US2851630A - High power traveling-wave tube - Google Patents

Description

Sept. 9,1958 c. K. BIRDSALL 2,851,630

HIGH POWER TRAVELING-WAVE TUBE Filed April 13, 1955 7 2 Sheets-Sheet 1 FIG.

CHARLES K BIRDSALL INVENTOR ATTORNEY INPUTK c. K. BIRDSALLY HIGH POWER TRAVELING-WAVE TUBE Sept. 9,

2 Sheets-Sheet 2 Filed" April 15, 1955 FIG. 2

M m R T S N 0 R T C m PITCH.

HELIX P3, & P4

mm L E H 7 I v f F a {5, FRE uENcY- G N V F mm H E W B H A U G T H 3 C Err- V M W G DG. F RN um m w emu A R .BTIA 0 ID FIG. 4,

FREQUENCY CHARLES K. BlRDSALL INVENTOR ATTORNEY United States Patent HIGH POWER TRAVELING-WAVE TUBE Charles K. Birdsall, Los Angeles, Calif., assignor to Hughes Aircraft Company, Culver City, Calif., a corporation of Delaware Application April 13, 1955, Serial No. 501,212

Claims. (Cl. 315-35) This invention relates to high power microwave tubes and more particularly to a traveling-wave tube incorporating a larg? diameter helical slow-wave structure which possesses characteristics that greatly increase the startoscillation current for backward-wave oscillations.

As is presently known, it is advantageous in a travelingwave tube incorporating a helix to have a helix circumference of the order of a half wavelength at the operating frequency of the device in order to achieve very high power outputs at the higher frequencies. Helices this large allow very large beam currents to be employed at practical current densities. A tube with a large diameter helix is disclosed in a copending application for patent Serial No. 401,303, entitled Traveling-Wave Tube" filed by Dean A. Watkins and Horace R. Johnson, on December 30, 1953. In this type of tube, however, it is necessary to provide means for preventing the device from commencing backward-wave oscillations, i. e., to increase the start-oscillationcurrent for backward-wave oscillations.

It has been found that slight variations in the pitch of the helix in a tube of the aforementioned type may have little or no effect on its forward-wave gain characteristics but may have ,a very pronounced effect on the startoscillation current for backward-wave oscillations. By way of example, a slight change in the pitchof the turns for one-half the length of a large diameter helix with respect to the pitch of the turns of the remaining half may increase the start-oscillation current by approximately .8 times that of helix having a uniform pitch along its entire length. It is thus apparent that with the pitch change, the beam current employed for forward-wave amplification in such a device may be substantially increased without having backward-wave oscillations commence, as would have been the case with uniform pitch.

In accordance with the present invention, a high power traveling-wave tube is provided that incorporates a periodic slow-wave structure such as, for example, a large diameter helix, which has a plurality of sections of different pitch. Alternatively, in order to avoid reflections due to the abrupt changes in pitch, a slow-wave structure such as a large diameter helix, having either a progressively increasing or decreasing pitch is employed. In this manner, the start-oscillation current for backward-wave oscillations is increased to the extent that the device may be used effectively as a forward wave amplifier without other means of preventing the backward-wave oscillations.

It is therefore an object of this invention to provide an improved high power traveling-wave amplifier tube.

Another object of this invention is to provide a traveling-wave amplifier tube incorporating a helical slowwave structure requiiing substantially more current to commence backward-wave oscillations than in conventional structures of this type.

Still another object of this invention is to provide a traveling-wave tube incorporating a helical slow-wave structure constituted of a plurality of sections having dif- 2,851,630 Patented Sept. 9, 1958 ferent pitch to prevent backward-wave oscillations from commencing.

A further object of this invention is to provide a traveling-wave tube incorporating a helical slow-wave structure having either a progressively increasing or decreasing pitch to prevent backward-wave oscillations from commencing.

The novel features which are believed to be characteristic of the invention, both as to its organization and method of operation, together with further objects and advantages thereof, will be better understood from the following description considered in connection with the accompanying drawings in which several embodiments of the invention are illustrated by way of example. It is to be expressly understood, however, that the drawings, are

for the purpose of illustration and description only, and are not intended as a definition of the limits of the invention.

Fig. 1 is a diagrammatic sectional view in partial elevation of an embodiment of the invention together with associated circuitry;

Fig. 2 is an elevational view of an alternate embodiment of the helical slow-wave structure of the present invention; and

Figs. 3 and 4 are illustrative diagrams of gain versus frequency.

Referring now to the drawings, Fig. 1 illustrates an embodiment of the present invention comprising an evacuated envelope 10 which consists of a long cylindrical portion 11 and an enlarged portion 12 at the left extremity, as viewed in the drawing. Enlarged portion 12 houses anelectron gun 14 which produces a hollow cylindrical elec tron stream. This electron stream is directed concentrically through the long cylindrical portion 11 to the opposite extremity thereof by asolenoid 15 where it is intercepted and collected by a collector electrode 16. In accordance with a preferred embodiment of the invention, a helical slow-wave structure 18 having a non-uniform pitch and provided with coaxial input andoutput cables 20 and 22, respectively, is disposed contiguously along the path of the electron stream intermediate theelectron gun 14 and the collector electrode 16.

More particularly,electron gun 14 comprises an annular cathode 24 with a heater 25 and an electron emitting surface 26, a focusing electrode 23, and anaccelerating electrode 30, theelectrodes 28 and 30 being provided with apertures in register with the electron emitting surface 26 of cathode 24 to allow passage therethrough of the hollow cylindrical electron stream. The electron emitting surface 26 is energized by means of abattery 32 connected across the heater 25, one terminal of which may be connected to the cathode 24, as shown. The focusing electrode 28 provides an inner and an outer surface of revolution adjacent to and about the electron emitting surface 26 of cathode 24 at an angle of approximately 67.5 with the longitudinal axis of thehelix 18, as shown in the drawing. Cathode 24 and focusing electrode 28 are connected together and are maintained at a potential of the order of 3000 volts negative with respect to ground by means of a connection therefrom to the negative terminal of abattery 34, the positive terminal of which is connected to ground.

Accelerating electrode 30 is disposed in a plane normal to the longitudinal axis ofhelix 18 and to the right of focusing electrode 28, as viewed in the drawing. Electrode 30 is maintained at a potential that is of the order of 200 volts positive with respect to ground by means of appropriate connections to a battery 36. An equipotential region is provided between theelectron gun 14 and thehelix 18 by means of a conductive coating 38 disposed about the inner periphery of the envelope 10 intermediate the focusing electrode 28 and thehelix 18. This '3 equipotential region is maintained at the same potential as the acceleratingelectrode 30 by means of a connection to the battery 36.

The hollow electron stream thus produced byelectron gun 14 is directed concentrically through thehelix 18 by means of thesolenoid 15 which is disposed concentrically about the envelope and is coextensive therewith. An appropriate direct current is made to flow through the solenoid to produce an axial magnetic field of the order of 600 gauss to constrain the electron stream throughout the active length of the tube. Thesolenoid 15 is thus energized by means of connections across a battery 38. The collector electrode 16, disposed so as to intercept the electron stream at the right extremity of envelope 10, as viewed in the drawing, is maintained at a potential more positive than that ofhelix 18 to suppress secondary electron emission. In the present case, this is accomplished by maintaining collector electrode 16 at a potential of the order of 50 volts positive with respect to ground by means of appropriate connections to abattery 40.

Disposed intermediate theelectron gun 14 and the collector electrode 16 is the helical slow-wave structure 18. An electromagnetic signal wave is launched on thehelix 18 by means of the input coaxial section 20. Coaxial section 20 has acenter conductor 42 which connects the high side ofinput terminals 44 directly to the first turn ofhelix 18 nearest theelectron gun 14. A resistor 46 is interconnected between thecenter conductor 42 of coaxial section 20 and ground in order to maintain thehelix 18 at quiescent ground potential. The outer conductor of coaxial section 20 is connected to aferrule 48 which is disposed concentrically about the first several turns of thehelix 18 on the outside of the envelope 10. The extremity offerrule 48 away fromelectron gun 14 is flared out in order to improve the impedance match between coaxial section 20 andhelix 18. The outer conductor of coaxial section 20 andferrule 48 may be maintained at any substantially fixed direct-current potential such as, for example, at ground by means of a connection thereto.

The output from the device of the present invention is provided by the outputcoaxial section 22.Section 22 has acenter conductor 50 which interconects the last turn ofhelix 18 farthest from theelectron gun 14 to the high side of output terminals 52. In addition, a matching ferrule 54 is disposed concentrically about the last several turns ofhelix 18 and connected to the outer conductor ofcoaxial section 22 which is, in turn, connected to ground in the same manner as is that of the input coaxial section 20.

As previously specified, the helical slow-wave structure 18 is of the type that has a large circumference as compared to a free space wavelength at its operating frequency, such as, for example, 0.2 to one-half a free space wavelength. The inner diameter of thehelical structure 18, on the other hand, is preferably of the order of 1.4 times the diameter of the hollow cylindrical electron stream produced byelectron gun 14. 'In accordance with a first embodiment of the invention, the length ofhelical structure 18 is constituted of a plurality of portions, each of which has a different pitch. As shown in Fig. 1, for example, the portions a, 1;, c, and d of thehelical structure 18 have pitches of p 2 p and p turns per inch, respectively. Alternatively, the pitch of the helical structure may be, in accordance with a second embodiment of the invention, made to progressively increase or decrease as represented by the helix 18a, shown in Fig. 2. Thehelix 18 or 18a maybe reversed, end for end, with respect to the direction of the electron stream, in which case the helix pitch would increase or decrease, respectively.

erated. For example, a typical backward-wave gain versus frequency characteristic 60 for a traveling-wave tube incorporating a helix having a uniform pitch is illustrated in Fig. 3. Referring to this figure, it is seen that the gain of a conventional tube increases sharply at the frequency,

This frequency, f is dependent upon the circumference and pitch of the helix and the velocity of the electron stream. It is thus apparent that, with a gain of this magnitude at the frequency i there would be a tendency for the tube to commence backward-wave oscillations as it only remains to satisfy the phase requirements for oscillation about the incremental feedback loop along the helix when the total gain about the equilavent feedback path is greater than unity.

However, it is possible to satisfy the conditions for backward-wave oscillations for only a portion of the length of the slow-wave structure. Hence, the backwardwave attenuation for a particular frequency over the remaining portion of its length cannot be relied upon to prevent backward-wave oscillations. Referring to Fig. 4, there are illustrated the gain characteristics for a constant velocity electron stream of thehelix 18 having pitches 121, 2 p and p and helix 18a having a progressively increasing or decreasing pitch, represented by dashedlines 62, 64, respectively. Thegain characteristic 62 ofhelix 18, for example, has backward-wave gain at frequencies f f ,f and f which correspond, respectively, to the pitches 1 1 p and The gain at any of the frequencies f f f and 1, may be of the order of l/ 64 that of a single helix having a single uniform pitch. Also, thegain characteristic 64 of the helix 18a extends over a comparatively broad portion of the frequency spectrum and may be of the order of l/ 20 that of a single uniform pitch helix, depending on the extent of the increase or decrease of pitch over the length of the helix. The forward wave gain, on the other hand, as represented by line 66 of Fig. 4, extends over a broad range of frequencies and is not substantially affected by the different pitches p 2 p and p ofhelix 18 or the progressively increasing or decreasing pitch of helix 18a. Thus, it is seen that thehelices 18 or 18a of the present invention may be employed as the slow-wave structure in a traveling-wave amplifier tube to substantially decrease the start-oscillation current for backward-wave oscillations.

More particularly, it may be shown that the conditions for backward-wave oscillations for a uniform pitch or periodic structure are met when the following relation exists:

CN 0.3 l4 l wherein C is the Pierce gain parameter of the device, and N is the total length of the uniform pitch or periodic slowwave structure in Wavelengths.

The Pierce gain parameter, C, however, is proportional to the one-third power of the beam current, i. e.

wherein I is the current represented by the electron beamproducedby electron gun 14. It is thus apparent that if I be designated as the start-oscillation current, i. e., the

current at which backward-wave oscillations commence, then I N=constant (3) ance with the device of the present invention, the length of the slow-wave structure is divided into n portions, prefer'ably of equal length, having different pitches. In this case, the Relation 3 for the commencement of backwardwave oscillations becomes I =c0nstant and from the ratio of Relations 3 and 4 An additional consideration is the extent of the allowable variation between the pitches p p p and 12 In order to ascertain the maximum allowable variation in pitch, consideration must be given to the forward-wave gain characteristics of the device. In general, it can be shown that the forward-wave gain is down 3 decibels from its maximum where the ratio of the greatest to the smallest velocity by which the slow-wave structure propagates an electromagnetic wave is approximately equal to the quantity (1+2C) where, as before, C is the Pierce gain parameter. In the case of thehelices 18 and 1801, the velocity at which an electromagnetic wave is propagated is directly proportional to the pitch. Thus p largest p smallest (6) In the case of a high power traveling-wave amplifier tube, a typical value of C is 0.1 or larger. Hence the ratio of the largest to the smallest pitch should be equal to or less than 1.1.

On the other hand, in order to determine the closeness with which the pitch of two different portions of the slow-Wave structure may differ, it is necessary to consider the variation of frequency with pitch. It may be shown that a 1% pitch variation is sufficient to shift the frequency, f at which maximum gain occurs by at least 1%. In that the width of the portion of the frequency spectrum amplified is only of the order of 0.2%, it is evident that a 1% change in frequency and hence pitch is more than adequate. Thus, from the foregoing it may be stated that the ratio of the pitch for any section of the slow-wave structure to the smallest pit-ch should be within the range from 1.01 to 1.10. It is, of course, desirable to make the changes in pitch as small as practicable and still satisfy the above relation so as to effect maximum forward wave gain and in addition make the changes occur over a transition region so as to minimize reflections.

What is claimed is:

1. A traveling-wave amplifier tube comprising a helical slow-Wave structure having a plurality of different pitches and a circumference per turn of not less than 0.2 free space wavelength at the mid-frequency of operation of the tube, means for launching an electromagnetic signal wave along said helical slow-wave structure, means for producing a hollow, cylindrical electron stream having a cross-sectional area that is small compared to the cross-sectional area of said helical slow-wave structure, and means for directing said electron stream contiguously along said helical slow-wave structure at a velocity to amplify said signal wave, whereby said different pitches of said helical slow-wave structure substantially decrease the maxium overall backward-wave gain of said tube to minimize backward-wave oscillations, the inner diameter of said slow-wave structure being of the order of 1.4 times the diameter of said electron stream.

2. The traveling-wave amplifier tube as defined in claim 1 wherein said plurality of different pitches of said helical slow-wave structure is provided by a progressively increasing pitch in the direction of electron flow along said electron stream.

3. The traveling-wave amplifier tube as defined in claim 1 wherein said plurality of different pitches of said helical slow-wave structure is provided by a progressively decreasing pitch in the direction of electron flow along said electron stream.

4. The traveling-wave amplifier tube as defined in claim 1 wherein said plurality of different pitches of said helical slow-wave structure is provided by several portions of the length of said structure, each having a different uniform pitch.

5. The traveling-wave amplifier tube as defined in claim 4 wherein the ratios of the pitches of said portions to the minimum pitch thereof is from 1.01 to 1.1.

References Cited in the file of this patent UNITED STATES PATENTS UNITED STATES PATENT OFFICE CERTIFICATE @F 'COREQ Patent No, 2 851,, 630

Column 4,

CharlesK. Birdsall line 32 3 for "'l/ZO' read 1' 1/120 o IHQN September 9 1958 appears in the-printed specification correction and that the said Letters Signed and sealed "this 18th day of November 1958 (SEAL) Attest:

KARL 1H,, AXLINE Attesting Officer ROBERT C. WATSON Commissioner of Patents

Images