WO2014113100A2 - Irradiation shutter for target injection into a fusion chamber - Google Patents

Irradiation shutter for target injection into a fusion chamber Download PDF

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Publication number
WO2014113100A2
WO2014113100A2 PCT/US2013/064544 US2013064544W WO2014113100A2 WO 2014113100 A2 WO2014113100 A2 WO 2014113100A2 US 2013064544 W US2013064544 W US 2013064544W WO 2014113100 A2 WO2014113100 A2 WO 2014113100A2
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WO
WIPO (PCT)
Prior art keywords
shutter
opening
cylinder
targets
target
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US2013/064544
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French (fr)
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WO2014113100A3 (en
Inventor
Paul Rosso
Robin Miles
Mary L. Spaeth
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Lawrence Livermore National Security LLC
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Lawrence Livermore National Security LLC
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Publication of WO2014113100A2 publication Critical patent/WO2014113100A2/en
Publication of WO2014113100A3 publication Critical patent/WO2014113100A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21BFUSION REACTORS
    • G21B1/00Thermonuclear fusion reactors
    • G21B1/11Details
    • G21B1/15Particle injectors for producing thermonuclear fusion reactions, e.g. pellet injectors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/10Nuclear fusion reactors

Definitions

  • the Laser Inertial Fusion Energy concept can operate as either a pure fusion or hybrid fusion-fission system.
  • the LIFE fusion chamber must, absorb the fusion energy, produce fusion fuel to replace that, burned in previous targets, and enable both target and laser beam transport to the ignition point.
  • One challenge with regard to the chamber is assuring that the targets injected into the chamber for each subsequent reaction, as well as the injection mechanism itself are protected from the environment of the fusion reactions.
  • the shutter includes a rotating cylindrical member having a curved slo there through, for example, adjacent one of the planar surfaces at the end of the cylinder.
  • targets are injected into the slot perpendicular to the axis of rotation.
  • rotation of the cylinder is coordinated with the velocity of an injected target to enable the target to pass into the slot, travel through the slot, without interference, and then emerge from the opposite end of the slot.
  • the rotation of the cylinder and the curved slot assure that there is never a line of sight path between one end of the curved slot facing the fusion chamber and the other end of the curved slot facing the injection mechanism where the next target awaits injection.
  • Figure 2 illustrates the architecture of a first embodiment having a helical path through which the targets pass
  • targets 50 are injected through the upper opening 22 in the shutter 10.
  • the shutter rotates at a rate such that the vertical velocity of the target keeps the target always within the helical passage.
  • the target ultimately emerges from the lower opening 24 of the helical passage and then travels toward the center of the fusion chamber, where laser beams ablate the DT capsule and create a fusion reaction.

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Physical Vapour Deposition (AREA)
  • Particle Accelerators (AREA)

Abstract

A shutter for an injection mechanism that injects targets into a fusion chamber includes a rotatable cylinder rotating about its axis. The cylinder includes a top opening for allowing targets to enter the shutter and a bottom opening for allowing targets to leave the shutter. A curved passage extends between the top opening and the bottom opening. Rotational velocity of the cylinder is coordinated with the velocity of an injected target to enable the injected target to pass through the curved passage without interference, and to emerge from the bottom opening to travel into the fusion chamber. The curvature of the passage is coordinated with the rotational rate of the cylinder allows the target to pass through the shutter without interference, yet protects targets waiting to be injected into the fusion chamber from being exposed to conditions in the fusion chamber.

Description

Irradiation Shutter for Target Injection Into a Fusion Chamber
STATEMENT AS TO RIGHTS TO INVENTIONS MADE UNDER FEDERALLY SPONSORED RESEARCH AND DEVELOPMENT
{0001] The United States Government has rights in this invention pursuant to Contract No. DE-AC52-07NA27344 between the United States Department of Energy and Lawrence Livermore N ational Security, L LC for the operation of Lawrence Livermore National Laboratory.
REFERENCE TO RELATED APPLICATION
[0002] This application claims priority from earlier filed U.S. Provisional Patent
Application serial number 61/719,224, filed October 26, 2012, and entitled: "'Constant Rotation irradiation Shutter for Target Injection Into a Fusion Chamber/'' Tins provisional patent application is incorporated by reference herein.
BACKGROUND OF THE INVENTION
[0003] The National Ignition Facility (NIF), the world's largest and most energetic laser system, is operational at Lawrence Livermore National Laboratory (LLNL) in
Livermore, California. One goal of operation, of the NIF is to demonstrate fusion ignition for the first time in the laboratory. Initial experiments are calculated to produce yields of the order of 20 MJ from an ignited, self-propagating fusion burn wave. The capability of the facility is such that yields of up to 150-200 MJ could ultimately be obtained. The NIF is designed as a research instrument, one in which single ''shots" on deuterium-tritium containing targets are performed for research. A description of the NIF can be found in Moses et al, Fusion Science and Technology, volume 60, pp 1 1-16 (201 1 ) and references therein.
[0004] There is a rapidly growing need worldwide for power, and especially for clean power. At LLNL a project known as Laser Inertial-confinement Fusion Energy, (often reierred to herein as "LIFE") is working toward introduction of fusion based electric power plants into the U.S. economy before 2030, and in a pre-commercial plant format before that. LIFE technology offers a pathway for the expansi on of carbon-free power around the world. It will provide clean carbon-free energy in a safe and sustainable manner, without risk of nuc ί ear pro 1 iierasi on .
[0005] One challenge with respect to LIFE, as well as any technology for generating electrical power to be distributed to large numbers of consumers, is reliability. Consumers expect to have extraordinarily high reliability in their electric power supply. The result is that utilities that, provide that electrical power maintai their facilities to assure the required high reliability. Thus, among the challenges with respect to fusion power, is to provide mechanisms by winch a reliable long-lived fusion chamber can be provided in which the fusion reactions occur, and with regard to which associated equipment has an appropriately long lifetime.
[0006] In the technology described herein, a fusion power plant is provided wit a fusion chamber into winch targets (hohlraums containing capsules with deuterium and tritium fuel) are introduced multiple times per second. As the individual fuel targets reach the center of the chamber, banks of lasers fire on the targets, heating and compressing the fuel within the capsule to create a fusion reaction.
[0007] The Laser Inertial Fusion Energy concept can operate as either a pure fusion or hybrid fusion-fission system. The LIFE fusion chamber must, absorb the fusion energy, produce fusion fuel to replace that, burned in previous targets, and enable both target and laser beam transport to the ignition point. One challenge with regard to the chamber is assuring that the targets injected into the chamber for each subsequent reaction, as well as the injection mechanism itself are protected from the environment of the fusion reactions.
[0008] In the environment, of the LITE engine fusion chamber, the target capsule and hohlraum cycle in temperature from near absolute zero to thousands of degrees Kelvin and are completely ionized with each laser pulse. Each shot is introduced with a frozen film of deuterium and tritiu (DT) inside the capsule. Thai frozen material must be protected from the heat and pressure of the fusion chamber until it is ready to be injected into the chamber. Because the targets are injected into the chamber at a rate of about nine targets per second, many targets are present in the injection system itself, and this system also must be protected from the temperatures and pressures inside the fusion chamber.
[0009] The overall fusion power plant architecture is described in "Inertial
Confinement Fusion Power Plant which Decouples Life-limited Components from Plant Availability," PCT application US 1 1/59820, filed November 8, 201 1. The fusion chamber is described in more detail in "Inertia! Confinement Fusion Chamber," PCT application US 1 1/59814, also filed November 8, 2011. The contents of these commonly assigned patent applications are incorporated by reference herein.
SUMMARY OF THE INVENTION
[0 10] In one embodiment, a shutter for an injection mechanism that injects targets into a fusion chamber includes a rotating cylinder having openings on the top and bottom of the cylinder. The top and bottom openings are connected to each other by a helical passage extending through the cylinder. Targets are injected parallel to the axis of rotation of the cylinder into the opening on the top of the cylinder. Rotation of the cylinder is coordinated with the velocity of an injected target to enable the target to pass through top opening, tra vel through the helical passage without interference, and then emerge from the opening on the bottom of the cylinder. After exiting the rotating cylinder, the target travels into the fusion chamber where the lasers compress and heat the fusion fuel within the capsule. The rotation of the cylinder and the helical passage assure that there is never a line of sigh path between the fusion chamber and the top of the cylinder where the next target awaits injection.
[00 i 1 ] In another embodiment the shutter includes a rotating cylindrical member having a curved slo there through, for example, adjacent one of the planar surfaces at the end of the cylinder. As the cylinder rotates around its axis, targets are injected into the slot perpendicular to the axis of rotation. In this embodiment, as in the first embodiment, rotation of the cylinder is coordinated with the velocity of an injected target to enable the target to pass into the slot, travel through the slot, without interference, and then emerge from the opposite end of the slot. The rotation of the cylinder and the curved slot assure that there is never a line of sight path between one end of the curved slot facing the fusion chamber and the other end of the curved slot facing the injection mechanism where the next target awaits injection.
BRIEF DESCRIPTION OF THE DRAWINGS
[0012] Figure 1 illustrates the overall target injection system for injecting targets into a fusion chamber;
[0013] Figure 2 illustrates the architecture of a first embodiment having a helical path through which the targets pass;
[00141 Figure 3 illustrates the architecture of a second embodiment having a slot through which the targets pass; [00151 Figure 4 is a diagram illustrating a correlation between shutter thickness and target heating.
DESCRIPTION OF THE INVENTION
[0016] As presently contemplated, a megawatt size LIFE power plant will require on the order of nine fusion targets per second. As these targets reach the center of the fusion chamber, lasers heat and compress the fusion fuel to cause the fusion reaction. Heat from the reaction can be then used to generate electrical power. Thus, inertia! confinement fusion target designers must consider many engineering requirements in addition to the physics requirements for a successful target implosion. Among these considerations is protection of the targets awaiting injection to the center of the chamber. For the fuel to implode and create a fusion reaction, the fuel capsule must arrive at the chamber center in substantially its original condition where it can be irradiated evenly with energy to ablate the capsule surface to compress and heat the DT fuel. An embodiment of an injection system for injecting the fusion targets is described in our commonly assigned PCT Patent Application "Fusion Target Injection and Tracking,''' filed November 8, 201 1 , as serial number PCT/US201 1/059791. The contents of that application are incorporated herein by reference.
[0017] In such a system, the multiple fusion reactions per second in the chamber create intense heat, pressure, and radiation that can damage not only the targets immediately outside the chamber in the injection mechanism waiting to be injected, but also the injection system itsel Herein we describe embodiments of a shutter to protect the targets and the target injection system from damage from the fusion reactions. The shutter described herein blocks heat, pressure, and radiation from the fusion reaction, preventing it from reaching targets outside the chamber, as well as preventing it from reaching the injection system.
[00181 Figure 1 is a perspective diagram of one implementation of the in jection system by which targets are injected into the fusion chamber. As illustrated there, concrete shielding protects the injection chamber from influences of the fusion chamber. A fuel target loading chamber enables the injection mechanism to be loaded with fusion targets (hohlraums with DT capsules) that have been prepared for injection into the fusion chamber. The targets are placed in cassettes which rotate into position via a fuel injector carousel. Once the appropriate portion of the carousel is in position, targets stored in that portion of the carousel are sequentially injected into the fusion chamber using the mechanism described in our above copending patent application. The shutter, which is described in more detail below, is shown near the bottom of Figure 1.
[0019] Figure 2 illustrates the archi lecture of our shutter in a first preferred embodiment. As illustrated there, a cylindrical shutter 10 rotating 15 about the axis 14 of the cylinder includes a helical passage 12. through the cylinder 10. The shutter 10 separates a fusion fuel target 50 that is in flight to the fusion chamber center to become the next target to be injected into the fusion chamber (not shown) where a fusion reaction 40 will occur. The dimensions of the shutter are such that its thickness C (measured along the vertical axis) is sufficient to shield fusion targets in the injection system awaiting injection, as well as the injection system itself, from the fusion reaction creating high-energy neutrons and alpha particles. The thickness C is the sum of thicknesses A and B representing the thickness of the shielding material less the "thickness" of the helical opening as measured along the vertical axis. Thus, the shutter is of a sufficient thickness such that at any position in its rotation the total solid material thickness is sufficient to shield the next fusion fuel target and the injection system from the fusion reaction.
[0020] In operation, targets 50 are injected through the upper opening 22 in the shutter 10. As the target moves downward toward the fusion chamber, the shutter rotates at a rate such that the vertical velocity of the target keeps the target always within the helical passage. The target ultimately emerges from the lower opening 24 of the helical passage and then travels toward the center of the fusion chamber, where laser beams ablate the DT capsule and create a fusion reaction.
[0021] In a typical implementation the shutter cylinder 10 is supported along its axis of rotation between plates 20 and 30 and is coupled to a motor (not shown) to cause it to spin at the desired rate of rotation. As mentioned above, when target 50 is first injected, it enters through an opening in the supporting structure 20. As the target 50 travels downward, its vertical velocity and the rotation of the shutter cylinder 0 are coordinated so that the vertical velocity of the target corresponds to an open portion of the helical slot 12. For example, if the rotating cylinder is 1000 mm thick and opening 22 in the top of the shutter is aligned directly over opening 24 in the bottom of the cylinder 10, and the two openings are connected by a slot of constant slope, then if the target velocity is such that it traverses the 1000 mm in the time it takes for the cylinder to make one rotation, the target will pass through the slot without interference from the interior surface of the slot. Yet while the target traverses the slot, the shutter cylinder 10 will never present a straight-line opening between its lower surface and its upper surface such that heat or radiation can pass from the fusion chamber to the targets awaiting injection above the shutter. [00221 Plates 20 and 30 may also perform the function of sealing the shutter top and bottom openings, 22 and 24, during shutter rotation while the openings are in rotational positions not concurrent with the target trajectory. The addition of passageway opening sealing prevents the transfer of environmental gases and debris through the shutter mechanism. Additionally, environmental control systems can interface with the shutter passageway during these sealed rotational position states for debris clearing and/or environmental gas exchange. Other means of sealing or obstructing the passageway exist, including intermediate plates or other structures within the shutter mechanism system to be timed with, shutter rotation.
[0023] Figure 3 is a diagram illustrating another embodiment of the invention.
Shown there is a cylindrical shutter 60 that rotates by means of a shaft 64. The cylinder 60 includes openings 70 and 72 at opposite ends of a passage 62. In contrast to the first embodiment, in this embodi ment the axis of rotation 75 of the cylinder 60 is perpendicular to the direction of travel of die fusion target 50. As shown by Figure 3a, the injection mechanism injects the target 50 into the opening 70 at the then top of the passage 62. Next as shown by Figures 3b and 3c, the curvature of the passage 62, coupled with the rotational velocity of the cylinder 60 enables the target 50 to pass through the remaining portion of passage 62, ultimately exiting from the far end 72 of passage 62. The curvature of the passage 62, rotational velocity 75 of the cylinder 60 and downward velocity of the target enable the target 50 to pass through the shutter without interference, and enter the fusion chamber. Figure 3d illustrates the next target 50 now ready for injection. In each of the two embodiments described, rotation of the shaft prevents the fusion chamber environment from ever having a direct iine-of-sight impact on targets stored in the injection mechanism. As with respect to Figure 2, thickness C is sufficient such that at any position in its rotation the total solid material thickness is shields die next fusion fuel target, and the injection system from the fusion reaction. Note that Figure 3 illustrates the passage as a groove in one end of the cylinder; however, the groove can be implemented as a completely enclosed curved passage through a cylinder.
[0024] Figure 4 is a diagram illustrating the relationship between shutter thickness and target heating. This diagram was prepared using simulation data. The diagram demonstrates that as the shutter thickness increases, the target heating decreases (the expected result). For example, as the shutter thickness increases from being absent (the zero thickness point) to a thickness of 66 cm, neutron heating of the next target waiting in the system for injection drops from approximately 1 ""' watts to 10"' watts. Increasing the shuttered thickness beyond 66 cm pro vides essentially no further reduction in target heating caused by ei her neutrons or photons. The data shown in Figure 4 includes factors other than shutter thickness, e.g. the surrounding structure, as well as photon production from neutron reaction in other materials.
{0025] The examples and embodiments described herein are for illustrative purposes only. Various modifications or changes in light thereof will be apparent to persons skilled in the art. These are to be included within the spirit and purview of this application, and the scope of the appended claims, which follow.

Claims

We claim:
1. A shutter for an injection mechanism that injects targets with a first velocity into a fusion chamber comprising:
a rotatable member rotating about an axis of rotation and having a top opening for allowing targets to enter the shutter, and having a bottom opening for allowing targets to leave the shutter, a curved passage extending between the top opemng and the bottom opening; and
wherein rotation velocity of the rotatable member is coordinated with the first velocity of an injected target to enable the injected target to pass through the curved passage without interference and to emerge from the bottom opening to travel into the fusion chamber.
2. A shutter as in claim 1 wherein the rotatable member comprises a cylinder and the axis of rotation is the axis of the cy linder.
3. A shutter as in claim 2 wherein:
the top opening is in a first end of the cylinder;
die bottom opemng is in an opposite end of the cylinder: and
the curved passage comprises a helical passage extending between the top opening and the bottom opening.
4. A shutter as in claim 3 wherein the injected target enters the helical passage through the top opening, passes through the helical passage, and emerges from the helical passage at the bottom opening to travel into the fusion chamber.
5. A shutter as in claim 4 wherein the top opemng is disposed directly opposite the bottom opening.
6. A shutter as in claim 5 wherein the first velocity is x, the rotatable member has a thickness y, and the rotatable member rotates at a rate z, where z is one rotation of the rotatable member every y/x.
7. A shutter as in claim i wherein there is never a line of sight opening between the top opening and the bottom opening.
8. A shutter as in claim 2 wherein:
each of the top opening and the bottom openin g are disposed on an exterior curved surface of the cylinder; and
the curved passage comprises a passage extending between the top opening and the bottom opening.
9. A shutter as in claim 8 wherem the curved passage is disposed adjacent an end of the cylinder.
10. A shutter as in claim 9 wherein there is never a line of sight opening between the top opening and the bottom opening.
1 1. A shutter as in claim 8 wherem the curved passage has a shape of an arc with respect to a plane perpendicular to the axis of rotation of the rotatable member.
12. A. method of protecting targets to be injected into a fusion chamber and injection systems from conditions in the fusion chamber comprising:
providing a rotatable shutter between the fusion chamber and the injection system, the rotatable shutter having a top opening, a bottom opening, and a curved passage extending between the top opening and the bottom opening; and
rotating the rotatable shutter as targets are injected so the targets pass through the shutter without interference, but the injection system is not exposed to conditions in the fusion chamber,
13. A method as in claim 12 wherein the rotatable shutter is a cylinder and coupled to a shaft that rotates the cylinder along a central axis.
14. A method as in claim 13 wherein the rotatable shutter rotates at a rate that allo ws a target to pass through the first opening and emerge from the second opening within a fraction of one revolution of the shutter.
15. A method as in claim 14 wherein the top opening is in one end of the cylinder, the bottom opening is in an opposite end of the cylinder, and the curved passage is a helical passage connecting the top opening to the bottom opening.
16. A method as in claim 14 wherein the top opening and the bottom opening are disposed on a curved surface of the cylinder.
17. A method as in claim 16 wherem the curved passage is arc shaped.
18. A method as in claim 17 wherein the curved passage is a groove extending into an end of the cylinder.
19. A method as in claim 12 wherein the top opening and the bottom opening are obstructed by stationary adjacent surfaces during rotational positions not concurrent with a time that a target is being injected.
20. A method as in claim 12 wherein at least some portion of the curved passage is sealed throughout full rotation of the shutter.
PCT/US2013/064544 2012-10-26 2013-10-11 Irradiation shutter for target injection into a fusion chamber Ceased WO2014113100A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261719224P 2012-10-26 2012-10-26
US61/719,224 2012-10-26

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WO2014113100A2 true WO2014113100A2 (en) 2014-07-24
WO2014113100A3 WO2014113100A3 (en) 2014-10-02

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Cited By (8)

* Cited by examiner, † Cited by third party
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WO2020081353A1 (en) * 2018-10-19 2020-04-23 Incom, Inc. Pellet-start process for making transverse anderson localization optical element
US11784454B1 (en) 2022-12-22 2023-10-10 Blue Laser Fusion, Inc. High intensity pulse laser generation system and method
US12160082B1 (en) 2023-01-04 2024-12-03 Blue Laser Fusion, Inc. Airplane configured with a high intensity pulse laser generation system and method
US12387853B1 (en) 2023-01-30 2025-08-12 Blue Laser Fusion, Inc. Synchronized light source for laser fusion system and method for energy generation
US12416822B1 (en) 2024-08-09 2025-09-16 Blue Laser Fusion, Inc. Laser beam extraction using distributed bragg reflector (DBR) mirror systems with a piezoelectric layer
US12476014B1 (en) 2024-08-01 2025-11-18 Blue Laser Fusion, Inc. Reduced neutron emission target for fusion energy generation
US12597528B1 (en) 2023-01-30 2026-04-07 Blue Laser Fusion, Inc. Single laser synchronized light source for fusion system and method for energy generation
US12597527B1 (en) 2023-03-01 2026-04-07 Blue Laser Fusion, Inc. Fuel pellet configured with internal reflection for an inertial fusion reaction

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Publication number Priority date Publication date Assignee Title
GB9525337D0 (en) * 1995-12-12 1996-02-14 Boc Group Plc Improvements in vacuum pumps
US7302043B2 (en) * 2004-07-27 2007-11-27 Gatan, Inc. Rotating shutter for laser-produced plasma debris mitigation
WO2012064668A1 (en) * 2010-11-08 2012-05-18 Lawrence Livermore National Security, Llc Indirect drive targets for fusion power

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020081353A1 (en) * 2018-10-19 2020-04-23 Incom, Inc. Pellet-start process for making transverse anderson localization optical element
US10884142B2 (en) 2018-10-19 2021-01-05 Incom, Inc. Pellet-start process for making transverse anderson localization optical element
US11784454B1 (en) 2022-12-22 2023-10-10 Blue Laser Fusion, Inc. High intensity pulse laser generation system and method
US12119609B2 (en) 2022-12-22 2024-10-15 Blue Laser Fusion, Inc. High intensity pulse laser generation system and method
US12160082B1 (en) 2023-01-04 2024-12-03 Blue Laser Fusion, Inc. Airplane configured with a high intensity pulse laser generation system and method
US12368279B2 (en) 2023-01-04 2025-07-22 Blue Laser Fusion, Inc. Airplane configured with a high intensity pulse laser generation system and method
US12387853B1 (en) 2023-01-30 2025-08-12 Blue Laser Fusion, Inc. Synchronized light source for laser fusion system and method for energy generation
US12597528B1 (en) 2023-01-30 2026-04-07 Blue Laser Fusion, Inc. Single laser synchronized light source for fusion system and method for energy generation
US12597527B1 (en) 2023-03-01 2026-04-07 Blue Laser Fusion, Inc. Fuel pellet configured with internal reflection for an inertial fusion reaction
US12476014B1 (en) 2024-08-01 2025-11-18 Blue Laser Fusion, Inc. Reduced neutron emission target for fusion energy generation
US12416822B1 (en) 2024-08-09 2025-09-16 Blue Laser Fusion, Inc. Laser beam extraction using distributed bragg reflector (DBR) mirror systems with a piezoelectric layer
US12422600B1 (en) 2024-08-09 2025-09-23 Blue Laser Fusion, Inc. Laser beam extraction using distributed bragg reflector (DBR) mirror systems with a piezoelectric layer

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