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US 11,095,088 B1Granted
Multi-pass coaxial molecular gas laser
AssigneeZoyka LLC
InventorAlexander V. Krasnov
Life of this patent
Estimating the term…
Abstract
A multi-pass coaxial molecular gas laser is described in both symmetrical and asymmetrical configuration. An anode vessel receives lasing gas and the gas flows through one or more plasma channels to a cathode vessel which receives the gas and redirects it in the closed system. A second anode vessel may alternatively be provided to double length of the plasma channel and increase surface area exposure of the optical beam to the energized gas. Non-laminar gas flow may be created using spiral nozzles at the entrance of the optical resonator.
Claims16
A multi-pass coaxial gas laser, comprising:
- a first anode vessel, a second anode vessel and a cathode vessel, the cathode vessel positioned between the first anode vessel and the second anode vessel;
- a first gas feed line extending from a turbo pump to the first anode vessel;
- a second gas feed line extending from the turbo pump to the second anode vessel;
- a return gas feed line connecting the cathode vessel to the turbo pump;
- a first open plasma channels extending from the first anode vessel to the cathode vessel, the first open plasma channel having a spiral gas flow nozzle adjacent to a first anode;
- a second open plasma channels extending from the second anode vessel to the cathode vessel, the second open plasma channel having a spiral gas flow nozzle adjacent to a second anode;
- each of the anodes having a DC power supply;
- wherein the first open plasma channel extending from the first anode vessel to the cathode vessel has the respective co-linear second open plasma channel extending from the cathode vessel to the second anode vessel forming a plasma channel pair;
- wherein the cathode vessel positions a cathode between the plasma channel pair;
- the return gas feed line connecting the cathode vessel to the turbo pump having a heat exchanger;
- an optical beam rear reflecting mirror reflecting an optical beam in the first anode vessel and into the open plasma channels extending from the first anode vessel to the cathode vessel to the second anode vessel;
- an optical beam exit output coupler allowing the optical beam to exit the first anode vessel;
- a plurality of angled mirrors positioned within the first anode vessel and at least one angled mirror in the second anode vessel to redirect the optical beam.
10 more elements
A multi-pass coaxial gas laser, comprising:
- a first anode vessel and a cathode vessel, the cathode vessel positioned downstream of the first anode vessel;
- a gas feed line extending from a turbo fan to the first anode vessel;
- a return gas feed line connecting the cathode vessel to the turbo fan;
- an open plasma channel extending from the first anode vessel to the cathode vessel, the open plasma channel forming an optical resonator and having a lasing gas flow entrance, the lasing gas flow entrance having a plurality of spiral gas flow nozzles adjacent to an anode and having a narrowed section downstream of the spiral gas flow nozzles;
- the anode in the plasma channel connected to a high voltage DC power supply;
- wherein the cathode vessel positions a cathode downstream of a lasing gas flow exit for the plasma channel;
- the return gas feed line connecting the cathode vessel to the turbo fan and having a heat exchanger;
- an optical beam rear reflecting mirror allowing an optical beam to reflect in the optical resonator;
- an optical beam exit output coupler allowing the optical beam to exit the first anode vessel;
- a plurality of angled mirrors positioned at a first end and a second end of the optical resonator for redirecting the optical beam through the optical resonator.
7 more elements
A multi-pass coaxial gas laser, comprising:
- a first and a second anode vessel with a cathode vessel, the cathode vessel positioned downstream of the first anode vessel and the second anode vessel and positioned therebetween;
- a first gas feed line extending from a turbo fan to the first anode vessel;
- a second gas feed line extending from the turbo fan to the second anode vessel;
- a return gas feed line connecting the cathode vessel to the turbo fan;
- an open plasma channel extending from the first anode vessel to the cathode vessel and to the second anode vessel, the open plasma channel forming an optical resonator and having a first and a second lasing gas flow entrance, each of the lasing gas flow entrance having:
- a plurality of spiral gas flow nozzles adjacent to an anode and having a narrowed section downstream of the spiral gas flow nozzles, the anode in the plasma channel connected to a high voltage DC power supply;
- wherein the cathode vessel positions a cathode downstream of a lasing gas flow exit;
- the return gas feed line connecting the cathode vessel to the turbo fan and having a heat exchanger;
- a small convex reflector in the first anode vessel;
- a singular spherical concave rear reflecting mirror in the second anode vessel opposing the small convex reflector allowing an optical beam to reflect in the optical resonator;
- a convex reflector in optical opposition to the spherical concave rear reflecting mirror
- an optical beam exit output coupler allowing the optical beam to exit the first anode vessel;
- a planar output coupler in optical alignment with the convex reflector to output a ring shaped laser beam.
10 more elements
Dependencies are inferred from the claim text.