# Patent

## Title
Terbium or lutetium containing scintillator compositions having increased resistance to radiation damage

## Abstract

In some aspects, a scintillator composition includes, prior to annealing, the composition (G1-x-yAxREy)aDzO12, wherein D is selected from the group consisting of Al, Ga and In, G is selected from the group consisting of Tb, Y, La, Gd, and Yb, A is selected from the group consisting of Lu, Y, La, Gd, and Yb, and RE is selected from the group consisting of Ho, Er, Tm and Ce, and x is in the range from 0 up to about 0.2774, inclusive, y is in the range from about 0.001 up to about 0.012, inclusive, a is in the range 2.884 up to about 3.032, inclusive, and z is in the range from about 4.968 up to about 5.116, inclusive.

## Background
CROSS REFERENCE TO RELATED APPLICATIONS
This application is a continuation-in-part of U.S. application Ser. No. 10/316,151, filed Dec 10, 2002, published as U.S. Publication No. 20030127630 A1, and issued on Sep. 21, 2004 as U.S. Pat. No. 6,793,848, which is a continuation-in-part of U.S. application Ser. No. 09/682,737, filed Oct. 11, 2001, now U.S. Pat. No. 6,630,077 B2, issued Oct. 7, 2003. Priority is hereby claimed to both applications, which are incorporated by reference herein in their entirety.


BACKGROUND OF THE INVENTION
The present invention relates to terbium or lutetium containing scintillators that are activated with a rare earth metal ion, such as cerium, and treated by annealing at high temperatures in a defined oxygen atmosphere, such that the annealed scintillator has an increased resistance to high-energy radiation damage as compared to a same scintillator not treated by the methods of the present invention.
Solid state scintillator materials have long been used as radiation detectors to detect penetrating radiation in such applications as x ray counters and image intensifiers. The scintillator materials emit visible or near visible radiation when stimulated by x rays or other high energy electromagnetic photons. In typical medical or industrial applications, the optical output from the scintillator is directed to a photoelectrically responsive device to produce electrical output signals, where the amplitude of the signals is proportional to the deposited energy. The electrical signals can than be digitized by a computer for display on a screen or other permanent medium. Such detectors play an important role in computerized tomography (CT) scanners, digital radiography (DR), and other x ray, gamma medical applications, it is especially desirable that the scintillator efficiently absorb nearly all the x rays that pass through a patient, so that the detector utilizes a maximal amount of the high energy administered, and the patient is not subject to a higher radiation dose than necessary.
Among the preferred scintillator compositions in the present generation of CT scanners are ceramic scintillators that employ at least one of the oxides of lutetium, yttrium, and gadolinium as matrix materials. These are described in detail, for example, in U.S. Pat. Nos. 4,421,671, 4,473,513, 4,525,628, and 4,783,596. These scintillators typically comprise a major proportion of yttria (Y2O3), up to about 50 mole percent gadolinia (Gd2O3), and a minor activating proportion (typically about 0.02–12, preferably about 1–6 and most preferably about 3 mole percent) of a rare earth activator oxide. Suitable activator oxides, as described in the aforementioned patents, include the oxides of europium, neodymium, ytterbium, dysprosium, terbium, and praseodymium. Europium-activated scintillators are often preferred in commercial X ray detectors because of their high luminescent efficiency, low afterglow level, and other favorable characteristics.
Improved scintillator materials for the continually evolving medical applications and technologies that employ radiation-based imaging techniques could be provided. To meet the requirements of typical medical radiographic applications, the scintillator must be an efficient converter of x ray radiation (or other high-energy radiation) into optical radiation for the regions of the electromagnetic spectrum detected by photodetection means. Also, the scintillator should transmit optical radiation efficiently, to avoid trapping of the signal generated within the scintillator body. The scintillator should also be characterized by high x ray stopping power, low hysteresis, spectral linearity, and short afterglow.
One important property of CT systems is scan time, which is the time required for a CT system to scan and acquire an image of a slice of the object under observation. Scan times are related to the primary decay time of the scintillator roughly by a factor of 1000. For example, a scan time of 1 second will typically require a scintillator having a decay time of 1 millisecond or less. Thus, shorter CT scan times require shorter scintillator decay times. The present generation of CT systems have scan times on the order of 1 second, and generally are not lower than about 0.4 second. Still shorter scan times are desired. Decreasing scan time increases the number of patients that can be seen, as well as the number of scans taken in a single measurement, as each measurement requires a patent to “hold their breath” during the measurement period. Shorter scan times also reduce image blurring due to the motion of internal organs or motion that occurs when taking scans of non-cooperating patients, such as small children.
Another consideration for scintillators is to reduce damage that occurs to the scintillator upon repeated exposure of the scintillator to high energy radiation. Radiographic equipment employing solid state scintillator materials for the conversion of high energy radiation to an optical image may experience changes in efficiency after exposure of the scintillator to high dosages of radiation. For example, radiation damage for bismuth germanate single crystal scintillators may be as high as 11% after a thirty minute exposure to ultraviolet radiation from a mercury lamp. Similar results are reported for higher energy gamma radiation. Furthermore, the variation in radiation damage from crystal to crystal of bismuth germanate scintillators is high, approximating a factor of at least 30. A similar change in efficiency can be found when polycrystalline type ceramic scintillators are exposed to high energy radiation dosages.
Radiation damage in scintillators is characterized by a change in light output and/or a darkening in color of the scintillator body with prolonged exposure to radiation. Radiation damage can lead to “ghost images” from prior scans which thereby reduce image resolution. The change in light output that occurs upon radiation damage is often found to be variable in magnitude from batch-to-batch of the same scintillator, making it difficult to predict how any individual scintillator will change over time and thus, making it difficult to implement quantitative correction measures. For example, yttria-gadolinia ceramic scintillators activated with europium exhibit a reduction in light output of 4 to 33%, depending upon the scintillator batch, for 450 roentgens of 140 kVP x rays. This amount of variation in light output which can occur as a result of x ray damage is undesirable in a quantitative x ray detector.
BRIEF DESCRIPTION OF THE INVENTION
Thus, in some configurations of the present invention, a scintillator composition is provided that includes, prior to annealing, the composition (G1-x-yAxREy)aDzO12, wherein D is selected from the group consisting of Al, Ga and In, G is selected from the group consisting of Tb, Y, La, Gd, and Yb, A is selected from the group consisting of Lu, Y, La, Gd, and Yb, and RE is selected from the group consisting of Ho, Er, Tm and Ce, and x is in the range from 0 up to about 0.2774, inclusive, y is in the range from about 0.001 up to about 0.012, inclusive, a is in the range 2.884 up to about 3.032, inclusive, and z is in the range from about 4.968 up to about 5.116, inclusive.
Other configurations of the present invention provide a method for preparing a terbium or lutetium containing garnet scintillator having increased resistance to radiation-induced changes in scintillator efficiency. The method includes annealing a garnet scintillator in a controlled atmosphere having a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency of signal generation than a same scintillator not treated by such annealing. The garnet scintillator includes at least one metal selected from (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm. The scintillator is capable of emitting visible light in response to excitation by high-energy radiation including X, β, or γ radiation. Also, prior to annealing, the scintillator includes the composition (G1-x-yAxREy)aDzO12, where D is selected from Al, Ga and In, G is selected from Tb, Y, La, Gd, and Yb, A is selected from Lu, Y, La, Gd, and Yb, and RE is selected from Ho, Er, Tm and Ce, and x is in the range from 0 up to about 0.2774, inclusive, y is in the range from about 0.001 up to about 0.012, inclusive, a is in the range 2.884 up to about 3.032, inclusive, and z is in the range from about 4.968 up to about 5.116, inclusive.
Yet other configurations of the present invention provide a scintillator having increased resistance to radiation-induced changes in scintillator efficiency. The scintillator includes a garnet scintillator capable of emitting visible light in response to excitation by high-energy radiation including X, β, or γ radiation. The garnet scintillator includes at least one metal selected from terbium (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm. The scintillator has been annealed in a controlled atmosphere containing a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiationinduced change in efficiency than a same scintillator not treated by such annealing. Prior to annealing, the scintillator includes the composition (G1-x-yAxREy)aDzO12, wherein D is selected from Al, Ga and In, G is selected from Tb, Y, La, Gd, and Yb, A is selected from Lu, Y, La, Gd, and Yb, and RE is selected from Ho, Er, Tm and Ce, and x is in the range from 0 up to about 0.2774, inclusive, y is in the range from about 0.001 up to about 0.012, inclusive, a is in the range 2.884 up to about 3.032, inclusive, and z is in the range from about 4.968 up to about 5.116, inclusive.
Some other configurations of the present invention provide a scintillator composition that includes, prior to annealing, the composition (Tb1-yCey)aDzO12; wherein D is at least one metal selected from Al, Ga, and In; a is in a range from about 2.8 up to and including 3.1; y is in a range from 0.0005 up to including 0.2; and z is in a range from 4 up to and including 5.1.
Some configurations of the present invention provide a scintillator composition that includes, prior to annealing, the composition (Lu1-yCey)aDzO12; wherein D is at least one metal selected from Al, Ga, and In; a is in a range from 2.8 up to and including 3.1; y is in a range from 0.0005 up to and including 0.2; and z is in a range from 4 up to and including 5.1.
Still other configurations of the present invention provide a scintillator composition that includes, prior to annealing, the composition (G1-x-yAxREy)aDzO12; wherein G is at least one metal selected from Tb and Lu; A is at least one rare earth metal selected from Y, La, Gd, Lu, and Yb when G is Tb and selected from Y, La, Gd, Tb, and Yb when G is Lu; RE is at least one rare earth metal selected from Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er, and Tm; D is at least one metal selected from Al, Ga, and In; a is a range from about 2.8 up to and including 3.1; x is in a range from 0 up to and including 0.5; y is in a range from 0.0005 up to and including 0.2; and z is in a range from 4 up to and including 5.1.
In still other configurations, the present invention provides a scintillator composition that includes, prior to annealing, the composition (Tb1-x-yLuxCey)3Al5O12, where 0<x≦0.5.
In yet other configurations, the present invention provides a scintillator composition that includes, prior to annealing, the composition (Tb1-yCey)3(Al1-r-sGarIns)zO12 where y is in the range from about 0.0005 up to and including 0.2, and z is in the range from about 4 up to and including 5.1, and 0≦r≦0.5 when 0<s≦0.5 and r+s<1, or 0<r≦0.5 when 0≦s≦0.5 and r+s<1.
Still other configurations of the present invention provide a scintillator composition that includes, prior to annealing, the composition (Tb1-y-u-v-wCeyYuGdvSmw)3AlzO12, where y is in the range from about 0.0005 up to and including 0.2; and z is in the range from about 4 up to and including 5.1, 0≦u, v, w≦0.5, and 0.0005≦y+u+v+w<1. In some of these configurations, w=0.
Yet other configurations of the present invention provide a scintillator composition that includes, prior to annealing, the composition (Tb1-x-yAxCey)3AlzO12, where A is Y or Gd, 0<x≦0.5, and y is in the range from about 0.0005 up to and including 0.2, and z is in the range from about 4 up to and including 5.1.
Still other configurations of the present invention provide a scintillator composition that includes, prior to annealing, the composition , the composition Lu0.8Tb2.2Al5O12 activated with Ce3+ ions.
In another aspect, the present invention comprises a scintillator having increased resistance to radiation-induced changes in scintillator efficiency comprising a garnet scintillator capable of emitting visible light in response to excitation by high-energy radiation comprising X, β, or γ radiation, wherein said garnet scintillator comprises at least one metal selected from the group consisting of terbium (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm, and wherein said scintillator has been annealed in a controlled atmosphere comprising a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency than a same scintillator not treated by said annealing.
In yet another aspect, the present invention comprises a detector element of an x ray CT scanner comprising a garnet scintillator having increased resistance to radiation-induced changes in scintillator efficiency comprising a garnet scintillator capable of emitting visible light in response to excitation by high-energy radiation comprising X, β, or γ radiation, wherein said garnet scintillator comprises at least one metal selected from the group consisting of terbium (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm, and wherein said scintillator has been annealed in a controlled atmosphere comprising a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency than a same scintillator not treated by said annealing.
Scintillator materials and detectors of the present invention advantageously provide short decay time (to minimize scanning time), and that show reduced damage upon repeated exposure to the high energy radiation typically employed in the applications requiring scintillators (to increase the reproducibility of the measurements). Methods for scintillator preparation of the present invention are also reproducible, but simple enough to be cost-effective and easily adapted to existing protocols for scintillator manufacture.



BRIEF DESCRIPTION OF THE DRAWING
The FIG. shows a scatter plot of percent radiation damage (% RD) from five different sets of samples: SC-H2, single crystals (SC) heated at 1500° C. for 10 hours in a hydrogen (H2) atmosphere (partial pressure of oxygen=5×10−13 atmospheres (atm)); SC-AsR, single crystals As Received (partial pressure of oxygen= ̃1×10−8 atm); SC-Air, single crystals heated at 1500° C. for 10 h in air (partial pressure of oxygen=0.22 atm); PC-Ar, a polycrystalline (PC) plate heated at 1400° C. for 4 h in argon (partial pressure of oxygen=1×10−8 atm); and PC-Air, a polycrystalline plate, heated at 1400° C. for 4 h in air (partial pressure of oxygen=0.22 atm), in accordance with an embodiment of the present invention.



DETAILED DESCRIPTION OF THE INVENTION
The present invention relates to terbium or lutetium aluminum oxide garnet X ray scintillators activated with a rare earth metal ion, such as cerium, and treated by heating (annealing) at high temperatures and in a defined oxygen atmosphere during or after sintering to reduce radiation damage that would otherwise occur when the scintillator material is exposed to high energy radiation. The scintillator may comprise either a single crystal or a polycrystalline scintillator having the general formula (G1-x-yAxREy)aDzO12; wherein G is at least one metal selected from the group consisting of Tb and Lu; A is at least one rare earth metal selected from the group consisting of Y, La, Gd, Lu, and Yb when G is Tb, and selected from the group consisting of Y, La, Gd, Tb, and Yb when G is Lu; RE is at least one rare earth metal selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er, and Tm; D is at least one metal selected from the group consisting of Al, Ga, and In; a is a range from about 2.8 to and including 3.1; x is in a range from 0 to about 0.5; y is in a range from about 0.0005 to about 0.2; and z is in a range from about 4 to and including 5.1, prior to annealing. In an embodiment, the scintillator comprises a single crystal or a polycrystalline scintillator comprising the general formula (Tb1-x-yLuxCey)3Al5O12, where 0<x≦0.5, and y is in the range from about 0.0005 to about 0.2, and more preferably from about 0.005 to about 0.1, prior to annealing. Thus, in one embodiment, the scintillator comprises Lu0.8Tb2.2Al5O12 activated with Ce3+ ions prior to annealing. The scintillators of the present invention have short decay times and show reduced damage upon exposure to high-energy radiation compared to scintillators not annealed by the method of the invention.
The present invention may be better understood by employing the following non-limiting definitions.
The terms “phosphor” and “scintillator” are used in an interchangeable way to mean a solid-state luminescent material that emits visible light in response to stimulation by high-energy radiation such as X, β, or γ radiation.
The term “high-energy radiation” means electromagnetic radiation having energy higher than that of ultraviolet radiation, including but not limited to, X radiation (also referred to as x ray radiation herein), gamma (γ) radiation, and beta (β) radiation. Solid-state scintillator materials are in common use as components of radiation detectors in apparatuses such as counters, image intensifiers, and computed tomography (“CT”) scanners.
The term “radiation damage” refers to the characteristic of a luminescent material in which the quantity of light emitted by the luminescent material in response to a given intensity of stimulating radiation changes after the material has been exposed to a high-energy radiation dose. The term “radiation damage” may also describe the change of scintillation efficiency due to defects created in the scintillator by the radiation dose.
As used herein, the term “light output” is the quantity of visible light emitted by the scintillator after being excited by a pulse of high energy radiation such as X ray radiation and the like.
The term “afterglow” is the light emitted by the scintillator at a defined time after the x ray excitation ceases, reported as a percentage of the light emitted while the scintillator is excited by the X radiation.
The term “decay time,” “primary decay,” or “primary speed” is the time required for the intensity of the light emitted to decrease to about 36.8% (or 1/e) of the light intensity at the time after the high-energy excitation ceases.
The term “stopping power” refers to the ability of a material to absorb X-radiation; this is also commonly called attenuation or absorption. A material having a high stopping power allows little or no X-radiation to pass through. The stopping power is proportional to the density of the scintillator and the elements contained therein. Thus, it is advantageous to produce scintillators having high density.
Thus, in one aspect, the present invention comprises a method for preparing a terbium or lutetium containing garnet scintillator having increased resistance to radiation-induced changes in scintillator efficiency comprising annealing a garnet scintillator in a controlled atmosphere comprising a predetermined amount of oxygen, for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency of signal generation than a same scintillator not treated by said annealing, wherein said garnet scintillator comprises at least one metal selected from the group consisting of terbium (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm, said scintillator being capable of emitting visible light in response to excitation by high-energy radiation comprising X, β, or γ radiation.
In another aspect, the present invention comprises a scintillator having increased resistance to radiation-induced changes in scintillator efficiency comprising a garnet scintillator capable of emitting visible light in response to excitation by high-energy radiation comprising X, β, or γ radiation, wherein said scintillator comprises at least one metal selected from the group consisting of terbium (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm, and wherein said scintillator has been annealed in a controlled atmosphere comprising a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency than a same scintillator not treated by said annealing.
In yet another aspect, the present invention comprises a detector element of an x ray CT scanner comprising a scintillator having increased resistance to radiation-induced changes in scintillator efficiency comprising a garnet scintillator capable of emitting visible light in response to excitation by high-energy radiation comprising X, β, or γ radiation, wherein said scintillator comprises at least one metal selected from the group consisting of terbium (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm, and wherein said scintillator has been annealed in a controlled atmosphere comprising a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency than a same scintillator not treated by said annealing.
In an embodiment, the scintillator is prepared by sintering. Where the scintillator is prepared by sintering, the garnet scintillator can comprise a polycrystalline scintillator such as a ceramic, or the like.
Alternatively, the scintillator may be prepared by a crystal growth process. Where the scintillator is prepared by a crystal growth process, the scintillator can comprise at least one isolated single crystal.
The annealing is conducted in a controlled (i.e. defined) atmosphere. Generally, the annealing occurs in the presence of oxygen. In some configurations, the controlled oxygen atmosphere comprises an oxygen partial pressure in the range from about 1×10−18 to about 1 atmosphere (atm). In some configurations, the controlled oxygen atmosphere comprises an oxygen partial pressure in the range from about 1×10−13 to about 1 atm. Also in some configurations, the controlled oxygen atmosphere comprises an oxygen partial pressure in the range from about 1×10−8 to about 0.5 atm. Also in some configurations, the controlled oxygen atmosphere comprises an oxygen partial pressure in the range from about 1×10−6 to about 0.22 atm.
Also in some configurations, the annealing temperature comprises a range from 1000° C. to 1500° C., or in some configurations, the annealing temperature ranges from 1400° C. to 1500° C.
The annealing step may be conducted during the normal cooling step which occurs after firing the scintillator material. Alternatively, the annealing may be conducted on a scintillator that has already been cooled to room temperature (i.e. by reheating). The time period for annealing can, in some configurations, comprise a range of from 0.5 to 12 hours (h), or in some configurations, the time period for annealing comprises a range of from 1 to 8 hours, or in some configurations, from 1 to 4 hours.
In some configurations, the scintillator is cooled to room temperature after the annealing step. In some configurations, the rate of cooling ranges between 15020 C. and 500° C. per hour, and in some configurations, a cooling rate of about 300° C. per hour is used.
The present invention in some configurations includes the application of annealing in the presence of oxygen as a way to decrease the susceptibility of rare earth (for example, cerium, praseodymium, and/or neodymium) activated terbium or lutetium containing garnet scintillators to radiation-induced damage. The rare earth activated terbium or lutetium containing garnet scintillators are advantageous because of their relatively short decay rates which as discussed herein, allow for CT systems having faster scan time.
In an embodiment, the annealing step changes the oxygen content of said scintillator. Although the exact amount of the change is difficult to quantify, it is believed that a small change in oxygen stoichiometry may occur upon treatment of garnet scintillators by the method of the present invention.
In an embodiment, prior to the annealing step, the scintillator comprises the formula (Tb1-yCey)aDzO12; wherein D is at least one metal selected from the group consisting of Al, Ga, and In; a is in a range from about 2.8 up to and including 3.1; y is in a range from about 0.0005 up to and including 0.2; and z is in a range from about 4 up to and including 5.1.
In another embodiment, the scintillator comprises the formula (Lu1-yCey)aDzO12; wherein D is at least one metal selected from the group consisting of Al, Ga, and In; a is in a range from about 2.8 to and including 3.1; y is in a range from about 0.0005 up to and including 0.2; and z is in a range from about 4 up to and including 5.1, prior to annealing.
In yet another embodiment, the scintillator comprises the formula (G1-x-yAxREy)aDzO12; wherein G is at least one metal selected from the group consisting of Tb and Lu; A is at least one rare earth metal selected from the group consisting of Y, La, Gd, Lu, and Yb when G is Tb, and selected from the group consisting of Y, La, Gd, Tb, and Yb when G is Lu; RE is at least one rare earth metal selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er, and Tm; D is at least one metal selected from the group consisting of Al, Ga, and In; a is a range from about 2.8 up to and including 3.1; x is in a range from 0 up to and including 0.5; y is in a range from about 0.0005 up to and including 0.2; and z is in a range from about 4 up to and including 5. 1, prior to annealing.
Also in some configurations, A is Lu, RE is Ce, and D is Al. Also in some configurations, the scintillator comprises the formula (Tbl-yCey)aAl5O12 where y is in a range from about 0.0005 up to and including 0.2, and a is in the range from about 2.8 up to and including 3.1, prior to annealing. In yet another embodiment, the scintillator comprises the formula (Tb1-x-yLuxCey)aAl5O12, where a is a range from about 2.8 up to and including 3.1; x is in a range from 0 to up to and including 0.5; y is in a range from about 0.0005 up to and including 0.2, prior to annealing. Also in some configurations, the scintillator comprises the formula (Tb1-x-yLuxCey)3Al5O12; where 0<x≦0.5 and y is in a range from about 0.0005 up to and including 0.2, prior to annealing.
In some configurations, for the scintillators described above, a is in a range from 2.9 up to and including 3.05. Also in some configurations, x is in a range from 0 to and including 0.3, and in some configurations, from 0 up to and including 0.2. Also in some configurations, y is in a range from 0.005 up to and including 0.1, and in some configurations, y is in a range from 0.005 up to and including 0.07. Also in some configurations, z is in a range from 4.5 up to and including 5.05, and in some configurations, from 4.6 up to and including 5.0.
In various embodiments, the garnet scintillator has the formula of (Tb1-yCey)3(Al1-r-sGarIns)zO2 where y is in the range from about 0.0005 up to and including 0.2, and z is in the range from about 4 up to and including 5.1, and 0≦r≦0.5 when 0<s≦0.5 and r+s<1, or 0<r≦0.5 when 0<s≦0.5 and r+s<1, prior to annealing.
In other embodiments, the garnet scintillator has the formula of (Tb1-y-u-v-wCeyYuGdvSmw)3AlzO12, where y is in the range from about 0.0005 up to and including 0.2; and z is in the range from about 4 up to and including 5.1, 0≦u, v, w≦0.5, and 0.0005≦y+u+v+w<1, prior to annealing. In some of these embodiments, w=0.
In yet other embodiments, the scintillator treated by the annealing of the present invention comprises Lu0.8Tb2.2Al5O12 activated with Ce3+ ions.
As described herein, the scintillator of the present invention may comprise a polycrystalline sintered scintillator or may be in the form of single crystals. For a polycrystalline sintered scintillator, the scintillator is prepared as follows in some configurations of the present invention:

    
    
        (1) providing amounts of:
        
            (a) oxygen-containing compounds of at least one first metal selected from the group consisting of terbium and lutetium;
            (b) oxygen-containing compounds of at least one rare-earth metal selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er, and Tm;
            (c) oxygen-containing compounds of at least one second metal selected from the group consisting of Al, Ga, and In;
        
        
        (2) mixing together said oxygen-containing compounds to form a mixture; and
        (3) firing said mixture by calcining at a temperature for a time sufficient to convert said mixture to a rare earth-activated garnet scintillator composition;

wherein said amounts of oxygen-containing compounds are chosen to obtain the final desired composition of said scintillator.

    
    


The step of firing to generate a garnet scintillator (calcining) may comprise a temperature ranging from 700° C. to about 1500° C., or, in some configurations, from 800° C. to about 1200° C., or, in some configurations, from about 850° C. to about 1150° C.
In an embodiment, the mixed oxygen-containing compounds are packed into compact comprising a scintillator body of the desired shape, either prior to, or after the calcining firing step (step (3)). The body is then sintered at high temperature to minimize porosity of the compact. In some configurations the step of sintering the compact comprises heating the pressed compact at high temperature. The sintering temperature in some configurations ranges from 1500° C. to 1800° C. In some configurations, sintering temperatures ranging from 1600° C. to 1780° C. and in some configurations temperatures ranging from 1675° C. to 1775° C. are used.
Radiation damage (RD) may be quantified by measuring change in the intensity of light output before and after a high energy radiation dose, where II is the initial (pre-radiation dose) intensity of light output and IF is the final (post-radiation dose) intensity of light output. Thus, the percent radiation damage (% RD)=[(IF−II)/II]×100. It can be seen that an increase in light output after a high-energy radiation treatment comprises a positive RD value and a decrease in light output after the radiation treatment comprises a negative RD value. However, the closer the RD value is to zero (negative or positive), the better the scintillator responds to high energy radiation without having a change in efficiency. Generally, RD values ranging from +2 to −2 percent are preferred, with values of +1 to −1 percent more preferred, and values from +0.5 to −0.5 percent even more preferred.
Thus, the present invention describes the application of annealing under a predetermined atmosphere to reduce susceptibility to radiation damage in a scintillator material. The present invention provides rare earth-activated scintillators having a garnet structure and containing terbium and/or lutetium. The present invention provides the surprising result that annealing in a defined oxygen atmosphere may be applied to either polycrystalline scintillators or a single crystal form of the scintillator as a means to increase the resistance of the scintillator to radiation damage. The finding that annealing may be used to reduce radiation damage in single crystals is not expected in light of the known poor diffusivity of oxygen through single crystal forms of such scintillators.
Radiation damage to scintillators changes the efficiency by which the scintillator is able to convert high-energy excitation radiation to a measurable signal. Thus, it is important to develop scintillators that are resistant to radiation damage so that the sensitivity of the scintillator to exciting radiation remains substantially constant over a long-term use. Stability and reproducibility of light output of a scintillator is critical to many applications. For example, radiation damage can lead to “ghost images” from prior scans which thereby reduce image resolution. Because the variation in scintillator response that occurs upon radiation damage is highly variable, it is difficult to develop quantitative correction measures. The amount and variation in scintillator efficiency that results upon x ray damage is generally undesirable in a quantitative x ray detector and limits the applicability of such imaging techniques.
In some cases, radiation damage may be controlled by homogeneous doping of scintillators with elements that reduce the concentration of defects (color centers) responsible for changing scintillator efficiency. Also, it has been shown that for a small class of (Y,Gd)203:Eu ceramic scintillators, varying the oxygen atmosphere during sintering influences damage characteristics (U.S. Pat. No. 4,783,596). However, this protective effect was found to work only for a limited class of rare earth doped yttria-gadolinia scintillator materials (U.S. Pat. No. 4,783,596).
Radiation damage causes defects in the scintillator that can then modify the scintillation efficiency for a specific radiation dose. Such defects are commonly color centers that have an electronic structure that imparts optical absorption bands at the scintillator emission wavelengths. The binding energy of the color center determines the longevity of the damage, but in general, this energy is sufficiently large that damage can last from seconds to days at room temperature.
It is difficult to account for the effects of radiation damage when using scintillators for radiographic imaging and thus, it is desirable to develop scintillators that show minimal change in efficiency upon exposure to high-energy radiation. Radiation damage is characterized experimentally by exposing the scintillator to a relevant dose of radiation and measuring the change in light output taken before and after the damage dose. The recovery can be plotted as a function of time after the end of the damage pulse. Such information may be used to distinguish radiation damage due to color center absorption or other defect centers that decrease activator emission efficiency, but is not particularly informative in predicting how a particular scintillator will respond when used clinically.
Also, several factors are important to quantifying the effect of radiation damage on scintillator function. For accurate measurements, it is important to compensate for variations in the source creating the measurement pulses. Also, scintillators with high afterglow must be compensated for residual afterglow from the radiation dose. In addition, since the absorption of the scintillation light depends on path length through the crystal, the measured damage can depend on scintillator geometry, such as crystal thickness and transparency. Also, although radiation damage typically decreases scintillation efficiency, there are some cases, e.g., CsI:TI scintillators, where the efficiency increases. Although not fully understood, it is believed that such increased efficiency may result from the modification or neutralization of defect centers that would otherwise reduce a scintillator's efficiency.
The present invention provides rare earth-activated scintillators having a garnet structure and containing terbium and/or lutetium. The scintillators of the present invention are responsive to high-energy excitation, such as x rays, and have high light output, reduced afterglow, short decay time, and high x ray stopping power. Higher light output is advantageous because a lower amount of high-energy excitation energy is required. Thus, the patient is exposed to a lower dose of high-energy radiation. Reduced afterglow is advantageous because the image is sharper and free from image artifacts, sometimes referred to as “ghost images.” Shorter decay time is preferred because the scan time can be reduced, resulting in more efficient use of the CT system. Higher stopping power is preferred because a smaller quantity of scintillator is needed. Thus, thinner detectors are possible, resulting in lower cost of manufacture. Low radiation damage is advantageous because the sensitivity of the scintillator to exciting radiation remains substantially constant over a long-term use.
The present invention provides a garnet scintillator that is efficiently excitable by x ray radiation and efficiently emits light in the visible range having a broad spectrum from blue to red (from about 500 nm to about 770 nm). The scintillator has an emission peak in the green to yellow range (from about 540 nm to about 600 nm), which includes the range of maximum sensitivity of x ray image intensifiers and photodetectors.
The scintillator of the present invention is a rare earth-activated garnet containing terbium and/or lutetium having a general formula (G1-x-yAxREy)aDzO12, wherein G is at least one metal selected from the group consisting of Tb and Lu; A is a member selected from the group consisting of Y, La, Gd, Lu, and Yb when G is Tb and selected from the group consisting of Y, La, Gd, Tb, and Yb when G is Lu; RE is at least one member selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er, and Tm; D is at least one member selected from the group consisting of Al, Ga, and In; a is in the range from about 2.8 to and including 3.1, in some configurations from about 2.9 to and including 3.05; x is in the range from 0 to about 0.5, in some configurations from 0 to about 0.3, and in some configurations from 0 to about 0.2; and y is in the range from about 0.0005 to about 0.2, in some configurations from about 0.005 to about 0.1, and in some configurations from about 0.005 to about 0.07; and z is in the range from about 4 to and including 5.1, in some configurations from about 4.5 to and including 5.05, and in some configurations from about 4.6 to and including 5.
In another embodiment, the scintillator is terbium aluminum garnet activated with cerium having the formula (Tb1-yCey)aAl5O12 where y is in the range from about 0.0005 to about 0.2, in some configurations from about 0.005 to about 0.1, and in some configurations from about 0.005 to about 0.07; and a is in the range from about 2.8 to and including 3.1, and in some configurations from about 2.9 to and including 3.05.
In another embodiment, terbium is partially substituted with lutetium, and the scintillator has the formula of (Tb1-x-yLuxCey)aAl5O12, wherein a is in the range from about 2.8 to and including 3.1, in some configurations from about 2.9 to and including 3.05; x is in the range from 0 to about 0.5, in some configurations from 0 to about 0.3, and in some configurations from 0 to about 0.2; and y is in the range from about 0.0005 to about 0.2, in some configurations from about 0.005 to about 0.1, and in some configurations from about 0.005 to about 0.07.
In still another embodiment, the scintillator has the formula of (Tb1-x-yLuxCey)3Al5O12; where 0<x≦0.5, and y is in the range from about 0.0005 to about 0.2, in some configurations from about 0.005 to about 0.1, and in some configurations from about 0.005 to about 0.07.
In another embodiment, aluminum is partially substituted with gallium, indium, or a combination thereof. In this case, the scintillator has the formula of (Tb1-yCey)3(Al1-r-sGarIns)zO12 where y is in the range from about 0.0005 to about 0.2, in some configurations from about 0.005 to about 0.1, and in some configurations from about 0.005 to about 0.07; and z is in the range from about 4 to and including 5.1, in some configurations from about 4.5 to and including 5.05, and in some configurations from about 4.6 to and including 5, and 0≦r≦0.5 when 0<s≦0.5 and r+s<1, or 0<r≦0.5 when 0≦s≦0.5 and r+s<1. In some configuration, is in a range from about 0.005 to about 0.3 and in some configurations from about 0.05 to about 0.2; and s in some configurations is in a range from about 0.005 to about 0.3 and in some configurations from about 0.05 to about 0.2.
Also, terbium may be partially substituted by one of Y, Gd, Sm, or a combination thereof and aluminum is not substituted. In this case, the scintillator has the formula of (T1-y-u-v-wCeyYuGdvSMw)3AlzO12, where y is in the range from about 0.0005 to about 0.2, in some configurations from about 0.005 to about 0.1, and in some configurations from about 0.005 to about 0.07; and z is in the range from about 4 to and including 5.1, in some configurations from about 4.5 to and including 5, and in some configurations from about 4.6 to and including 5, 0≦u, v, w≦0.5, and 0.0005≦y+u+v+w<1. Each of u, v, and w is, in some configurations, in a range from about 0.005 to about 0.3 and in some configurations from about 0.005 to about 0.1. In some of these embodiments, w=0.
In still other embodiments, the scintillator has the formula of (Tb1-x-yAxCey)3AlzO12, where A is Y or Gd, 0<x≦0.5, and y is in the range from about 0.0005 to about 0.2, in some configurations from about 0.005 to about 0.1, and in some configurations from about 0.005 to about 0.07; and z is in the range from about 4 to and including 5.1, in some configurations from about 4.5 to and including 5, and in some configurations from about 4.6 to and including 5.
A scintillator composition of the present invention may be prepared by a dry or wet synthesis method. A scintillator of the present invention useful for a detection of high-energy radiation such as X, β, or γ radiation is produced by a dry synthesis method comprising the steps of: (1) providing amounts of oxygen-containing compounds of at least one first metal selected from the group consisting of terbium and lutetium; oxygen-containing compounds of at least one rare-earth metal selected from the group consisting of Y, La, Ce, Pr, Nd, Sm, Eu, Gd, Dy, Ho, Er, Tm, and Yb; and oxygen-containing compounds of at least one second metal selected from the group consisting of Al, Ga, and In; the amounts of oxygen-containing compounds being selected such that the final composition of the scintillator is achieved; (2) mixing together the oxygen-containing compounds to form a mixture; (3) firing (calcining) the mixture at a temperature and for a time sufficient to convert the mixture to a rare earth-activated terbium-containing garnet scintillator and optionally, packing the mixture into a scintillator body of the desired shape; (4) sintering the compacted powder at a temperature and for a time sufficient to remove porosity and yield a translucent or transparent wafer; and (5) annealing the scintillator a controlled oxygen-containing atmosphere for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced efficiency loss than a same scintillator not treated by said annealing.
The oxygen-containing compounds may be mixed together by any mechanical method including, but not limited to, stirring or blending in a high-speed blender or a ribbon blender. The oxygen-containing compounds may be combined and pulverized together in a bowl mill, a hammer mill, or a jet mill. The mixing may be carried out by wet milling especially when the mixture of the oxygen-containing compounds is to be made into a solution for subsequent precipitation. If the mixture is wet, it may be dried first before being fired.
Thus, in some embodiments, three distinct heating steps (calcining, sintering and annealing) may be used to prepare a scintillator of the present invention. Depending on the reactivity of the precursor powder, calcining may comprise various temperature ranges. For powder scintillant, calcining may comprise a temperature from about 700° C. to about 1500° C., in some configurations from about 800° C. to about 1200° C., and in some configurations from about 850° C. to about 1150° C. for a time sufficient to convert all of the mixture to the final garnet composition. For the compact (solid body) scintillant, sintering may comprise a temperature from about 1500° C. to about 1800° C., in some configurations from about 1600° C. to about 1780° C., and in some configurations from about 1675° C. to about 1775° C. for a time sufficient to convert all of the mixture to the final garnet composition. Finally, as described herein, annealing comprises heating the scintillator in a defined oxygen atmosphere for a predetermined time at 1000° C. to about 1500° C., in some configurations from about 1400° C. to about 1500° C.
For the wet synthesis method, drying may be conducted at atmospheric or subatmospheric pressure in air or under a flow of a suitable gas including inert gases and mixtures of air and inert gases at a temperature sufficient to remove a portion of or substantially all solvent used in the wet milling process. The firing (calcining) may be conducted in a batchwise or continuous process, in some configurations with a stirring or mixing action to promote good gas-solid contact, or in some configurations, without a stirring or mixing action. The firing time depends on the quantity of the mixture to be fired, the rate of gas conducted through the firing equipment, and the quality of the gas-solid contact in the firing equipment. Typically, a firing time up to about 10 hours is adequate.
The powder may be cast with the addition of a binder into a green element, then the binder is fully pyrolized between 500° C. and 1100° C., then further sintered at temperature in the range of from about 1500° C. to about 1800° C. to increase the density of the element. In some embodiments, the scintillator material is packed into compact comprising a scintillator body of the desired shape. The body is then sintered at high temperature to minimize porosity of the compact. In some configurations, the step of sintering the compact scintillator body comprises heating the pressed compact at high temperature. For firing a compact, the temperature in some configurations ranges from 1500° C. to 1800° C. In some configurations, temperatures ranging from 1600° C. to 1780° C. and in certain configurations, 1675° C. to 1775° C. are used.
After the step of firing (i.e., sintering), annealing under a defined atmosphere of oxygen is performed. The annealing may take place while the scintillator is still hot from the firing (as a partial cooling in combination with annealing). Alternatively, the annealing may be performed to scintillators that have already been cooled, by reheating the scintillator to 1000° C. to 1500° C., or in some configurations, from 1400° C. to 1500° C. in the presence of oxygen. The partial pressure of oxygen during the annealing may range from 1×10−18 atm up to and including 1 atm, in some configurations from 1×10−13 atm up to and including 1 atm, in some configurations from 1×10−8 atm up to and including 0.5 atm, and in some configurations from 1×10−6 atm up to and including 0.22 atm. In an embodiment, the scintillator is cooled to room temperature after the annealing step.
Thus, a particular anneal treatment given to the scintillators of the present invention provides increased resistance to radiation damage and can be carried out in a simple as well as direct manner. As the sintering operation is ordinarily achieved by heating a pressed compact of the high purity metal oxide ingredients at temperatures in the range 1600° C. to 1800° C., the anneal can be achieved while the sintered material is cooled to ambient conditions. Such an annealing modification simply requires that the sintered material be cooled in the temperature range about 1500° C. to 1000° C. for several hours in a controlled oxygen containing atmosphere at partial oxygen pressures between about 1×10−18 to 1 atmosphere. Alternately, a suitable anneal can be achieved by reheating the already sintered ceramic to the upper annealing temperature (1500° C.) for several hours at the appropriate atmosphere, and thereafter cooling said ceramic at a typical cooling rate. For example, in an embodiment a typical cooling rate is 150° C. to 500° C. per hour. Preferably, the cooling rate is about 300° C. per hour. A suitable atmosphere for either type of annealing step can be provided with an inert gas, such as argon, which includes the required oxygen partial pressures. Also, pure oxygen and air maintained at sub-atmospheric conditions may also be used.
In an embodiment, polycrystalline scintillator material is subjected to annealing in a defined oxygen atmosphere. Alternatively, single crystals may be annealed in an oxygen atmosphere to thereby to reduce susceptibility to radiation damage. This result is surprising in that it would not be expected that the diffusivity of oxygen would be high enough in a single crystal to change the stoichiometry of the scintillator. In most systems, the oxygen diffusivity is many more orders of magnitude faster along the grain boundaries than through the actual grains. For example, in an embodiment, the oxygen diffusivity in an approximately 2 mm thick plate of Lu0.8Tb2.2Al5012 is sufficiently high to permit oxygen stoichiometric adjustments. Thus, when single crystalline plates were subjected to oxygen partial pressure of 3×10−18 at 1500° C. for 10 hours (h), the plate turned from a light yellow to a dark green, indicative of a scintillator having reduced oxygen content. The plate was homogeneous in color without any sign of color gradients, indicating that the oxygen diffusivity is high in a single crystal.
EXAMPLE
As shown in the FIG., radiation damage (% RD) from five different sets of samples that were either measured “As Received” or subjected to various conditions of annealing. All experiments used scintillators of Lu0.8Tb2.2Al5012 activated with Ce3+ ions.
Polycrystalline scintillator ceramic was prepared by sintering the garnet powder in a furnace at 1725° C. Single crystals were purchased commercially from Poly-Scientific (Northrop Grumman, N.C.). One method to prepare single crystals is by the Czochralski method, in which the elements are mixed in a crucible and then melted using low energy radio frequency induction or by resistance heating. A pull rod with a chuck containing a seed crystal at its lower end is then dipped into the crucible. The melt temperature is adjusted so that a meniscus is formed along the seed crystal. The pull rod is simultaneously rotated and lifted. Upon adjustment of power to the melt, a crystal is pulled from the melt.
To measure radiation-induced changes in single crystal scintillators, radiation damage was measured for 4 single crystal wafers. Initial measurements of the intensity of initial (pre-high energy radiation dose) light output (II) using a Si-photodiode over an emission band centered at about 590 nm (but which includes from about 500 to 700 nm) were taken using an input radiation of 60 kvp (kilo volt power), 5 mA x rays for 0.5 seconds (a standard radiation pulse). The wafers were then subjected to a high energy dose of radiation 120 kvp, 250 mA x rays for 12 seconds. The post-radiation light output (Final Intensity=IF) was then measured 35 seconds later, again using an input radiation of 60 kvp, 5 mA x rays for 0.5 seconds. Radiation damage is then quantified as RD (%)=(IF−II)/II,×100, such that an increase in light output after the radiation treatment comprises a positive RD value and a decrease in light output after the radiation treatment comprises a negative RD value. The closer the RD value is to zero, the better the scintillator responds to high energy radiation without having a change in efficiency. Generally, RD values ranging from +2 to −2 percent are preferred, with values of +1 to −1 percent more preferred, and values from +0.5 to −0.5 percent even more preferred.
Results are shown in the FIG. SC-AsR describes experiments measuring radiation damage for single crystals (n=4) As Received (partial pressure of oxygen = ̃1×10−8 atm) with no annealing performed. For these crystals, radiation damage was found to be 2.4515% (1 standard deviation (SD)=0.149449).
The four single crystal scintillator plates were then annealed by heating at 1500° C. for 10 h in air (partial pressure of oxygen=0.22 atm) (Sc-Air) and radiation damage measured as above. It was found that there was a reduction in radiation-induced damage, such that the mean radiation damage over the four crystals was about 1.24% (1 SD=0.7384).
Radiation damage was also measured for ceramic polycrystalline scintillators. Thus, PC-Ar describes an experiment for a polycrystalline plate heated at 1400° C. for 4 hours in an argon atmosphere (partial pressure of oxygen=1×10−8 atm), resulting in an percent RD value of −0.14. Finally PC-Air, describes an experiment in which a polycrystalline plate was heated at 1400° C. for 4 h in air (partial pressure of oxygen=0.22 atm). It was found that for this material, the RD value upon treatment as described above was −1.526 percent. Without any annealing (i.e., directly from the hydrogen furnace) the polycrystalline plates are dark red in color and will emit little light.
Thus, it was found that samples at about 1400° C. to 1500° C. in an atmosphere comprising a partial pressure of 5×10−3 to 0.22 atm oxygen results in a significant change in radiation damage. Surprisingly, the effect was seen for single crystals as well as polycrystalline material.
Thus, the present invention provides a simple procedure to reduce radiation damage in this particular family of scintillators. It is not a straightforward matter to correct for irregularities in scintillator response due to radiation damage. Software corrections can be extremely complex to implement, and often do not account for hysteresis behavior of the light output from radiation damage under the many environments encountered during field use. Essentially, effective software corrections require tracking the absorbed dose for each pixel and then making a gain adjustment (to compensate for radiation damage) with each exposure. The methods of the present invention provide significant improvements in reducing radiation damage. Additionally, the methods and compositions described in the present invention provide increased resistance to radiation damage with little to no impact on other important scintillator properties such as light output or afterglow.
Moreover, the present invention, in some configurations, provides scintillator compositions, which, when annealed, have high light output and excellent afterglow performance. The light output is nearly as high (or, in some cases, as high or higher) than that produced by HiLightTM polycrystalline ceramic scintillator material described in U.S. Pat. No. 4,525,628, issued Jun. 25, 1985, and used in various computed tomographic (CT) rotating gantry imaging system products that are available from GE Medical Systems Global Technology Company, LLC, Waukesha, Wis. Advantageously, the afterglow of various compositions of the present invention, when annealed, is very low.
Forty-one (41) examples of scintillator compositions of the present invention are listed below in Tables I and II, where the parameters X, Y, A, and Z are given of the scintillator composition (G1-x-yAxREy)aDzO12, wherein in each case, D is Al, G is Tb, A is Lu, and RE is Ce. Due to their close chemical and electronic relationships, it will be recognized that Ga or In can be substituted for Al as D. Similarly, Pr, Nd, Sm, Eu, Dy, Ho, Er, and Tm can be substituted for Ce as RE. Also, Y, La, Gd, and Yb can be substituted for Lu as A; and Y, La, Gd, and Yb can be substituted for Tb as G.
Each table light output production as a percentage of that produced by HiLight scintillators and an afterglow percentage. The light output (LO) test was performed using x-ray tube operated at 120 kVp, 5 mA for a pulse of 0.5 s duration. The afterglow test measured the light output as a percentage of the peak output for the sample, at a time 100 ms after a 60 kVp, 50 mA, 0.5 s pulse.
Compositions in these tables are illustrative of satisfactory scintillator composition comprising, prior to annealing, ranges for x that include 0 to about 0.2774; inclusive, for y that include about 0.001 to about 0.012, inclusive, for a that include about 2.884 to about 3.024, inclusive, and for z that include about 4.996 to about 5.116, inclusive.
Compositions of Table I are particularly illustrative of satisfactory scintillator compositions comprising, prior to annealing, the composition (G1-x-yAxREy)aDzO12, wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 3.004, z is about 4.996, x is in the range from about 0 up to about 0.267, inclusive, and y is in the range from about 0.002 to about 0.012, inclusive.
Compositions of Table II are particularly illustrative of satisfactory scintillator compositions comprising, prior to annealing, the composition (G1-x-yAxREy)aDzO12, wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 2.984, z is about 5.016, x is in the range from 0 up to and including about 0.2774, inclusive, and y is in the range from about 0.001 up to and including about 0.0104, inclusive.













TABLE I










% of Production



Sam-




HiLight LO


ple
X
Y
A
Z
120 kvp
AG (%)





















 1
0
0.003
3.0040
4.9960
100
0.0005


 2
0
0.003
3.0040
4.9960
99
0.0011


 3
0.066
0.003
3.0040
4.9960
85
<0.0003


 4
0.066
0.003
3.0040
4.9960
85
0.0008


 5
0.066
0.003
3.0040
4.9960
102
0.0014


 6
0.133
0.003
3.0040
4.9960
93
0.0013


 7
0.133
0.003
3.0040
4.9960
87
0.0008


 8
0.267
0.003
3.0040
4.9960
74
0.0019


 9
0.267
0.003
3.0040
4.9960
75
0.0021


10
0.066
0.002
3.0040
4.9960
81
0.003


11
0.066
0.005
3.0040
4.9960
74
0.0044


12
0.066
0.005
3.0040
4.9960
75
0.0052


13
0.066
0.0065
3.0040
4.9960
78
0.0018


14
0.066
0.0065
3.0040
4.9960
78
0.0027


15
0.066
0.008
3.0040
4.9960
71
0.0047


16
0.066
0.008
3.0040
4.9960
69
0.0009


17
0.066
0.01
3.0040
4.9960
79
0.0254


18
0.066
0.01
3.0040
4.9960
70
0.0062


19
0.066
0.012
3.0040
4.9960
60
0.0074


20
0.066
0.012
3.0040
4.9960
65
0.0035


21
0
0.003
3.0040
4.9960
82
0.0031


22
0
0.003
3.0040
4.9960
79
0.012


23
0
0.003
3.0040
4.9960
82
0.0029


24
0.066
0.003
3.0040
4.9960
90
0.0003


25
0.066
0.003
3.0040
4.9960
90
0.0021


26
0.066
0.0065
3.0040
4.9960
90
0.0015


27
0.066
0.0065
3.0040
4.9960
90
0.0009


28
0.066
0.008
3.0040
4.9960
76
0.0027


29
0.066
0.008
3.0040
4.9960
82
0.0017


Min
0
0.002


Max
0.267
0.012






















TABLE II










LO with 120 kvp



Sample




% of Production
AG


ID
X
Y
A
Z
Lumex
%





















30
0.2681
0.0101
2.984
5.016
49
0.023


31
0.2684
0.0067
2.984
5.016
57
0.022


32
0.2681
0.0034
2.984
5.016
53
0.015


33
0.2681
0.001
2.984
5.016
46
0.02


34
0.1786
0.0101
2.984
5.016
60
0.019


35
0.0895
0.0101
2.984
5.016
57
0.028


36
0
0.0067
2.984
5.016
57
0.056


37
0
0.0034
2.984
5.016
68
0.032


38
0.2639
0.0099
3.032
4.968
58
0.005


39
0.2646
0.002
3.024
4.976
63
0.025


40
0.2774
0.0104
2.884
5.116
40
0.42


Min
0
0.001
2.884
4.968


Max
0.2774
0.0104
3.032
5.116









While the invention has been described in terms of various specific embodiments, those skilled in the art will recognize that the invention can be practiced with modification within the spirit and scope of the claims.

## Claims

1. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition (Tb1yCey)aDzO12; wherein D is at least one metal selected from the group consisting of Al, Ga, and In; a is in a range from about 2.8 up to and including 3.1; y is in a range from 0.0005 up to including 0.2; and z is in a range from 4 up to and including 5.1.

2. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition (Lu1yCey)aDzO12; wherein D is at least one metal selected from the group consisting of Al, Ga, and In; a is in a range from 2.8 up to and including 3.1; y is in a range from 0.0005 up to and including 0.2; and z is in a range from 4 up to and including 5.1.

3. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition (G1-x-yAxREy)aDzO12; wherein G is at least one metal selected from the group consisting of Tb and Lu; A is at least one rare earth metal selected from the group consisting of Y, La, Gd, Lu, and Yb when C is Tb and selected from the group consisting of Y, La, Gd, Tb, and Yb when G is Lu; RE is at least one rare earth metal selected from the group consisting of Ce, Nd, Sm, Eu, Dy, Ho, Er, and Tm; D is at least one metal selected from the group consisting of Al, Ga, and In; a is a range from about 2.8 up to and including 3.1; x is in a range from 0 up to and including 0.5; y is in a range from 0.0005 up to and including 0.2; and z is in a range from 4 up to and including 5.1.

4. A scintillator composition in accordance with claim 3, wherein A is Lu, RE is Ce, and D is Al.

5. A scintillator composition in accordance with claim 3 comprising the composition (Tb1-yCey)aAl5O12.

6. A scintillator composition in accordance with claim 3 comprising the composition (Tb1-x-yLuxCey)aAl5O12.

7. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition where 0<x ≦0.5 and y is in the range from about 0.0005 to about 0.2.

8. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition (Tb1-yCey)3(Al1-r-sGarIns)zO12 where y is in the range from about 0.0005 up to and including 0.2, and z is in the range from about 4 up to and including 5.1, and 0≦r≦0.5 when 0<s≦0.5 and r+s<1, or 0<r≦0.5 when 0≦s≦0.5 and r+s<1.

9. A sintered ceramic scintillator compositions ,which is transparent or translucent comprising, prior to annealing, the composition (Tb1-y-u-v-wCeyYuGdvSMw)3AlzO12, where y is in the range from about 0.0005 up to and including 0.2; and z is in the range from about 4 up to and including 5.1, 0≦u, v, w≦0.5, and 0.0005≦y+u+v+w<1.

10. A scintillator in composition in accordance with claim 9 wherein w=0.

11. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition (Tb1-x-yAxCey)3AlzO12, where A is Y or Gd, 0<x≦0.5, and y is in the range from about 0.0005 up to and including 0.2, and z is in the range from about 4 up to and including 5.1.

12. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition Lu0.8Tb2.2Al5O12 activated with Ce3+ ions.

13. A sintered ceramic scintillator composition, which is transparent or translucent, comprising, prior to annealing, the composition (G1-x-yAxREy)aDzO12, wherein D is selected from the group consisting of Al, Ga and In, G is selected from the group consisting of Tb, Y, La, Gd, and Yb, A is selected from the group consisting of Lu, Y, La, Gd, and Yb, and RE is selected from the group consisting of Ho, Er, Tm and Ce, and x is in the range from 0 up to about 0.2774, inclusive, y is in the range from about 0.001 up to about 0.012, inclusive, a is in the range 2.884 up to about 3.032, inclusive, and z is in the range from about 4.968 up to about 5.116, inclusive.

14. A scintillator composition in accordance with claim 13 wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 3.004, z is about 4.996, x is in the range from about 0 up to about 0.267, inclusive, and y is in the range from about 0.002 to about 0.012, inclusive.

15. A scintillator composition in accordance with claim 13 wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 2.984, z is about 5.016, x is in the range from 0 up to and including about 0.2774, inclusive, and y is in the range from about 0.001 up to and including about 0.0104, inclusive.

16. A method for preparing a terbium or lutetium containing garnet scintillator having increased resistance to radiation-induced changes in scintillator efficiency comprising annealing a sintered ceramic garnet scintillator that is transparent or translucent in a controlled atmosphere comprising a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency of signal generation than a same scintillator not treated by said annealing, wherein said garnet scintillator comprises at least one metal selected from the group consisting of terbium (Tb) and lutetium (Lu), arid is activated with at least one rare earth element selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm, said scintillator being capable of emitting visible light in response to excitation by high-energy radiation comprising X, β, or γ radiation, and wherein prior to annealing, said scintillator comprises the composition (G1-x-yAxREy)aDzO12, wherein D is selected from the group consisting of Al, Ga and In, G is selected from the group consisting of Tb, Y, La, Gd, and Yb, A is selected from the group consisting of Lu, Y, La, Gd, and Yb, and RE is selected from the group consisting of Ho, Er, Tm and Ce, and x is in the range from 0 up to about 0.2774, inclusive, y is in the range from about 0.001 up to about 0.012, inclusive, a is in the range 2.884 up to about 3.032, inclusive, and z is in the range from about 4.968 up to about 5.116, inclusive.

17. A method in accordance with claim 16 wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 3.004, z is about 4.996, x is in the range from about 0 up to about 0.267, inclusive, and y is in the range from about 0.002 to about 0.012, inclusive.

18. A method in accordance with claim 16 wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 2.984, z is about 5.016, x is in the range from 0 up to and including about 0.2774, inclusive, and y is in the range from about 0.001 up to and including about 0.0104, inclusive.

19. A sintered sintered ceramic scintillator composition, which is transparent or translucent, having increased resistance to radiation-induced changes in scintillator efficiency comprising a garnet scintillator capable of emitting visible light in response to excitation by high-energy radiation comprising X, β, or γ radiation, wherein said garnet scintillator comprises at least one metal selected from the group consisting of terbium (Tb) and lutetium (Lu), and is activated with at least one rare earth element selected from the group consisting of Ce, Pr, Nd, Sm, Eu, Dy, Ho, Er and Tm, and wherein said scintillator has been annealed in a controlled atmosphere containing a predetermined amount of oxygen for a predetermined time and temperature, such that the annealed scintillator comprises a smaller radiation-induced change in efficiency than a same scintillator not treated by said annealing, and wherein prior to annealing, said scintillator comprises the composition (G1-x-yAxREy)aDzO12, wherein, D is selected from the group consisting of Al, Ga and In, G is selected from the group consisting of Tb, Y, La, Gd, and Yb, A is selected from the group consisting of Lu, Y, La, Gd, and Yb, and RE is selected from the group consisting of Ho, Er, Tm and Ce, and x is in the range from 0 up to about 0.2774, inclusive, y is in the range from about 0.001 up to about 0.012, inclusive, a is in the range 2.884 up to about 3.032, inclusive, and z is in the range from about 4.968 up to about 5.116, inclusive.

20. A detector element of an x ray CT scanner comprising the scintillator of claim 19.

21. A scintillator in accordance with claim 19 wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 3.004, z is about 4.996, x is in the range from about 0 up to about 0.267, inclusive, and y is in the range from about 0.002 to about 0.012, inclusive.

22. A detector element of art x ray CT scanner comprising the scintillator of claim 21.

23. A scintillator in accordance with claim 19 wherein G is Tb, A is Lu, RE is Ce, and D is Al, and further wherein a is about 2.984, z is about 5.016, x is in the range from 0 up to and including about 0.2774, inclusive, and y is in the range from about 0.001 up to and including about 0.0104, inclusive.

24. A detector element of an x ray CT scanner comprising the scintillator of claim 23.