초록 ▼

A chemical oxygen-iodine laser (COIL) comprises an oxygen generator and a nozzle for accelerating generated oxygen to a high or supersonic velocity. A laser cavity is coupled to the nozzle, wherein the accelerated fluid, with injected iodine, is employed as a laser gain medium. A Brayton cycle outle

A chemical oxygen-iodine laser (COIL) comprises an oxygen generator and a nozzle for accelerating generated oxygen to a high or supersonic velocity. A laser cavity is coupled to the nozzle, wherein the accelerated fluid, with injected iodine, is employed as a laser gain medium. A Brayton cycle outlet pump employs the accelerated oxygen and iodine as a component of a process fluid in a Brayton cycle to raise the static pressure of the accelerated fluid to ambient conditions. The Brayton cycle pump comprises a compressor having an inlet and an outlet, the inlet being coupled to the laser cavity to receive and compress accelerated oxygen. A combustor is coupled to the outlet of the compressor to receive compressed oxygen and ignite and combust it A turbine is coupled to the outlet of the combustor to expand the ignited and combusted gas, wherein the turbine powers the compressor. Multiple reheat stages may be used and regeneration and intercooling may also be used. The use of reheat, regeneration, and intercooling depends on the application.

대표청구항 ▼

I claim: 1. A gas laser comprising: a supply of fluid; a nozzle for accelerating supplied fluid to high velocity; a laser cavity coupled to the nozzle, wherein the accelerated fluid is employed as a laser gain medium; and a Brayton cycle outlet pump having an inlet coupled to the laser cavity, the

I claim: 1. A gas laser comprising: a supply of fluid; a nozzle for accelerating supplied fluid to high velocity; a laser cavity coupled to the nozzle, wherein the accelerated fluid is employed as a laser gain medium; and a Brayton cycle outlet pump having an inlet coupled to the laser cavity, the Brayton cycle outlet pump employing the fluid from the laser cavity as a component of a process fluid in a Brayton cycle to raise the static pressure of the accelerated fluid. 2. The laser according to claim 1, wherein the Brayton cycle outlet pump comprises: a compressor having an inlet and an outlet, the inlet coupled to the laser cavity; a combustor having an inlet and an outlet, the combustor inlet coupled to the outlet of the compressor; and a turbine having an inlet and an outlet, the turbine inlet coupled to the outlet of the combustor, wherein the turbine powers the compressor. 3. The laser according to claim 1, wherein the Brayton cycle outlet pump comprises multiple stages. 4. The laser according to claim 1 further comprising a diffuser between the laser cavity and the Brayton cycle outlet pump. 5. The laser according to claim 1, wherein the Brayton cycle outlet pump includes at least one reheat stage. 6. The laser according to claim 2, wherein the compressor is a multi-stage compressor. 7. The laser according to claim 2, wherein the turbine is a multi-stage turbine. 8. The laser according to claim 1, wherein the Brayton cycle outlet pump includes a regeneration stage. 9. The laser according to claim 1, wherein the Brayton cycle outlet pump includes an intercooling stage. 10. The laser according to claim 2, wherein the turbine has a work output that exceeds the work required to operate the compressor, wherein there is net work output from the Brayton cycle pump. 11. A chemical oxygen-iodine laser (COIL) comprising: an oxygen generator; a nozzle for accelerating generated oxygen, to supersonic velocity; a laser cavity coupled to the nozzle, wherein the accelerated oxygen, with injected iodine, is employed as a laser gain medium; and a Brayton cycle outlet pump employing the accelerated oxygen and iodine as a process fluid in a Brayton cycle to raise the static pressure of the accelerated oxygen and iodine to ambient conditions, the Brayton cycle outlet pump including: a compressor having an inlet and an outlet, the inlet coupled to the laser cavity to receive and compress the process fluid; a combustor having an inlet and an outlet, the combustor inlet coupled to the outlet of the compressor to receive compressed process fluid, add a fuel, and ignite and combust the process fluid and fuel; and a turbine having an inlet and an outlet, the turbine inlet coupled to the outlet of the combustor to expand the ignited and combusted gas, wherein the turbine powers the compressor. 12. The laser according to claim 11, wherein the Brayton cycle outlet pump comprises multiple stages. 13. The laser according to claim 11, further comprising a diffuser between the laser cavity and the Brayton cycle outlet pump. 14. The laser according to claim 11, wherein the Brayton cycle outlet pump includes at least one reheat stage. 15. The laser according to claim 11, wherein the compressor is a multi-stage compressor. 16. The laser according to claim 11, wherein the turbine is a multi-stage turbine. 17. The laser according to 11, wherein the Brayton cycle outlet pump includes a regeneration stage. 18. The laser according to claim 11, wherein the turbine has a work output that exceeds the work required to operate the compressor, wherein there is net work output from the Brayton cycle pump. 19. The laser according to claim 11, wherein the Brayton cycle outlet pump includes an intercooling stage. 20. A chemical oxygen-iodine laser (COIL) comprising: an oxygen generator; a nozzle for accelerating generated oxygen to supersonic velocity; a laser cavity coupled to the nozzle, wherein the accelerated oxygen, with injected iodine, is employed as a laser gain medium; a diffuser coupled to the laser cavity to decelerate oxygen and iodine to below supersonic velocity; a compressor coupled to the diffuser to receive and compress the oxygen and iodine; a combustor coupled to the compressor to ignite and combust the compressed oxygen and iodine and an added fuel; and a turbine coupled to the combustor to expand the ignited and combusted oxygen and iodine, wherein the turbine powers the compressor. 21. The laser according to claim 20, wherein the compressor is a multi-stage compressor. 22. The laser according to claim 20, wherein the turbine is a multi-stage turbine. 23. The laser according to claim 20, wherein the turbine has a work output that exceeds the work required to operate the compressor.