Method and apparatus for radiation detection

• US 6,236,050 B1
• Filed: 08/17/1998
• Issued: 05/22/2001
• Est. Priority Date: 02/02/1996
• Status: Expired due to Term

• Current Assignee: Nova R&D Incorporated (Kromek Group PLC)
• Original Assignee: Tümer, Tümay O.
• Inventors: Tümer, Tümay O.
• Primary Examiner(s): Hannaher, Constantine
• Assistant Examiner(s): Gabor, Otilia
• Application Number:
  US09/135,184
• Time in Patent Office: 1,009 Days
• Field of Search: 250/370.09, 250/363.03
• US Class Current: 250/370.09
• CPC Class Codes: A61B 6/037 Emission tomography
• CPC Class Codes: G01T 1/006 Total absorption calorimeters; Shower detectors
• CPC Class Codes: G01T 1/2928 using solid state detectors
• CPC Class Codes: G01T 1/2985 In depth localisation, e.g. using positron emitters; Tomographic imaging (longitudinal and transverse section imaging; apparatus for radiation diagnosis sequentially in different planes, steroscopic radiation diagnosis); using external radiation sources A61B6/02
• CPC Class Codes: H01L 27/14659 Direct radiation imagers structures
• CPC Class Codes: H01L 31/115 Devices sensitive to very short wavelength, e.g. X-rays, gamma-rays or corpuscular radiation

Abstract

A detection system is provided. In one embodiment a silicon Compton recoil electron detector uses the Compton double scatter technique with recoil electron tracking to detect medium energy gamma rays from 0.05 to 10 MeV. Two detector layers are required; a silicon microstrip hodoscope and a calorimeter. The incoming photon Compton scatters in the hodoscope. The calorimeter is placed at a location with respect to the hodoscope wherein the calorimeter is effectively shielded from incident emitted x-rays. The second scatter layer is the calorimeter where the scattered gamma ray is totally absorbed. The recoil electron in the hodoscope is tracked through several detector planes until it stops. The x and y position signals from the first two planes of the electron track determine the direction of the recoil electron while the energy loss from all planes determines the energy of the recoil electron. In another embodiment of the invention, the Compton double scatter technique with recoil electron tracking is used to detect x-rays from 300 to 5,000 keV. This embodiment is useful for nondestructive, real time imaging for use in medical imaging and the inspection of munitions items. In another embodiment, a high sensitivity, high spatial resolution and electronically collimated single photon emission computed tomography system which is sensitive from 81 keV to 511 keV gamma ray photons is provided. In another embodiment, a Compton scatter positron emission tomography system is provided.

Claims

1. An imaging system for imaging an object, comprising:

an x-ray source emitting x-rays;

a detection system comprised of a hodoscope, wherein said object is located between said x-ray source and said hodoscope, said hodoscope comprised of a plurality of position sensitive detector planes, wherein a portion of said x-rays passing through said object pass into said hodoscope and are scattered within said hodoscope;

a calorimeter placed at a location with respect to the hodoscope wherein the calorimeter is effectively shielded from incident emitted x-rays;

a multi-channel readout system coupled to said plurality of position sensitive detector planes;

a shielding member, said shielding member substantially preventing exposure of said multi-channel readout system to said emitted x-rays;

a processor coupled to said multi-channel readout system; and

a monitor coupled to said processor, said monitor displaying an image of said object.

2. The imaging system of claim 1, wherein said shielding member collimates said emitted x-rays.

3. The imaging system of claim 1, wherein said plurality of position sensitive detector planes is comprised of a plurality of silicon detection planes.

4. The imaging system of claim 3, wherein each of said plurality of silicon detection planes has an area between 4 square centimeters and 1,000 square centimeters.

5. The imaging system of claim 3, wherein each of said plurality of silicon detection planes has an area between 16 square centimeters and 144 square centimeters.

6. The imaging system of claim 3, wherein each of said plurality of silicon detection planes has a thickness between about 0.1 and about 10 millimeter.

7. The imaging system of claim 3, wherein each of said plurality of silicon detection planes has a thickness between about 0.5 and about 1 millimeter.

8. The imaging system of claim 3, wherein a portion of said emitted x-rays undergo at least one Compton scatter within said plurality of silicon detection planes to yield a track direction corresponding to each of said portion of emitted x-rays, wherein a total energy corresponding to each of said portion of said emitted x-rays is absorbed within said plurality of silicon detection planes, and wherein said track direction and said total energy corresponding to each of said portion of emitted x-rays is combined by said processor to generate said image.

9. The imaging system of claim 3, wherein a recoil electron is formed by a portion of said emitted x-rays undergoing Compton scatter within said plurality of silicon detection planes, said recoil electron passing through a portion of said plurality of silicon detection planes, wherein a position of said recoil electron is recorded for each of said portion of said plurality of silicon detection planes.

10. The imaging system of claim 3, wherein said plurality of silicon detection planes have a predetermined orientation with respect to said emitted x-rays, said predetermined orientation selected from the group consisting of parallel, perpendicular, or an angle.

11. The imaging system of claim 3, wherein said plurality of silicon detection planes is selected from the group consisting of silicon microstrip detectors, silicon strip detectors, silicon pad detectors, silicon pixel detectors, double-sided silicon microstrip detectors, and double-sided silicon strip detectors.

12. The imaging system of claim 3, wherein said multi-channel readout system is comprised of ASIC chips, wherein said plurality of silicon detection planes is comprised of silicon strip detectors, and wherein said strips are fanned in to match a chip bonding pitch corresponding to said ASIC chips.

13. The imaging system of claim 1, wherein said plurality of position sensitive detector planes is selected from the group consisting of CdTe microstrip detectors, CdTe strip detectors, CdTe pad detectors, CdTe pixel detectors, double-sided CdTe microstrip detectors, double-sided CdTe strip detectors, CdZnTe microstrip detectors, CdZnTe strip detectors, CdZnTe pad detectors, CdznTe pixel detectors, double-sided CdZnTe microstrip detectors, and double-sided CdZnTe strip detectors.

14. The imaging system of claim 1, wherein said emitted x-rays have an energy in the range of 50 to 600 keV.

15. The imaging system of claim 1, wherein said emitted x-rays have an energy in the range of 600 to 5000 keV.

16. The imaging system of claim 1, wherein said emitted x-rays are monoenergetic.

17. The imaging system of claim 1, wherein said emitted x-rays are from a radioactive source with multiple emission lines.

18. The imaging system of claim 1, wherein said x-ray source is a continuous energy x-ray source.

19. The imaging system of claim 18, wherein said image includes energy spectrum information.

20. The imaging system of claim 19, wherein different energy spectra of said energy spectrum information are represented in said image by different colors.

21. The imaging system of claim 20, wherein an intensity corresponding to each of said different energy spectra is represented by a color intensity corresponding to said different colors.

22. The imaging system of claim 1, wherein said calorimeter is shielded from said emitted x-rays not passing through said object.

23. The imaging system of claim 1, wherein said calorimeter is comprised of Csl(Tl) crystals.

24. The imaging system of claim 23, wherein said CsI(Tl) crystals are coupled to PIN photodiodes.

25. The imaging system of claim 1, wherein said calorimeter is selected from the group of calorimeter detector materials consisting of BPGe, BGO, LSO, GSO, CdWO₄, CsF, Nal(Tl), CsI(Na), CsI(Tl), CdTe, CdZnTe, HgI₂, GaAs, and PbI₂.

26. The imaging system of claim 1, further comprising a rotation stage coupled to said object, wherein said rotation stage rotates said object relative to said detection system, wherein said image is a three-dimensional tomographic image.

27. The imaging system of claim 1, wherein said image is a two-dimensional image.

28. The imaging system of claim 1, wherein said image is a three-dimensional image.

29. The imaging system of claim 1, wherein said calorimeter is coupled to said multi-channel readout system.

30. The imaging system of claim 1, wherein said scattered x-rays passing through said hodoscope form recoil electrons during passage through said plurality of position sensitive detector planes, wherein said hodoscope determines a track direction by a first scatter vertex and an energy associated with said recoil electrons, wherein said scattered x-rays are totally absorbed within said calorimeter, and wherein an energy of said absorbed x-rays is determined by said calorimeter.

31. The imaging system of claim 1, comprising a second shielding member proximate to an entrance aperture of said hodoscope.

32. A radiation detector for detecting gamma rays, comprising:

a detector aperture, said aperture limiting said detector to a predetermined field-of-view;

a detection system comprised of a hodoscope, said hodoscope comprised of a plurality of position sensitive detector planes, wherein a portion of said gamma rays pass through said aperture into said hodoscope and are scattered within said hodoscope;

a calorimeter placed at a location with respect to the hodoscope wherein the calorimeter is effectively shielded from incident x-rays;

a multi-channel readout system coupled to said detection system;

a processor coupled to said multi-channel readout system; and

an output device to said multi-channel readout system, said output device outputting information corresponding to said detected gamma rays.

33. The radiation detector of claim 32, wherein said plurality of position sensitive detector planes is comprised of a plurality of silicon detection planes.

34. The radiation detector of claim 33, wherein a portion of said gamma rays undergo at least one Compton scatter within said plurality of silicon detection planes to yield a track direction corresponding to each of said portion of gamma rays, wherein a total energy corresponding to each of said portion of said gamma rays is absorbed within said plurality of silicon detection planes, and wherein said track direction and said total energy corresponding to each of said portion of gamma rays is combined by said processor to generate said outputted information.

35. The radiation detector of claim 33, wherein a recoil electron is formed by a portion of said gamma rays undergoing Compton scatter within said plurality of silicon detection planes, said recoil electron passing through a portion of said plurality of silicon detection planes, wherein a position of said recoil electron is recorded for each of said portion of said plurality of silicon detection planes.

36. The radiation detector of claim 33, wherein said plurality of silicon detection planes have a predetermined orientation with respect to said gamma rays, said predetermined orientation selected from the group consisting of parallel, perpendicular, or an angle.

37. The radiation detector of claim 33, wherein said plurality of silicon detection planes is selected from the group consisting of silicon microstrip detectors, silicon strip detectors, silicon pad detectors, silicon pixel detectors, double-sided silicon microstrip detectors, and double-sided silicon strip detectors.

38. The radiation detector of claim 33, wherein said multi-channel readout system is comprised of ASIC chips, wherein said plurality of silicon detection planes is comprised of silicon strip detectors, and wherein said strips are fanned in to match a chip bonding pitch corresponding to said ASIC chips.

39. The radiation detector of claim 32, wherein said gamma rays have an energy between about 0.05 and 10 MeV.

40. The radiation detector of claim 32, wherein said output device is a monitor, said monitor displaying an image corresponding to said detected gamma rays.

41. The radiation detector of claim 32, wherein said plurality of position sensitive detector planes is selected from the group consisting of CdTe microstrip detectors, CdTe strip detectors, CdTe pad detectors, CdTe pixel detectors, double-sided CdTe microstrip detectors, double-sided CdTe strip detectors, CdZnTe microstrip detectors, CdZnTe strip detectors, CdZnTe pad detectors, CdZnTe pixel detectors, double-sided CdZnTe microstrip detectors, and double-sided CdZnTe strip detectors.

42. The radiation detector of claim 32, wherein said calorimeter is coupled to said multi-channel readout system.

43. The radiation detector of claim 32, wherein said calorimeter is selected from the group of calorimeter detector materials consisting of HPGe, BGO, LSO, GSO, CdWO₄, CsF, Nal(Tl), CsI(Na), CsI(Tl), CdTe, CdZnTe, HgI₂, GaAs, and PbI₂.

44. The radiation detector of claim 32, wherein said scattered gamma rays passing through said hodoscope form recoil electrons during passage through said plurality of position sensitive detector planes, wherein said hodoscope determines a track direction by a first scatter vertex and an energy associated with said recoil electrons, wherein said scattered gamma rays are totally absorbed within said calorimeter, and wherein an energy of said absorbed gamma rays is determined by said calorimeter.

45. The radiation detector of claim 32, further comprising an anti-coincidence shield substantially surrounding said hodoscope, said anti-coincidence shield not covering said detector aperture.

46. The radiation detector of claim 32, further comprising an anti-coincidence shield substantially surrounding said calorimeter.

47. The radiation detector of claim 32, said detection system further comprising a position sensitive detection layer interposed between said hodoscope and said calorimeter.

48. The radiation detector of claim 32, said position sensitive detection layer having a thickness between about 0.1 millimeter and 1 centimeter.

49. The radiation detector of claim 32, further comprising a scout interceptor missile, wherein said detection system is located within said scout interceptor missile.

50. The radiation detector of claim 49, wherein a portion of said gamma rays is emitted by warheads.

51. The radiation detector of claim 50, wherein said warheads are launched from an ICBM bus.

52. The radiation detector of claim 50, wherein said warheads are irradiated by an external source.

53. The radiation detector of claim 52, wherein said external source is selected from the group consisting of directed energy sources, particle beams, and neutron bombs.

54. The radiation detector of claim 49, wherein a portion of said gamma rays is emitted by a nuclear powered satellite.