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US3728541A - X-ray diffractometer - Google Patents

X-ray diffractometer
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US3728541A
US3728541AUS00215486AUS3728541DAUS3728541AUS 3728541 AUS3728541 AUS 3728541AUS 00215486 AUS00215486 AUS 00215486AUS 3728541D AUS3728541D AUS 3728541DAUS 3728541 AUS3728541 AUS 3728541A
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axis
detector
crystal
ray diffractometer
drum
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US00215486A
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D Rabinovich
G Schmidt
E Schmidt
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Yeda Research and Development Co Ltd
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Abstract

An X-ray diffractometer has a yoke on which a crystal is mounted so that a particular rational axis thereof intersects the axis of the X-ray beam at a predetermined angle. A direct counting detector mounted on the yoke is selectively positionable in both azimuth and elevation with respect to the particular rational axis of the crystal. The yoke is constructed and arranged to effect precession of both the particular rational axis of the crystal and the detector about the axis of the beam.

Description

ite States atent Rabinovich et al.
[45] Apr. 17, 1973 X-RAY DIFFRACTOMETER Inventors: Dov Rabinovich, Rehovoth, Israel; Gerhard M. J. Schmidt, deceased, late of Rehovoth, Israel by Ester Schmidt, administrator Yale Research and Development Co., Ltd., Rehovoth, Israel Filed: Jan. 5, 1972 Appl. No.: 215,486
Assignee:
Related U.S. Application Data Continuation-impart of Ser. No. 37,202, May 14,
I970, abandoned.
Foreign Application Priority Data May 20, 1969 Israel ..32247 US. Cl ..250/5L5, 250/52 Int. Cl. ..GOln 23/20 Field of Search ..250/5 l .5
[56] References Cited OTHER PUBLICATIONS Elimination of Spot Doubling In Precession Photography, J. N. Einstein Journal of Applied Crystalography 1970 pp. 180-181 (9/8/69).
Primary Examiner-James W. Lawrence Assistant ExaminerC. E. Church Attorney-Browdy and Neimark 5 7 ABSTRACT An X-ray diffractometer has a yoke on which a crystal is mounted so that a particular rational axis thereof intersects the axis of the X-ray beam at a predetermined angle. A direct counting detector mounted on the yoke is selectively positionable in both azimuth and elevation with respect to the particular rational axis of the crystal. The yoke is constructed and arranged to effect precession of both the particular rational axis of the crystal and the detector about the axis of the beam.
14 Claims, 6 Drawing Figures PATENTED APR] 7 I973 SHEET 1BF 5 PATENTEDAPR 1 H915 3,728,541
SHEET 2 BF 5 Inventor;
.m/ 77, Jamar A Home yg PAIENIEBA 3.728.541
SHEET 3 0F 5 M giiwgu/w Attorney;
X-RAY DIFFRACTOMETER The invention relates to an improved X-ray diffractometer. The present application is a continuation-inpart of a co-pending application Ser. No. 37,202 filed May 14, 1970 now abandoned.
X-ray techniques have been widely used for many years in the study of the structure of matter and are capable of yielding detailed information on the structure of complicated molecules. The main disadvantage, however, in the use of such X-ray techniques is to be found in the extremely large amount of data which is required for structural analysis and which can amount, even in relatively modest cases, to well over 1000 individual spectra.
Two main techniques are employed in order to record the intensities of X-ray spectra. The first technique involves photographically recording the X- rays whilst the second technique involves counting the individual X-ray quanta by means of a radiation counter such as a geiger, proportional or scintillation counter.
Whilst the use of photographic techniques involve X- ray cameras which are relatively cheap, compact and simple in design and operation and have the advantage of yielding a permanent record, the integrated intensity of each reflection must be estimated either visually or photometrically from the density of the corresponding spots on the film and this procedure is slow and yields only relatively low quality data.
Radiation counters, on the other hand, are commonly used with diffractometers where each reflecting plane of the crystal is successively brought into its Bragg angle and the integrated intensity of the reflection from that plane is measured directly by the counter. The disadvantage associated with conventional apparatus using radiation counters lies in the complexity of the means by which the crystal is oriented in the beam and the detector brought into a known position both in relation to the crystal and the incident X-ray beam. Such means conventionally take the form of complex mountings for the crystal and the detector to give each the required degrees of freedom to properly orient the crystal and the counter. Depending on the type of cradle used, three or four angular settings are required in order to establish the desired orientation of the crystal relative to the beam and the required position of the detector relative to the crystal. As a consequence conventional apparatus is very expensive and requires relatively large and costly computers for control and operation.
It is an object of the present invention to provide a new and improved X-ray diffractometer using a direct counting device wherein the above referred to disadvantages are substantially reduced or overcome.
The present invention is based on the so-called coneaxis method described in full detail in the book The precession method by MJ. Buerger, published by .iohn Wiley and Sons, copyright 1964.
The following is a short summary of the method including the definition of parameters and concepts essential for the understanding of the mode of operation of the present invention.
The cone-axis method makes use of the fact that the diffracted reflections of the various planes of a crystal, irradiated by an X-ray beam, lie along the generators of the Laue cones co-axial with rational directions in that crystal. The term rational direction means here, a direc tion in the crystal defined by a vector Fn Z "217 n 0 where a, b and care vectors specifying the unit cell of the crystal under consideration and n n and n;, are small integers.
in order to obtain a cone-axis photograph the socalled Buerger precession camera may be used in which a photographic plate is fixed in a plane perpendicular to a particular rational direction of a crystal that is mounted in such a way as to permit that particular rational direction to precess about the in incident beam at a preselected angle u, without undergoing any pure rotation. The various orders of the Laue cones associated with the particular rational direction will intercept the photographic plate and define a set of concentric circles. Thus, during one full precession cycle, the various planes of the crystal are brought, each at its own specific phase of the cycle, into their reflecting positions and the reflected beams are recorded on the film as spots of different densities arranged in such a manner as to form the set of concentric circles described above. Each reflection is, conventionally, specified by three integers, hkl, known as the Miller indices of that reflection; the precession phase angle, mentioned above, of a given reflection hkl will therefore be denoted by I' Similarly, the azimuth angle of the spot associated with the hkl reflection, which is measured around the circle from a predetermined point, is denoted by All reflections lying on the nth circle (nth Laue cone) have one Miller index, n, in common and are said to belong to the nth order or level. All such nkl reflections have thesame elevation angle 11, i.e., the halfopening angle of the nth Laue cone, and a circle radius r,,. In this manner each and every reflection is uniquely specified by the following parameters: the precession angle ;1., the elevation angle of thenth order 11,,, the phase angle l and the azimuth angle da Given the uni t cell dimensions and chosing the rational direction 1 and the precession angle u, the rest of the parameters may be calculated by appropriate crystallographic formulae.
In the X-ray diffractometer of the present invention, the photographic plate of the Buerger precession camera used to obtain cone-axis photographs is replaced by a radiation counter whose aperture is selectively positionable inelevation 11 and azimuth d). The photon-sensitive area of the counter is suitably masked so as to permit the recording of only one reflection at a time and to cut down the amount of background radiation. The angular opening Ad), and the radial height, Ar, chosen so as to exclude unwanted reflections and to minimize the background count, are computed from the known unit cell parameters, the instrument parameters, the radiation wave length and the physical dimensions and properties of the crystal.
-By choosing a particular rational direction and by fixing the mechanical parameters of the instrument, i.e., the precession angle 1, the aperture radial distance r,,, the angular opening and radial height of the aperture, Ad: and Ar,,, the nth order (nth circle of the set of concentric circles) is selected and all reflections of this order may now be measured successively. Thus, in order to record the intensity of a nkl reflection the particular rational direction is precessed to the required phase angle I' and, the aperture is rotated about the rational direction to the required azimuth angle 4%, At these angular positions one, and only one, reflection will be recorded; the output of the detector yields the integrated intensity of this reflection. By changing the pair of angles I and d), the complete set of the nth order reflections can be measured.
BRIEF DESCRIPTION OF THE INVENTION Briefly, a direct radiation detector is coupled to a crystal so that both the detector and a particular rational axis of the crystal precess together about an incident X-ray beam. The detector, which is mounted so as to be selectively positionable in both azimuth and elevation with respect to the particular rational axis of the crystal, is suitably masked to limit its field of view in such a way as to exclude unwanted reflections, and reduce background radiation.
In one embodiment of the invention the detector is mounted on an axial end of a drum which is rotatable about the particular'rational direction of the crystal. The detector is eccentrically positioned on the drum so that the axis of the detector is parallel to the drum axis. Rotation of the drum will place the detector at the required azimuth angle. The elevation angle is established by suitable adjustment to the aperture means that mask the detector, such adjustment serving to effectively move the aperture radially of the surface.
Alternatively, or in addition, the detector can be radially displaceable on the drum.
In another embodiment of the invention, the drum is in the form of a ring to which is attached a cylindrical guide, the axis of which is normal to the rotational axis of the ring and passes through the point where the X- ray beam intersects the axis of the ring. The detector, in this embodiment, is slidably mounted in the guide for arcuate movement about the crystal to establish the desired elevation angle of the detector. The azimuth angle is established by suitably rotating the ring. In this embodiment, the detector axis is always aligned with v the reflected beams. In the first described embodiment,
the detector axis is inclined with respect to the reflected beams.
BRIEF DESCRIPTION OF DRAWINGS For a better understanding of the present invention, and to show how it can be carried out in practice, reference should be made to the accompanying drawings, wherein:
FIG. 1 is a schematic representation showing the mounting of a crystal in a Buerger precession camera in preparation for making a cone-axis photograph;
FIG. 2 is a top plan view of the first embodiment ofa diffractometer according to the present invention;
FIG. 3 is a front elevation of the diffractometer shown in FIG. 1;
FIG. 4 is a side elevation of the diffractometer shown in FIG. 1 with the gimbal rotated to make an angle ,u. with the incident X-ray beam; and
FIG. 5 is a schematic representation of a precession diffractometer system in accordance with the present invention; and
FIG. 6 is a pictorial perspective showing a second embodiment of the invention.
DETAILED DESCRIPTION OF THE INVENTION In the first embodiment of the invention shown in FIGS. 2 5 of the drawings, a firstvertical gimbal fork 5 comprises a pair of vertically disposed spacedgimbal limbs 6 and 7 coupled together by ahorizontal gimbal beam 8. A vertical tube attached tobeam 8 is rotatably mounted on avertical gimbal shaft 9 which is, in turn, fixedly mounted on aturntable 10.Fork 5 is thus vertically rotatable aboutaxis 101 ofshaft 9. Theturntable 10 is rotatably mounted onbase beams 11 which are supported with respect to a support surface by means of levelling screws 12. Theturntable 10 is provided with a turntable lock 13 by means of which the turntable can be locked in any desired angular position with respect to the base beams 1 l.
A pair of short horizontally alignedgimbal shafts 14 and 15 are respectively rotatably mounted inball bearings 16 and 17, journalled in the upper bifurcated ends of thevertical gimbal limbs 6 and 7. Thehorizontal gimbal shaft 14 is formed integrally, on one end thereof, with an extendedhorizontal shaft 18 of the gimbal which is, in turn, coupled to a goniometer head 19 which supports acrystal 20. The crystal is located at that point at which theaxis 101 intersects the axis 102, which is the common axis of alignedhorizontal shafts 14 and 15. The other end of thehorizontal gimbal shaft 14 is coupled to a crystaltranslation adjustment mechanism 21 via adial 23 and dialaxis vernier 22. Themechanism 21 is provided with a crystaltranslation adjustment screw 24 for selectively moving the crystal along the axis 102.
Asecond gimbal fork 25 comprises a pair ofyoke arms 26, 27 which project into the bifurcated ends of the verticalgimbal fork limbs 6, 7 and are rigidly secured to the shorthorizontal gimbal shafts 15, 14. Theyoke arms 26, 27 are rigidly secured together by rear andintermediate cross beams 28 and 29. Thesecond gimbal fork 25 is thus mounted on thefirst gimbal fork 5 for pivotal movement about the horizontal axis 102.
Asupport shaft 103, whose axis passes through theintersection of theaxes 101 and 102, projects through and is rotatably mounted in therear cross beam 28.Vernier 31, rigidly mounted onbeam 28, cooperates with 11dial 30 rigidly attached to and rotatable withshaft 103. The free end ofshaft 103 projects into and is rotatably mounted in a suitable bearing incoupling collar 32 which can freely slide onarcuate member 33 and thus positionfork 25 relative tolimbs 6 and 7 offork 5 so that theaxis 104 ofshaft 103 will make the desired angle p. with a horizontal X-ray beam passing through the intersection ofaxes 101 and 102. In such position, thecollar 32 can be clamped toarcuate member 33 which itself is rigidly attached to a I driveshaft 34 journalled in aframe 35 within which is supported a I drivemotor 36. The output of themotor 36 is transmitted via a worm andgear 37 coupled to thedrive shaft 34. By means of lockingscrew 40, theI dial 38 is rigidly attached to and rotatable withshaft 34. Dial38 is cooperable withvernier 39 which is rigidly attached to frame 35.
The end ofshaft 103 remote from the bearing incollar 32 is attached to and supports one end ofradiation counter drum 41 which is mounted infork 25 for rotation about theaxis 104 ofshaft 103. The other end of thedrum 41 is mounted in anannular drum frame 42 by means of angularly spaced apart drum supports 43, respectively held insupport holders 44 secured to theframe 42 and respectively provided with drum support adjustment screws 45. The rear end of the drum is formed integrally with aqb gear wheel 46 which meshes with a 4:pinion 47 coupled to anoutput shaft 48 of a 4drive motor 49 also supported by theyoke 25. Thus thedrum 41 can be rotated aboutaxis 104 through the angle 4) by thedrive motor 49 whilst supported on the drum supports 43.
Located within thedrum 41 is a radiation counter 50 (shown in dotted lines in FIG. 3) whose longitudinal axis is parallel to, but spaced apart from thelongitudinal axis 104 of thedrum 41. The front aperture of thecounter 50 is located opposite a sector-like aperture 51 formed in an end face of the drum. Selective rotation ofdrive motor 49 will rotate the counter aboutaxis 104 until the photon-sensitive surface is positioned at the desired azimuth angle relative toaxis 104.
Superimposed on the end face of the drum is a first metal disc which is supported on the end face for rotation aboutaxis 104. A sector-like aperture 52 formed in the first metal disc corresponds to the sector-like aperture formed in the fixed end face. Thus, by rotating the first metal disc with respect to the end face of the drum, the apertures 51 and 52 may be misaligned to the extent necessary to mask of the photon-sensitive surface of thecounter 50 except for theaperture 53 having the desired angular width Ad The relative position of the two apertures 51 and 52 and in consequence the magnitude of A4) can be measured by means of a rotatable disc dial and vernier arrangement 54. Asecond metal disc 55 is also rotatably mounted on the end face of the drum and is provided with a plurality of annular slots 56 of differing radii corresponding to the differing radii of the cone axis circles. The radial width of each slot establishes the height Ar of the aperture for the counter. By rotating the second disc on the end face of the drum, a selected one ofthe slots 56 can be positioned opposite the aperture 51 and 52 to establish the radial position r of the aperture. A pair of radially spaced apart locking screws 57 and 58 are provided for securing theadditional disc 55 in the required position.
The end face of the drum, in cooperation with the first and second discs, selectively masks the photonsensitive surface of the counter establishing a detector with a limited field of view. By rotating the drum on theyoke 25, and by rotating the first-and second discs on the end face of the drum, the detector can be positioned at azimuth and elevation angles with respect to the rational direction I of the crystal corresponding to a particular reflection to be studied. In addition, the required aperture size Ad) and Ar to prevent recariation of simultaneous reflections will also be achieved.
Finally, anX-ray collimator 59 is supported in a collimator holder 60 and is provided with a collimator lock mechanism 61, the collimator holder 60 being located fixedly with respect to the turn table 10. Thecollimator 59 is aligned with theI drive shaft 34.
In operation the precession diffractometer turntable is rotated so as to align thecollimator 59 in the direction of the X-ray source and theturntable 10 is clamped in this position by means of the turntable lock 13. The horizontalaxis dial mechanism 21 is then rotated so as to bring the horizontal axis 102 into the appropriate position wherein the desired rational direction of the crystal is correctly orientated with respect to the collimated X-ray beam. Thecollar 32 is thereupon unclamped and is slid on thearc member 33 until theaxis 104 orients the crystal at the predetermined angle p. with respect to the incident X-ray beam. When so orientated thecollar 32 is clamped in position.
The first metal disc on the end face ofdrum 41 is rotated so as to define a predetermined angular width of aperture A4: which, as indicated above, is predetermined in accordance with the conditions for avoiding the detection of unwanted reflections. Similarly, thesecond metal disc 55 is rotated so as to superimpose on the aperture that annular slot corresponding to the predetermined height Ar and radial position of the aperture in which measurements are to be effected. A detector is now established at the desired elevation angle to measure the reflected energy from a particular nth level of the crystal.
Measurement can now be obtained in any one of the following modes:
In accordance with a first mode of operation the and (1) drivemotors 36 and 49 are actuated so as to set the instrument in the required P and da setting for any particular nkl reflection, the I' and d) settings being read on the respective dials 40 and 30. The instrument, (i.e., the crystal and the counter) is maintained stationary in this particular setting and the reflection intensity is measured over a predetermined period of time in terms of the electric pulses from the counter which are fed to a spectrometer which together with the counter constitutes a standard counting channel.
In accordance with a second mode of operation thedrive motor 36 is arranged to displace the instrument to a value of I which corresponds to, but is somewhat less 7 than the predetermined value of I' corresponding to the particular reflection to be measured. The (1) drivemotor 49 then rotates the drum to the required (b position and now, a predetermined number of discrete stepping pulses are successively fed to the I drive motorso as to drive the instrument by small discrete steps into and slightly beyond the predetermined P value, at each step the intensity of reflection being measured. In this way scanning of the range is obtained.
Preferably stepping motors are used for both the I and ti drives. These motors were chosen because they offer two important advantages over continuous motors. First, they can be conveniently used in open loop control logic, i.e., there is no need for feedback, from digitizer or other position detecting devices, to stop the motor when the required setting is achieved; a predetermined number of electrical pulses being all that is needed to rotate the motor to its specified settings. Secondly, such a motor may be electrically locked by applying direct current, thus avoiding drift of the drive shaft.
The motor drive preferably consists of an electronic pulse generator whose pulses are fed into the motors. Manual control switches can be provided for selecting the required motor operation and its sense.
An automatic control may be used to supervise the operationof the various components of the precession diffractometer system in order to collect the data of a complete level. As seen in FIG. 5, automatic control is effected by means of an on-line desk-top computer assembly 71. Thecomputer assembly 71 consists of a desk-top calculator, a programmer and an auxiliary storage memory. Aninterface 72 connects the output of thecomputer assembly 71 to a motor drive control '73, to thespectrometer 74 and to asealer printout control 75 andteletype unit 76. A suitable program controls the system. Input parameters for this program comprises (a) crystallographic parameters, (b) operation instructions, (c) status parameters. Using these data the computer assembly is capable of computing and controlling the data collection of a set of reflections belonging to a given level.
In the embodiment of the invention shown in FIGS. 2 of the drawings, the axis ofdetector 50 is substantially parallel to theaxis 104 of thedrum 41 and thesupport shaft 103, which axis is also congruent with the particular rational axis of the crystal. When steppingmotor 49 is operated,detector 50 is caused to rotate aboutaxis 104. The photon-sensitive surface ofdetector 50 under these conditions will not be normal to beams reflected from the crystal; and beams reflected from the crystal will impinge on the photon-sensitive surface ofdetector 50 at the elevation angle v,,.
Referring now to FIG. 6, the second embodiment of the invention is designated generally byreference numeral 200. The device ofembodiment 200 includes afirst gimbal fork 5, a second gimbal fork 25',support shaft 103,coupling collar 32,arcuate drive member 33, and I driveshaft 34. The first gimbal fork, the support shaft, the coupling collar, the arcuate drive member, and the I drive shaft inembodiment 200 are the same as the corresponding elements in the first described embodiment.
The second gimbal fork 25' comprises afirst support ring 201, a second support ring'202 and acurved guide 203. Rigidly attached to and perpendicular to the plane offirst support ring 201 are a pair of diametrically opposed bearing lugs 204 which form bearings for gimbal shafts l4 and 15. The axis 102 of these gimbal shafts is perpendicular to and intersects theaxis 101 about whichfork 5 is rotatable. The point of intersection is designated P. While not shown in FIG. 6, a shaft integral withgimbal shaft 14 extends toward the intersection of theaxes 101 and 102 and carries a goniometer head which suitably supports, at point P, a crystal which is to be studied. This shaft is the same asshaft 18 of the first described embodiment.
Thesecond support ring 202 is rotatably mounted on thefirst support ring 201.Axis 104, about which thesecond support ring 202 rotates, is congruent with the axis ofsupport shaft 103. To provide for the angular positioning ofring 202 onring 201, the outer circumference ofring 202 may be provided with gear teeth which mesh with apinion 47 rigidly attached toshaft 48 of theaximuth motor 49. This motor is rigidly attached to supportring 201. By energizingmotor 49, it is possible to rotatering 202 aboutaxis 104 and place the ring in any angular position.
Curved guide 203 is defined by a pair of arcuate ribs which diametrically spanring 202 and are rigidly connected thereto. The plane of each of these arcuate ribs is normal to the plane ofring 202. The inner curved surface of these ribs establish a cylindrical guide sur face, the axis of which surface is perpendicular toaxis 104 and passes through the point P at the intersection ofaxes 101 and 102.
Slidably mounted on the ribs ofcurved guide 203 isadjustable clamp 205 which releasably carriesdetector 50. With this arrangement the axis of detector 50' will always pass through the point P at the intersection ofaxis 101 with axis 102 regardless of the location of theadjustable clamp 205 on theguide 203, and regardless of the angular position ofring 202 onsupport ring 201.
AU-shaped support 206 is attached to guide 203 in the middle thereof and extends away from the guide in a radial direction. The space between the legs of this support provide clearance for passage of detector 50' andadjustable clamp 205. Carried on the bridge between the two legs ofsupport 206 issupport shaft 103 whose axis is colinear withaxis 104. The free end ofshaft 103 projects into and is rotatably mounted in a suitable bearing incoupling collar 32 which can freely slide onarcuate member 33 and thus pivot for 25' about axis 102. In thismanner axis 104 can be positioned at the desired angle p. with respect to a horizontal X-ray beam passing through the point P at the intersection ofaxes 101 and 102 by clamping thecollar 32 toarcuate member 33 which itself is rigidly attached to I driveshaft 34 journalled in the same manner as in the previously described embodiment. Suitable scales and indicia may be provided in the embodiment shown in FIG. 6 to provide for reading out the angles v d) and 1 between the various components as shown in FIG. 6.
The operation ofembodiment 200 is substantially the same as the operation of the first described embodiment except as to the manner in which the elevation angle of the detector is changed. Thus,collar 32 may be moved onarcuate member 33 until the plane ofrings 201 and-202 is tilted to establish theaxis 104 at the desired angle p. with the X-ray beam. In this position,axis 104 is colinear with a particular rational axis of a crystal under study. Knowing the angle 1 the detector 50' is moved on the ribs ofcurved guide 203 until the axis ofdetector 50 makes theangle 11,, with the axis of the X-ray beam. The detector is held at this location by tighteningadjustable clamp 205. Asshaft 34 is rotated by the I drive motor (not shown in FIG. 6),fork 5 will oscillate aboutaxis 101 through an angle of 2 y. while, at the same time, gimbal fork 25' will oscillate about axis 102 through the same angle. With this arrangement, the particular rational axis of the crystal under study precess about the X-ray beam in a conventional manner.Motor 49 may be energized in a selective manner to positionring 202 so that the detector 50' is at the proper azimuth angle for the reflection under consideration. All three modes of operation described in connection with the first embodiment of the invention can be utilized with the embodiment shown in FIG. 6. Different Laue cones are investigated by changing the elevation angle v The detector 50' may be fitted with a suitable adjustable aperture for discriminating against simultaneous reflections.
What is claimed is:
1. An X ray diffractometer for positioning a crystal in an X-ray beam and measuring the intensity of reflected radiation comprising: a yoke on which a crystal can be mounted so that a particular rational direction thereof intersects the axis of the beam at a predetermined angle, a photon-sensitive detector movably mounted on the yoke and selectively positionable in azimuth and elevation with respect to the particular rational direction of the crystal, the output of the detector being proportional to the intensity of the reflected radiation intercepted by the detector, and the yoke being constructed and arranged to effect precession of both the particular rational direction of the crystal and the detector about the axis of the X-ray beam.
2. An X-ray diffractometer according to claim 1, wherein the yoke comprises a first gimbal fork mounted for pivotal movement about a first axis intersecting the beam at a right angle, a second gimbal fork mounted on the first fork for pivotal movement about a second axis perpendicular to the first axis and passing through the point where the beam intersects the first axis, a drive member mounted for rotation about the axis of the beam, and a pivotal connection between the drive member and the second fork, the axis of the pivotal connection passing through the point at which the first and second axes intersect with the beam.
3. An X-ray diffractometer according toclaim 2, wherein the drive member is arcuate in shape, the center of curvature of the drive member being the point at which the first and second axes intersect the beam.
4. An X-ray diffractometer according toclaim 3, including a drive motor for moving the drive member to preselected angular positions, and an azimuth motor for rotating the detector about the axis of the pivotal connection between the drive member and the second fork.
5. An X-ray diffractometer according to claim 4, including a drum rotatable on the second gimbal yoke about the same axis as the pivotal connection; the detector being mounted eccentrically in the drum and the azimuth motor serving to move the drum to preselected angular positions.
6. An X-ray diffractometer according toclaim 5, wherein the drive motor and the azimuth motor are stepping motors that impart incremental movement to the drive member and the drum respectively.
7. An X-ray diffractometer according toclaim 6, including motor control means for controlling the drive and drum motors in accordance with a computer controlled program.
8. A method for using the X-ray diffractometer according to claim 1, wherein the yoke is operated to cause precession of both the particular rational axis of the crystal and the detector about the beam direction, and the azimuth and elevation of the detector are periodically changed in a manner to cause the detector to map the intensity of the reflected beam.
9. An X-ray diffractometer according to claim 1, wherein the detector is constituted by a counter having an aperture defining means masking the counter and limiting the field of view of the detector for preventing unwanted reflections from reaching the surface.
10. An X-ray diffractometer according toclaim 9, including a drum mounted on the yoke so as to be rotatable about the particular rational direction of the crystal, the counter being eccentrically mounted on the drum so that rotation of he drum changes the aximuth of the detector.
11. An X-ray diffractometer according to claim 1, wherein the axis of the detector is substantially parallel to the particular rational direction of the crystal.
12. An X-ray diffractometer according to claim 1 wherein the axis of the detector passes through the point where the beam intersects the particular rational direction of the crystal.
13. An X-ray diffractometer according to claim 4, wherein the axis of the detector passes through the point at which the first and second axes intersect with the X-ray beam.
14. An X-ray diffractometer according to claim 13 wherein the second gimbal fork includes a first support ring pivotally connected to the first gimbal fork, a second support ring mounted on a first support ring for rotation thereon about the axis of the pivotal connection between the drive member and the second gimbal fork, a curved guide diametrically spanning and rigidly connected to the second support ring for establishing a cylindrical guide surface whose axis of perpendicular to the axis of the pivotal connection between the drive member and the second gimbal fork and passes through the intersection of the first and second axes, the detector being adjustably mounted on the second support ring so that the axis of the detector is perpendicular to the cylindrical guide surface period.
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTKGN vPatent No. 3,728,541 7 D d April 17, 1973 Inventofls) DOV RABINOVICH et a1.
It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
The Assignee should read:
--YEDA Research and'Development Co. Ltd."
instead of "Yale Research and Development Co. Ltd."
Signed and sealed this 26th day of March 1974.
(SEAL) Attest:
EDWARD M.FLETCHER,JR. C. MARSHALL DANN Attesting Officer Commissioner of Patents =ORM P0-1050 10-69 USCOMM-DC 60376-P69 U. 5.GOVERNMENT PRINTING OFFICE 2 i969 0-356-33l

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Cited By (11)

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US3868506A (en)*1973-02-201975-02-25Rigaku Denki Co LtdX-ray diffraction instrument
US4016420A (en)*1975-05-301977-04-05Dekanat Prirodovedecke Fakulty University KarlovyPrecession-type x-ray diffraction camera
US4071758A (en)*1975-08-041978-01-31Max-Planck-Gesellschaft Zur Forderung Der Wissenschafter E.V.Multiple test X-ray goniometer
US4644761A (en)*1984-08-111987-02-24Kernforschungsanlage Julich Gesellschaft Mit Beschrankter HaftungLow-temperature goniometer for X-ray and neutron diffractometry
US4723075A (en)*1985-06-121988-02-02The United States Of America As Represented By The Secretary Of The Air ForceTranslational mount for large optical elements
US6764051B2 (en)*1999-08-182004-07-20Richard KnightMoving yoke
WO2006003430A1 (en)*2004-07-052006-01-12Dage Precision Industries Ltd.X-ray manipulator
US20070291899A1 (en)*2004-11-292007-12-20Lasse SuominenGoniometer
ITVI20100351A1 (en)*2010-12-282012-06-29Fond Bruno Kessler X-RAY DIFFRATTOMETER OF THE PERFECT PORTABLE TYPE
US20140270090A1 (en)*2013-03-152014-09-18Proto Manufacturing Ltd.X-Ray Diffraction Apparatus And Method
EP3112815A1 (en)*2015-07-012017-01-04Microtecnica S.r.l.Sensor mount

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Cited By (20)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3868506A (en)*1973-02-201975-02-25Rigaku Denki Co LtdX-ray diffraction instrument
US4016420A (en)*1975-05-301977-04-05Dekanat Prirodovedecke Fakulty University KarlovyPrecession-type x-ray diffraction camera
US4071758A (en)*1975-08-041978-01-31Max-Planck-Gesellschaft Zur Forderung Der Wissenschafter E.V.Multiple test X-ray goniometer
US4644761A (en)*1984-08-111987-02-24Kernforschungsanlage Julich Gesellschaft Mit Beschrankter HaftungLow-temperature goniometer for X-ray and neutron diffractometry
US4723075A (en)*1985-06-121988-02-02The United States Of America As Represented By The Secretary Of The Air ForceTranslational mount for large optical elements
US6764051B2 (en)*1999-08-182004-07-20Richard KnightMoving yoke
US7497617B2 (en)2004-07-052009-03-03Nordson CorporationX-ray manipulator
JP4886684B2 (en)*2004-07-052012-02-29デイジ プレシジョン インダストリーズ リミテッド X-ray operating device
JP2008505340A (en)*2004-07-052008-02-21デイジ プレシジョン インダストリーズ リミテッド X-ray operating device
US20080232551A1 (en)*2004-07-052008-09-25Benjamin Kingsley Stuart PeecockX-Ray Manipulator
WO2006003430A1 (en)*2004-07-052006-01-12Dage Precision Industries Ltd.X-ray manipulator
CN1985162B (en)*2004-07-052011-03-23达格精度工业有限公司X-ray manipulator
US7646848B2 (en)*2004-11-292010-01-12Stresstech OyGoniometer
US20070291899A1 (en)*2004-11-292007-12-20Lasse SuominenGoniometer
ITVI20100351A1 (en)*2010-12-282012-06-29Fond Bruno Kessler X-RAY DIFFRATTOMETER OF THE PERFECT PORTABLE TYPE
EP2472252A1 (en)*2010-12-282012-07-04Fondazione Bruno KesslerPortable x-ray diffractometer
US20140270090A1 (en)*2013-03-152014-09-18Proto Manufacturing Ltd.X-Ray Diffraction Apparatus And Method
US9613728B2 (en)*2013-03-152017-04-04Proto Manufacturing Ltd.X-ray diffraction apparatus and method
EP3112815A1 (en)*2015-07-012017-01-04Microtecnica S.r.l.Sensor mount
US10557728B2 (en)2015-07-012020-02-11Microtecnica S.R.L.Sensor mount

Also Published As

Publication numberPublication date
IL32247A (en)1972-08-30
FR2048551A5 (en)1971-03-19
DE2023646A1 (en)1970-11-26
GB1307570A (en)1973-02-21
IL32247A0 (en)1969-07-30
CH519171A (en)1972-02-15
NL7007274A (en)1970-11-24

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