EP0874385B1 - Verfahren zur herstellung einer Anode für Röntgenröhren - Google Patents
Verfahren zur herstellung einer Anode für Röntgenröhren Download PDFInfo
- Publication number
- EP0874385B1 EP0874385B1 EP98201236A EP98201236A EP0874385B1 EP 0874385 B1 EP0874385 B1 EP 0874385B1 EP 98201236 A EP98201236 A EP 98201236A EP 98201236 A EP98201236 A EP 98201236A EP 0874385 B1 EP0874385 B1 EP 0874385B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- anode
- covering
- ray tubes
- production
- plasma
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 28
- 238000000034 method Methods 0.000 claims description 30
- 238000007750 plasma spraying Methods 0.000 claims description 20
- 230000008569 process Effects 0.000 claims description 20
- 239000002245 particle Substances 0.000 claims description 15
- 239000000843 powder Substances 0.000 claims description 15
- 230000001939 inductive effect Effects 0.000 claims description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 8
- 239000007921 spray Substances 0.000 claims description 8
- 238000000137 annealing Methods 0.000 claims description 7
- 229910002804 graphite Inorganic materials 0.000 claims description 7
- 239000010439 graphite Substances 0.000 claims description 7
- 238000009826 distribution Methods 0.000 claims description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 4
- 229910000691 Re alloy Inorganic materials 0.000 claims description 4
- 238000000151 deposition Methods 0.000 claims description 4
- 230000008021 deposition Effects 0.000 claims description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 239000011733 molybdenum Substances 0.000 claims description 4
- 238000011282 treatment Methods 0.000 claims description 4
- 229910001182 Mo alloy Inorganic materials 0.000 claims description 3
- DECCZIUVGMLHKQ-UHFFFAOYSA-N rhenium tungsten Chemical compound [W].[Re] DECCZIUVGMLHKQ-UHFFFAOYSA-N 0.000 claims description 3
- 238000000576 coating method Methods 0.000 description 25
- 239000011248 coating agent Substances 0.000 description 19
- 239000000463 material Substances 0.000 description 12
- 239000010410 layer Substances 0.000 description 10
- 238000004663 powder metallurgy Methods 0.000 description 10
- 238000007788 roughening Methods 0.000 description 9
- 238000012360 testing method Methods 0.000 description 7
- 238000002844 melting Methods 0.000 description 5
- 238000010290 vacuum plasma spraying Methods 0.000 description 4
- 238000010894 electron beam technology Methods 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
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- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000007872 degassing Methods 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000010943 off-gassing Methods 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 239000003870 refractory metal Substances 0.000 description 2
- 229910052702 rhenium Inorganic materials 0.000 description 2
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000012159 carrier gas Substances 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
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- 238000004320 controlled atmosphere Methods 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 210000003298 dental enamel Anatomy 0.000 description 1
- 230000001687 destabilization Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
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- 230000002045 lasting effect Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 238000005240 physical vapour deposition Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J9/00—Apparatus or processes specially adapted for the manufacture, installation, removal, maintenance of electric discharge tubes, discharge lamps, or parts thereof; Recovery of material from discharge tubes or lamps
- H01J9/02—Manufacture of electrodes or electrode systems
- H01J9/14—Manufacture of electrodes or electrode systems of non-emitting electrodes
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J35/00—X-ray tubes
- H01J35/02—Details
- H01J35/04—Electrodes ; Mutual position thereof; Constructional adaptations therefor
- H01J35/08—Anodes; Anti cathodes
- H01J35/10—Rotary anodes; Arrangements for rotating anodes; Cooling rotary anodes
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2235/00—X-ray tubes
- H01J2235/08—Targets (anodes) and X-ray converters
- H01J2235/083—Bonding or fixing with the support or substrate
Definitions
- the invention relates to a method for producing an anode for X-ray tubes consisting of a base body and one of these different X-ray emitting coating.
- Such materials are used to generate X-rays, when subjected to a focused electron beam Emit x-rays.
- the refractory metals tungsten and Molybdenum and its alloys are, for example, such materials that depending on the desired type of X-ray radiation.
- rotating anodes are often used for X-ray tubes in the form of axially symmetrical blanks for the production of X-rays used.
- the so-called focal path in area directly affected by the electron beam from the X-ray generating material as a comparatively thin coating executed while the main body of the rotating anode made of others high-melting materials.
- the focal track covering is mainly made using powder metallurgy Process made by pressing, sintering and forging.
- metallic He is preferably materials for the base body in one operation produced with the base body by layering the powder mixtures, with which Density values from 96% to 98% of theoretical density achieved as standard become.
- Such a manufacturing process for the focal track covering is inexpensive, but leads to properties, particularly with regard to his fatigue crack behavior are not yet optimal.
- the object of the invention is therefore to provide a method for producing anodes for X-ray tubes, by means of which the cost-effective production of the X-ray-emitting coating is made possible, the coating with regard to its usage behavior, in particular its fatigue crack resistance, at least fully corresponds to the standard which is still common today or even exceeds it. According to the invention this is achieved in that the X-ray emitting coating is applied by inductive plasma spraying.
- the coating emitting X-rays is applied by overlaying individual spray layers with a total thickness between 0.4 mm and 0.7 mm. As a rule, it is advisable to overlay individual layers of the spray layer 20 to 50 times.
- a particularly favorable variant of the method according to the invention is achieved if a recess of somewhat more than the depth of the desired covering thickness is worked into the base body of the anode in the area of this covering before the application of the X-ray radiation-covering. In this way, the surface of the coating can be brought to a level with the adjacent surface of the anode base body by simple grinding.
- the Separation under an inductively coupled power between 50 kW and 100 kW and under a delivery rate of the wettable powder between 10 g / min and 50 g / min takes place. Under these conditions there is a total Melting and sufficient overheating of the melt droplets.
- the plasma jet and the base body are used to produce rotating anodes the rotating anode moves against each other in such a way that the central point of impact of the plasma particle stream on the anode surface and the Rotating anode axis concentric center line of the active Focal path area coincide at least approximately, the Particle flow of the plasma jet is set so that the within the particle stream of the plasma jet that only hits the active focal path region includes that area which is within the half-width of the Gaussian Particle distribution of the generated complete plasma jet lies.
- the edge region of the layer which is less favorable for the layer construction Plasma rays largely shifted to areas of the anode surface that are outside the active focal path area.
- the focal path area is that for the generation of X-rays directly from Understand the electron beam area.
- the rotating anode is finally one Is subjected to annealing treatment.
- the purpose of this annealing is both one further improvement of the structural properties through diffusion processes as also degassing the anode.
- the type of annealing treatment is among others depending on the material from which the base body of the rotating anode is made has been. In the case of a base body made of high-melting metal, the Annealing treatment at temperatures between 1,200 ° C and 1,600 ° C during 1 to 20 hours while rotating anodes where graphite is used for the body was used, usually at temperatures up to 1,300 ° C is carried out for up to about 10 hours. in case of a Graphite base body is the possible formation of disadvantageous carbides in the border area by known diffusion barrier layers, e.g. Rhenium, advantageously delayed.
- the method according to the invention can be used in a particularly advantageous manner be applied when the base body of the anode is made of graphite, molybdenum or a molybdenum alloy and the X-ray emitting coating consists of a tungsten-rhenium alloy.
- Disc-shaped base bodies for rotating anodes made of TZM, a molybdenum alloy with 0.5% titanium, 0.08% zirconium, up to 0.04% carbon, the rest molybdenum, with a diameter of 120 mm and a frustoconical outer area with a 20 ° opening angle were made on one mounted with a rotary drive and installed in a vacuum chamber.
- the individual base bodies were coated by means of an inductively heated plasma gun with an inner diameter of 50 mm and an output of 65 kW with spray powder made of a Wo.fram alloy with 5% rhenium in a powder fraction between 15 and 63 ⁇ m.
- the wettable powder was introduced axially at a rate of 30 g / min using Ar carrier gas.
- the base bodies were heated to 1500 ° C.
- the speed of rotation of the base body was 10 rpm.
- the plasma cannon was moved laterally to the center line of the focal track covering concentric to the rotating anode axis, in such a way that the axis of the plasma cannon continuously exceeded this center line alternately on both sides up to a maximum of 5 mm at a speed of 2 mm / sec.
- a focal track covering with a total thickness of about 1 mm and a width of 25 mm was applied in this way through approximately 50 individual layers deposited one above the other.
- the rotating anodes which had cooled to below 100 ° C., were removed from the vacuum chamber and then the focal track covering was ground to a thickness of 0.7 mm. Finally, the rotary anodes finished in this way were subjected to high vacuum annealing at a temperature of 1600 ° C. for 90 minutes.
- the same disk-shaped base bodies as were used for the application of the method according to the invention were produced with a 0.8 mm thick focal track covering from a tungsten-5-rhenium alloy by powder metallurgy.
- a layer of the TZM powder mixture for the base body on the one hand and the tungsten-rhenium alloy for the focal track coating on the other hand was produced and pressed, the compact was sintered and the final shape was produced by forging and mechanical processing. Finally, the rotating anodes were subjected to the same high vacuum annealing as those produced according to the invention.
- the focal track coverings applied according to the invention had a Density of 97.2% of the theoretical density, while the Powder metallurgy produced focal track coverings a density of 97.4% had theoretical density.
- a similar Rotating anode base body as in production example 1 in the area of Burning path incorporated an annular groove of 0.8 mm depth. After that was the rotating anode body with the substantially similar Coating conditions according to the inventive method coated according to production example 1.
- the rotary anodes produced according to the invention or according to the prior art according to production example 1 were installed in a test bench for X-ray rotary anodes and cyclically tested under the usual conditions using the following parameters: tube voltage 90 kV tube current 400 mA shot duration 2 sec break time 58 sec
- the test was randomly interrupted at specified times in order to determine the firing path roughening which had occurred up to that point as a measure of the fatigue crack resistance and the associated reduction in the X-ray dose yield.
- the respective mean values of the roughness depths Ra of the data determined on three rotating anodes per variant are shown in FIG. The much more favorable course of the roughening -B- in the case of the rotating anodes produced according to the invention is clearly recognizable.
- the average roughness Ra measured in the circumferential direction, was 24% lower than the corresponding comparison value of the roughening -A- of the comparative rotary anodes produced by powder metallurgy.
- the roughening of the rotary anode according to the invention as was present after 100 hours at the end of the test, is already achieved on average after approximately 20 hours of test in the comparison anodes.
- a ground section was produced in each case from a rotating anode coated according to the invention and from a rotating metallode produced by powder metallurgy. A picture of these cuts in 200 times magnification can be seen in FIGS. 3 and 4.
- the structure of the induction plasma-sprayed combustion path according to FIG. 3 shows one fundamentally different morphology than that of powder metallurgy produced focal path according to Figure 4.
- the inductive plasma spraying striking enamel droplets crystallize transcrystalline as they solidify from, which in turn serve as a crystallization surface for the subsequent melting droplets. This will do it once present growth direction of the layer at least over many Maintain melt droplets largely and they do not form lamellar usually observed in conventional plasma spraying Structural structures with poorly bound grain boundaries as shown in FIG. 5 clearly using the example of one produced by conventional plasma spraying Focal path coating of a rotating anode can be seen.
- Fatigue of the focal track covering at Rotary anode produced according to the invention occurs in the form of essentially microcracks running perpendicular to the surface appear however less harmful in terms of roughening the surface impact as those cracks in the powder metallurgically manufactured rotating anode.
- the greater roughening and the destabilization of the surface structure in the case of the rotary anode produced by powder metallurgy by failure of the Grain boundaries can be clearly seen in FIG. 4.
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Coating By Spraying Or Casting (AREA)
Description
Eine Anwendung des Induktiven Plasmaspritzens für die Herstellung von Röntgenstrahlung emittierenden Belägen bei Anoden für Röntgenröhren ist bisher aufgrund der Erfahrungen vom konventionellen Plasmaspritzen hinsichtlich der unbefriedigenden Ergebnisse des Ermüdungsverhaltens nicht erfolgt.
Erfindungsgemäß wird dies dadurch erreicht, daß der Röntgenstrahlung emittierende Belag durch Induktives Plasmaspritzen aufgebracht wird.
Eine besonders günstige Variante des erfindungsgemäßen Verfahrens wird erreicht, wenn vor dem Aufbringen des Röntgenstrahlung emittierenden Belages im Bereich dieses Belages in den Grundkörper der Anode eine Ausnehmung von etwas mehr als der Tiefe der gewünschten Belagstärke eingearbeitet wird. Auf diese Weise kann die Oberfläche des Belages durch einfaches Überschleifen auf eine Ebene mit der angrenzenden Oberfläche des Anodengrundkörpers gebracht werden.
- Figur 1
- die Prinzipskizze einer Variante des erfindungsgemäßen Verfahrens nach den Ansprüchen 3 und 6
- Figur 2
- die graphische Darstellung der Mittelwerte der Brennbahnaufrauhung Ra von erfindungsgemäß und pulvermetallurgisch hergestellten Brennbahnbelägen von Drehanoden
- Figur 3
- die Schliffaufnahme der Brennbahn einer erfindungsgemäß hergestellten Drehanode im Schnitt in 200-facher Vergrößerung
- Figur 4
- die Schliffaufnahme der Brennbahn einer Drehanode mit pulvermetallurgisch hergestellten Brennbahnbelägen im Schnitt in 200-facher Vergrößerung
- Figur 5
- die Schliffaufnahme der Brennbahn einer Drehanode, die durch konventionelles Plasmaspritzen hergestellt wurde, im Schnitt in 200-facher Vergrößerung
Für Vergleichszwecke wurden dieselben scheibenförmigen Grundkörper wie sie für die Anwendung des erfindungsgemäßen Verfahrens verwendet wurden mit einem 0,8 mm starken Brennbahnbelag aus einer Wolfram-5-Rheniumlegierung auf pulvermetallurgischem Wege hergestellt. Dazu wurde in einer Matrize eine Schichtung der TZM-Pulvermischung für den Grundkörper einerseits und der Wolfram-Rhenium-Legierung für den Brennbahnbelag andererseits hergestellt und gepreßt, der Preßling gesintert und durch Schmieden und mechanische Bearbeitung die endgültige Form hergestellt. Abschließend wurden die Drehanoden derselben Hochvakuumglühung wie die erfindungsgemäß hergestellten unterzogen.
| Röhrenspannung | 90 kV |
| Röhrenstrom | 400 mA |
| Schußdauer | 2 sec |
| Pausenzeit | 58 sec |
Die jeweiligen Mittelwerte der Rauhtiefen Ra der an jeweils drei Drehanoden pro Variante ermittelten Daten sind in Figur 2 dargestellt.
Der wesentlich günstigere Verlauf der Aufrauhung -B- im Falle der erfindungsgemäß hergestellten Drehanoden ist klar erkennbar. Nach 100 Stunden Testdauer war die mittlere Rauhtiefe Ra, in Umfangsrichtung gemessen, um 24 % niedriger als der entsprechende Vergleichswert der Aufrauhung -A- der pulvermetallurgisch hergestellten Vergleichsdrehanoden. In einer anderen Betrachtungsweise wird die Aufrauhung der erfindungsgemäßen Drehanode, wie sie bei Testende nach 100 Stunden vorgelegen hat, bei den Vergleichsanoden im Schnitt bereits nach ca. 20 Stunden Testdauer erreicht. Nach Abschluß des Vergleichstests wurde von einer erfindungsgemäß beschichteten Drehanode und von einer pulvermetallurgisch hergestellten Drehanode jeweils ein Schliff hergestellt. Eine Aufnahme dieser Schliffe in 200-facher Vergrößerung ist in den Figuren 3 und 4 zu sehen.
Claims (8)
- Verfahren zur Herstellung einer Anode für Röntgenröhren, bestehend aus einem Grundkörper und einem von diesem unterschiedlichen Röntgenstrahlung emittierenden Belag,
dadurch gekennzeichnet, daß der Röntgenstrahlung emittierende Belag durch induktives Plasmaspritzen aufgebracht wird. - Verfahren zur Herstellung einer Anode für Röntgenröhren nach Anspruch 1, dadurch gekennzeichnet, daß der Röntgenstrahlung emittierende Belag durch mehrmaliges Überlagern einzelner Spritzschichten mit einer Gesamtdicke zwischen 0,4 mm und 0,6 mm aufgebracht wird.
- Verfahren zur Herstellung einer Anode für Röntgenröhren nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, daß vor dem Aufbringen des Röntgenstrahlung emittierenden Belages im Bereich dieses Belages eine Ausnehmung mit etwa der Tiefe der gewünschten Belagsstärke in den Grundkörper eingearbeitet wird.
- Verfahren zur Herstellung einer Anode für Röntgenröhren nach Anspruch 1 oder 3, dadurch gekennzeichnet, daß die Abscheidung unter einer induktiv eingekoppelten Leistung zwischen 50 kW und 100 kW und einer Förderrate des Spritzpulvers zwischen 10 g/min und 50 g/min erfolgt.
- Verfahren zur Herstellung einer Anode für Röntgenröhren nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß die Anode vor der Aufbringung des Belages auf eine Temperatur zwischen 1.000°C und 1.500°C vorgewärmt wird und die lokale Abscheidetemperatur im Bereich des Belages zwischen 1.400°C und 2.400 C beträgt.
- Verfahren zur Herstellung einer Anode für Röntgenröhren nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß der Plasmastrahl und der Grundkörper derart gegeneinander bewegt werden, daß der zentrale Auftreffpunkt des Plasmapartikelstromes auf der Anodenoberfläche und die zur Drehanodenachse konzentrische Zentrumslinie des aktiven Brennbahnbereiches zumindest näherungsweise zusammenfallen, wobei der Partikelstrom des Plasmastrahles so eingestellt wird, daß der innerhalb des aktiven Brennbahnbereiches auftreffende Partikelstrom des Plasmastrahles nur jenen Bereich umfaßt, der innerhalb der Halbwertsbreite der gaußförmigen Partikelverteilung des erzeugten vollständigen Plasmastrahles liegt.
- Verfahren zur Herstellung einer Anode für Röntgenröhren nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß die Anode abschließend einer Glühbehandlung unterzogen wird.
- Anode für Röntgenröhren, hergestellt nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, daß der Grund körper aus Graphit, Molybdän oder einer Molybdänlegierung und der Röntgenstrahlung emittierende Belag aus einer Wolfram-Rhenium-Legierung besteht.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT244/97U | 1997-04-22 | ||
| AT0024497U AT1984U1 (de) | 1997-04-22 | 1997-04-22 | Verfahren zur herstellung einer anode für röntgenröhren |
| AT24497U | 1997-04-22 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0874385A1 EP0874385A1 (de) | 1998-10-28 |
| EP0874385B1 true EP0874385B1 (de) | 2002-06-12 |
Family
ID=3485389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP98201236A Expired - Lifetime EP0874385B1 (de) | 1997-04-22 | 1998-04-17 | Verfahren zur herstellung einer Anode für Röntgenröhren |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6132812A (de) |
| EP (1) | EP0874385B1 (de) |
| JP (1) | JPH10302624A (de) |
| AT (2) | AT1984U1 (de) |
| DE (1) | DE59804388D1 (de) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2168235C1 (ru) * | 2000-04-04 | 2001-05-27 | Государственный научно-исследовательский институт Научно-производственного объединения "Луч" | Способ изготовления анода рентгеновской трубки |
| RU2179767C2 (ru) * | 2000-04-12 | 2002-02-20 | Государственный научно-исследовательский институт Научно-производственного объединения "Луч" | Способ изготовления анода рентгеновской трубки |
| DE102005049519B4 (de) * | 2005-01-31 | 2014-10-30 | Medicoat Ag | Drehanodenteller für Röntgenröhren |
| DE102005033799B4 (de) * | 2005-01-31 | 2010-01-07 | Medicoat Ag | Verfahren zur Herstellung eines Drehanodentellers für Röntgenröhren |
| US20070207338A1 (en) * | 2006-03-01 | 2007-09-06 | Plasma Processes, Inc. | X-ray target and method for manufacturing same |
| US20080081122A1 (en) * | 2006-10-03 | 2008-04-03 | H.C. Starck Inc. | Process for producing a rotary anode and the anode produced by such process |
| US7601399B2 (en) * | 2007-01-31 | 2009-10-13 | Surface Modification Systems, Inc. | High density low pressure plasma sprayed focal tracks for X-ray anodes |
| CN101779266A (zh) * | 2007-08-08 | 2010-07-14 | 皇家飞利浦电子股份有限公司 | 用于将材料涂抹到x射线源的阳极表面的方法和装置、阳极以及x射线源 |
| US20090060139A1 (en) * | 2007-08-28 | 2009-03-05 | Subraya Madhusudhana T | Tungsten coated x-ray tube frame and anode assembly |
| US9159523B2 (en) | 2007-08-28 | 2015-10-13 | General Electric Company | Tungsten oxide coated X-ray tube frame and anode assembly |
| AT10598U1 (de) * | 2007-09-28 | 2009-06-15 | Plansee Metall Gmbh | Ríntgenanode mit verbesserter warmeableitung |
| US8509386B2 (en) * | 2010-06-15 | 2013-08-13 | Varian Medical Systems, Inc. | X-ray target and method of making same |
| JP2014506377A (ja) * | 2010-12-16 | 2014-03-13 | コーニンクレッカ フィリップス エヌ ヴェ | 高融点中間層及びvps焦点軌道を伴うアノード・ディスク素子 |
| AT14854U1 (de) | 2015-07-03 | 2016-07-15 | Plansee Se | Behälter aus Refraktärmetall |
| CN113049616B (zh) * | 2019-12-26 | 2024-06-14 | 北航(四川)西部国际创新港科技有限公司 | 一种热障涂层内部裂纹的无损检测方法及系统 |
| EP4386807A1 (de) | 2022-12-13 | 2024-06-19 | Plansee SE | Röntgendrehanode mit zwei unterschiedlichen kornstrukturen im brennbahnbelag |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AT325164B (de) * | 1970-03-23 | 1975-10-10 | Dl Kom Veb Keramische Werke He | Anode für hochleistungsrontgenrohren |
| DE2400717C3 (de) * | 1974-01-08 | 1979-10-31 | Vsesojuznyj Nautschno-Issledovatelskij I Proektnyj Institut Tugoplavkich Metallov, I Tvjerdych Splavov Vniits, Moskau | Röntgenröhrendrehanode und Verfahren zu deren Herstellung |
| AT337314B (de) * | 1975-06-23 | 1977-06-27 | Plansee Metallwerk | Rontgenanode |
| JPS5588843A (en) * | 1978-12-27 | 1980-07-04 | Matsushita Electric Ind Co Ltd | Production of amorphous body |
| NL8300251A (nl) * | 1983-01-25 | 1984-08-16 | Philips Nv | Werkwijze voor het vervaardigen van een draaianode voor roentgenbuizen en zo verkregen anode. |
| US4573185A (en) * | 1984-06-27 | 1986-02-25 | General Electric Company | X-Ray tube with low off-focal spot radiation |
| NL8402828A (nl) * | 1984-09-14 | 1986-04-01 | Philips Nv | Werkwijze voor de vervaardiging van een roentgendraaianode en roentgendraaianode vervaardigd volgens de werkwijze. |
| JPS62170138A (ja) * | 1986-01-22 | 1987-07-27 | Toshiba Corp | X線管用陽極およびその製造方法 |
| US4853250A (en) * | 1988-05-11 | 1989-08-01 | Universite De Sherbrooke | Process of depositing particulate material on a substrate |
| US4920012A (en) * | 1989-06-09 | 1990-04-24 | General Electric Company | Articles having coatings of fine-grained and/or equiaxed grain structure |
| AT394643B (de) * | 1989-10-02 | 1992-05-25 | Plansee Metallwerk | Roentgenroehrenanode mit oxidbeschichtung |
| US5030517A (en) * | 1990-01-18 | 1991-07-09 | Allied-Signal, Inc. | Plasma spraying of rapidly solidified aluminum base alloys |
| US4972449A (en) * | 1990-03-19 | 1990-11-20 | General Electric Company | X-ray tube target |
| JP2716844B2 (ja) * | 1990-06-11 | 1998-02-18 | 三菱重工業株式会社 | 溶射複合膜形成方法 |
| US5070228A (en) * | 1990-06-18 | 1991-12-03 | General Electric Company | Method for plasma spray joining active metal substrates |
| US5126529A (en) * | 1990-12-03 | 1992-06-30 | Weiss Lee E | Method and apparatus for fabrication of three-dimensional articles by thermal spray deposition |
| JP2975145B2 (ja) * | 1991-04-04 | 1999-11-10 | 豊信 吉田 | 熱プラズマ成膜方法 |
| JPH06299315A (ja) * | 1993-04-14 | 1994-10-25 | Sansha Electric Mfg Co Ltd | アルミニウム及びチタニウムの表面改質方法 |
| JPH07220630A (ja) * | 1994-02-02 | 1995-08-18 | Rigaku Corp | X線発生装置のターゲット製造方法 |
| JPH08279344A (ja) * | 1994-12-22 | 1996-10-22 | Toshiba Electron Eng Corp | X線管及びその製造方法 |
| JPH08199372A (ja) * | 1995-01-26 | 1996-08-06 | Nisshin Steel Co Ltd | 傾斜機能材料の製法および装置 |
| US5844192A (en) * | 1996-05-09 | 1998-12-01 | United Technologies Corporation | Thermal spray coating method and apparatus |
-
1997
- 1997-04-22 AT AT0024497U patent/AT1984U1/de not_active IP Right Cessation
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1998
- 1998-04-13 US US09/059,233 patent/US6132812A/en not_active Expired - Lifetime
- 1998-04-17 DE DE59804388T patent/DE59804388D1/de not_active Expired - Lifetime
- 1998-04-17 AT AT98201236T patent/ATE219289T1/de active
- 1998-04-17 EP EP98201236A patent/EP0874385B1/de not_active Expired - Lifetime
- 1998-04-21 JP JP10128209A patent/JPH10302624A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| EP0874385A1 (de) | 1998-10-28 |
| DE59804388D1 (de) | 2002-07-18 |
| JPH10302624A (ja) | 1998-11-13 |
| AT1984U1 (de) | 1998-02-25 |
| US6132812A (en) | 2000-10-17 |
| ATE219289T1 (de) | 2002-06-15 |
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