US2774005A - Slow-wave structures for travelling wave tubes - Google Patents
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- US2774005A US2774005A US249611A US24961151A US2774005A US 2774005 A US2774005 A US 2774005A US 249611 A US249611 A US 249611A US 24961151 A US24961151 A US 24961151A US 2774005 A US2774005 A US 2774005A
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J23/00—Details of transit-time tubes of the types covered by group H01J25/00
- H01J23/16—Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
- H01J23/24—Slow-wave structures, e.g. delay systems
Definitions
- FIG. 1 SLOW-WAVE STRUCTURES FOR TRAVELLING WAVE TUBES Dec. 11, 1956 Filed Oct. 3, 195] FIG.
- This invention relates to high frequency amplifiers of the travelling wave type and more particularly to travelling wave tube electromagnetic propagating wave structures for slowing the phase velocity thereof.
- Travelling wave tube amplifiers heretofore known include a conductor, either in the form of a helix or a series of inter-connected baffles, past which an electromagnetic wave can propagate.
- the phase velocity of the electromagnetic wave as measured along the axis of the conducting structure is small comparedto the velocity along the surface of the conductor.
- An electron beam source is arranged to direct a stream of electrons adjacent the conductor, and where the conductor is in the form of a helix, the beam is usually directed axially through or adjacent the helix.
- the axial phase velocity of the electromagnetic wave is so related to the axial electron path that the electrons travel at a slightly hi her velocity than the axial phase velocity of the electromagnetic wave. This difference in travel velocity results in part of the kinetic energy of the electrons being converted into radio frequency energy and the electromagnetic wave propagated in the direction of the electron flow is thereby amplified.
- Such travelling wave tubes are particularly suited for employment as an amplifier of microwave frequencies.
- the axial phase velocity of the electromagnetic wave is limited by both the pitch and radius, or diameter, of the helix. Because of the helical pitch, the travelling wave fieldpropagated along the helix is skewed with respect to the axis thereof. Since the electrons interact with only those portions of the field parallel to the axis of the helix, it is apparent that if the skewed nature of the field can be eliminated, then a greater, or more favorable interaction, may occur, thereby increasing the gain of the tube. Also, it is Well known that for efficient operation at very high frequencies, each helix turn should be only a fraction of the operating Wavelength. Hence, helices with relatively small diameters must be utilized together with a very narrow electron beam. For controlling such a narrow beam, unusually high operating voltages and very strong magnetic fields are required.
- an electromagnetic wave phase slowing structure for a travelling wave tube comprising a cylindrical wire mesh network with the electron stream passing adjacent the cylindrical mesh in the direction of the axis of the cylinder.
- An electromagnetic wave is propagated along the cylindrical mesh network and the axial electric field interacts with the electron stream to amplify the propagated signal.
- the phase slowing structure comprises a plurality of planar wire mesh networks stacked one above the other in parallel arrangement.
- a flat, ribbon-like, electron stream is projected between each pair of said wire mesh networks to interact with an electromagnetic wave propagated substantially in phase on each of said planar mesh networks.
- Fig. 1 shows a travelling wave tube amplifier employing a cylindrical wire mesh as the electromagnetic wave propagating circuit
- Fig. 2 shows the plane wire mesh structure from which the cylindrical mesh of Fig. 1 may be formed
- Fig. 3 illustrates a modification of the cylindrical wire mesh employed in Fig. 1;
- Fig. 4 shows the plane wire mesh structure from which the cylindrical mesh of Fig. 3 may be formed
- Fig. 5 illustrates a modification of the cylindrical wire mesh of Fig. l in which one end is shaped for suitable matching
- Fig. 6 illustrates another modification of a matching termination for the cylindrical mesh shown in Fig. 1;
- Fig. 7 shows a travelling wave tube amplifier arrangement using a plurality of flat wire meshes as the phase slowing structures
- Fig. 8 illustrates another form of mesh structure.
- a travelling wave tube designated generally at 2 comprising an electron gun section 4, a collector anode 8, and a cylindrical wire mesh network 6 intermediate electron gun 4 and anode 8.
- Electron gun section 4 is shown as made up of a cathode 10 and an accelerating electrode 12.
- An axial electron stream indicated by line 14 is projected from the cathode 10 to collector anode 8. It is to be understood that structures for producing an axial electron stream are broadly old and that other structures than those described may be employed.
- Cylindrical wire mesh network 6 surrounds axial stream 14 and is axially aligned therewith. If desired, the axial electron stream may be directed adjacent the outer surface of said cylindrical mesh. As shown, cylindrical wire mesh 6 is provided with input lead 16 and output lead 18. Portions of waveguides or coaxial cable, not shown, may be coupled to said input and output leads in the conventional manner to serve as the radio frequency signal input and output circuits.
- a direct-current source of potential is applied between input lead 16 and cathode 10 by a battery 20, or any other suitable source. This potential is of such a magnitude that the velocity of electron stream 14, as it passes axially through or adjacent cylindrical mes-h 6, is adjusted so that amplification of the externally applied radio frequency signal is achieved as it is propagated along said cylindrical mesh.
- a source of positive potential B+ is applied to collector anode 8 in the usual manner.
- cylindrical mesh 6 is illustrated in Fig. 2 which shows said cylindrical mesh as being made up of a fiat lattice-like structure 6 consisting of co-planar diagonally intersecting wires. Although not essential to the invention, it is preferable to provide uniform spacing between successive wires in each diagonal plane.
- the serrated longitudinal edges 22 and 24 are so" arranged that when lattice-lil e structure 6' is formed into a right circular cylinder having a longitudinal axis corresponding to the longitudinal dimension L, the peaks 26 of serrated edge'22 will coincide with the peaks 28- of serrated edge 24;
- the diameter of the right circular cylinder thus formed is a function of the wide dimension D of said lattice-like structure.
- Wide dimension D may be conveniently chosen inasmuch as the phase velocity slowing characteristics of such a cylindrical mesh structure is independent of the diameter.
- the ends of lattice-like structure 6 may be terminated by parallel wires 36 and 32, respectively, which are perpendicular to the longitudinal dimension L.
- input lead 16 and output lead 18 are connected respectively to the midpoints of wiresfitl and 32.
- a wave front starting at input lead 16 willp roceed uniformly along the axis of cylindrical mesh 6 so-that, at any cross section perpendicular to the longitudinal axis of the cylinder there will be a Wave of constant phase around the circumference thereof.
- the phase velocity of the propagated wave is dependent only on the mesh structure employed. Accordingly, the mesh structure may be shaped to cylinders of any diameter without aifecting the phase velocity of the propagated electromagnetic wave.
- Fig. 3 illustrates a preferred embodiment of the invention.
- ends 36 and 38 of cylindrical mesh 4i? are linearly tapered in opposite directions so that the longitudinal dimension-of said cylindrical mesh gradually decreases from a maximum L1 to a minimum L2.
- This tapered cylindrical mesh may be constructed from the lattice-like hexagonal structure 39 consisting of co-planar diagonally intersecting wires as shown in Fig. 4. Successive wires of each diagonal plane may be uniformly spaced.
- Parallel serrated longitudinal edges 42 and 44 are of equal length and are so arranged that when hexagonal lattice-like structure 39' is formed into a longitudinal cylinder, the peaks of serrated edge 42 willcoincidewith the peaks of serrated'edge -3- to form the minimum longitudinal dimension L2 of Fig. 3.
- the diameter of the cylinder thus formed is a function of the wide dimension-D of said hexagonallattice-like structure.
- Apices A- and B of said hexagonal structure are both equidistant from serrated longitudinal edges 42 and 44 and the dimension A-B corresponds to the maximum longitudinal dimension L1 of Fig. 2.
- Input lead 16 and output lead 13 are connected respectively to apices A and B; By this arrangement, an electromagnetic wave starting at point A will'arrive at the same moment at all points along the line XX of'lattice-like structure 39.
- Fig. 7- illustrates a travelling wave tube amplifier embodying a plurality of flat or planar wire meshes of the type shown in Fig. 2 as the phase velocity'slowing structure.
- -- Flat lattice-like wire meshes 48, t and 52 are stacked one above the other in parallel arrangement.
- Ribbon-like electron streams 54 and 56 pass respectively between eachpair of wire nies'hes n'amely, 48 and 50 311656 anc'l 52, at'a' predetermined velocity.
- Figi' 7 illustrates a travelling wave tube amplifier embodying a plurality of flat or planar wire meshes of the type shown in Fig. 2 as the phase velocity'slowing structure.
- -- Flat lattice-like wire meshes 48, t and 52 are stacked one above the other in parallel arrangement.
- Ribbon-like electron streams 54 and 56 pass respectively between eachpair of wire nies'hes n'amely, 48 and 50 311656 anc'l 52, at'
- any other suitable number of wire meshes may be used, so long as they are stacked one above the other in parallel arrangement.
- antennas 58, 60 and 62 are connected to the input, or left hand, end of each of the planar wire meshes by Wires 64, 66, and" 68' respectively.
- the wave front of the input wave, indicated by arrows 59, is shown as arriving" at an angle to the direction of the electron how and the axial direction of the parallel arranged phase slowing mesh structuis' 48 52.
- the electron gun and collector anodes may be positioned conventionally at each end without interfering with the input radio-frequency signal.
- a particular incoming electromagnetic wavefront will excite the input antennas 5$-62 successively in time.
- the lengths of antenna connecting wires 64-68 are successively increased. Since the phase velocity along connecting wires 6463 is much greater than the phase velocity along the stacked wire meshes .4852, the electromagnetic waves arriving at a plane such a YY will he in phase.
- Antennas Til, 72, and 76 may be similarly connected to the respective output ends of planar wire meshes 58 52.
- Fig. 8 illustrates another form of phase'delaying structure which maybe employedin the embodimentsshown in Fig. l and Fig. 7
- This type of phase delaying structure may constitute a fiat metal sheet '78 having oblongshaped perforations 36. As shown, the perforations are staggered so as to interleave with each other.
- an electromagnetic wave slowing structure comprising a wire mesh cylinder intermediate said electron source and said collector anode, means associated with said electron source for propagating an electron stream through the longitudinal axis of said Wire mesh cylinder, and means for propagating an electromagnetic wave along the surface of said wire mesh cylinder whereby amplification of said propagating wave is achieved by the interaction of said wave and said electron stream.
- an electromagnetic wave slowing structure comprising a Wire mesh'cylinder intermediate said electron source and said collector anode; means associated with said electron source forprojecting-an electron stream about the periphery of said wire mesh cylinder from said source to said collector anode at'a predetermined velocity, and means for propagating an electromagnetic wave along the surface of said wire mesh cylinderwhereby amplification'of said propagating wave is achieved by the interactionof said wave and said electron stream.
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Description
B. KAZAN 2,774,005
SLOW-WAVE STRUCTURES FOR TRAVELLING WAVE TUBES Dec. 11, 1956 Filed Oct. 3, 195] FIG.
RF OUTPUT RFINPUT FIG. 2
INVENTOR.
BENJAMIN KAZAN A/fraey RF OUT FIG. 5
United States Patent G SLOW-WAVE STRUCTURES FOR TRAVELLING WAVE TUBES Benjamin Kazan, Long Branch, N. J., assignor to the United States of America as represented by the Secretary of the Army Application October 3, 1951, Serial No. 249,611
Claims. (Cl. SIS-35) (Granted under Title 35, U. S. Code (1952), see. 266) The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the payment of any royalty thereon.
This invention relates to high frequency amplifiers of the travelling wave type and more particularly to travelling wave tube electromagnetic propagating wave structures for slowing the phase velocity thereof.
Travelling wave tube amplifiers heretofore known include a conductor, either in the form of a helix or a series of inter-connected baffles, past which an electromagnetic wave can propagate. The phase velocity of the electromagnetic wave as measured along the axis of the conducting structure is small comparedto the velocity along the surface of the conductor. An electron beam source is arranged to direct a stream of electrons adjacent the conductor, and where the conductor is in the form of a helix, the beam is usually directed axially through or adjacent the helix. In operation, the axial phase velocity of the electromagnetic wave is so related to the axial electron path that the electrons travel at a slightly hi her velocity than the axial phase velocity of the electromagnetic wave. This difference in travel velocity results in part of the kinetic energy of the electrons being converted into radio frequency energy and the electromagnetic wave propagated in the direction of the electron flow is thereby amplified. Such travelling wave tubes are particularly suited for employment as an amplifier of microwave frequencies.
However, when utilizing a conventional helix as the propagating or phase velocity slowing means, the axial phase velocity of the electromagnetic wave is limited by both the pitch and radius, or diameter, of the helix. Because of the helical pitch, the travelling wave fieldpropagated along the helix is skewed with respect to the axis thereof. Since the electrons interact with only those portions of the field parallel to the axis of the helix, it is apparent that if the skewed nature of the field can be eliminated, then a greater, or more favorable interaction, may occur, thereby increasing the gain of the tube. Also, it is Well known that for efficient operation at very high frequencies, each helix turn should be only a fraction of the operating Wavelength. Hence, helices with relatively small diameters must be utilized together with a very narrow electron beam. For controlling such a narrow beam, unusually high operating voltages and very strong magnetic fields are required.
It is therefore an object of this invention to provide an electromagnetic wave phase velocity slowing structure in a travelling wave tube which overcomes the aforesaid limitations.
It is a further object of this invention to provide an electromagnetic wave slowing structure in a travelling Wave tube wherein the axial phase velocity of the electromagnetic wave is independent of pitch and/or diameter.
It is still a further object of this invention to provide a Wire mesh as the electromagnetic wave phase velocity slowing structure in a travelling Wave tube amplifier.
In accordance with one feature of the present invention,
ice
there is provided an electromagnetic wave phase slowing structure for a travelling wave tube comprising a cylindrical wire mesh network with the electron stream passing adjacent the cylindrical mesh in the direction of the axis of the cylinder. An electromagnetic wave is propagated along the cylindrical mesh network and the axial electric field interacts with the electron stream to amplify the propagated signal. At any cross-section perpendicular to the axis of the cylinder, there will be an electromagnetic wave of constant phase around the circumference thereof.
In accordance with another feature of the present invention, the phase slowing structure comprises a plurality of planar wire mesh networks stacked one above the other in parallel arrangement. A flat, ribbon-like, electron stream is projected between each pair of said wire mesh networks to interact with an electromagnetic wave propagated substantially in phase on each of said planar mesh networks.
For a better understanding of the invention, together with other and further objects thereof, reference is had to the following description, taken in connection with the accompanying drawing in which:
Fig. 1 shows a travelling wave tube amplifier employing a cylindrical wire mesh as the electromagnetic wave propagating circuit;
Fig. 2 shows the plane wire mesh structure from which the cylindrical mesh of Fig. 1 may be formed;
Fig. 3 illustrates a modification of the cylindrical wire mesh employed in Fig. 1;
Fig. 4 shows the plane wire mesh structure from which the cylindrical mesh of Fig. 3 may be formed;
Fig. 5 illustrates a modification of the cylindrical wire mesh of Fig. l in which one end is shaped for suitable matching;
Fig. 6 illustrates another modification of a matching termination for the cylindrical mesh shown in Fig. 1;
Fig. 7 shows a travelling wave tube amplifier arrangement using a plurality of flat wire meshes as the phase slowing structures; and
Fig. 8 illustrates another form of mesh structure.
Referring now to the drawing, there is shown in Figure 1, a travelling wave tube designated generally at 2 comprising an electron gun section 4, a collector anode 8, and a cylindrical wire mesh network 6 intermediate electron gun 4 and anode 8. Electron gun section 4 is shown as made up of a cathode 10 and an accelerating electrode 12. An axial electron stream indicated by line 14 is projected from the cathode 10 to collector anode 8. It is to be understood that structures for producing an axial electron stream are broadly old and that other structures than those described may be employed.
Cylindrical wire mesh network 6 surrounds axial stream 14 and is axially aligned therewith. If desired, the axial electron stream may be directed adjacent the outer surface of said cylindrical mesh. As shown, cylindrical wire mesh 6 is provided with input lead 16 and output lead 18. Portions of waveguides or coaxial cable, not shown, may be coupled to said input and output leads in the conventional manner to serve as the radio frequency signal input and output circuits. A direct-current source of potential is applied between input lead 16 and cathode 10 by a battery 20, or any other suitable source. This potential is of such a magnitude that the velocity of electron stream 14, as it passes axially through or adjacent cylindrical mes-h 6, is adjusted so that amplification of the externally applied radio frequency signal is achieved as it is propagated along said cylindrical mesh. A source of positive potential B+ is applied to collector anode 8 in the usual manner.
The detailed construction of cylindrical mesh 6 is illustrated in Fig. 2 which shows said cylindrical mesh as being made up of a fiat lattice-like structure 6 consisting of co-planar diagonally intersecting wires. Although not essential to the invention, it is preferable to provide uniform spacing between successive wires in each diagonal plane. The serrated longitudinal edges 22 and 24 are so" arranged that when lattice-lil e structure 6' is formed into a right circular cylinder having a longitudinal axis corresponding to the longitudinal dimension L, the peaks 26 of serrated edge'22 will coincide with the peaks 28- of serrated edge 24; The diameter of the right circular cylinder thus formed is a function of the wide dimension D of said lattice-like structure. Wide dimension D may be conveniently chosen inasmuch as the phase velocity slowing characteristics of such a cylindrical mesh structure is independent of the diameter. The ends of lattice-like structure 6 may be terminated by parallel wires 36 and 32, respectively, which are perpendicular to the longitudinal dimension L. As shown, input lead 16 and output lead 18 are connected respectively to the midpoints of wiresfitl and 32.
In'operation, a wave front starting at input lead 16 willp roceed uniformly along the axis of cylindrical mesh 6 so-that, at any cross section perpendicular to the longitudinal axis of the cylinder there will be a Wave of constant phase around the circumference thereof. Thus the phase velocity of the propagated wave is dependent only on the mesh structure employed. Accordingly, the mesh structure may be shaped to cylinders of any diameter without aifecting the phase velocity of the propagated electromagnetic wave.
Fig. 3 illustrates a preferred embodiment of the invention. As shown in Fig. 3, ends 36 and 38 of cylindrical mesh 4i? are linearly tapered in opposite directions so that the longitudinal dimension-of said cylindrical mesh gradually decreases from a maximum L1 to a minimum L2. This tapered cylindrical mesh may be constructed from the lattice-like hexagonal structure 39 consisting of co-planar diagonally intersecting wires as shown in Fig. 4. Successive wires of each diagonal plane may be uniformly spaced. Parallel serrated longitudinal edges 42 and 44 are of equal length and are so arranged that when hexagonal lattice-like structure 39' is formed into a longitudinal cylinder, the peaks of serrated edge 42 willcoincidewith the peaks of serrated'edge -3- to form the minimum longitudinal dimension L2 of Fig. 3. The diameter of the cylinder thus formed is a function of the wide dimension-D of said hexagonallattice-like structure. Apices A- and B of said hexagonal structure are both equidistant from serrated longitudinal edges 42 and 44 and the dimension A-B corresponds to the maximum longitudinal dimension L1 of Fig. 2. Input lead 16 and output lead 13 are connected respectively to apices A and B; By this arrangement, an electromagnetic wave starting at point A will'arrive at the same moment at all points along the line XX of'lattice-like structure 39. Appropriate portions of waveguide or coaxial cable, not shown, maybe provided to match the input and outputcircuits. p
Other forms of matching may be employed, such as allowing the output end of the lattice-like network to taper down to a point, as shown in Fig. 5, or gradually have the diagonal Wires of the lattice-like structure change their angle, becoming more and more parallel to the axis ofithe cylindrical mesh'and then joining them to a solid cylinder' l-fi, as shown iii-Fig. 6.
Fig. 7- illustrates a travelling wave tube amplifier embodying a plurality of flat or planar wire meshes of the type shown in Fig. 2 as the phase velocity'slowing structure.-- Flat lattice-like wire meshes 48, t and 52 are stacked one above the other in parallel arrangement. Ribbon-like electron streams 54 and 56 pass respectively between eachpair of wire nies'hes n'amely, 48 and 50 311656 anc'l 52, at'a' predetermined velocity. 'Although three stacked sheets 'of wire mesh are shown in Figi' 7,
it is to be understood that any other suitable number of wire meshes may be used, so long as they are stacked one above the other in parallel arrangement. In order to propagate an electromagnetic wave along each of said wire meshes, antennas 58, 60 and 62 are connected to the input, or left hand, end of each of the planar wire meshes by Wires 64, 66, and" 68' respectively. In Fig; 7, the wave front of the input wave, indicated by arrows 59, is shown as arriving" at an angle to the direction of the electron how and the axial direction of the parallel arranged phase slowing mesh structuis' 48 52. By tilting the incoming wave front in such a manner, the electron gun and collector anodes may be positioned conventionally at each end without interfering with the input radio-frequency signal. As a result, a particular incoming electromagnetic wavefront will excite the input antennas 5$-62 successively in time. In order to compensate for this effect, the lengths of antenna connecting wires 64-68 are successively increased. Since the phase velocity along connecting wires 6463 is much greater than the phase velocity along the stacked wire meshes .4852, the electromagnetic waves arriving at a plane such a YY will he in phase. Antennas Til, 72, and 76 may be similarly connected to the respective output ends of planar wire meshes 58 52.
Fig. 8 illustrates another form of phase'delaying structure which maybe employedin the embodimentsshown in Fig. l and Fig. 7 This type of phase delaying structure may constitute a fiat metal sheet '78 having oblongshaped perforations 36. As shown, the perforations are staggered so as to interleave with each other.
While there have been described what at present is considered to he the preferred embodiments of the invention, it will be understood by those skilled in the art that various changes and modifications may be made herein without departing from the invention, and it is, therefore, aimed in the appended claims to cover all such modifications and changes as fall within the spirit and scopeof the invention.
What is claimed is:
1. In a travelling wave tube having an electron source at one'e'ndithereof and a collector anode at theother end, an electromagnetic wave slowing structure comprising a wire mesh cylinder intermediate said electron source and said collector anode, means associated with said electron source for propagating an electron stream through the longitudinal axis of said Wire mesh cylinder, and means for propagating an electromagnetic wave along the surface of said wire mesh cylinder whereby amplification of said propagating wave is achieved by the interaction of said wave and said electron stream. 7 I
2. In a travelling wave tube having an electron source at one end thereof and a collector anode at the other end, an electromagnetic wave slowing structure comprising a Wire mesh'cylinder intermediate said electron source and said collector anode; means associated with said electron source forprojecting-an electron stream about the periphery of said wire mesh cylinder from said source to said collector anode at'a predetermined velocity, and means for propagating an electromagnetic wave along the surface of said wire mesh cylinderwhereby amplification'of said propagating wave is achieved by the interactionof said wave and said electron stream.
3. The claim as define'd'in vclaim- 2 wherein said wire mesh cylinder: comprises alattice-like structure having coplanar diagonally intersecting wires.
4.The claim as defined in'claim3 wherein successive wires ineach diagonal plane are uniformly spaced;
5,. The claim; as'defined in claim 1 wherein the ends'of said wire mesh cylinder are linearly tapered in opposite directions whereby the longitudinal dimension of said mesh decreases gradually from a-maximum to aminimum.
References Cited in the file of this patent UNITED STATES PATENTS Snow June 12, 1934 Lindenblad Oct. 27, 1942 Allen Aug. 16, 1949 Hollingsworth et a1 June 20, 1950 6 Barnett Aug. 1, 1950 Lindenblad Dec. 11, 1951 Pierce May 10, 1955 FOREIGN PATENTS France July 18, 1951
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US249611A US2774005A (en) | 1951-10-03 | 1951-10-03 | Slow-wave structures for travelling wave tubes |
US627717A US2831142A (en) | 1951-10-03 | 1956-10-26 | Slow-wave structures |
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US249611A US2774005A (en) | 1951-10-03 | 1951-10-03 | Slow-wave structures for travelling wave tubes |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2836758A (en) * | 1953-10-12 | 1958-05-27 | Varian Associates | Electron discharge device |
US2880417A (en) * | 1955-02-11 | 1959-03-31 | Lockheed Aircraft Corp | Traveling wave device |
US2898507A (en) * | 1953-08-14 | 1959-08-04 | M O Valve Co Ltd | Electric travelling wave amplifiers |
US2932761A (en) * | 1956-05-31 | 1960-04-12 | Csf | Traveling wave tube |
US2957103A (en) * | 1954-08-19 | 1960-10-18 | Hughes Aircraft Co | High power microwave tube |
US2992356A (en) * | 1956-07-31 | 1961-07-11 | Rca Corp | Traveling wave amplifier tube |
US2997618A (en) * | 1959-07-21 | 1961-08-22 | Dean A Watkins | Bar-strapped multifilar helix for traveling-wave tube |
US3002123A (en) * | 1957-01-11 | 1961-09-26 | Rca Corp | Traveling wave tube structure |
US3076115A (en) * | 1956-07-05 | 1963-01-29 | Rca Corp | Traveling wave magnetron amplifier tubes |
US3944326A (en) * | 1972-10-17 | 1976-03-16 | Max-Planck-Gesellschaft Zur Forderung Der Wissenschaften E.V. | Waveguide |
US4612476A (en) * | 1984-08-06 | 1986-09-16 | The United States Of America As Represented By The Secretary Of The Army | Broadband transverse field interaction continuous beam amplifier |
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US1962218A (en) * | 1931-04-03 | 1934-06-12 | Rca Corp | Vacuum tube |
US2300052A (en) * | 1940-05-04 | 1942-10-27 | Rca Corp | Electron discharge device system |
US2479288A (en) * | 1944-03-08 | 1949-08-16 | Allen William Douglas | Flexible electromagnetic wave guide |
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US2516944A (en) * | 1947-12-18 | 1950-08-01 | Philco Corp | Impedance-matching device |
FR993156A (en) * | 1949-06-08 | 1951-10-29 | Thomson Houston Comp Francaise | Structure ensuring a reduction in the propagation speed of an electromagnetic wave |
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US2708236A (en) * | 1950-03-18 | 1955-05-10 | Bell Telephone Labor Inc | Microwave amplifiers |
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US1962218A (en) * | 1931-04-03 | 1934-06-12 | Rca Corp | Vacuum tube |
US2300052A (en) * | 1940-05-04 | 1942-10-27 | Rca Corp | Electron discharge device system |
US2479288A (en) * | 1944-03-08 | 1949-08-16 | Allen William Douglas | Flexible electromagnetic wave guide |
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US2578434A (en) * | 1947-06-25 | 1951-12-11 | Rca Corp | High-frequency electron discharge device of the traveling wave type |
US2516944A (en) * | 1947-12-18 | 1950-08-01 | Philco Corp | Impedance-matching device |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
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US2898507A (en) * | 1953-08-14 | 1959-08-04 | M O Valve Co Ltd | Electric travelling wave amplifiers |
US2836758A (en) * | 1953-10-12 | 1958-05-27 | Varian Associates | Electron discharge device |
US2957103A (en) * | 1954-08-19 | 1960-10-18 | Hughes Aircraft Co | High power microwave tube |
US2880417A (en) * | 1955-02-11 | 1959-03-31 | Lockheed Aircraft Corp | Traveling wave device |
US2932761A (en) * | 1956-05-31 | 1960-04-12 | Csf | Traveling wave tube |
US3076115A (en) * | 1956-07-05 | 1963-01-29 | Rca Corp | Traveling wave magnetron amplifier tubes |
US2992356A (en) * | 1956-07-31 | 1961-07-11 | Rca Corp | Traveling wave amplifier tube |
US3002123A (en) * | 1957-01-11 | 1961-09-26 | Rca Corp | Traveling wave tube structure |
US2997618A (en) * | 1959-07-21 | 1961-08-22 | Dean A Watkins | Bar-strapped multifilar helix for traveling-wave tube |
US3944326A (en) * | 1972-10-17 | 1976-03-16 | Max-Planck-Gesellschaft Zur Forderung Der Wissenschaften E.V. | Waveguide |
US4612476A (en) * | 1984-08-06 | 1986-09-16 | The United States Of America As Represented By The Secretary Of The Army | Broadband transverse field interaction continuous beam amplifier |
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