The invention particularly relates to the RF windows of electron tubes, especially but not exclusively magnetrons. The electron tubes pass RF/microwave energy from a vacuum environment to an air/gaseous environment through the RF window.
A problem which has been encountered with high power, such as 100 kW magnetrons operated in continuous wave (CW) mode is that of cracking of the RF window in operation of the valve, resulting in loss of vacuum and failure of the device. The reasons for this problem are not fully understood, but one possible explanation is that glow discharge takes place in gas released from the ceramic dome as it becomes heated by the radiating RF/microwave power, which causes localised heating of the dome. Alternatively, heating may be clue to a multipactor discharge on the surface of the window, which could in itself cause gas release from the ceramic dome.
The usual method of counteracting this problem is to run the magnetrons for a long period, such as 24 hours, at low power, before operating them at peak power. It is thought that any gases absorbed in the ceramic dome would be released over this period but without gas discharge being able to take place because of the low power output. Then full power can be applied without the risk of gas discharge taking place.
While this has greatly reduced the incidence of such catastrophic failures in use, the low power ageing operation is a time-consuming step in the manufacture of the magnetron.
The invention provides an electron tube having an RF output window of ceramic material, in which the window has a coating of glass on the inner surface.
This reduces or eliminates the need for the very long preliminary period of low power operation.
The RF window may be bonded to the body of the electron tube at a region of metallisation, and the inner surface of the window is advantageously free of glazing in an adjoining region. The adjoining region may be chamfered to be free of the glazing.
The RF window may be made of alumina, and the glass is advantageously high temperature glass, preferably becoming mobile at above 1500 degrees centigrade. The glass may be borosilicate glass. The thickness of the glass layer is preferably within the range of from 0.05 mm to 3 mm.
One way of carrying out the invention will now be described in detail, by way of example, with reference to the accompanying drawings, in which:
The magnetron of the invention differs from known magnetrons of the type described with reference to
Referring to
In practice, the glazing may be applied so as to terminate a little short of the bottom of the dome, because of the need to keep the glass clear of the base during the high temperatures of the metallising operation. Neverthelesss, the grinding step is advisable, because glazing has a tendency to spread during its firing, and there is a risk that it could have spread right down to the base of the dome.
Because of the subsequent metallising operation, the glass coating is high temperature glass, that is, it becomes mobile at above 1500 degrees centigrade. In addition, the glass must have low RF loss, although this is unlikely to be a problem, since the coating is thin. The glass must also have a coefficient of expansion which is compatible with that of the material of the dome.
A suitable ceramics material is alumina (Al2O3), preferably of purity better than 90% to ensure low loss to the transmitted RF. A suitable glass layer is borosilicate glass. However, other high temperature glass coatings could also be used, and other ceramics materials with low RF loss could also be used.
It has been found that the internally glazed domes are not prone to the catastrophic failure sometimes encountered with prior art magnetrons, even though they have not been subject to the low power ageing operation. The reason for this is not fully understood, but it may be because the glaze prevents the discharge of gas from the alumina. However, glass is less prone to multipactor, and the catastrophic failures may not take place for this reason, alternatively, or in addition.
The ceramic thickness is typically approximately 6 mm and the glaze coating approximately 0.2111111.
If desired, the ceramic window could be glazed on its internal and external surfaces. The glaze on the external surface would play no part in preventing the discharge, but it would not be a disadvantage. There is, of course, no need for the RF window to be dome-shaped. The glazed interior can be used on any shape of RF window, including a flat shape.
Although the invention has been described in relation to a magnetron, the glazed RF window could also be applied to other types of electron tubes, such as inductive output tubes, klystrons, travelling wave tubes, or gyro-travelling wave amplifiers. The technique can be used in any situation where there is a window that passes RF/microwave energy from a vacuum environment to an air/gaseous environment, and is particularly useful where the frequency and power combine to produce some form of discharge. Thus, the invention is useful for high power tubes where the RF output power exceeds 50 kW, especially where it exceeds 75 kW, particularly when operated in continuous wave mode. This is especially true at high frequencies in excess of 1 GHz, where the area of the window is likely to be smaller, for example for frequencies in the range 1 GHz to 20 GHz, more particularly, 1 GHz to 3 GHz.
Number | Date | Country | Kind |
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1008263.4 | May 2010 | GB | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/GB2011/050897 | 5/11/2011 | WO | 00 | 1/31/2013 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2011/144918 | 11/24/2011 | WO | A |
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Number | Date | Country | |
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20130221844 A1 | Aug 2013 | US |