US2530171A - Magnetron output terminal - Google Patents

Magnetron output terminal Download PDF

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US2530171A
US2530171A US538971A US53897144A US2530171A US 2530171 A US2530171 A US 2530171A US 538971 A US538971 A US 538971A US 53897144 A US53897144 A US 53897144A US 2530171 A US2530171 A US 2530171A
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enlargement
chamber
generator
waveguide
passage
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Ernest C Okress
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CBS Corp
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Westinghouse Electric Corp
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/36Coupling devices having distributed capacitance and inductance, structurally associated with the tube, for introducing or removing wave energy
    • H01J23/40Coupling devices having distributed capacitance and inductance, structurally associated with the tube, for introducing or removing wave energy to or from the interaction circuit
    • H01J23/46Loop coupling devices

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  • This invention relates to output terminals and more particularly to magnetron output terminals which feed into a hollow wave guide.
  • the present invention contemplates use of a Y proper matching of impedances, energy transition, and enclosure in vacuum of parts subject to high voltage gradients, so as to avoid detrimental effects when the device is used under varying conditions oi external atmospheric pressure.
  • an object of the invention is to provide a construction presenting proper input admittance to the magnetron in vacuum while maintaining a suliciently low standing wave ratio in the remaining portions of the terminal exposed to prevailing atmospheric pressure.
  • a further object of the invention is to provide a terminal which, in its entirely, inclusive of the Wave guide in whole or in part, need not be maintained at vacuum or other xed pressure in order to prevent breakdown in use at high altitudes.
  • Yet another object of the invention is to mim'- mize the extent oi the region having to be evacuated and maintained under vacuum, and to otherwise provide a simplied sturdy construction.
  • Figure 1 is a sectional view of a portion of a magnetron and of a wave guide with my invention associated therewith;
  • Figure 2 is a sectional view on line II-II of Fig. 1;
  • Figure 3 is a sectional view on line III- III of Fig. 1.
  • the reference numeral I0 designates a part of a known ultra-high frequency generator, here shown as a magnetron,
  • a coaxial line means which includes a current probe or loop I l ofsuitable shape situated within a cavity I2 of the generator.
  • the interior of said generator is evacuated.
  • the desideratum is to transfer energy picked up by the loop II to a hollow wave guide I3 situated exterior to the generator and the hollow interior or passage of which is not evacuated and accordingly subject to the prevailing atmospheric pressure and condition where the device is in actual use whether that be next to the earth or at a high altitude where the air is more rareed.
  • Wave guides in general are known to the art and constitute a mean by which electromagnetic energy is propagated from one place to another before its ultimate transmission in free space orv utilization in some other instrumentality.
  • wave guides are rectangular in cross-section with one dimension greater than the other for purposes of obtaining the desired mode of oscillation and polarization of the Wave that may be transmitted.
  • the energy transmission means from generator to wave guide is identified by the general appellation thereto of terminal, and it is a feature of the present invention to construct this terminal with the part thereof next the wave guide sealed in order that the part next the generator may be evacuated with and subject to the same vacuum as the interior ⁇ of the generator, and to utilize the evacuated region in obtaining the desired electrical characteristics for the terminal.
  • the coaxial line means constituted by said terminal comprises, in addition to loop II abovementioned, a rod-like portion or inner coaxial member It, which extends into the wave guide, and tubular portion orY outer hollow member I5 coaxial with the rod portion and extending from the generator to the wave guide, and attached to both.
  • Said tubular portion I5 is constituted by a conductive base or thimble I6 which is hollow and preferably formed as a body of revolution.
  • One end of said thimble I6 has a threaded neck or basal' portion Il which screws into a side opening for the purpose in the magnetron and sealed, as by solder I8 therein.
  • One end of the loop I'I is secured to the inner end of this neck or basal portion Il so the loop is within the cavity I2 and so that the rod portion I t passes outward from the cavity coaxially through the central hole or I6.
  • the interior cylindrical wall is provided with an internal annular rabbet I9 and the exterior wall is provided with an external peripheral rabbet 20.
  • An end margin of an internal collar 2l is seated in the internal rabbet i9 and sealed, as by solder, to the thimble thereat.
  • the outer end of this collar is flanged outwardly, as at 22, so the flange is perpendicular to the axis of the collar and in a plane coincident with the near wall of the wave guide wall as a continuation of the inner surface thereof.
  • a glass bead 26 of predetermined thickness.
  • a borosilicate glass is employed in conjunction with which the said collar 2l and portion 21 of the rod i4 passing through the glass, are made of material having a corresponding coeicient of expansion, such a material being described in Patent 2,062,335 of December l, 1936, to Howard Scott and sold in the trade under the trade-mark Kovan Outside of and coaxial with collar 2l isr'a sleeve 28 of adequate strength for support purposes, such as brass, which has one end soldered in rabbet and its other end soldered against the near wall of wave guide I3.
  • rod HI is provided with an antenna head 2B preferably of flaring shape which has a transitional increase in diameter from the portion 21 of the rod toward the outer end of the head, and being shown as frustoconical and hollow.
  • the controlling factor for configuration of this antenna head is to obtain a smooth impedance transition from the coaxial line to the Wave guide, thereby obtaining gradual change without setting up the usual localized high electrical gradients thereat.
  • This antenna head at its larger end is sealed to the far wall of the wave guide i3 for obtaining a good electrical connection therewith.
  • said head is shown projecting through the said far wall of the wave guide, thereby enabling the soldering thereof to that wall to be accomplished at the outer side of the wall.
  • the axial length of the tapered antenna is less than half a wave guide wave length.
  • the thickness of glass bead 2B lengthwise of the rod is preferably a half wave vlength in dimension in the dielectric medium composing the bead referred to free space wave length.
  • the interior of the evacuated hollow portion of member l5 is provided with a transformer section of ypredetermined dimensions.
  • the preferred construction utilizes a passage in the neck portion of said member of smaller diameter than the diameter of passage or chamber 3
  • the passage 30 is of predetermined length and formed within a wall which protrudes as a ring 32 at its upper end into the lower part of the chamber 3
  • the end of the neck portion I1 of the member I5 terminating at the inner wall of the magnetron cavity has been designated as in a plane Po
  • the upper end of the smaller passage terminated by ring 32 has been designated as in a plane P1
  • plane of the inner surface of the near wall of the waveguide has been designated as plane P2.
  • the open end of the waveguide, which is shown flanged for attachment to any desired instrumentality is designated as at a plane P3.
  • Configuration and distance between planes Po and Pi have definite relationship for establishing the proper input admittance at the base of the loop at plane Po.
  • a constant voltage or current Rieke diagram is run with reference to plane P3 by means of a conventional waveguide coaxial terminal provided with means whereby variable react-ance and radiation resistance may be obtained.
  • the variable section is preadjusted, first for maximum output into a matched load in the waveguide and the Rieke taken, another Rieke is taken with the matching section set at of maximum power under the same conditions.
  • a Rieke diagram is a radio frequency output diagram of frequency, power and voltage contours, for constant current (or voltage, in which case the current contours are plotted), as a function of load impedance with respect to some plane of reference between the load and the base of the coupling loop of the magnetron.
  • the load impedance may be represented on a polar diagram whose radial coordinate denotes the real reflection coefficients and the angular coordinate denotes the phase angle with respect to the reference plane. One convolution of the angular coordinate corresponds to one-half wavelength.
  • the load impedance may also be represented on a circle diagram, or other suitable tranformation, in which case resistance and reactance comprise the coordinates.
  • a suitable operating point is selected from the above data and the corresponding impedance at the plane P3 obtained from the position of the minimum of standing wave pattern from the reference plane Ps of the magnetron, and standing Wave ratio (voltage).
  • Said operating point is an optimum point 0f operation as defined by the load impedance (or reflection coefficient and position of minimum) on a Rieke diagram referred to the reference plane of the magnetron, where a definite power output and pulling figure, consistent with a given anode voltage, anode current and magnetic field is obtained characteristic of the load and magnetron.
  • the terminal constructed in :accordance 'with my invention presents the .proper input admittance to the magnetron, in vacuum, while maintaining a low s tanding wave Yratio in the remaining portions ⁇ of the terminal, 'exposed to the prevailing atmospheric pressure. Since the hief-h electrical gradient of the transformer is within the evacuated region, it is not affected by change of external atmospheric-conditions and the device, inclusive of the waveguide section, functions as well at one elevation as another notwithstanding the atmospheric conditions may vary in the waveguide.
  • An output coupling from an ultra high frequency generator to a waveguide comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage there-in, said passage having an enlargement thereof at the end of the passage remote from the generator, said hollow member providing a chamber of greater diameter than said enlargement, a coaxial inner member extending from said generator to said waveguide coaxially of and through said passage, enlargement and chamber, a ring seated in said enlargement and projecting into said chamber and constituting with the wall of said chamber a transformer, and a vacuum seal for said chamber at the end thereof toward the waveguide whereby the passage, chamber and transformer are at the same vacuum as the generator, and the location and seating of said ring in the enlargement enabling the coupling to be assembled with a desired length of ring pro-- truding into the chamber and obtaining desired transformer characteristics.
  • An output coupling from an ultra high frequency generator to a waveguide comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage therein, said passage having a stepped enlargement at the end of the passage remote from the generator, said hollow member providing a chamber of greater diameter than said enlargement thereby constituting a second stepped enlargement of the hollow of said member, a coaxial inner member extending from said generator to said waveguide coaxially of the stepped hollow of said holiow member, a ring seated in the first mentioned enlargement and projecting into said chamber and constituting with the wall of said chamber a transformer, means vacuum sealing the end of said chamber remote from the generator and with the vacuum of the generator effective in said chamber and maintained by said means, and the location and seating of said ring in the first said enlargement and protruding into the second said enlargement enabling the coupling to be assembled with a desired length of ring protruding .into ⁇ the chamber :
  • Anoutput coupling from an ultra high frequency generator to a waveguide comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage therein, said passage having an enlargement thereof at the end of the passage remote from the generator, said hollow member, providing a chamber of greater diameter than said enlargement, a coaxial inner member extending from said generator to said waveguide coaxially of and through said passage, enlargement and chamber, a ring seated in said enlargement and projecting into said chamber and constituting with the wall of said chamber a transformer, said ring having an internal diameter equal to the diameter of the passage and an outer diameter equal to that of the first said enlargement, and a vacuum seal for said chamber at the end thereof toward the waveguide whereby the passage, chamber and transformer are at the same vacuum as the generator, and the location and seating of said ring in the enlargement enabling the coupling to be assembled with a desired length of ring protruding into the chamber and obtaining desired transformer characteristics.
  • An output coupling from an ultra high frequency generator to a waveguide comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage therein, said passage having a stepped enlargement at the end of the passage remote from the generator, said hollow member providing a chamber of greater diameter than said enlargement thereby constituting a second stepped enlargement of the hollow of said member and said second stepped enlargement of said member being again enlarged by a rabbet at the end of said member toward the waveguide, a collar seated in said rabbet and having a flange at its end toward the waveguide, said flange being connected to said waveguide,
  • a coaxial inner member extending from said generator to said waveguide coaxially of and through said hollow member and the passage, enlargement, chamber and rabbet thereof, a ring seated in the rst mentioned enlargement and projecting into said chamber and constituting with the 1 wall of said chamber a transformer, a glass bead sealed peripherally to said collar and sealed on and to said coaxial inner member and comprising a closure for said chamber at the end thereof toward the waveguide, a sleeve coaxial with and at the outside of said collar, said sleeve being rigidly connected at its ends to the said hollow member and waveguide respectively and protecting said collar from strains and distortions, the successve stepped enlargements of the hollow of the hollow member enabling the coupling to be assembled and a ring of desired length seated in the first enlargement and protruded into the second enlargement for obtaining desired transg@ former characteristics.

Description

Nov. 14, 1950 E. c. oKREss MAGNETRQN UTPUT TERMINAL Filed June 6. 1944 l l. ww 7 l m l MVM ATTORNEY Patented Nov. 14, 1950 TENT .OFFICE MAGNETRN OUTPUT TERMINAL Ernest il. Glrress, Montclair, N. J., assignor to Westinghouse Electric Corporation, East Pittsburgh, Pa., a corporation of Pennsylvania Application June 6, 1944, Serial No. 538,971
Claims.
This invention relates to output terminals and more particularly to magnetron output terminals which feed into a hollow wave guide.
In my prior application, Serial No. 461,135, led October 7, 1942, an output terminal is shown wherein energy transition from the coaxial conductor to the wave guide is accomplished as an open line exposed to atmospheric pressure. That structure is accordingly subject to high voltage gradient in air between the exposed end of the coaxial conductor and surrounding metallic parts. When the device is used at high altitudes, for instance in an airplane, the high voltage gradient and raried atmosphere combine to cause break-down or sparking between said exposed end of the coaxial conductor and the surrounding metallic parts.
The present invention contemplates use of a Y proper matching of impedances, energy transition, and enclosure in vacuum of parts subject to high voltage gradients, so as to avoid detrimental effects when the device is used under varying conditions oi external atmospheric pressure.
More specifically, an object of the invention is to provide a construction presenting proper input admittance to the magnetron in vacuum while maintaining a suliciently low standing wave ratio in the remaining portions of the terminal exposed to prevailing atmospheric pressure.
A further object of the invention is to provide a terminal which, in its entirely, inclusive of the Wave guide in whole or in part, need not be maintained at vacuum or other xed pressure in order to prevent breakdown in use at high altitudes.
Yet another object of the invention is to mim'- mize the extent oi the region having to be evacuated and maintained under vacuum, and to otherwise provide a simplied sturdy construction.
Still further objects will appear to those skilled in the art as the description progresses both lby direct recitation thereof and by inference from the context.
In the accompanying drawing wherein like numerals of reference indi-cate similar parts throughout the several views:
Figure 1 is a sectional view of a portion of a magnetron and of a wave guide with my invention associated therewith;
Figure 2 is a sectional view on line II-II of Fig. 1; and
Figure 3 is a sectional view on line III- III of Fig. 1.
In the specific embodiment of the invention i1- lustrated in said drawing, the reference numeral I0 designates a part of a known ultra-high frequency generator, here shown as a magnetron,
from which wave energy is derivable through a" coaxial line means which includes a current probe or loop I l ofsuitable shape situated within a cavity I2 of the generator. The interior of said generator is evacuated.
The desideratum is to transfer energy picked up by the loop II to a hollow wave guide I3 situated exterior to the generator and the hollow interior or passage of which is not evacuated and accordingly subject to the prevailing atmospheric pressure and condition where the device is in actual use whether that be next to the earth or at a high altitude where the air is more rareed. Wave guides in general are known to the art and constitute a mean by which electromagnetic energy is propagated from one place to another before its ultimate transmission in free space orv utilization in some other instrumentality. Usually wave guides are rectangular in cross-section with one dimension greater than the other for purposes of obtaining the desired mode of oscillation and polarization of the Wave that may be transmitted.
The energy transmission means from generator to wave guide is identified by the general appellation thereto of terminal, and it is a feature of the present invention to construct this terminal with the part thereof next the wave guide sealed in order that the part next the generator may be evacuated with and subject to the same vacuum as the interior` of the generator, and to utilize the evacuated region in obtaining the desired electrical characteristics for the terminal.
The coaxial line means constituted by said terminal comprises, in addition to loop II abovementioned, a rod-like portion or inner coaxial member It, which extends into the wave guide, and tubular portion orY outer hollow member I5 coaxial with the rod portion and extending from the generator to the wave guide, and attached to both.
Said tubular portion I5 is constituted by a conductive base or thimble I6 which is hollow and preferably formed as a body of revolution. One end of said thimble I6 has a threaded neck or basal' portion Il which screws into a side opening for the purpose in the magnetron and sealed, as by solder I8 therein. One end of the loop I'I is secured to the inner end of this neck or basal portion Il so the loop is within the cavity I2 and so that the rod portion I t passes outward from the cavity coaxially through the central hole or I6. At the outer endof the thimble the interior cylindrical wall is provided with an internal annular rabbet I9 and the exterior wall is provided with an external peripheral rabbet 20. An end margin of an internal collar 2l is seated in the internal rabbet i9 and sealed, as by solder, to the thimble thereat. The outer end of this collar is flanged outwardly, as at 22, so the flange is perpendicular to the axis of the collar and in a plane coincident with the near wall of the wave guide wall as a continuation of the inner surface thereof.
Within collar 2l the passage through hollow member i is sealed vacuum tight by -a glass bead 26 of predetermined thickness. Preferably a borosilicate glass is employed in conjunction with which the said collar 2l and portion 21 of the rod i4 passing through the glass, are made of material having a corresponding coeicient of expansion, such a material being described in Patent 2,062,335 of December l, 1936, to Howard Scott and sold in the trade under the trade-mark Kovan Outside of and coaxial with collar 2l isr'a sleeve 28 of adequate strength for support purposes, such as brass, which has one end soldered in rabbet and its other end soldered against the near wall of wave guide I3.
' Within the wave guide, rod HI is provided with an antenna head 2B preferably of flaring shape which has a transitional increase in diameter from the portion 21 of the rod toward the outer end of the head, and being shown as frustoconical and hollow. The controlling factor for configuration of this antenna head is to obtain a smooth impedance transition from the coaxial line to the Wave guide, thereby obtaining gradual change without setting up the usual localized high electrical gradients thereat. This antenna head at its larger end is sealed to the far wall of the wave guide i3 for obtaining a good electrical connection therewith. For ease of manufacture, said head is shown projecting through the said far wall of the wave guide, thereby enabling the soldering thereof to that wall to be accomplished at the outer side of the wall. This direct attachment of the antenna head of rod I4 to the wave guide wall completes the coaxial terminal as a closed line. Since the wave guide is operated in the fundamental mode, the axial length of the tapered antenna is less than half a wave guide wave length. The thickness of glass bead 2B lengthwise of the rod is preferably a half wave vlength in dimension in the dielectric medium composing the bead referred to free space wave length.
The interior of the evacuated hollow portion of member l5 is provided with a transformer section of ypredetermined dimensions. The preferred construction utilizes a passage in the neck portion of said member of smaller diameter than the diameter of passage or chamber 3| in the body of the said member. Furthermore, the passage 30 is of predetermined length and formed within a wall which protrudes as a ring 32 at its upper end into the lower part of the chamber 3|. This combination of different sizes of passage and chamber and length of smaller passage with the rabbeted section, and abrupt change of surface direction constitutes a transformer.
For convenience of reference, the end of the neck portion I1 of the member I5 terminating at the inner wall of the magnetron cavity has been designated as in a plane Po, and the upper end of the smaller passage terminated by ring 32 has been designated as in a plane P1, whereas plane of the inner surface of the near wall of the waveguide has been designated as plane P2. The open end of the waveguide, which is shown flanged for attachment to any desired instrumentality is designated as at a plane P3. Configuration and distance between planes Po and Pi have definite relationship for establishing the proper input admittance at the base of the loop at plane Po. When once determined and the device constructed, these dimensions and congurations remain constant. Determination of these dimensions and configurations has been realized by following a practical procedure outlined below, namely:
(a) A constant voltage or current Rieke diagram is run with reference to plane P3 by means of a conventional waveguide coaxial terminal provided with means whereby variable react-ance and radiation resistance may be obtained. The variable section is preadjusted, first for maximum output into a matched load in the waveguide and the Rieke taken, another Rieke is taken with the matching section set at of maximum power under the same conditions. By way of definition it may be stated a Rieke diagram is a radio frequency output diagram of frequency, power and voltage contours, for constant current (or voltage, in which case the current contours are plotted), as a function of load impedance with respect to some plane of reference between the load and the base of the coupling loop of the magnetron. The load impedance may be represented on a polar diagram whose radial coordinate denotes the real reflection coefficients and the angular coordinate denotes the phase angle with respect to the reference plane. One convolution of the angular coordinate corresponds to one-half wavelength. The load impedance may also be represented on a circle diagram, or other suitable tranformation, in which case resistance and reactance comprise the coordinates.
(b) A suitable operating point is selected from the above data and the corresponding impedance at the plane P3 obtained from the position of the minimum of standing wave pattern from the reference plane Ps of the magnetron, and standing Wave ratio (voltage). Said operating point is an optimum point 0f operation as defined by the load impedance (or reflection coefficient and position of minimum) on a Rieke diagram referred to the reference plane of the magnetron, where a definite power output and pulling figure, consistent with a given anode voltage, anode current and magnetic field is obtained characteristic of the load and magnetron.
(c) The conventional terminal is then reset to either maximum power output or 80% output into a matched line depending upon which setting produces the better Rieke contour from a functional point of view.
(d) The conventional output terminal (waveguide and coaxial feed) to plane Po is removed from the magnetron intact and to each end are attached lengths of line such that a four terminal net-work may be obtained which is an ideal transformer defined in terms of three constants, the transformer constant and two lengths of line.
(e) The operating point defined by the admittance at the plane P3 of the conventional terminal can then be transformed through this network to the base of the loop of the conventional terminal (plane Po) with the aid of four terminal network theory. z i
(f) Now, with amatched line beyond plane P1 in vthi-:proposed terminal, a transformer between Pn and P1 can be provided to give the desired admittance at plane Po.
(g) Next an adjustment of the terminal section looking toward plane P2 is required to obtain a standing wave ratio which is substantially lunity for the wavelength or wavelength band under consideration. lThis is done by providing a dummy terminal between plane P1 and P3 with extended sections of equivalent dimensions, `each withr probes, andthen feeding the desired energy into the coaxialprobed line to thematched `load in the waveguide.
i The terminal constructed in :accordance 'with my invention presents the .proper input admittance to the magnetron, in vacuum, while maintaining a low s tanding wave Yratio in the remaining portions `of the terminal, 'exposed to the prevailing atmospheric pressure. Since the hief-h electrical gradient of the transformer is within the evacuated region, it is not affected by change of external atmospheric-conditions and the device, inclusive of the waveguide section, functions as well at one elevation as another notwithstanding the atmospheric conditions may vary in the waveguide.
I claim:
1. An output coupling from an ultra high frequency generator to a waveguide, comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage there-in, said passage having an enlargement thereof at the end of the passage remote from the generator, said hollow member providing a chamber of greater diameter than said enlargement, a coaxial inner member extending from said generator to said waveguide coaxially of and through said passage, enlargement and chamber, a ring seated in said enlargement and projecting into said chamber and constituting with the wall of said chamber a transformer, and a vacuum seal for said chamber at the end thereof toward the waveguide whereby the passage, chamber and transformer are at the same vacuum as the generator, and the location and seating of said ring in the enlargement enabling the coupling to be assembled with a desired length of ring pro-- truding into the chamber and obtaining desired transformer characteristics.
2. An output coupling from an ultra high frequency generator to a waveguide, comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage therein, said passage having a stepped enlargement at the end of the passage remote from the generator, said hollow member providing a chamber of greater diameter than said enlargement thereby constituting a second stepped enlargement of the hollow of said member, a coaxial inner member extending from said generator to said waveguide coaxially of the stepped hollow of said holiow member, a ring seated in the first mentioned enlargement and projecting into said chamber and constituting with the wall of said chamber a transformer, means vacuum sealing the end of said chamber remote from the generator and with the vacuum of the generator effective in said chamber and maintained by said means, and the location and seating of said ring in the first said enlargement and protruding into the second said enlargement enabling the coupling to be assembled with a desired length of ring protruding .into `the chamber :and obtaining :desired:
transformer characteristics.
3. YAn output coupling from an ultra high frequency .generator to ya waveguide, comprising a hollow member having a basal end next to and projecting'fr'om said generator and saidbasal vend having a longitudinal passage therein, said ypassage having .a stepped enlargement at the end of the passage remote from the generator, said hollow y'member providing a chamber yof greater diameter than said enlargement thereby constituting 'a second stepped enlargement of the hollow of said member and said second stepped enlargement of rsaid member ybeing again enlargedby a rabbet at the end of said member towardv n the waveguide, a collar seated in :said Vrabbety fand having aange atits end toward the waveguide, said flange being connected to said waveguide, a coaxial 'inner member extendingfrom said generator to said waveguide coaxiallyof and through said hollow member and the passage, enlargement, chamber andrabbet thereof, a ring seated in the first mentioned enlargement and projecting into said chamber and constituting with the wall of said chamber a transformer, a glass bead sealed peripherally to said collar and sealed on and to said coaxial inner member and comprising a closure for said chamber at the end thereof toward the waveguide, the successive stepped enlargements of the hollow of the hollow member enabling the coupling to be assembled and a ring of desired length seated in the rst enlargement and protruded into the second enlargement for obtaining desired transformer characteristics.
4. Anoutput coupling from an ultra high frequency generator to a waveguide, comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage therein, said passage having an enlargement thereof at the end of the passage remote from the generator, said hollow member, providing a chamber of greater diameter than said enlargement, a coaxial inner member extending from said generator to said waveguide coaxially of and through said passage, enlargement and chamber, a ring seated in said enlargement and projecting into said chamber and constituting with the wall of said chamber a transformer, said ring having an internal diameter equal to the diameter of the passage and an outer diameter equal to that of the first said enlargement, and a vacuum seal for said chamber at the end thereof toward the waveguide whereby the passage, chamber and transformer are at the same vacuum as the generator, and the location and seating of said ring in the enlargement enabling the coupling to be assembled with a desired length of ring protruding into the chamber and obtaining desired transformer characteristics.
5. An output coupling from an ultra high frequency generator to a waveguide, comprising a hollow member having a basal end next to and projecting from said generator and said basal end having a longitudinal passage therein, said passage having a stepped enlargement at the end of the passage remote from the generator, said hollow member providing a chamber of greater diameter than said enlargement thereby constituting a second stepped enlargement of the hollow of said member and said second stepped enlargement of said member being again enlarged by a rabbet at the end of said member toward the waveguide, a collar seated in said rabbet and having a flange at its end toward the waveguide, said flange being connected to said waveguide,
7 a coaxial inner member extending from said generator to said waveguide coaxially of and through said hollow member and the passage, enlargement, chamber and rabbet thereof, a ring seated in the rst mentioned enlargement and projecting into said chamber and constituting with the 1 wall of said chamber a transformer, a glass bead sealed peripherally to said collar and sealed on and to said coaxial inner member and comprising a closure for said chamber at the end thereof toward the waveguide, a sleeve coaxial with and at the outside of said collar, said sleeve being rigidly connected at its ends to the said hollow member and waveguide respectively and protecting said collar from strains and distortions, the successve stepped enlargements of the hollow of the hollow member enabling the coupling to be assembled and a ring of desired length seated in the first enlargement and protruded into the second enlargement for obtaining desired transg@ former characteristics.
' ERNEST C. OKRESS.
REFERENCES CITED The following references are of record in the iile of this patent:
UNITED STATES PATENTS Number Name Date 1,927,393 Darbord Sept. 19, 1933 2,147,717 Schelkunoff Feb. 21, 1939 2,193,859 Buschbeck Mar. 19, 1940 2,216,170 George Oct. 1, 1940 2,312,919 Litton Mar. 2, 1943 2,394,398 Mouromtseff Feb. 5, 1946 2,407,911 Tonks Sept. 17, 1946 2,408,032 Beck Sept, 24, 1946 2,417,789 Spencer Mar. 18, 1947 2,429,243 Snow Oct. 21, 1947 2,432,093 Fox Dec. 9, 1947 2,433,074 Tuller Dec. 23, 1947 2,434,925 Haxby Jan. 27, 1948 2,476,732 Hollingsworth July 19, 1949
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2627551A (en) * 1948-12-15 1953-02-03 Gen Electric Ultrahigh-frequency transmission structure
US2698421A (en) * 1952-05-23 1954-12-28 Raytheon Mfg Co Wave guide seal and filter structure
US2850704A (en) * 1955-02-04 1958-09-02 Hughes Aircraft Co Waveguide coupling
US2875417A (en) * 1955-04-27 1959-02-24 Jr Ben H Griffith Coaxial connector
US2922127A (en) * 1957-01-16 1960-01-19 Edward C Dench Output coupling
US2962677A (en) * 1945-10-04 1960-11-29 Bell Telephone Labor Inc Wave guide joint
US3086181A (en) * 1960-05-06 1963-04-16 Gen Electric Coaxial line to waveguide transition
US3309631A (en) * 1959-12-16 1967-03-14 Varian Associates High frequency tube coaxial transmission line
US3681718A (en) * 1969-11-12 1972-08-01 Baytron Co Inc Millimeter wave translating device with changeable insert element
FR2478869A1 (en) * 1980-03-18 1981-09-25 Thomson Csf SHF tube coaxial window - uses centre conductor and crossbeam support of same thermal expansion coefficient at its sealing temp.

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US2433074A (en) * 1943-07-02 1947-12-23 Raytheon Mfg Co High-frequency coupling device
US2434925A (en) * 1942-05-27 1948-01-27 Sperry Gyroscope Co Inc Coupling means for relatively movable wave guides
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US2147717A (en) * 1935-12-31 1939-02-21 Bell Telephone Labor Inc Guided wave transmission
US2193859A (en) * 1936-11-28 1940-03-19 Telefunken Gmbh Ultra short wave antenna
US2216170A (en) * 1939-07-25 1940-10-01 Roscoe H George Ultra high frequency oscillator
US2312919A (en) * 1940-09-19 1943-03-02 Int Standard Electric Corp Modulation system for velocity modulation tubes
US2417789A (en) * 1941-12-01 1947-03-18 Raytheon Mfg Co Magnetron anode structure
US2408032A (en) * 1942-02-03 1946-09-24 Bell Telephone Labor Inc Coupling arrangement
US2394398A (en) * 1942-03-20 1946-02-05 Westinghouse Electric Corp Coaxial line seal
US2407911A (en) * 1942-04-16 1946-09-17 Gen Electric Wave propagation
US2434925A (en) * 1942-05-27 1948-01-27 Sperry Gyroscope Co Inc Coupling means for relatively movable wave guides
US2429243A (en) * 1942-06-18 1947-10-21 Sperry Gyroscope Co Inc High-frequency tube structure
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2962677A (en) * 1945-10-04 1960-11-29 Bell Telephone Labor Inc Wave guide joint
US2627551A (en) * 1948-12-15 1953-02-03 Gen Electric Ultrahigh-frequency transmission structure
US2698421A (en) * 1952-05-23 1954-12-28 Raytheon Mfg Co Wave guide seal and filter structure
US2850704A (en) * 1955-02-04 1958-09-02 Hughes Aircraft Co Waveguide coupling
US2875417A (en) * 1955-04-27 1959-02-24 Jr Ben H Griffith Coaxial connector
US2922127A (en) * 1957-01-16 1960-01-19 Edward C Dench Output coupling
US3309631A (en) * 1959-12-16 1967-03-14 Varian Associates High frequency tube coaxial transmission line
US3086181A (en) * 1960-05-06 1963-04-16 Gen Electric Coaxial line to waveguide transition
US3681718A (en) * 1969-11-12 1972-08-01 Baytron Co Inc Millimeter wave translating device with changeable insert element
FR2478869A1 (en) * 1980-03-18 1981-09-25 Thomson Csf SHF tube coaxial window - uses centre conductor and crossbeam support of same thermal expansion coefficient at its sealing temp.

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