X-ray tube anode comprising a coolant tube

Information

  • Patent Grant
  • 9263225
  • Patent Number
    9,263,225
  • Date Filed
    Wednesday, July 15, 2009
    14 years ago
  • Date Issued
    Tuesday, February 16, 2016
    8 years ago
Abstract
An anode for an X-ray tube includes at least one thermally conductive anode segment in contact with a rigid support member and cooling means arranged to cool the anode. The anode may further include a plurality of anode segments aligned end to end, each in contact with the support member.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS

The present application is a national stage application of PCT/GB2009/001760, filed on Jul. 15, 2009. The present application further relies on Great Britain Patent Application Number 0812864.7, filed on Jul. 15, 2008, for priority. Both priority applications are herein incorporated by reference in their entirety.


FIELD OF THE INVENTION

The present invention relates to X-ray tubes and in particular to the cooling of the anode of an X-ray tube.


BACKGROUND OF THE INVENTION

It is well known to provide an X-ray tube comprising an electron source and a metal anode, wherein the anode is at a positive potential with respect to the electron source. The electric field accelerates the emitted electron towards the anode. When they strike the anode they lose some, or all, of their kinetic energy, the majority of which is released as heat. This heat can reduce the target lifetime and it is therefore common to cool the anode. Conventional methods include air cooling, wherein the anode is typically operated at ground potential with heat conduction to ambient through an air cooled heatsink, and a rotating anode, wherein the irradiated point is able to cool as it rotates around before being irradiated once more.


In some circumstances a moving X-ray source is required, which is generated by scanning an electron beam along an arcuate or linear anode. These anodes may extend to a length of several meters and it is generally complex and expensive to fabricate a single piece anode.


SUMMARY OF THE INVENTION

Accordingly, a first aspect of the invention provides an anode for an X-ray tube comprising at least one thermally conductive anode segment in contact with a rigid support member and cooling means arranged to cool the anode.


Preferably, the cooling means comprises a cooling conduit arranged to carry coolant through the anode. This conduit may comprise a coolant tube housed within a cooling channel, which may be defined by the anode segment and the support member.


Preferably, the anode comprises a plurality of anode segments aligned end to end. This enables an anode to be built of a greater length than would easily be achieved using a single piece anode. Each anode segment may be coated with a thin film. The thin film may coat at least an exposed surface of the anode segment and may comprise a target metal. For example, the film may be a film of any one of tungsten, molybdenum, uranium and silver. Application of the metal film onto the surface of the anode may be by any one of sputter coating, electro deposition and chemical deposition. Alternatively, a thin metal foil may be brazed onto the anode segment. The thin film may have a thickness of between 30 microns and 1000 microns, preferably between 50 microns and 500 microns.


Preferably, the anode segments are formed from a material with a high thermal conductivity such as copper. The rigid backbone may preferably be formed from stainless steel. The excellent thermal matching of copper and stainless steel means that large anode segments may be fabricated with little distortion under thermal cycling and with good mechanical stability.


The plurality of anode segments may be bolted onto the rigid backbone. Alternatively, the rigid backbone may be crimped into the anode segments using a mechanical press. Crimping, in particular if used as the sole means of attaching the anode segments to the backbone, reduces the number of mechanical processes required and removes the need for bolts, which introduce the risk of gas being trapped at the base of the bolts.


The integral cooling channel may extend along the length of the backbone and may either be cut into the anode segments or into the backbone. Alternatively, the channel may be formed from aligned grooves cut into both the anode segments and the backbone. A cooling tube may extend along the cooling channel and may contain cooling fluid. Preferably, the tube is an annealed copper tube. The cooling channel may have a square or rectangular cross section or, alternatively, may have a semi-circular or substantially circular cross section. A rounded cooling channel allows better contact between the cooling tube and the anode and therefore provides more efficient cooling.


The cooling fluid may be passed into the anode through an insulated pipe section. The insulated pipe section may comprise two ceramic tubes with brazed end caps, connected at one end to a stainless steel plate. This stainless steel plate may have two ports formed through it, and each of the insulated pipe sections may be aligned with one of the ports. The plate may be mounted into the X-ray tube vacuum housing. The ceramic tubes may be connected to the cooling channel by two right-angle pipe joints and may be embedded within the anode.





BRIEF DECRIPTION OF THE DRAWINGS

An embodiment of the present invention will now be described, by way of example only, with reference to the accompanying drawings in which:



FIG. 1
a is a sectioned perspective view of an anode according to an embodiment of the invention;



FIG. 1
b is a sectioned perspective view of an anode according to a further embodiment of the invention;



FIG. 2 is a section through an anode segment crimped to a backbone according to a further embodiment of the invention;



FIG. 3 is a section through an anode according to a further embodiment of the invention a round-ended cooling channel;



FIG. 4 shows a crimping tool used to crimp an anode segment to a backbone;



FIG. 5 shows a connection arrangement for the coolant tube of the anode of FIG. 1; and



FIG. 6 is a section through a connection arrangement for a coolant tube according to a further embodiment of the invention.





DETAILED DECRIPTION OF THE INVENTION

Referring to FIG. 1a, an anode 1 according to one embodiment of the invention comprises a plurality of thermally conductive anode segments 2 bolted to a rigid single piece support member in the form of a backbone 4 by bolts 6. A cooling channel 8, 10 extends along the length of the anode 1 between the thermally conductive anode segments 2 and the backbone 4 and contains a coolant conduit in the form of a coolant tube 12 arranged to carry the cooling fluid.


The anode segments 2 are formed from a metal such as copper and are held at a high voltage positive electrical potential with respect to an electron source. Each anode segment 2 has an angled front face 14, which is coated with a suitable target metal such as molybdenum, tungsten, silver or uranium selected to produce the required X-rays when electrons are incident upon it. This layer of target metal is applied to the front face 14 using one of a number of methods including sputter coating, electro-deposition, chemical vapour deposition and flame spray coating. Alternatively, a thin metal foil with a thickness of 50-500 microns is brazed onto the copper anode front face 14.


Referring to FIG. 1a, the cooling channel 8 is formed in the front face of the rigid backbone 4 and extends along the length of the anode 1. The cooling channel 8 has a square or rectangular cross-section and contains an annealed copper coolant tube 12, which is in contact with both the copper anode segments 2, the flat rear face of which forms the front side of the cooling channel 8, and the backbone 4. A cooling fluid such as oil is pumped through the coolant tube 12 to remove heat from the anode 1.



FIG. 1
b shows an alternative embodiment in which the cooling channel 10 is cut into the plurality of anode segments 2. The cooling channel 10 has a semi-circular cross section with a flat rear surface of the cooling channel 10 being provided by the backbone 4. The semi-circular cross-section provides better contact between the coolant tube 12 and the anode segments 2, therefore improving the efficiency of heat removal from the anode 1. Alternatively, the cooling channel 10 may comprise two semi-circular recesses in both the backbone 4 and the anode segments 2, forming a cooling channel 10 with a substantially circular cross-section.


The rigid single piece backbone 4 is formed from stainless steel and can be made using mechanically accurate and inexpensive processes such as laser cutting while the smaller copper anode segments 2 are typically fabricated using automated machining processes. The backbone 4 is formed with a flat front face and the anode segments 2 are formed with flat rear faces, which are in contact with and held against the front face of the backbone 4, so as to ensure good thermal contact between them when these flat faces are in contact. Due to the excellent thermal matching of copper and stainless steel and the good vacuum properties of both materials, large anode segments 2 may be fabricated with little distortion under thermal cycling and with good mechanical stability.


The bolts 6 fixing the anode segments 2 onto the backbone 4 pass through bores that extend from a rear face of the backbone, through the backbone 4 to its front face, and into threaded blind bores in the anode segments 2. During the assembly of the anode 1, there is the potential for gas pockets to be trapped around the base of these bolts 6. Small holes or slots may therefore be cut into the backbone 4 or anode 1 to connect these blind bores to the outer surface of the backbone 4 or anode 1, allowing escape of the trapped pockets of gas.


Bolting a number of anode segments 2 onto a single backbone 4, as shown in FIGS. 1a and 1b, enables an anode to be built that extends for several meters. This would otherwise generally be expensive and complicated to achieve.



FIG. 2 shows an alternative design in which a single piece rigid backbone 24 in the form of a flat plate is crimped into the anode segments 22 using a mechanical press. A square cut cooling channel 28 is cut into the back surface of the anode segments 22 and extends along the length of the anode 1, being covered by the backbone 24. Coolant fluid is passed through an annealed copper coolant tube 12, which is located inside the cooling channel 28, to remove heat generated in the anode 1. This design reduces the machining processes required in the anode 1 and also removes the need for bolts 6 and the associated potential trapped gas volumes at the base of the bolts 6.



FIG. 3 shows a similar design of anode 1 to that shown in FIG. 2, wherein a rigid backbone 24 is crimped into anode segments 22. In this embodiment, a cooling channel 30 of curved cross-section, in this case semi-elliptical, extends along the length of the anode 1 and is cut into the anode segments 22 with a round-ended tool. A coolant tube 12 is located inside the cooling channel 30 and is filled with a cooling fluid such as oil. The rounded cooling channel 30 provides superior contact between the coolant tube 12, which is of a rounded shape to fit in the cooling channel 30, and the anode segments 22.


Referring to FIG. 4, the anode 1 of FIGS. 2 and 3 is formed using a crimp tool 32. The coated copper anode segments 22 are supported in a base support 34 with walls 37 projecting upwards from the sides of the rear face of the anode segments 22. The rigid backbone 24 is placed onto the anode segments 22, fitting between the projecting anode walls 37. An upper part 36 of the crimp tool 32 has grooves 38 of a rounded cross section formed in it arranged to bend over and deform the straight copper walls 37 of the anode segments 22 against the rear face of the backbone as it is lowered towards the base support 34, crimping the backbone 24 onto the anode segments 22. Typically a force of about 0.3 - 0.7 tonne/cm length of anode segments 22 is required to complete the crimping process. As a result of the crimping process the crimped edges of the anode segments 22 form a continuous rounded ridge along each side of the backbone 24. It will be appreciated that other crimping arrangements could be used, for example the anode segments 22 could be crimped into grooves in the sides of the backbone 24, or the backbone 24 could be crimped into engagement with the anode 1.


In use, the anode segments 22 are held at a relatively high electrical potential. Any sharp points on the anode 1 can therefore lead to a localised high build up of electrostatic charge and result in electrostatic discharge. Crimping the straight copper walls 37 of the anode segments 22 around the backbone 24 provides the anode segments 22 with rounded edges and avoids the need for fasteners such as bolts 6. This helps to ensure an even distribution of charge over the anode 1 and reduces the likelihood of electrostatic discharge from the anode 1.


To pass the coolant fluid into the anode 1 it is often necessary to use an electrically insulated pipe section, or assembly, 500, since the anode 1 is often operated at positive high voltage with respect to ground potential. Non-conducting, in this case ceramic breaks, 40 may be used to provide an electrically isolated connection between the coolant tubes 12 and an external supply of coolant fluid. The coolant fluid is pumped through the ceramic tubes into the coolant tube 12, removing the heat generated as X-rays are produced. FIG. 5 shows an insulated pipe section comprising two ceramic breaks 40 (ceramic tubes with brazed end caps) welded at a first end to a stainless steel plate 42. The plate 42 has ports 43 formed through it, and the end of each of the ceramic breaks 40 is located over a respective one of these ports 43. The stainless steel plate 42 is then mounted into the X-ray tube vacuum housing. Two right-angle pipe sections 44 are each welded at one end to a second end of one of the ceramic breaks 40. The other ends of the right-angle pipe sections 44 are then brazed to the coolant tube 12, which extends along the cooling channel 8, 10 of the anode 1. A localized heating method is used such as induction brazing using a copper collar 46 around the coolant tube 12 and right angle pipe sections 44. Threaded connectors 48 are screwed into the ports 43, which are threaded towards their outer ends. These threaded connectors 48 on the external side of the stainless steel plate 42 attach the insulated pipe section 500 to external coolant circuits. These threaded connectors 48 may be welded to the assembly 500 or screwed in using O-ring seals 47, for example.


In order to maximize the electrostatic performance of the anode 1, it is advantageous to embed the high voltage right-angle pipe sections 44 of the coolant assembly, such as those shown in FIG. 5, within the anode 1 itself. Following connection of the insulated pipe section 500 to the coolant tube 12 it may not be possible to crimp the backbone 24 in the anode segments 22, as shown in FIGS. 2 and 3. In this case, a mechanical fixing such as the bolts 6 shown in FIGS. 1a and 1b are used.


Alternatively, the pipe section can be connected to a crimped anode such as those shown in FIGS. 2 and 3 from outside of the anode 1. Referring to FIG. 6, a gap 25 is cut into the rigid backbone 24. The right angle pipe sections 44 extend through the gap 25 in the rigid backbone 24 and are brazed at one end onto the coolant tube 12. On the external side of the rigid backbone 24 the right angle pipe sections 44 are welded onto ceramic breaks 40, which are connected to external cooling circuits, for example as in FIG. 5.

Claims
  • 1. An anode for an X-ray tube prepared by a process comprising the steps of: obtaining at least one thermally conductive anode segment having a top surface and having a first side wall extending out from, and longitudinally along, the top surface and a second side wall opposing the first side wall and extending out from, and longitudinally along, the top surface wherein the at least one thermally conductive anode segment comprises a plurality of thermally conductive anode segments aligned end to end;placing a rigid support member on the top surface of the at least one thermally conductive anode segment and between the first side wall and the second side wall, wherein each anode segment of the plurality of thermally conductive anode segments is in contact with the rigid support member;securing the rigid support member to the at least one thermally conductive anode segment between the first side wall and the second side wall; andarranging a coolant tube between the rigid support member and the at least one thermally conductive anode segment to cool the at least one thermally conductive anode segment.
  • 2. An anode according to claim 1, wherein the coolant tube comprises a cooling conduit arranged to carry coolant through the at least one thermally conductive anode segment.
  • 3. An anode according to claim 2, wherein the cooling conduit is at least partially cut into the at least one thermally conductive anode segment.
  • 4. An anode according to claim 2, wherein the cooling conduit is at least partially cut into the rigid support member.
  • 5. An anode according to claim 2, wherein the cooling conduit has a curved cross-section.
  • 6. An anode according to claim 2, wherein the coolant tube is an annealed copper tube.
  • 7. An anode according to claim 1, wherein each anode segment of said plurality of thermally conductive anode segments is coated with a target metal.
  • 8. An anode according to claim 7, wherein the target metal is applied as a thin film.
  • 9. An anode according to claim 7, wherein the target metal is a metal foil.
  • 10. An anode according to claim 9, wherein the metal foil has a thickness of between 50 microns and 500 microns.
  • 11. An anode according to claim 7, wherein the target metal is applied to a front face of each anode segment of said plurality of thermally conductive anode segments.
  • 12. An anode according to claim 7, wherein the target metal comprises at least one of tungsten, molybdenum, uranium and silver.
  • 13. An anode according claim 1 , wherein each anode segment of said plurality of thermally conductive anode segments is made of copper.
  • 14. An anode according to claim 1, wherein the rigid support member is made of stainless steel.
  • 15. An anode according to claim 1, further comprising arranging an insulated pipe section to feed cooling fluid into the coolant tube.
  • 16. An anode according to claim 15, wherein the insulated pipe section comprises a ceramic tube connected to the coolant tube; anda connector plate attached to one end of said ceramic tube.
Priority Claims (1)
Number Date Country Kind
0812864.7 Jul 2008 GB national
PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/GB2009/001760 7/15/2009 WO 00 10/5/2011
Publishing Document Publishing Date Country Kind
WO2010/007375 1/21/2010 WO A
US Referenced Citations (209)
Number Name Date Kind
2101143 Laidig Dec 1937 A
2333525 Cox Nov 1943 A
2842694 Hosemann Jul 1958 A
2952790 Steen Sep 1960 A
3138729 Henke Jun 1964 A
3239706 Farrell Mar 1966 A
3768645 Conway Oct 1973 A
3867637 Braun et al. Feb 1975 A
4045672 Watanabe Aug 1977 A
4057725 Wagner Nov 1977 A
4064411 Iwasaki et al. Dec 1977 A
4105922 Lambert Aug 1978 A
4165472 Wittry Aug 1979 A
4171254 Koenecke Oct 1979 A
4228353 Johnson Oct 1980 A
4238706 Yoshihara et al. Dec 1980 A
4241404 Lux Dec 1980 A
4259721 Kuznia Mar 1981 A
4266425 Allport May 1981 A
4274005 Yamamura Jun 1981 A
4309637 Fetter Jan 1982 A
4340816 Schott Jul 1982 A
4344011 Hayashi Aug 1982 A
4352021 Boyd Sep 1982 A
4352196 Gabbay Sep 1982 A
4405876 Iversen Sep 1983 A
4420382 Riedl Dec 1983 A
4461020 Hubner et al. Jul 1984 A
4468802 Friedel Aug 1984 A
4531226 Peschmann Jul 1985 A
4622687 Whitaker et al. Nov 1986 A
4625324 Blaskis Nov 1986 A
4670895 Penato et al. Jun 1987 A
4672649 Rutt Jun 1987 A
4675890 Plessis Jun 1987 A
4677651 Hartl Jun 1987 A
4719645 Yamabe et al. Jan 1988 A
4736400 Koller et al. Apr 1988 A
4763345 Barbaric Aug 1988 A
RE32961 Wagner Jun 1989 E
4866745 Akai Sep 1989 A
4868856 Frith Sep 1989 A
4887604 Shefer Dec 1989 A
4894775 Kritchman Jan 1990 A
4928296 Kadambi May 1990 A
4945562 Staub Jul 1990 A
4991194 Laurent et al. Feb 1991 A
5018181 Iversen et al. May 1991 A
5033106 Kita Jul 1991 A
5056127 Iversen et al. Oct 1991 A
5065418 Bermbach Nov 1991 A
5068882 Eberhard Nov 1991 A
5073910 Eberhard Dec 1991 A
5091924 Bermbach Feb 1992 A
5091927 Golitzer Feb 1992 A
5159234 Wegmann Oct 1992 A
5191600 Vincent Mar 1993 A
5195112 Vincent Mar 1993 A
5247556 Eckert Sep 1993 A
5259014 Brettschneider Nov 1993 A
5268955 Burke Dec 1993 A
5272627 Maschhoff Dec 1993 A
5305363 Burke Apr 1994 A
5313511 Annis May 1994 A
5329180 Popli Jul 1994 A
5367552 Peschmann Nov 1994 A
5375156 Kuo-Petravic Dec 1994 A
5414622 Walters May 1995 A
5467377 Dawson Nov 1995 A
5511104 Mueller Apr 1996 A
5515414 d'Achard Van Enschut et al. May 1996 A
5541975 Anderson Jul 1996 A
5568829 Crawford Oct 1996 A
5596621 Schwarz Jan 1997 A
5600700 Krug Feb 1997 A
5604778 Polacin Feb 1997 A
5633907 Gravelle May 1997 A
5654995 Flohr Aug 1997 A
5680432 Voss Oct 1997 A
5689541 Schardt Nov 1997 A
5712889 Lanzara Jan 1998 A
5798972 Lao Aug 1998 A
5841831 Hell Nov 1998 A
5859891 Hibbard Jan 1999 A
5879807 Inoue Mar 1999 A
5889833 Silver Mar 1999 A
5907593 Hsieh May 1999 A
5966422 Dafni Oct 1999 A
5974111 Krug Oct 1999 A
5987097 Salasoo Nov 1999 A
6014419 Hu Jan 2000 A
6018562 Willson Jan 2000 A
6075836 Ning Jun 2000 A
6088426 Miller Jul 2000 A
6108575 Besson Aug 2000 A
6122343 Pidcock Sep 2000 A
6130502 Kobayashi Oct 2000 A
6181765 Sribar Jan 2001 B1
6183139 Solomon Feb 2001 B1
6188747 Geus Feb 2001 B1
6218943 Ellenbogen Apr 2001 B1
6229870 Morgan May 2001 B1
6236709 Perry May 2001 B1
6240157 Danielsson May 2001 B1
6269142 Smith Jul 2001 B1
6298110 Ning Oct 2001 B1
6324243 Edic Nov 2001 B1
6324249 Fazzio Nov 2001 B1
6341154 Besson Jan 2002 B1
6404230 Cairns Jun 2002 B1
6430260 Snyder Aug 2002 B1
6449331 Nutt Sep 2002 B1
6470065 Lauther Oct 2002 B1
6480571 Andrews Nov 2002 B1
6546072 Chalmers Apr 2003 B1
6553096 Zhou Apr 2003 B1
6556653 Chalmers Apr 2003 B2
6580780 Miller Jun 2003 B1
6624425 Nisius Sep 2003 B2
6674838 Barrett Jan 2004 B1
6721387 Naidu Apr 2004 B1
6751293 Barrett Jun 2004 B1
6760407 Price et al. Jul 2004 B2
6785359 Lemaitre Aug 2004 B2
6819742 Miller Nov 2004 B1
6975703 Wilson et al. Dec 2005 B2
6993115 McGuire et al. Jan 2006 B2
7079624 Miller Jul 2006 B1
7184520 Sano Feb 2007 B1
7192031 Ying Mar 2007 B2
7197116 Dunham Mar 2007 B2
7203269 Huber Apr 2007 B2
7203282 Brauss Apr 2007 B2
7218700 Huber et al. May 2007 B2
7233644 Bendahan Jun 2007 B1
7248673 Miller Jul 2007 B2
7349525 Morton et al. Mar 2008 B2
7466799 Miller Dec 2008 B2
7508916 Frontera Mar 2009 B2
7664230 Morton Feb 2010 B2
7697665 Yonezawa Apr 2010 B2
7728397 Gorrell Jun 2010 B2
7738632 Popescu Jun 2010 B2
8094784 Morton Jan 2012 B2
8243876 Morton Aug 2012 B2
8331535 Morton Dec 2012 B2
8654924 Behling Feb 2014 B2
20010033635 Kuwabara Oct 2001 A1
20020031202 Callerame Mar 2002 A1
20020082492 Grzeszczuk Jun 2002 A1
20020094064 Zhou Jul 2002 A1
20020097836 Grodzins Jul 2002 A1
20020140336 Stoner Oct 2002 A1
20020176531 McClelland Nov 2002 A1
20030021377 Turner et al. Jan 2003 A1
20030031352 Turner Jan 2003 A1
20030043957 Pelc Mar 2003 A1
20030048868 Bailey Mar 2003 A1
20030076921 Mihara Apr 2003 A1
20030076924 Mario Apr 2003 A1
20030091148 Bittner May 2003 A1
20040120454 Seppi Jan 2004 A1
20040022292 Morton Feb 2004 A1
20040057554 Bjorkholm Mar 2004 A1
20040066879 Machida Apr 2004 A1
20040094064 Taguchi May 2004 A1
20040202282 Miller Oct 2004 A1
20040213378 Zhou et al. Oct 2004 A1
20040252807 Skatter Dec 2004 A1
20040258305 Burnham Dec 2004 A1
20050002492 Rother Jan 2005 A1
20050031075 Hopkins Feb 2005 A1
20050053189 Gohno Mar 2005 A1
20050058242 Peschmann Mar 2005 A1
20050100135 Lowman May 2005 A1
20050105682 Heumann May 2005 A1
20050111610 Heumann May 2005 A1
20050123092 Mistretta Jun 2005 A1
20050157925 Lorenz Jul 2005 A1
20050175151 Dunham Aug 2005 A1
20050276377 Carol Dec 2005 A1
20050276382 Lesiak Dec 2005 A1
20060050842 Wang Mar 2006 A1
20060233297 Ishiyama Oct 2006 A1
20070053495 Seppi Jan 2007 A1
20070064873 Gabioud Mar 2007 A1
20070172023 Morton Jul 2007 A1
20070183575 Lemaitre Aug 2007 A1
20070297570 Kerpershoek Dec 2007 A1
20080019483 Andrews Jan 2008 A1
20080043920 Liu Feb 2008 A1
20080056436 Pack Mar 2008 A1
20080056437 Pack Mar 2008 A1
20080112540 Rogers May 2008 A1
20080123803 DeMan May 2008 A1
20080130974 Xu Jun 2008 A1
20090022264 Zhou Jan 2009 A1
20090097836 Tanaka Apr 2009 A1
20090159451 Tomantschger Jun 2009 A1
20090185660 Zou Jul 2009 A1
20100046716 Freudenberger Feb 2010 A1
20010022346 Morton Mar 2010 A1
20100111265 Holm May 2010 A1
20100246754 Morton Sep 2010 A1
20100316192 Hauttmann Dec 2010 A1
20110188725 Yu Aug 2011 A1
20110222662 Behling Sep 2011 A1
20130156161 Andrews Jun 2013 A1
20130195253 Andrews Aug 2013 A1
Foreign Referenced Citations (121)
Number Date Country
1138743 Dec 1996 CN
1172952 Feb 1998 CN
1194718 Sep 1998 CN
1795527 Jun 2006 CN
2729353 Jan 1979 DE
3638378 May 1988 DE
3840398 Jun 1989 DE
4432205 Jan 1996 DE
4425691 Feb 1996 DE
19745998 Mar 1999 DE
10036210 Nov 2001 DE
10319547 Nov 2004 DE
10319549 Dec 2004 DE
0142249 May 1985 EP
0432568 Jun 1991 EP
03198975 Aug 1991 EP
0531993 Mar 1993 EP
05135721 Jun 1993 EP
05182617 Jul 1993 EP
05290768 Nov 1993 EP
0584871 Mar 1994 EP
0924742 Jun 1999 EP
0930046 Jul 1999 EP
1277439 Jan 2003 EP
1374776 Jan 2004 EP
1558142 Aug 2005 EP
2328280 May 1977 FR
2675629 Oct 1992 FR
1149796 Apr 1969 GB
1272498 Apr 1972 GB
1497396 Jan 1978 GB
1526041 Sep 1978 GB
2015245 Sep 1979 GB
2089109 Jun 1982 GB
2212903 Aug 1989 GB
2212975 Aug 1989 GB
2360405 Sep 2001 GB
2418529 Mar 2006 GB
50081080 Jul 1975 JP
S51055286 May 1976 JP
S51078696 Jul 1976 JP
S52050186 Apr 1977 JP
S52124890 Oct 1977 JP
5493993 Jul 1979 JP
S55046408 Apr 1980 JP
56086448 Jul 1981 JP
S56167464 Dec 1981 JP
5717524 Jan 1982 JP
S57110854 Jul 1982 JP
570175247 Oct 1982 JP
S57175247 Oct 1982 JP
58212045 Dec 1983 JP
590016254 Jan 1984 JP
S591625 Jan 1984 JP
S5916254 Jan 1984 JP
59075549 Apr 1984 JP
S5975549 Apr 1984 JP
600015546 Jan 1985 JP
S601554 Jan 1985 JP
S602144 Jan 1985 JP
600021440 Feb 1985 JP
S6038957 Feb 1985 JP
S60181851 Dec 1985 JP
61107642 May 1986 JP
62044940 Feb 1987 JP
S62121773 Aug 1987 JP
63016535 Jan 1988 JP
1296544 Nov 1989 JP
3198975 Aug 1991 JP
H0479128 Mar 1992 JP
H04319237 Nov 1992 JP
5135721 Jun 1993 JP
5182617 Jul 1993 JP
5290768 Nov 1993 JP
060038957 Feb 1994 JP
H0638957 Feb 1994 JP
06162974 Jun 1994 JP
H06261895 Sep 1994 JP
H07093525 Apr 1995 JP
H09171788 Jun 1997 JP
H10211196 Aug 1998 JP
H10272128 Oct 1998 JP
H11500229 Jan 1999 JP
H11273597 Oct 1999 JP
2000175895 Jun 2000 JP
2001023557 Jan 2001 JP
2001502473 Feb 2001 JP
2001176408 Jun 2001 JP
2001204723 Jul 2001 JP
2002343291 Nov 2002 JP
2003092076 Mar 2003 JP
2003121392 Apr 2003 JP
2003126075 May 2003 JP
2003257347 Sep 2003 JP
2004000605 Jan 2004 JP
2004079128 Mar 2004 JP
2004311245 Nov 2004 JP
2005013768 Jan 2005 JP
2006128137 May 2006 JP
2006351272 Dec 2006 JP
2007265981 Oct 2007 JP
2008166059 Jul 2008 JP
100211196 Sep 2010 JP
1022236 Jun 1983 SU
9528715 Oct 1995 WO
9718462 May 1997 WO
9960387 Nov 1999 WO
0231857 Apr 2002 WO
03051201 Jun 2003 WO
2004010127 Jan 2004 WO
2004042769 May 2004 WO
2004097386 Nov 2004 WO
2004097889 Nov 2004 WO
WO 2004097888 Nov 2004 WO
2006130630 Dec 2006 WO
2007068933 Jun 2007 WO
2008068691 Jun 2008 WO
2009012453 Jan 2009 WO
2010007375 Jan 2010 WO
2010086653 Aug 2010 WO
2010141659 Dec 2010 WO
Non-Patent Literature Citations (22)
Entry
US 5,987,079, 11/1999, Scott (withdrawn)
Search Report PCT/GB2009/001760, Jan. 21, 2010, Morton et al.
International Search Report, PCT/GB2004/001729, Aug. 12, 2004, Rapiscan Systems, Inc.
International Search Report, PCT/GB2004/001732, Feb. 25, 2005.
International Search Report for PCT/US2010/037167, Sep. 7, 2010.
Office Action dated Oct. 21, 2014 for U.S. Appl. No. 13/674,086.
Second office action for Japanese Application No. JP2012-514109 mailed on Oct. 20, 2014.
International Search Report, PCT/US2010/41871, Jan. 20, 2011, Rapiscan Systems, Inc.
Notice of Allowance dated Jan. 30, 2015 for U.S. Appl. No. 13/405,117.
Bruder et al. “Efficient Extended Field of View (eFOV) Reconstructuion Techniques for Multi-Slice Helical CT”, Medical Imaging 2008: Physics of Medical Imaging, edited by Jiang Hsieh, Ehsan Samei, Proc. of SPIE vol. 6913, 69132E, (2008).
Chinese Patent Application No. 200980114807.X, Second Office Action, Nov. 21, 2013.
Great Britain Patent Application No. GB0816823.9, Search Report, Oct. 20, 2009.
Great Britain Patent Application No. GB1104148.0, Examination Report, Mar. 29, 2011.
International Search Report, PCT/GB2004/001741, Mar. 3, 2005.
International Search Report, PCT/GB2004/001731, May 27, 2005.
International Search Report, PCT/GB2004/001751, Mar. 21, 2005.
STMicroelectronics, “Dual Full-Bridge Driver”, Datasheet for L298, 2000, pp. 1-13, XP002593095.
Notice of Allowance dated Dec. 4, 2014 for U.S. Appl. No. 13/313,854.
Office Action dated Nov. 26, 2014 for U.S. Appl. No. 13/146,645.
Supplementary European Search Report, EP10784058, Dec. 6, 2013.
European Search Opinion, EP10784058, Dec. 18, 2013.
International Search Report, PCT/GB2004/001747, Aug. 10, 2004.
Related Publications (1)
Number Date Country
20120014510 A1 Jan 2012 US