GB2237140A - Magnetrons - Google Patents

Magnetrons Download PDF

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Publication number
GB2237140A
GB2237140A GB8923322A GB8923322A GB2237140A GB 2237140 A GB2237140 A GB 2237140A GB 8923322 A GB8923322 A GB 8923322A GB 8923322 A GB8923322 A GB 8923322A GB 2237140 A GB2237140 A GB 2237140A
Authority
GB
United Kingdom
Prior art keywords
vanes
magnetron
cavities
anode
circle
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.)
Withdrawn
Application number
GB8923322A
Other versions
GB8923322D0 (en
Inventor
Peter Lewis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Teledyne UK Ltd
Original Assignee
EEV Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by EEV Ltd filed Critical EEV Ltd
Priority to GB8923322A priority Critical patent/GB2237140A/en
Publication of GB8923322D0 publication Critical patent/GB8923322D0/en
Priority to FR9012762A priority patent/FR2653267A1/en
Priority to JP27888190A priority patent/JPH03179641A/en
Publication of GB2237140A publication Critical patent/GB2237140A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J25/00Transit-time tubes, e.g. klystrons, travelling-wave tubes, magnetrons
    • H01J25/50Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field
    • H01J25/52Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field with an electron space having a shape that does not prevent any electron from moving completely around the cathode or guide electrode
    • H01J25/58Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field with an electron space having a shape that does not prevent any electron from moving completely around the cathode or guide electrode having a number of resonators; having a composite resonator, e.g. a helix
    • H01J25/587Multi-cavity magnetrons
    • H01J25/593Rising-sun magnetrons
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/16Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
    • H01J23/165Manufacturing processes or apparatus therefore

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Microwave Tubes (AREA)

Abstract

A magnetron includes a cathode 1 and a surrounding anode structure 2 having vanes 4 defining two sets of cavities 5 and 6 between them. The cavities 5 of one set are of a larger volume than those of the other set 6, the two sets being arranged alternately. The inner ends 8 of the vanes 4 are arranged equidistant around a circle defined by a radius b and their outer ends 7 are unequally spaced around a circle of radius a. The inner ends 8 of the vanes 4 are radiused to give a smooth curved surface without edges, enabling the vanes to be distributed symmetrically about the interaction space of the magnetron, even although the vanes 4 are not aligned radially with the centre of the cathode 1. <IMAGE>

Description

MAGNETRONS This invention relates to magnetrons.
One known type of magnetron has an anode, called a rising sun anode, which defines large and small resonant cavities arranged alternately around its circumference.
Such a structure enables stable oscillation in a single mode to be produced.
Conventionally, a rising sun anode is manufactured by machining a block of metal, usually copper, to produce a hollow cylinder having resonant cavities extending into the cylinder wall from its inner surface. For optimum performance, the sections of the inner wall between the cavities must be spaced equally apart, being of uniform width and radius so that they appear as symmetrical as possible to rotating electron streams in the interaction space between the anode and the magnetron cathode. In order to accommodate both large and small volume cavities whilst retaining this symmetrical configuration around the interaction space, the larger cavities must have a greater radial depth than the smaller cavities. The anode cylinder tends to be bulky as it must therefore be of a large enough diameter to accommodate the large cavities.Also, it is expensive to manufacture such an anode because of the accurate machining required.
According to a first aspect of the invention there is provided a magnetron comprising an anode having two sets of resonant cavities, the cavities of each set being of the same volume which is different from that of the other set, the cavities being arranged around the circumference of a circle and being partly defined by anode vanes having outer ends which are at substantially the same outer radial distance, and inner ends which are at substantially the same inner radial distance, from the centre of the circle, the inner ends being spaced substantially equidistant around a circle having a radius which is the inner radial distance. To implement the invention, the outer ends of the vanes are not equally spaced around the circumference of the circle defined by the outer radial distance.Thus, the vanes have different angular separations to produce the desired ratio of frequency of adjacent cavities, not being aligned along radii of the same circle. By ensuring that the inner ends of the vanes are symmetrically arranged about the interaction space, good performance of the magnetron may be achieved. Also, as both sizes of cavity have substantially the same radial depth, the resulting anode structure is less bulky than a conventional device in which the larger volume cavities extend further in a radial direction than the smaller ones.
It is preferred that the inner end of each vane is radiused. By "radiused" it is meant that the end of the vane is smoothly curved, such that there are no edges at the interaction space. Preferably, the radiused end of each vane is curved in a surface having a uniform radius from a point on the centre-line of the vane parallel to its two major surfaces. The advantage of using radiused inner ends of the vanes is that they may be arranged at equal spacings around the interaction space even though the vanes themselves are not aligned along radii of the same circle.
Advantageously, the anode comprises a hollow cylinder formed separately from the vanes and the vanes are fixed at their outer ends to slots in the inner surface of the cylinder. Alternatively, the anode may be machined as an integral structure. However, by using seperately manufactured vanes, a simple constructional technique may be used which can be inexpensively implemented.
The invention arose from the consideration of magnetron having a "rising sun" type anode in which large and small volume resonant cavities are alternately arranged around the anode. However, it is envisaged that other forms of anode which utilise different size resonant cavities may also be advantageously configured in accordance with the invention.
According to a second aspect of the invention a magnetron comprises an anode structure having vanes defining resonant cavities, wherein the inner ends of the vanes adjacent to the interaction space of the magnetron are radiused. The use of radiused ends is advantageous even for anode configurations in which all the resonant cavities are of the same volume, or where the cavities have different radial dimensions, as it enables tolerances to be increased whilst still ensuring that the part of the anode structure adjacent to the interaction space is symmetrical.
One way in which the invention may be performed is now described by way of example with reference to the accompanying drawings in which: Figure 1 is a transverse section of a magnetron in accordance with the invention; and Figure 2 is an enlarged view of part of Figure 1.
With reference to Figure 1, a magnetron comprises a central cylindrical cathode 1 surrounded by an anode structure 2 which consists of a copper cylinder 3 and anode vanes 4 projecting inwards from the inner surface of the cylinder 3 towards the cathode 1. The anode structure 2 defines two sets of resonant cavities arranged circumferentially about the cathode 1. The resonant cavities of one set 5 are of a large volume and are arranged alternately with cavities of the other set 6 to give a "rising sun" configuration. The outer ends 7 of the vanes 4 are located in slots in the cylinder wall 3 and are arranged on a circle having a radius a from the centre of the cathode 1. The inner ends 8 of the vanes 4 are also arranged at the same distance as each other from the centre of the cathode 1, this distance being shown as b in Figure 1.The inner ends 8 of the vanes 4 are arranged substantially equidistant around the circle of radius b as can be seen more clearly in Figure 2. Thus, the anode structure 2 is symmetrical about the interaction region of the magnetron between the anode vane ends 8 and the cathode 1. The outer ends 7 of the vanes 4 are spaced at unequal distances around the circle having radius a, as can be clearly seen from Figure 1. Thus, the vanes 4 are not aligned radially with respect to the centre of the cathode 1, as is demonstrated by the broken lines of Figure 1 along the centre-lines of some of the anode vanes 4.
The inner ends 8 of the vanes 4 are radiused, having smoothly curving surfaces. Thus, even though the vanes 4 are not aligned radially with the centre of the cathode 1, the part of the anode structure adjacent to the interaction space is symmetrical, giving good performance.
In an alternative embodiment of the invention, pairs of anode vanes may be located in such a way as to provide a set of cavities having parallel walls.

Claims (7)

1. A magnetron comprising an anode having two sets of resonant cavities, the cavities of one set each being of the same volume which is different from that of the other set, the cavities being arranged around the circumference of a circle and being partly defined by anode vanes having outer ends which are at substantially the same outer radial distance, and inner ends which are at substantially the same inner radial distance, from the centre of the circle the inner ends being spaced substantially equidistant around a circle having a radius which is the inner radial distance.
2. A magnetron as claimed in claim 1 wherein the inner ends of each vane is radiused.
3. A magnetron as claimed in claim 2 wherein the radiused end of each vane is curved in a surface having a uniform radius from a point on the centre-line of the vane parallel to its two major surfaces.
4. A magnetron as claimed in claim 1, 2 or 3 wherein the anode comprises a hollow cylinder formed separately from the vanes and the vanes are fixed at their outer ends in slots in the inner surface of the cylinder.
5. A magnetron as claimed in any preceding claim wherein the cavities of one set are arranged alternately around the circumference with cavities of the other set.
6. A magnetron substantially as illustrated in and described with reference to the accompanying drawings.
7. A magnetron comprising an anode structure having vanes defining resonant cavities, wherein the inner ends of the vanes adjacent to the interaction space of the magnetron are radiused.
GB8923322A 1989-10-17 1989-10-17 Magnetrons Withdrawn GB2237140A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB8923322A GB2237140A (en) 1989-10-17 1989-10-17 Magnetrons
FR9012762A FR2653267A1 (en) 1989-10-17 1990-10-16 MAGNETRON COMPRISING AN ANODE STRUCTURE WHICH DEFINES TWO SETS OF RESONANT CAVITIES OF RESPECTIVELY DIFFERENT VOLUMES.
JP27888190A JPH03179641A (en) 1989-10-17 1990-10-17 Magnetron

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8923322A GB2237140A (en) 1989-10-17 1989-10-17 Magnetrons

Publications (2)

Publication Number Publication Date
GB8923322D0 GB8923322D0 (en) 1989-12-06
GB2237140A true GB2237140A (en) 1991-04-24

Family

ID=10664679

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8923322A Withdrawn GB2237140A (en) 1989-10-17 1989-10-17 Magnetrons

Country Status (3)

Country Link
JP (1) JPH03179641A (en)
FR (1) FR2653267A1 (en)
GB (1) GB2237140A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2289370A (en) * 1994-05-12 1995-11-15 Litton Systems Inc Magnetrons
US5569980A (en) * 1994-07-29 1996-10-29 Litton Systems, Inc. Non-concentric support for crossed-field amplifier
EP0781454A1 (en) * 1994-09-12 1997-07-02 Primex Technologies, Inc. Frequency tunable magnetron

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB595868A (en) * 1944-05-24 1947-12-19 Bernard Vincent Rollin Improvements in or relating to multi-resonator magnetrons
GB666689A (en) * 1947-04-18 1952-02-20 Csf Improvements in or relating to magnetrons for short or ultra-short wave working
GB776215A (en) * 1954-05-13 1957-06-05 Csf Improvements in or relating to electron discharge tubes with crossed electric and magnetic fields
GB848920A (en) * 1957-01-07 1960-09-21 British Thomson Houston Co Ltd Improvements relating to multi-cavity magnetrons
GB946621A (en) * 1961-10-04 1964-01-15 English Electric Valve Co Ltd Improvements in or relating to cavity magnetrons
GB1134734A (en) * 1966-08-10 1968-11-27 Westinghouse Electric Corp Coaxial magnetron
GB2224882A (en) * 1988-10-24 1990-05-16 Eev Ltd Tuning magnetrons

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3384783A (en) * 1965-12-16 1968-05-21 Bell Telephone Labor Inc Mode suppression in coaxial magnetrons having diverse size anode resonator
DE1904448A1 (en) * 1968-02-02 1969-08-28 English Electric Valve Co Ltd Magnetron with flag anode
JPS5223253A (en) * 1975-08-15 1977-02-22 Toshiba Corp Anode structure of magnetron
JPS61126737A (en) * 1984-11-21 1986-06-14 Sanyo Electric Co Ltd Magnetron

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB595868A (en) * 1944-05-24 1947-12-19 Bernard Vincent Rollin Improvements in or relating to multi-resonator magnetrons
GB666689A (en) * 1947-04-18 1952-02-20 Csf Improvements in or relating to magnetrons for short or ultra-short wave working
GB776215A (en) * 1954-05-13 1957-06-05 Csf Improvements in or relating to electron discharge tubes with crossed electric and magnetic fields
GB848920A (en) * 1957-01-07 1960-09-21 British Thomson Houston Co Ltd Improvements relating to multi-cavity magnetrons
GB946621A (en) * 1961-10-04 1964-01-15 English Electric Valve Co Ltd Improvements in or relating to cavity magnetrons
GB1134734A (en) * 1966-08-10 1968-11-27 Westinghouse Electric Corp Coaxial magnetron
GB2224882A (en) * 1988-10-24 1990-05-16 Eev Ltd Tuning magnetrons

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5680012A (en) * 1993-04-30 1997-10-21 Litton Systems, Inc. Magnetron with tapered anode vane tips
GB2289370A (en) * 1994-05-12 1995-11-15 Litton Systems Inc Magnetrons
GB2289370B (en) * 1994-05-12 1998-04-01 Litton Systems Inc Magnetrons
US5569980A (en) * 1994-07-29 1996-10-29 Litton Systems, Inc. Non-concentric support for crossed-field amplifier
EP0781454A1 (en) * 1994-09-12 1997-07-02 Primex Technologies, Inc. Frequency tunable magnetron
EP0781454A4 (en) * 1994-09-12 1998-06-24 Primex Tech Inc Frequency tunable magnetron

Also Published As

Publication number Publication date
FR2653267A1 (en) 1991-04-19
JPH03179641A (en) 1991-08-05
GB8923322D0 (en) 1989-12-06

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)