ROTATING ANODE AND METHOD FOR PRODUCING A ROTATING ANODE
20170169985 ยท 2017-06-15
Assignee
Inventors
- Peter Klaus Bachmann (Berlin-Kaulsdorf, DE)
- Hans Joachim Meys (Alsdorf, DE)
- Gereon VOGTMEIER (Aachen, DE)
- Christoph Tobias Wirth (Vellmar, DE)
Cpc classification
H01J35/10
ELECTRICITY
H01J35/105
ELECTRICITY
International classification
Abstract
The present invention relates to a rotating anode (100) comprising: an outer ring compound (6) comprising a first carbon material with a first material property and carbon fibres substantially aligned to a contour of the outer ring compound (6), wherein the outer ring compound (6) is configured to mechanically stabilize the rotating anode (100); an intermediate ring compound (5) comprising a second carbon material with a second material property differing from the first material property; a inner disc compound (2) comprising a layered fibre structure and a third carbon material with a third material property differing from the first and the second material property, wherein the inner disc compound (2) and the intermediate ring compound (5) are configured to provide a thermally conductive interface between the intermediate ring compound (5) and the inner disc compound (2); and an interface compound (3) comprising a metallic or a semi-metallic material, wherein the interface compound is coupled to the intermediate ring compound (5) and the inner disc compound (2).
Claims
1. A rotating anode comprising: an outer ring compound comprising a first carbon material with a first material property and carbon fibres substantially aligned to a contour of the outer ring compound, wherein the outer ring compound is configured to mechanically stabilize the rotating anode; an intermediate ring compound comprising a second carbon material with a second material property differing from the first material property; an inner disc compound comprising a layered fibre structure and a third carbon material with a third material property differing from the first and the second material property, wherein the inner disc compound and the intermediate ring compound are configured to provide a thermally conductive interface between the intermediate ring compound and the inner disc compound; and an interface compound comprising a metallic or a semi-metallic material, wherein the interface compound is coupled to the intermediate ring compound and the inner disc compound.
2. The rotating anode according to claim 1, wherein the intermediate ring compound comprises as the second carbon material graphitic carbon.
3. The rotating anode according to claim 1, wherein the interface compound comprises as the metallic or semi-metallic material from the group comprising Titanium, Vanadium, Chromium, Manganese, Iron, Cobalt, Nickel, Copper, Zinc, Aluminium, Silicon, Zirconium, Niobium, Molybdenum, Palladium, Silver, Indium, Tin, Platinum or Gold.
4. The rotating anode according to claim 1, wherein the interface compound comprises as the metallic or semi-metallic material a mixture or an alloy from the group comprising Titanium, Vanadium, Chromium, Manganese, Iron, Cobalt, Nickel, Copper, Zinc, Aluminium, Silicon, Zirconium, Niobium, Molybdenum, Palladium, Silver, Indium, Tin, Platinum or Gold.
5. The rotating anode according to claim 3, wherein the interface compound comprises a melting or liquidus temperature above 1000 C.
6. The rotating anode according to claim 1, wherein the inner disc compound and the intermediate ring compound are configured to transport heat from the intermediate ring compound via the inner disc compound to an inner contour of the inner disc compound.
7. The rotating anode according to claim 6, wherein the outer ring compound is configured to limit thermal expansions of the rotating anode or to limit centrifugal forces or to limit other mechanical forces.
8. The rotating anode according to claim 7, wherein the intermediate ring compound comprises a metallic coating on a lateral side of the intermediate ring compound.
9. The rotating anode according to claim 7, wherein the intermediate ring compound is configured to transport heat from the intermediate ring compound to a surface of the rotating anode.
10. The rotating anode according to claim 1, wherein the inner disc compound comprises as the layered fibre structure a textile layer structure with a first preferred direction of fibre orientation and a second preferred direction of fibre orientation.
11. The rotating anode according to claim 10, wherein a first type of fibres is aligned along the first preferred direction and a second type of fibres is aligned along the second preferred direction.
12. The rotating anode according to claim 11, wherein the fibres of the first type are configured to mechanically stabilize the inner disc compound and the fibres of the second type are configured to provide thermal conductivity.
13. The rotating anode according to claim 1, wherein the outer ring compound is configured to limit a thermal expansion of the inner disc compound and the intermediate ring compound.
14. X-ray tube comprising a high voltage generator, a cathode, and a rotating anode according to claim 1.
15. Method for producing a rotating anode, the method comprising the steps of: Providing an outer ring compound comprising a first carbon material with a first material property and carbon fibres substantially aligned to a contour of the outer ring compound, wherein the outer ring compound is configured to mechanically stabilize the rotating anode; Providing an intermediate ring compound comprising a second carbon material with a second material property differing from the first material property and providing an inner disc compound comprising a layered fibre structure and a third carbon material with a third material property differing from the first and the second material property, wherein the inner disc compound and the intermediate ring compound are configured to provide a thermally conductive interface between the intermediate ring compound and the inner disc compound; and Providing an interface compound comprising a metallic or a semi-metallic material, wherein the interface compound is coupled to the intermediate ring compound and the inner disc compound.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0031] A more complete appreciation of the invention and the attendant advantages thereof will be more clearly understood by reference to the following schematic drawings, which are not to scale, wherein:
[0032]
[0033]
[0034]
[0035]
[0036]
DETAILED DESCRIPTION OF EMBODIMENTS
[0037] The illustration in the drawings is purely schematic and does not intend to provide scaling relations or size information. In different drawings or Figs, similar or identical elements are provided with the same reference numerals. Generally, identical parts, units, entities or steps are provided with the same reference symbols in the description.
[0038]
[0039]
[0040] According to an exemplary embodiment of the present invention, the at least two different ring compounds, for instance the outer ring compound and the inner disc compound, comprise substantially a rotational symmetric shape, for instance they comprise the shape of rings or disks. Substantially rotationally symmetric as used by the present invention means for instance that the outer ring compound and/or the inner disc compound and/or the interface compound comprise a rotating unbalance as an uneven distribution of mass around an axis of rotation of less than a mass eccentricity of less than 8 mm.
[0041] The substantially rotationally symmetry advantageously allows that the mass of the rotating anode is evenly distributed about an axis of rotation. This advantageously allows that moments are prevented which give the rotating anode a wobbling movement characteristic or any other kind of vibration of rotating structures.
[0042] According to an exemplary embodiment of the present invention, a rotating anode 100 may comprise an outer ring compound 6, an intermediate ring compound 5, an inner disc compound 2, and an interface compound 3.
[0043] An outer ring compound 1 may be formed by the outer ring compound 6 and an intermediate ring compound 5.
[0044] The outer ring compound 6 may comprise a first carbon material with a first material property and carbon fibres substantially aligned to a contour of the outer ring compound 6, wherein the outer ring compound 6 may be configured to mechanically stabilize the rotating anode 100, or in other words, to mechanically stabilize the intermediate ring compound 5, the inner disc compound 2, and the interface compound 3.
[0045] The intermediate ring compound 5 may comprise a second carbon material with a second material property differing from the first material property, wherein the intermediate ring compound 5 is configured to provide a thermally conductive interface between the outer ring compound 6 and a inner disc compound 2.
[0046] The inner disc compound 2 may comprise a layered fibre structure and a third carbon material with a third material property differing from the first and the second material property. The outer ring compound 6, the intermediate ring compound 5, and the inner disc compound 2 may comprise carbon materials, graphitic carbon materials or carbon composite materials.
[0047] The carbon composite materials may also be named carbon fiber-reinforced carbon (abbreviated C/C or CFRC) or reinforced carbon-carbon (RCC) or carbon fiber carbon matrix composite (CFC). The graphitic carbon materials may also be named graphite. Carbon fibre-reinforced carbon (in the following the abbreviation C/C is used) is a composite material comprising carbon fibre reinforcement in a matrix of graphitic carbon or graphite. The graphitic carbon and carbon composite materials may comprise amorphous carbon.
[0048] The carbon materials of the outer ring compound 6, the intermediate ring compound 5, and the inner disc compound 2 may be all differing carbon materials or may be at least partially, for instance, two out of three, differing materials or maybe the same carbon materials.
[0049] According to an exemplary embodiment of the present invention, the inner disc compound may comprise as the layered fiber structure a textile layer structure with a first preferred direction of fiber orientation and a second preferred direction of fiber orientation.
[0050] A first type of fibers may be aligned along the first preferred direction and a second type of fibers may be aligned along the second preferred direction, wherein the fibers of the first type are configured to mechanically stabilize the inner disc compound 2 and the fibers of the second type are configured to provide thermal conductivity.
[0051] The first direction may be substantially radial or tangential with respect to an outer contour of the rotating anode. A filling material may be used, for instance a C/C material. The properties of the C/C material can be tuned by selecting various types of fiber, adjusting fiber volume content, defining fiber orientation, assembly of various layers, and selection of infiltrating filler material. This advantageously provides a rotating anode with advantages like a high specific heat capacity, excellent high-temperature friction, and excellent wear characteristics. The fibers may be woven or laid.
[0052] The outer ring compound 1 may comprise a C/C material.
[0053] An interface compound 3 may comprise a metallic or semi-metallic material and the interface compound may be configured to connect the outer ring compound and the inner disc compound. The interface compound 3 may form a metallic interface between the at least two different forms of carbonthe outer ring compound 1 and the inner disc compound 2forming the rotating anode of the X-ray tube and the interface compound 3 may have a melting or liquidus temperature of 1000 C. or higher.
[0054] The interface compound 3 may comprise the metallic or semi-metallic material like, for instance, Titanium, Vanadium, Chromium, Manganese, Iron, Cobalt, Nickel, Copper, Zinc, Aluminium, Silicon, Zirconium, Niobium, Molybdenum, Palladium, Silver, Indium, Tin, Platinum or Gold or any mixture or any alloy of these materials.
[0055] The carbon fibre-reinforced carbon (C/C) outer ring or the outer ring compound 1 may be used for an increased mechanical stability of the rotating anode.
[0056] The intermediate ring compound 5 of the outer ring compound 1 may provide a highercompared to the other carbon materialsthermal conductivity. The intermediate ring compound 5 may be configured to accept a coating on top, wherein the coating is suitable as X-ray generating focal track for the impinging electron beam inside an X-ray tube.
[0057] The inner disc compound 2 may be fabricated from carbon fibre-reinforced carbon disk materials. The inner disc compound may comprise a central hole or any other central recess, which is configured to connect the rotating anode to a drive motor.
[0058] The interface compound 3 may be fabricated as a ring-shaped metallic interface composed of for instance, 15% nickel, 5% chromium, 80% iron, forming an alloy or metallic compound with a liquidus temperature of more than 1300 C.
[0059] As the metallic coating on a top side 5a of the intermediate ring compound 5 for instance wolfram or rhenium may be used as materials tracking the impinging electron beam.
[0060]
[0061] In step 1 of the method for producing a rotating anode, the outer C/C ring and the graphite ring are mechanically pressed into each other.
[0062] In step 2, a metallic composite of approximately 15% nickel, approximately 5% chromium, approximately 80% Iron is put onto the innermost surface of the graphite ring. Approximately as used by the present invention may refer to a relative deviation of less than 10%.
[0063] In step 3, a centrally positioned layered C/C disk is pressed with a well-defined mechanical force into the outer structure or outer ring compound 1, in this step a forming press, commonly shortened to press, may be used which is a machine tool that changes the shape of a work piece by the application of pressure, as shown in the Fig.
[0064] In step 4, the rotating anode as assembled and previous to any heating treatment is shown.
[0065] In step 5, the rotating anode is heated to, for instance, more than 1300 C. to facilitate the joining. The heating may be performed in a vacuum oven or in oven purged by a chemical inert or inactive, protective gas atmosphere, e.g. a gas atmosphere which does not undergo chemical reactions with the rotating anode under a set of given conditions, in step 5 a oven may be used to provide the heating, as shown in the Fig.
[0066] In step 6, after cooling down to room temperature, the multi-carbon-material-based anode may be dismounted. The individual carbon-compounds of different heights that make up the anode may be machined and shaped to arrive at a uniform smooth surface with a desired shape. Height differences may be in the range of 1 mm to 7 mm, or 0.5 mm to 4 mm, for instance.
[0067] In step 7, the multi-carbon composite anode may be transferred to a suitable unit that allows depositing a metallic focal track onto at least the graphite ring of the multi-carbon composite anode.
[0068] In step 8, chemical vapour deposition or physical vapour deposition processes, for instance plasma spray methodologies or plasma CVD methods are used to deposit a metallic focal track at elevated or non elevated temperatures onto the multi-carbon composite anode to arrive at a rotating anode.
[0069] A post-processing may comprise further steps like grinding, polishing or cleaning which may be performed to generate a surface finishing of the rotating anode.
[0070] The method for producing a rotating anode may comprise the following steps:
[0071] As a first step of the method, providing S1 an outer ring compound 6 comprising a first carbon material with a first material property and carbon fibres substantially aligned to a contour of the outer ring compound 6 may be performed, wherein the outer ring compound 6 is configured to mechanically stabilize the rotating anode 100.
[0072] As a second step of the method, providing S2 an intermediate ring compound 5 may be performed, the intermediate ring compound 5 comprising a second carbon material with a second material property differing from the first material property and providing the inner disc compound 2 comprising a layered fibre structure and a third carbon material with a third material property differing from the first and the second material property, wherein the inner disc compound 2 and the intermediate ring compound 5 are configured to provide a thermally conductive interface between the intermediate ring compound 5 and the inner disc compound 2.
[0073] As a third step of the method, providing S3 an interface compound 3 comprising a metallic or a semi-metallic material may be performed, wherein the interface compound is coupled to the intermediate ring compound 5 and the inner disc compound 2.
[0074] The interface compound 3 may comprise a metallic or semi-metallic material, wherein the interface compound 3 is coupled to the outer ring compound 1 and the inner disc compound 2.
[0075] Further, an assembling of the rotating anode may be conducted, wherein the rotating anode is assembled.
[0076]
[0077] In step S11 heating the outer C/C ring and the graphite ring and mechanically pressing the C/C ring and the graphite ring into each other may be performed.
[0078] In step S12, putting a metallic layer composed of nickel, chromium, iron or other metals onto the innermost surface of the graphite ring may be conducted.
[0079] In step S13, a centrally positioned layer C/C disk may be pressed with a well-defined mechanical force into the outer structure composed of outer C/C ring, graphite ring and metallic layer.
[0080] In step S14, the rotating anode may be assembled and prepared for a subsequent heating process. For instance, the rotating anode may be clean by solvents or purged with nitrogen gas.
[0081] In step S15, the anode may be heated up to 1300 C. to facilitate joining. The heating process may be performed in a vacuum oven.
[0082] In step S16, After cooling down to room temperature, the multi C-based anode may be dismounted. The individual C-components of different heights that make up the anode are machined and shaped to arrive at a uniform smooth surface with a desired shape (e.g. flat or curved).
[0083] In step S17, the multi C-anode may be transferred to a suitable unit that allows depositing a metallic focal track, forming the metallic coating on a top side 5a, onto at least the graphite ring of the multi-C-anode.
[0084] In step S18, a CVD or PVD processes may be performed, e.g. plasma spray methodologies or plasma CVD methods may be used to deposit the metallic focal track, forming the metallic coating on a top side 5a, at elevated temperatures onto the multi-C-anode to arrive at the product shown in the center of this picture. Additional steps like grinding, polishing etc. are sometimes performed to generate a surface finish of the e-beam focal track suitable for X-ray generation.
[0085]
[0086] The X-ray tube 300 may comprise a high voltage generator 220, a cathode 210 and a rotating anode 100.
[0087] The rotating anode 100 may be rotated by electromagnetic induction from a series of stator windings outside the X-ray tube 300.
[0088] Heat removal or direct cooling may be performed by conduction or convection the rotating anode may be suspended on ball bearings with silver powder lubrication providing cooling by conduction.
[0089] The rotating anode may be used in an X-ray tube which is generating X-rays for high performance computer tomography, CT, scanning and angiography systems or for any other high performance medical X-ray tube.
[0090] The X-ray tubes may have power ratings of up to 80 or 100 kW and more, for instance up to 200 kW.
[0091] It has to be noted that embodiments of the present invention are described with reference to different subject-matters. In particular, some embodiments are described with reference to method type claims, whereas other embodiments are described with reference to the device type claims.
[0092] However, a person skilled in the art will gather from the above and the foregoing description that, unless otherwise notified, in addition to any combination of features belonging to one type of the subject-matter also any combination between features relating to different subject-matters is considered to be disclosed with this application.
[0093] However, all features can be combined providing synergetic effects that are more than the simple summation of these features.
[0094] While the present invention has been illustrated and described in detail in the drawings and foregoing description, such illustration and description are to be considered illustrative or exemplary and not restrictive; the present invention is not limited to the disclosed embodiments. Other variations to the disclosed embodiments can be understood and effected by those skilled in the art and practicing the claimed invention, from a study of the drawings, the disclosure, and the appended claims.
[0095] In the claims, the word comprising does not exclude other elements or steps, and the indefinite article a or an does not exclude a plurality. Any reference signs in the claims should be construed not as limiting the scope.