IP Library Granted Patent US 9,609,729
Granted Patent B2
US 9,609,729 · App. 13/866,908 · Granted Mar 28, 2017

X-ray cells and other components having gas cells with thermally-induced density gradients

Inventors: Eric J. Griffin (Rancho Palos Verdes, CA); Kalin Spariosu (Thousand Oaks, CA); David A. Vasquez (Gardena, CA)
Assignee: RAYTHEON COMPANY
H05G2/003H05G2/008
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,609,729
App. No.
13/866,908
Granted
Mar 28, 2017
Kind
B2
Abstract

A method includes creating a gas flow in a gas cell and cooling a portion of the gas flow to create a thermally-induced temperature gradient in the gas flow. The method also includes directing at least one laser beam through at least a portion of the gas flow with the thermally-induced temperature gradient. The gas flow can be directed axially along a length of the gas cell or transverse to the length of the gas cell, and the at least one laser beam can be directed axially along the length of the gas cell through at least the portion of the gas flow. The gas flow may represent a first gas flow, and the method may further include creating a second gas flow in the gas cell and cooling a portion of the second gas flow to create a thermally-induced temperature gradient in the second gas flow.

Claims (53)

1. A method comprising:

creating a gas flow in a gas cell;

cooling a portion of the gas flow using a cryocooler thermally coupled to the gas cell to create a thermally-induced temperature gradient in the gas flow axially along a length of the gas cell, wherein cooling the portion of the gas flow comprises directly cooling the portion of the gas flow in the gas cell using a cold tip of the cryocooler; and

directing at least one laser beam axially along the length of the gas cell through at least a portion of the gas flow with the thermally-induced temperature gradient.

2. The method of claim 1 , wherein creating the gas flow comprises directing the gas flow axially along the length of the gas cell.

3. The method of claim 1 , wherein:

the gas flow comprises a first gas flow; and

the method further comprises:

creating a second gas flow in the gas cell; and

cooling a portion of the second gas flow to create a thermally-induced temperature gradient in the second gas flow.

4. The method of claim 3 , wherein the first gas flow and the second gas flow are directed axially along the length of the gas cell.

5. The method of claim 1 , wherein the gas cell has a gas pressure of approximately 6894.76 Pascals or less or one pound per square inch or less.

6. A method comprising:

creating a gas flow in a gas cell;

cooling a portion of the gas flow using a heat exchanger to create a thermally-induced temperature gradient in the gas flow axially along a length of the gas cell, wherein a central portion of the heat exchanger is thermally coupled to a cryocooler; and

directing at least one laser beam axially along the length of the gas cell through at least a portion of the gas flow with the thermally-induced temperature gradient.

7. The method of claim 6 , wherein creating the gas flow comprises directing the gas flow transversely to the length of the gas cell.

8. The method of claim 6 , wherein:

the gas flow comprises a first gas flow; and

the method further comprises:

creating a second gas flow in the gas cell; and

cooling a portion of the second gas flow to create a thermally-induced temperature gradient in the second gas flow.

9. The method of claim 6 , wherein the gas cell has a gas pressure of approximately 6894.76 Pascals or less or one pound per square inch or less.

10. An apparatus comprising:

a gas cell configured to receive a gas flow; and

a cryocooler configured to cool a portion of the gas flow and create a thermally-induced temperature gradient in the gas flow axially along a length of the gas cell, wherein the cryocooler comprises a cold tip thermally coupled to the gas cell proximate to an end of the gas cell;

wherein the gas cell is configured to receive at least one laser beam axially along the length of the gas cell that passes through at least a portion of the gas flow with the thermally-induced temperature gradient.

11. The apparatus of claim 10 , wherein the gas cell is configured to receive the gas flow axially along the length of the gas cell.

12. The apparatus of claim 10 , wherein:

the gas flow comprises a first gas flow;

the gas cell is further configured to receive a second gas flow; and

the cryocooler is further configured to cool a portion of the second gas flow and create a thermally-induced temperature gradient in the second gas flow.

13. The apparatus of claim 12 , wherein the first gas flow and the second gas flow are directed axially along the length of the gas cell.

14. The apparatus of claim 10 , wherein the gas cell has a gas pressure of one pound per square inch or less.

15. A system comprising:

the apparatus of claim 10 ; and

at least one laser configured to generate the at least one laser beam;

wherein the gas cell and the cryocooler form at least part of an X-ray cell configured to receive the at least one laser beam and to generate X-rays.

16. An apparatus comprising:

a gas cell configured to receive a gas flow;

a cryocooler; and

a heat exchanger configured to cool a portion of the gas flow and create a thermally-induced temperature gradient in the gas flow axially along a length of the gas cell, a central portion of the heat exchanger thermally coupled to the cryocooler;

wherein the gas cell is further configured to receive at least one laser beam axially along the length of the gas cell that passes through at least a portion of the gas flow with the thermally-induced temperature gradient.

17. The apparatus of claim 16 , wherein the gas cell is configured to receive the gas flow transversely to the length of the gas cell.

18. The apparatus of claim 16 , wherein:

the gas flow comprises a first gas flow;

the gas cell is further configured to receive a second gas flow; and

the cryocooler is further configured to cool a portion of the second gas flow and create a thermally-induced temperature gradient in the second gas flow.

19. The apparatus of claim 16 , wherein the gas cell has a gas pressure of approximately 6894.76 Pascals or less or one pound per square inch or less.

20. A system comprising:

the apparatus of claim 16 ; and

at least one laser configured to generate the at least one laser beam;

wherein the gas cell and the cryocooler form at least part of an X-ray cell configured to receive the at least one laser beam and to generate X-rays.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 19, 2013
From: GRIFFIN, ERIC J.; SPARIOSU, KALIN; VASQUEZ, DAVID A.
To: RAYTHEON COMPANY
Reel/Frame 030255/0810 →
Continuity (1)
Related Publication 20140314210A1 · Oct 23, 2014