US2410396A - High efficiency magnetron - Google Patents

High efficiency magnetron Download PDF

Info

Publication number
US2410396A
US2410396A US473557A US47355743A US2410396A US 2410396 A US2410396 A US 2410396A US 473557 A US473557 A US 473557A US 47355743 A US47355743 A US 47355743A US 2410396 A US2410396 A US 2410396A
Authority
US
United States
Prior art keywords
cavity
anode
magnetron
oscillating
loop
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
Application number
US473557A
Inventor
Percy L Spencer
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.)
Raytheon Co
Original Assignee
Raytheon Manufacturing Co
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 Raytheon Manufacturing Co filed Critical Raytheon Manufacturing Co
Priority to US473557A priority Critical patent/US2410396A/en
Application granted granted Critical
Publication of US2410396A publication Critical patent/US2410396A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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

Definitions

  • This invention relates to a magnetron, and more particularly to a magnetron which generates oscillations within one or more cavities formed within its anode structure, and in which the frequency of said oscillations is determined primarily by the geometry of said cavities.
  • An object of the present invention is to increase the ease of transfer of energy from one oscillating anode cavity to another in a plural cavity magnetron.
  • A-further object is to decrease the effect of the spacing between the anode arms at the entrance to the anode cavity on the generated frequency.
  • a still further object isto contribute to each of the foregoing objects by increasing the ratio between the inductance and capacity of each oscillating cavity within certain limits.
  • Fig. 1 is a transverse section of a magnetron embodying my invention, taken along line l-l of Fig. 2; 1
  • Fig. 2 is a longitudinal cross-section taken along line 2-2 of Fig. 1;
  • Fig. 3 is a cross-section similar to that of Fig. l of another embodiment of my invention taken along line 3-3 of Fig. 4;
  • Fig. 4 is a longitudinalcross-section taken along line l--4. of Fig. 3.
  • the magnetron illustrated in Figs. 1 and 2 comprises an envelope l which is preferably made of a block of conducting material, such as copper. This block forms the anode structure of the magnetron.
  • the block has hollow end sections which are covered by caps 2 and 3, likewise of conductive West t er 2 l t... material, such as popper.
  • the portion i is provided with a central bore 5 within which is supported, substantially at the center thereof, a cathode 6 which may be of, the indirectly-heated oxidecoated thermionic type.
  • Light conducting shields l and 8 may be supported adjacent the upper and lower ends of the cathode 6 so as to prevent electron beams from being projected out toward the end caps 2 and 3.
  • the cathode is supported by a pair of cathode lead-in conductors 9 and IE! sealed through the glass seals 1 l andlZ mounted at the outer ends of pipes l3 and M hermetically fastened within the walls of the block I adjacent the upper and lowerhollovv. end sections.
  • a plurality of cavities l 5 is formed in the bridging portion 4, and xtend radially from the central bore 5.
  • Each cavity it possesses apair of side arms it, the arms 56 between adjacent cavities serving jointly as one of the side arms forsaidadjacent cavities.
  • the forward faces of the arms l5 form electron-receiving anode segments with relatively small spacing between each arm, thus presenting a plurality of slots to the electron stream emanating from the cathode 5.
  • each anode cavity of a plural cavity magnetron have extended back from the entrance slots. substantially parallel with each other.
  • the operation of such a device is improved when the side arms of each anode cavity [5 diverge from each other, preferably to as great an extent as possible.
  • the side arms l6 diverge in this way substantially to the rear of their associated cavities, Where the back wall of each cavityextends around to join the two side Walls toeach other.
  • each side arm 6 with straight side walls which converge from the inner end of said arm toward the rear of the associated cavity l5 for an appreciable distance.
  • the frequency of the oscillations generated by each anode cavity i5 is determined primarily by the space between the side Walls of the cavity and the size of the cavity loop. Diverging the side arms of the cavity. as described above, does two things. First, by introducing a greater separation between the side walls of the cavity, the capacity is decreased; and second',,b y increasing Between the hollow end sections of the block l. is located.- a centrallye.
  • the inductance thereof is increased.
  • the product of capacity and inductance is a constant.
  • the inductance may be increased relative to the decrease in capacity so that the resonant frequency of my device remains substantially the same as that of prior devices of similar size.
  • R efiective resistance of the oscillating circuit to the oscillatory currents.
  • each anode oscillating loop With a relatively small gap between the ends of the side arms and having those arms diverge sharply from the gap as above described, I have found that the improvements due to decreased capacity, increased inductance and correspondingly increased values of Q readily can be obtained. If an attempt were made to secure these improvements by increasing the size of the gap at the entrance to the oscillating loop, several adverse effects would be produced. With such an enlarged gap, in order to produce the desired frequency, the physical size of the loop would have to be increased to such an extent as to unduly enlarge the overall tube dimensions. Also the propagation of energy from one oscillating loop to the next would be slowed down, introducing relatively large phase diiferences between vartrons describe orbits about the cathode. For
  • the circular component of electronic speed around the cathode adjacent the anode surfaces should be substantially equal to the rate at which the generated wave is propagated from loop to loop around the tube.
  • the slowing down of the propagated wave which would result from an increase in the size of the entrance gap to each oscillating loop would tend to upset this desired condition of equality, and thus decrease the effectiveness of operation of the tube.
  • the most satisfactory spacing between the side arms of each oscillating loop at the entrance gap thereto is of the order of that at which the transit time of electrons passing across the gap is less than about a quarter of a cycle of the oscillations which the tube is adapted to gener ate.
  • the other end of the coupling loop I9 is connected to a lead wire 20 which passes through .
  • mounted at the outer end of a pipe 22 likewise hermetically fastened through the wall of the envelope I.
  • An additional conducting pipe, not shown, may be electrically connected to the pipe 22, and forms with the wire 20 a concentric line through which the high frequency oscillations generated by the magnetron may be conducted to a, suitable utilization circuit.
  • the device shown in these figures comprises an envelope 3! which is likewise made of a block of conducting material, such as copper.
  • the ends of the block are covered by caps 32 and 33 likewise formed of conductive material, such as copper.
  • is formed with'a central annular projection 34 in which are cut a number of longitudinal slots 35.
  • a plurality of radial plates 36 is fastened into the slots 35, preferably by being soldered therein with a silver solder.
  • the plates 36 may be stamped out of a sheet of highly conductive copper.
  • the plates 36 thus form side arms of a plurality of oscillatin anode cavities similar to those described in connection with Fig. l.
  • the inner ends of the plates 36 form anode faces which cooperate with a cathode 31 supported substantially centrally of said anode faces.
  • the cathode 31 may be of a type similar to the cathode 6 of Fig. 1.
  • light conducting shields 38 and 39 may be supported adjacent the upper and lower ends of the cathode 31.
  • the cathode itself is supported by a pair of cathode lead-in conductors 40 and 4
  • the oscillations which are set up Wtihin the device shown in Figs. 3 and 4 may be led out from the tube by means of a couplin loop M connected to a lead wire 45 which passes from the tube through a pipe 36 in a manner similar to that described in connection with the loop l9 and conductor 20 of the arrangement shown in Figs. 1 and 2.
  • An anode structure for an electron-discharge device of the magnetron type comprising: a cylindrical body provided with a plurality of inwardly-directed, radially-disposed vanes; each of said vanes having straight side walls which converge from the inner ends thereof toward said cylindrical body for an appreciable distance from said inner ends; adjacent vanes being connected to each other through said cylindrical body, and

Landscapes

  • Microwave Tubes (AREA)

Description

Oct. 29, 1946.
P. L. SPENCER I HIGH EFFICIENCY MAGNETRON Filed Jan. 25, 1945 2 Sheets-Sheet 1 INVENTOR.
Patented Oct. 29, 1943 HIGH EFFHJIENCY MAGNETRON Percy L. Spencer, West Newton, Mass, assignor to Raytheon Manufacturing Company, Newton, Mass, a corporation of Delaware Application January 25, 1943, Serial No. 473,557 7 2 Claims. 1
This invention relates to a magnetron, and more particularly to a magnetron which generates oscillations within one or more cavities formed within its anode structure, and in which the frequency of said oscillations is determined primarily by the geometry of said cavities.
With prior devices of the above type, where a plurality of oscillating cavities were used and the oscillations were led off through coupling means associated with one of said cavities, energy was fed from one cavity to the next with subsequent difiiculty, resulting in a decrease in efiiciency. Alsosaid prior devices were very critical as to the spacing between the side walls at the entrance to the cavity, thus introducing the problem of extensive andtimeeconsuming machine work and constructing such cavities within the necessary critical tolerances.
An object of the present invention is to increase the ease of transfer of energy from one oscillating anode cavity to another in a plural cavity magnetron.
A-further object is to decrease the effect of the spacing between the anode arms at the entrance to the anode cavity on the generated frequency.
A still further object isto contribute to each of the foregoing objects by increasing the ratio between the inductance and capacity of each oscillating cavity within certain limits.
The foregoing and other objects of this invention will be best understood from the following description of exemplifications thereof, reference being had to the accompanying drawings, wherein:
Fig. 1 is a transverse section of a magnetron embodying my invention, taken along line l-l of Fig. 2; 1
Fig. 2 is a longitudinal cross-section taken along line 2-2 of Fig. 1;
Fig. 3 is a cross-section similar to that of Fig. l of another embodiment of my invention taken along line 3-3 of Fig. 4; and
Fig. 4 is a longitudinalcross-section taken along line l--4. of Fig. 3.
The magnetron illustrated in Figs. 1 and 2 comprises an envelope l which is preferably made of a block of conducting material, such as copper. This block forms the anode structure of the magnetron. The block has hollow end sections which are covered by caps 2 and 3, likewise of conductive West t er 2 l t... material, such as popper.
bridging portion i. The portion i is provided with a central bore 5 within which is supported, substantially at the center thereof, a cathode 6 which may be of, the indirectly-heated oxidecoated thermionic type. Light conducting shields l and 8 may be supported adjacent the upper and lower ends of the cathode 6 so as to prevent electron beams from being projected out toward the end caps 2 and 3. The cathode is supported by a pair of cathode lead-in conductors 9 and IE! sealed through the glass seals 1 l andlZ mounted at the outer ends of pipes l3 and M hermetically fastened within the walls of the block I adjacent the upper and lowerhollovv. end sections. A plurality of cavities l 5 is formed in the bridging portion 4, and xtend radially from the central bore 5. Each cavity it possesses apair of side arms it, the arms 56 between adjacent cavities serving jointly as one of the side arms forsaidadjacent cavities. The forward faces of the arms l5 form electron-receiving anode segments with relatively small spacing between each arm, thus presenting a plurality of slots to the electron stream emanating from the cathode 5.
Heretofore the side arms of each anode cavity of a plural cavity magnetron have extended back from the entrance slots. substantially parallel with each other. However, the operation of such a device is improved when the side arms of each anode cavity [5 diverge from each other, preferably to as great an extent as possible. As shown in Fig. 1, the side arms l6 diverge in this way substantially to the rear of their associated cavities, Where the back wall of each cavityextends around to join the two side Walls toeach other.
This divergence is attained by providing each side arm 6 with straight side walls which converge from the inner end of said arm toward the rear of the associated cavity l5 for an appreciable distance.
The frequency of the oscillations generated by each anode cavity i5 is determined primarily by the space between the side Walls of the cavity and the size of the cavity loop. Diverging the side arms of the cavity. as described above, does two things. First, by introducing a greater separation between the side walls of the cavity, the capacity is decreased; and second',,b y increasing Between the hollow end sections of the block l. is located.- a centrallye.
the transverse area of the cavity, the inductance thereof is increased. For a predetermined resonant frequency, the product of capacity and inductance is a constant. In accordance with my invention, the inductance may be increased relative to the decrease in capacity so that the resonant frequency of my device remains substantially the same as that of prior devices of similar size. According to well-known circuit theory at lower wave lengths,
LIL R where w=21rf f=frequency of the oscillations produced L=inductance of the oscillating circuit, and
R=efiective resistance of the oscillating circuit to the oscillatory currents.
By analogy with the above theory, we may consider that the inductance of each oscillating loop in my ultra-high frequency tube is increased enough to raise the Q of my system to a considerable degree. The higher the Q of such a device as I have disclosed becomes, the less will be the influence exerted by changes in voltage and electronic conditions, such as cathode emission, upon the frequency at which the device operates. Since under normal practical operating conditions, changes of the above nature inevitably occur, the increased Q of my device results in operation with a much more constant frequency.
By constructing each anode oscillating loop with a relatively small gap between the ends of the side arms and having those arms diverge sharply from the gap as above described, I have found that the improvements due to decreased capacity, increased inductance and correspondingly increased values of Q readily can be obtained. If an attempt were made to secure these improvements by increasing the size of the gap at the entrance to the oscillating loop, several adverse effects would be produced. With such an enlarged gap, in order to produce the desired frequency, the physical size of the loop would have to be increased to such an extent as to unduly enlarge the overall tube dimensions. Also the propagation of energy from one oscillating loop to the next would be slowed down, introducing relatively large phase diiferences between vartrons describe orbits about the cathode. For
maximum effectiveness, the circular component of electronic speed around the cathode adjacent the anode surfaces should be substantially equal to the rate at which the generated wave is propagated from loop to loop around the tube. Thus the slowing down of the propagated wave which would result from an increase in the size of the entrance gap to each oscillating loop would tend to upset this desired condition of equality, and thus decrease the effectiveness of operation of the tube. The most satisfactory spacing between the side arms of each oscillating loop at the entrance gap thereto is of the order of that at which the transit time of electrons passing across the gap is less than about a quarter of a cycle of the oscillations which the tube is adapted to gener ate. Due to diverging arrangements of the anode arms in my construction, slight variations in the spacing between the ends of the arms produce smaller changes in capacity than in the case of 4 previous constructions. Therefore, the over-all effect of my novel construction is to produce a device in which the spacing between the anode arms is not critical, and in which the tolerances of any machine work which might be necessary are substantially increased.
As already pointed out, my structure produces an increase in the transverse cross-sectional opening of each loop I5. I have found that in addition to this factor, increasing the inductance of the cavity, the ease of transfer of energy from one oscillating loop to the next is substantially increased, thus producing an increase in efficiency of the device.
When a magnetron such as I have described above is placed between suitable magnetic poles l! and I8 to create a longitudinal magnetic field and the device is energized, oscillations are set up in each of the oscillating loops l5. The oscillatory energy thus generated in each of the loops I5 is readily propagated through the tube by transfer from one loop to the next, so that this energy may be led out readily from the tube by means of a coupling loop l9 extending into one of the oscillating loops l5 and having one end thereof fastened to the inner wall of said oscillating loop. The other end of the coupling loop I9 is connected to a lead wire 20 which passes through .a glass seal 2| mounted at the outer end of a pipe 22 likewise hermetically fastened through the wall of the envelope I. An additional conducting pipe, not shown, may be electrically connected to the pipe 22, and forms with the wire 20 a concentric line through which the high frequency oscillations generated by the magnetron may be conducted to a, suitable utilization circuit.
Since the spacing between theends of the an ode arms which forms the gap at the entrance to each oscillating cavity is not critical, my invention lends itself to constructions in which fine machine work is completely eliminated and which may be assembled from approximately machined parts and stamped members. Such an arrangement is shown in Figs. 3 and 4. The device shown in these figures comprises an envelope 3! which is likewise made of a block of conducting material, such as copper. The ends of the block are covered by caps 32 and 33 likewise formed of conductive material, such as copper. The envelope 3| is formed with'a central annular projection 34 in which are cut a number of longitudinal slots 35. The machine work necessary for the formation of the envelope 3| and the slots 35 need not be of a very fine nature, since slight variations in the dimensions of the resulting structure do not have very marked effects on the operation of the device. A plurality of radial plates 36 is fastened into the slots 35, preferably by being soldered therein with a silver solder. The plates 36 may be stamped out of a sheet of highly conductive copper. The plates 36 thus form side arms of a plurality of oscillatin anode cavities similar to those described in connection with Fig. l. The inner ends of the plates 36 form anode faces which cooperate with a cathode 31 supported substantially centrally of said anode faces. The cathode 31 may be of a type similar to the cathode 6 of Fig. 1. Here likewise light conducting shields 38 and 39 may be supported adjacent the upper and lower ends of the cathode 31. The cathode itself is supported by a pair of cathode lead-in conductors 40 and 4| which pass out from the envelope 3! through pipes 42 and 43 in a manner similar to that described in connection with the lead-in conductors 9 and ll! of the arrangement in Figs. 1 and 2. The oscillations which are set up Wtihin the device shown in Figs. 3 and 4 may be led out from the tube by means of a couplin loop M connected to a lead wire 45 which passes from the tube through a pipe 36 in a manner similar to that described in connection with the loop l9 and conductor 20 of the arrangement shown in Figs. 1 and 2.
It will be seen that the point at which the plates 36 approach each other most closely forms the entrance gap to each of the oscillating anode loops, which gap is presented to the electron stream emanating from the cathode 31. Furthermore the side walls of each of the oscillating gaps diverge from each other from the entrance gap as described in connection with the arrangement shown in Figs. 1 and 2, and thus the arrangement of Figs. 3 and 4 possesses the advantages of my invention as already described.
Of course it is to be understood that this invention is not limited to the particular details as described above as many equivalents will suggest themselves to those skilled in the art.
What is claimed is:
1. An anode structure for an electron-discharge device of the magnetron type comprising: a cylindrical body provided with a plurality of inwardly-directed, radially-disposed vanes; each of said vanes having straight side walls which converge from the inner ends thereof toward said cylindrical body for an appreciable distance from said inner ends; adjacent vanes being connected to each other through said cylindrical body, and
forming with the connecting portion of said body, 7
.-Perc'y L. Spencer, West Newton, Mass. HIGH EFFICIENCY MAGNETRON. Patent dated Oct. 29, 1946. Disclaimer filed June 15, 1950, by the inventor; the assignee, Raytheon Manufacturing Company, assenting.
Hereby enters this disclaimer to claim 201 said patent.
[Ofiicial Gazette July 11, 1950.]
US473557A 1943-01-25 1943-01-25 High efficiency magnetron Expired - Lifetime US2410396A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US473557A US2410396A (en) 1943-01-25 1943-01-25 High efficiency magnetron

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US473557A US2410396A (en) 1943-01-25 1943-01-25 High efficiency magnetron

Publications (1)

Publication Number Publication Date
US2410396A true US2410396A (en) 1946-10-29

Family

ID=23880029

Family Applications (1)

Application Number Title Priority Date Filing Date
US473557A Expired - Lifetime US2410396A (en) 1943-01-25 1943-01-25 High efficiency magnetron

Country Status (1)

Country Link
US (1) US2410396A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2429291A (en) * 1943-07-01 1947-10-21 Westinghouse Electric Corp Magnetron
US2437240A (en) * 1943-06-07 1948-03-09 Raytheon Mfg Co Space discharge device
US2438194A (en) * 1946-06-18 1948-03-23 Westinghouse Electric Corp Magnetron
US2452032A (en) * 1944-06-10 1948-10-26 Raytheon Mfg Co Electron discharge device of the magnetron type
US2458142A (en) * 1944-03-08 1949-01-04 Rca Corp Electrode assembly for electron discharge devices
US2475960A (en) * 1943-08-25 1949-07-12 Rca Corp Electron discharge device
US2585741A (en) * 1945-11-06 1952-02-12 Us Sec War Magnetron having modulating means
US2591976A (en) * 1945-03-22 1952-04-08 Rca Corp Electron discharge device utilizing cavity resonators
US2635210A (en) * 1946-03-01 1953-04-14 Millman Sidney Magnetron
US2639407A (en) * 1946-04-09 1953-05-19 Us Sec War Closed end magnetron
US2765425A (en) * 1946-03-01 1956-10-02 Millman Sidney Magnetron
US3078387A (en) * 1960-09-08 1963-02-19 Philips Corp Magnetron

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437240A (en) * 1943-06-07 1948-03-09 Raytheon Mfg Co Space discharge device
US2429291A (en) * 1943-07-01 1947-10-21 Westinghouse Electric Corp Magnetron
US2475960A (en) * 1943-08-25 1949-07-12 Rca Corp Electron discharge device
US2458142A (en) * 1944-03-08 1949-01-04 Rca Corp Electrode assembly for electron discharge devices
US2452032A (en) * 1944-06-10 1948-10-26 Raytheon Mfg Co Electron discharge device of the magnetron type
US2591976A (en) * 1945-03-22 1952-04-08 Rca Corp Electron discharge device utilizing cavity resonators
US2585741A (en) * 1945-11-06 1952-02-12 Us Sec War Magnetron having modulating means
US2635210A (en) * 1946-03-01 1953-04-14 Millman Sidney Magnetron
US2765425A (en) * 1946-03-01 1956-10-02 Millman Sidney Magnetron
US2639407A (en) * 1946-04-09 1953-05-19 Us Sec War Closed end magnetron
US2438194A (en) * 1946-06-18 1948-03-23 Westinghouse Electric Corp Magnetron
US3078387A (en) * 1960-09-08 1963-02-19 Philips Corp Magnetron

Similar Documents

Publication Publication Date Title
US2550614A (en) High-efficiency magnetron
US2566087A (en) Tube of the magnetron type for ultra-short waves
US2320860A (en) Electron discharge apparatus
US2304186A (en) Velocity modulated tube
US2410396A (en) High efficiency magnetron
US2411953A (en) Electron discharge device of the magnetron type
US2416303A (en) Secondary emissive shell resonator tube
US2243537A (en) Resonator grid structure
US2405611A (en) Electron beam amplifier
US2428612A (en) Magnetron
US2402983A (en) Electronic discharge tube
US2890384A (en) Traveling wave electronic devices
US2411535A (en) High-frequency electron discharge apparatus
US3096457A (en) Traveling wave tube utilizing a secondary emissive cathode
US2450023A (en) Electron discharge device of the magnetron type
USRE23337E (en) High efficiency magnetron
US2432827A (en) High efficiency magnetron
US2678404A (en) High-frequency electron discharge apparatus
US2464801A (en) Velocity-modulated electrondischarge device
US2992356A (en) Traveling wave amplifier tube
US2888609A (en) Electronic devices
US2984764A (en) Electron discharge devices of the magnetron type
US2437240A (en) Space discharge device
US2835844A (en) Electron beam deflection tube
US2423161A (en) Electron discharge device of the plural cavity resonator type