Method and apparatus for performing active neutron interrogation of containters

• US 9,024,261 B2
• Filed: 12/14/2010
• Issued: 05/05/2015
• Est. Priority Date: 12/15/2009
• Status: Active Grant

• Current Assignee: Shine Technology Company Limited
• Original Assignee: Phoenix Nuclear Labs, LLC
• Inventors: Piefer, Gregory
• Primary Examiner(s): TANINGCO, MARCUS H
• Application Number:
  US13/515,487
• Publication Number:
  US 20120286164A1
• Time in Patent Office: 1,603 Days
• Field of Search: 250/358.1
• US Class Current: 250/358.1
• CPC Class Codes: G01V 5/281 detecting special nuclear material [SNM], e.g. Uranium-235, Uranium-233 or Plutonium-239
• CPC Class Codes: H05H 3/06 Generating neutron beams targets for producing nuclear reactions H05H6/00; neutron sources G21G4/02

Abstract

An apparatus for inspecting the contents of a cargo container includes a neutron source having an ion source configured to provide deuterium or tritium ions and an accelerator configured to accelerate the ions toward a target having at least one of deuterium or tritium. The apparatus further includes a radiation detector where the neutron source is configured to deliver a neutron flux into the container and the radiation detector is configured to detect radiation exiting the container subsequent to the delivery of the neutron flux into the container.

Claims

1. An apparatus for inspecting the contents of a cargo container, comprising:

a neutron source comprising;

an ion source configured to provide deuterium or tritium ions;

an accelerator operatively coupled to the ion source to define an accelerator/ion source region, the accelerator operating at a first gas pressure and configured to receive the deuterium or tritium ions and accelerate the deuterium or tritium ions;

a gaseous target system operatively coupled to the accelerator, the gaseous target system comprising a target chamber operating at a second gas pressure, higher than the first gas pressure, the target chamber holding a target gas comprising at least one of deuterium or tritium; and

a plurality of differential pumping stages, each stage configured to reduce a pressure in the neutron source by a factor of between 10 and 1000 to maintain a first pressure differential between an outside atmosphere and the ion source/accelerator region, a second pressure differential between the outside atmosphere and the gaseous target system, and a third pressure differential between the ion source/accelerator region and the gaseous target system; and

a radiation detector;

wherein the neutron source is configured to deliver a neutron flux into the container and the radiation detector is configured to detect radiation exiting the container subsequent to the delivery of the neutron flux into the container.

2. The apparatus of claim 1, wherein the radiation detector is a neutron sensitive film for imaging the interior of the container.

3. The apparatus of claim 1, wherein the detector is a cadmium wrapped neutron detector.

4. The apparatus of claim 1, wherein the radiation detector is shielded from thermal neutrons.

5. The apparatus of claim 1, wherein the radiation detector is a scintillation or solid state gamma detector.

6. The apparatus of claim 1, wherein the neutron source is configured to provide a steady state neutron flux.

7. The apparatus of claim 1, wherein the neutron source is configured to be pulsed such that the neutron flux is provided for a set period of time.

8. The apparatus of claim 1, wherein the radiation detector is an electronic detector comprising a plurality of neutron detectors configured provide data to a imaging computer for display on a screen or reconstruction into an image.

9. The apparatus of claim 1, wherein the plurality of differential pumping stages are configured to maintain the first gas pressure in the accelerator at less than 100 μ

torr.

10. The apparatus of claim 1, wherein the plurality of differential pumping stages are configured to maintain the second gas pressure in a range of about 1-10 Torr.

11. A method of identifying material in a cargo container, comprising:

generating a neutron flux with a neutron source apparatus comprising;

an ion source for producing an ion beams;

an accelerator operatively coupled to the ion source to define an accelerator/ion source region, the accelerator operating at a first gas pressure and configured to receive the ion beam and accelerate the ion beam to yield an accelerated ion beam;

a gaseous target system operatively coupled to the accelerator, the gaseous target system comprising a target chamber operating at a second gas pressure, higher than the first gas pressure, the target chamber containing a target gas which is reactive with the accelerated beam to emit the neutron flux, wherein the target gas comprises at least one of deuterium or tritium; and

a plurality of differential pumping stages, each stage configured to reduce a pressure in the neutron source by a factor of between 10 and 1000 to maintain a first pressure differential between an outside atmosphere and the ion source/accelerator region, a second pressure differential between the outside atmosphere and the gaseous target system, and a third pressure differential between the ion source/accelerator region and the gaseous target system;

irradiating the cargo container with the neutron flux, wherein a radiation signature is produced by the material after the neutron flux contacts the material;

detecting the radiation signature; and

evaluating the radiation signature to identify the material.

12. The method of claim 11, wherein the evaluating step comprises determining the ratio of different elements identified in the container.

13. The method of claim 11, wherein the evaluating step comprises detecting a fission event in order to identify special nuclear material in the container.

14. The method of claim 11, wherein the detecting step is performed while the neutron flux is not being provided.

15. The method of claim 11, wherein the detecting step comprises detecting delayed neutrons for the purpose of identifying special nuclear material.

16. The method of claim 11, wherein a evaluating step comprises using a differential die away evaluation for the purpose of identifying special nuclear material.

17. The method of claim 16, wherein the detecting step uses a neutron detector that is shielded from thermal neutrons.

18. The method of claim 17, wherein the irradiating step comprises pulsing the neutron source, and the detecting step is commenced after the irradiating step.

19. The method of claim 11, wherein the detecting step uses a gamma detector and the evaluating step comprises evaluating the gamma signature to identify the material.

20. The method of claim 11, wherein the generating step further comprises maintaining the first gas pressure in the accelerator at less than 100 μ

torr via the plurality of differential pumping stages.

21. The method of claim 11, wherein the generating step further comprises maintaining the second gas pressure in a range of about 1-10 Torr via the plurality of differential pumping stages.

22. An apparatus for inspecting the contents of a cargo container, comprising:

a neutron source comprising;

an ion source configured to provide deuterium or tritium ions;

an accelerator operatively coupled to the ion source to define an accelerator/ion source region, the accelerator operating at a first gas pressure and configured to receive the deuterium or tritium ions and accelerate the deuterium or tritium ions;

a gaseous target system operatively coupled to the accelerator, the gaseous target system comprising a target chamber operating at a second gas pressure, higher than the first gas pressure, the target chamber holding a target gas comprising at least one of deuterium or tritium; and

a plurality of differential pumping stages, each stage configured to reduce a pressure in the neutron source by a factor of between 10 and 1000 to maintain a first pressure differential between an outside atmosphere and the ion source/accelerator region, a second pressure differential between the outside atmosphere and the gaseous target system, and a third pressure differential between the ion source/accelerator region and the gaseous target system; and

a radiation detector;

wherein the neutron source is configured to deliver a neutron flux into the container and the radiation detector is configured to detect radiation exiting the container subsequent to the delivery of the neutron flux into the container; and

wherein the neutron source and radiation detector are coupled to a crane configured to unload cargo containers from a ship.

23. The apparatus of claim 22, wherein the plurality of differential pumping stages are configured to maintain the second gas pressure in a range of about 1-10 Torr.

24. The apparatus of claim 23, wherein the plurality of differential pumping stages are configured to maintain the first gas pressure in the accelerator at less than 100 μ

torr.