able to enter the hohlraum. One effect of having these large holes is that radiation is then allowed to escape the hohlraum and that energy then becomes unusable by target. Another effect of a long laser pulse is that although the hohlraum walls are fairly reflective to radiation, a significant portion of the laser energy is lost to the heating of the hohlraum walls. This means NIF targets are unable to efficiently use the energy from the laser.
Since the time scale of the laser pulse length must be long for this ablation process, the target and/or hohlraum may move during the laser pulse. If this happens there may be increased non-uniformity of the energy deposition on the target's surface. This increased non-uniformity may lead to increased Raleigh-Taylor instability growth at the shell/fuel interface and ignition failure.
NIF targets have, up to now, never ignited. The areal density (pr) of the fuel and the temperature of the fuel has, to date, fallen short of the 0.3 g/cm2 and 10 keV they believe they require. It is not clear why the NIF targets have not achieved ignition, but it may be due to lower than expected shell velocities and greater than expected Raleigh-Taylor instability growth.
Unless otherwise indicated herein, the materials described in this section are not prior art to the claims in this application and are not admitted to be prior art by inclusion in this section.
ICF targets and their designs are discussed in which less energy is lost to heating the hohlraum, as well as less energy escaping the laser entrance holes by reducing the size of these holes. This necessarily reduces the laser pulse length in time and changes the requirements for how those targets are driven. These targets may then also benefit from improved stability and symmetry requirements.
In accordance with the present invention, a system and method for driving an ICF target with a thermal wave is described. The ICF target is located within a hohlraum which comprises one or more laser entrance apertures sized accordingly. A laser assembly irradiates a laser pulse through the laser entrance apertures to reradiate as x-ray radiation within the inner walls of the hohlraum to penetrate the ICF target as a thermal wave. A drive region is then evenly heated to a sufficient temperature to expand in an inward and outward direction wherein a shell region is launched into a fuel region to drive the ICF target.
A supersonic radiative thermal wave (thermal wave) is a direct heat transfer by radiation (x-ray or laser photons) and has the characteristic of propagating through the medium at a speed greater than the speed of sound. For incident radiation of temperature (T) 110, radiative thermal conductivity is a strong and rapidly increasing function of T (˜T45-55) resulting in a temperature profile 112 (
Areal Density=∫0rdr′ρ(r′) or ∫r104rdr′ρ(r′)
At lower intensities/shorter pulse lengths for qex, a subsonic ablative heating wave 114 (
As shown in
As shown in
Some amount of the laser energy entering hohlraum 300 will heat hohlraum wall 304. This energy never reaches the target and may be thought of as a loss. This loss is highly dependent on the time in which the laser is active. One advantage of this process is the pulse length requirement for the laser. Since the initial heating of ablator region (206,
Another loss of energy occurs as radiation leaves the hohlraum through holes 302. The larger the holes are, the more energy that is lost through them. The required size of holes 302 is dependent on the length of the laser pulse. Since the wall surrounding hole 302 will be ablated by the radiation field and shrink and possibly close, hole 302 must be large enough to remain open during the time when the laser is active.
Another advantage of this invention is that no significant hydrodynamic motion occurs within target assembly 400 during the time in which the laser is active. However, in conventional ICF targets, a long ablation process where the laser is active for tens of nanoseconds, the target may shift or move in relation to hohlraum 300 and thus create asymmetries in the energy deposited on the surface of the target. These asymmetries may then lead to an asymmetrical implosion, and if the asymmetries are great enough the target may not ignite.
In conventional targets which are driven by ablation, the ablation process is used to tailor the pressure profile on the outside of shell 204. In targets driven by a thermal wave penetrating drive region 206, it may be preferred to tailor the pressure profile on the outside shell 204 by structuring drive region 206 in different fashions. One can imagine many variations. Ablator region 206 could, instead of being a homogenous region, be layered with different materials or the same material at different densities. For instance, if the density of drive region 206 smoothly transitioned from the greatest density on the outside to the least dense on the inside, a longer pressure pulse on the outside of shell 204 would be created as the inner material would push earlier in time and the material further out would follow. The material in ablator region 206 could be chosen for its opacity, or lack thereof, to radiation of a certain spectrum or temperature.
In some embodiments fuel region 202 may have a higher ratio of deuterium to tritium, or conversely, a higher ratio of tritium to deuterium. Fuel region 202 could be filled with other types of fusion fuel, such as: pure deuterium fuel, lithium deuteride, lithium deuteride with lithium tritide, equimolar deuterium and tritium (DT) or DT with a reduced or increased fraction of tritium, or proton-Boron 11 (p11B).
Other materials could be substituted for tungsten in shell 204. For instance, copper could be used. The requirement for the material in shell 204 is that it must contain the radiation in fuel region 202 up until ignition. High-Z materials may be preferred to accomplish this as they will be more reflective to said radiation.
Embodiments of this invention discussed in this application were designed using numerical simulations and hand calculations. This design process necessarily involves making approximations and assumptions. The description of the operation and characteristics of the embodiments presented above is intended to be prophetic, and to aid the reader in understanding the various considerations involved in designing embodiments, and is not to be interpreted as an exact description of how embodiments will perform, an exact description of how various modifications will change the characteristics of an embodiment, nor as the results of actual real-world experiments.
Additionally, the set of embodiments discussed in this application is intended to be exemplary only, and not an exhaustive list of all possible variants of the invention. Certain features discussed as part of separate embodiments may be combined into a single embodiment. Additionally, embodiments may make use of various features known in the art but not specified explicitly in this application.
Embodiments can be scaled-up and scaled-down in size, and relative proportions of components within embodiments can be changed as well. The range of values of any parameter (e.g. size, thickness, density, mass, etc.) of any component of an embodiment of this invention, or of entire embodiments, spanned by the exemplary embodiments in this application should not be construed as a limit on the maximum or minimum value of that parameter for other embodiments, unless specifically described as such.
This application claims the benefit of U.S. Provisional Application No. 62/587,169 filed on Nov. 16, 2017, which is incorporated herein by reference.
| Number | Date | Country | |
|---|---|---|---|
| 62587169 | Nov 2017 | US |
