US2692977A - Resonant cavity wavemeter for microwave energy - Google Patents
Resonant cavity wavemeter for microwave energy Download PDFInfo
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- US2692977A US2692977A US212991A US21299151A US2692977A US 2692977 A US2692977 A US 2692977A US 212991 A US212991 A US 212991A US 21299151 A US21299151 A US 21299151A US 2692977 A US2692977 A US 2692977A
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- piston
- shell
- wavemeter
- microwave energy
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
- H01P7/00—Resonators of the waveguide type
- H01P7/06—Cavity resonators
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R23/00—Arrangements for measuring frequencies; Arrangements for analysing frequency spectra
- G01R23/02—Arrangements for measuring frequency, e.g. pulse repetition rate; Arrangements for measuring period of current or voltage
- G01R23/04—Arrangements for measuring frequency, e.g. pulse repetition rate; Arrangements for measuring period of current or voltage adapted for measuring in circuits having distributed constants
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- General Physics & Mathematics (AREA)
- Control Of Motors That Do Not Use Commutators (AREA)
Description
R. G. KOPPEL Get. 26, 1954 RESONANT CAVITY WAVEMETER FOR MICROWAVE ENERGY fl Filed Feb. 27, 1951 h OPPEL R m N E V 5 ATTORNEY Patented Oct. 26, 1954 RESONANT CAVITY WAVEMETER FOR MICROWAVE ENERGY Ruth G. Koppel, Forest Hills, N. Y., assignor to The Sperry Corporation, a corporation of Delaware Application February 27, 1951, Serial No. 212,991
3 Claims.
The present invention relates to microwave resonator systems, and is particularly concerned with an improved wavemeter system for microwave energy.
Calibrated cavity resonators are often employed for the determination of the wavelength or the frequency of energy at microwaves, and particularly at frequencies of the order of cycles per second. A usable structure for this purpose may comprise a cylindrical shell closed at one end, and an adjustable piston element for use as the other end boundary of the resonator. The piston usually is provided with a precision drive mechanism, and is calibrated to enable the user to make frequency or wavelength determinations from the indicated position thereof.
In some prior cavity resonator wavemeters, direct friction contact pistons have been used. These suffer the disadvantage that the contact may become erratic, or may develop appreciable resistance due to surface scoring, or due to foreign matter, or to corrosion or oxidation of the surfaces. I
As set forth in U. S. patent application Serial No. 102,276, filed June 30, 1949, in the names of E. L. Ginzton and F. L. Salisbury, these problems may be avoided by use of a series of impedance-transforming transmission line sections, wherein the cylindrical outer surfaces of the piston are spaced slightly from the inner surface of the outer shell, and cooperate therewith as transmission line sections of very low impedance. Intermediate transmission line sections of higher characteristic impedance are provided. in the piston. These transmission line sections of alternately low and high characteristic impedance, in cooperation, sometimes referred to as traps, serve to provide an extremely low effective impedance value across the gap at the periphery of the face of the piston, enabling it to work substantially as though an ideal direct connec tion were provided thereat.
A difficulty arises, however, when a condition of resonance exists in the space at the opposite end of the piston. This may occur at one or more frequencies in the tuning range of the wavemeter, and can result in ambiguities and/or discontinuities in the calibration of the wavemeter.
to provide a wavemeter system free from the ,vulnerability of friction contacts to wear, cor- ,rosion, and foreign matter; and free from the {spurious response effects which arise from use f a series of alternate transmission line sections.
A principal object of the present invention is A further object is to provide a reliable wavemeter of economical construction, with a simple and effective spurious mode suppressor.
A preferred embodiment of the invention is shown in the appended drawings, wherein Fig. l is a side elevation, partly in section, of the wavemeter system, and Fig. 2 is a cross-sectional view taken on the line 22 in Fig. 1.
Referring now to Fig. l, the wavemeter of the present invention comprises an outer cylindrical shell i l of conductive material, and a longitudinally movable piston I3 therein. Both of these elements are made of highly conductive material such for example as brass, which may be silver plated if desired for very high conductivity. Calibrated means are provided for effecting gradual longitudinal movement of piston l3, and for accurately noting the position thereof, for
translation into wavelength or frequency. Such means may comprise a screw drive mechanism,
including a large diameter micrometer thimble i5 provided with a scale of divisions around the end thereof, the shell H being provided with an index mark therefor and with a longitudinal scale of divisions, to be referred to along with the angular divisions in the manner of the calibration system ordinarily employed for micrometers.
An input coupling such as a coaxial line connector I! with a coupling loop l9 formed in the inner conductor thereof is provided for introducing energy into the wavemeter system i l I3. An additional coupler may be provided for the resonator, including a further coupling loop 2! and a housing and radio-frequency by-pass capacitor 23 for a crystal detector element. Output connections from the crystal detector and the shell of the housing and by-pass unit f-"Zi extend to an indicating galvanometer such as milliammeter or microammeter 25.
If the cavity resonator formed in the left-hand end of the shell H is to be coupled to a wave guide, either a coaxial line adapter may be used in conjunction with the coupler ll, or an aperture coupling may be provided in the end of the shell ll instead of the coaxial coupler system ll, iii.
A microwave energy source such as a klystron 29 is shown connected to the input energy coupler i i, is for supplying microwave energy to the cavity resonator.
The piston I3 comprises two large-diameter sections 3! and 33, separated by a section 35 of relatively small diameter. Section 3|, which is nearly as great in diameter as the inside diameter of shell H, cooperates with the adjacent inher surface of the shell H as a quarter-wavelength coaxial transmission line section of very low characteristic impedance. Section 33 similarly cooperates with the adjacent inner surface of shell H as a further coaxial transmission line section of very low characteristic impedance. The small diameter section between these two sections ,of piston -13, providing radial current conduction paths of substantially quarter-wavelength extent, serves the purpose of an inter-' mediate quarter-wavelength transmission line section of relatively high characteristic imped v 102,276 .in the names of E. .L. Ginzton and F. L. Salisbury.
In accordance with the present invention, the piston I3 is so arranged as to prevent spurious resonance efiects arising from microwave energy fields in the region back .of piston 13, i. e. the region bounded at the left-hand end in Fig. 1 by end 39 of piston 13. It has been found that microwave energy fields existing in this region can cause considerable disturbance to the continuity and smoothness of the calibration of the wavemeter system, and can cause some ambiguity of the calibration thereof.
In addition, circumferential resonances occur along the section of coaxial line formed by the non-contacting piston 13 and shell ll of the TEmn mode type, which resonances occur where the circumference of the piston is of the order of a wavelength or multiple thereof. Two such resonances have been found .over the tuning range of the wavemeter without the mode suppression of the present invention.
To overcome these resonance effects, relatively deep slots are milled diametrally through the rear end of the piston I3 prior to its assembly .on the .drive screw 4!, and slabs 43 of lossy material are inserted therein. The preferred material for this purpose is polyiron, a material which was developed primarily for use as cores of transformers and other inductance devices, for high permeability and relatively low eddy-current loss at moderately high frequencies. This is composed of finely divided particles of ferromagnetic material suspended in a dielectric binder. At the microwaves, such material introduces both dielectric losses and eddy-current losses, and is quite effective for suppressing local voltage and current concentrations.
With the polyiron slabs 43 aranged as in dicated in Figs. 1 and 2, there is appreciable resistance to circular currents around the end sur face 39, and likewise around the cylindrical surface at the rear end of the piston l3, and accordingly, such currents are substantially suppressed. Therefore, the region to the right-hand side of piston l3 (as viewed in Fig. 1) is prevented from supporting a resonant field condition and causing objectionable interaction to the principal cavity resonance in the left-hand end of the system.
The circumferential currents associated with 4 the coaxial-type parasitic resonances, occurring along the piston I3 as mentioned above, are attenuated by the'exposed attenuating surfaces formed by the ends of the slabs 43 along the cylindrical surface of the piston, since the circumferential currents must flow across these exposed surfaces. At the same time, by virtue of their limited area in =.the cuter. cylindrical surface of the piston, the slabs 43 do not attenuate currents associated with the axial flowing TEM wave, and so have negligible effect on the TEM impedance of the piston.
The slabs 43 of lossy material can be wedgeshaped, if desired, so that the interfaces between these slabs and the brass body of piston 13 would all be radially disposed. However, for economy of construction with the retention of the desired effectivenes, provision of the rectangular slabs is preferred, particularly for simplicity of the milling operations in the end of the piston.
A table of dimensions is set forth below as a guide to construction of a wavemeter system for operation throughout a frequency range of v2575 to 3780 me.
Inside diameter of shell ll Outside diameter of piston l3 Overall length of piston I3 Length of section 31 of piston l3 Length of section 33 of piston l3 3.125 inches.
3.000 inches.
2.220 inches.
0.840 inch.
1.130 inches.
Diameter of section 35 of piston l3 1.380 inches.
Diameter of shaft 4| 1.500 inches. Thicknes of elements 43 0.125 inch. Axial length of elements 43 0.400 inch.
Material of elements Grade D-l Polyiron 43 (H. L. Crowley & 00.).
In addition to the slabs or elements of polyiron arranged as spokes in the end of piston l3, and having exposed narrow faces in the end surface and the cylindrical surface thereof, an annular polyiron element is provided in the back-cavity space surrounding screw-shaft 4i.
While a ring of this high-loss material could be recesed in the end surface of the piston, intersecting the exposed surfaces of the slabs 43, it is simpler to attach the annular body to the opposite fixed surface as shown at 45 in Fig. 1. This annular body may be secured to the right-hand interior surface of the shell II by screws and cement. The annular polyiron body 45 not only contributes somewhat to the suppression of circumferential currents, but also it is particularly effective in the suppression of the mode of oscillation involving radial currents therein, longitudinal currents along the screw-shaft 4| and the inner cylindrical surface of the shell H, and radial currents in the rear end surface 39 of the piston l3. Since the spokes are so oriented as to contribute relatively little to suppression of these modes, the back plate body 45 and the set of spokes 43 complement each other in rendering the wavemeter system substantially free from spurious response effects.
Since many changes could be made in the above construction and many apparently widely di'fferent embodiments of this invention could be made without departing from the scope thereof, it is intended that all matter contained in the above description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. A tunable cavity comprising a cylindrical conductive shell having first and second conductive ends, a conductive cylindrical piston of slightly smaller diameter than the inner diameter of the shell and longitudinally movable within the shell, one end of the shell and the adjacent end of the piston combining with the shell to define a cavity resonator, the piston having a reduced diameter portion positioned intermediate the ends of the piston forming an annular groove having a radial depth of substantially a quarter Wavelength at the mid-band operating frequency, the reduced diameter portion dividing the piston into two regions, each of which provides in combination with the shell a coaxial line section of relatively low characteristic impedance and of the order of a quarter wavelength in length, means for coupling microwave energy through the shell into the resonator, a drive shaft extending axially through the end of the shell opposite the end defining the cavity resonator and secured at one end thereof to the end of the piston opposite the end thereof defining the cavity resonator, the drive shaft combining with the outer shell to provide a coaxial line section of relatively high characteristic impedance, the end of the piston connected to the drive shaft having a plurality of radially extending slots therein that extend through the outer cylindrical surface of the piston, the slots having an appreciable depth as measured parallel to the longitudinal axis of the piston, inserts of high-loss material positioned in the slots, the inserts providing axially extending exposed surfaces in the cylindrical surface of the piston adjacent one end thereof, and an annular body of high-loss material surrounding the drive shaft and secured to the inner surface of the end of the shell through which the drive shaft extends.
2. A tunable cavity comprising a cylindrical conductive shell having first and second conductive ends, a conductive cylindrical piston having a portion thereof extending axially a distance of the order of a quarter wavelength, said portion having a slightly smaller diameter than the inner diameter of the shell, the piston being longitudinally movable within the shell, one end of the shell and the adjacent end of the piston combining with the shell to define a cavity resonator, a drive shaft extending axially through the end of the shell opposite the end defining the cavity resonator and secured at one end thereof to the end of the piston opposite the end thereof defining the cavity resonator, the drive shaft combining with the outer shell to provide a coaxial line section of relatively high characteristic impedance, the end of the piston connected to the drive shaft having a plurality of radially extending slots therein that extend through the outer cylindrical surface of the piston, the slots having an appreciable depth as measured parallel to the longitudinal axis of the piston, and inserts of high-loss material positioned in the slots, the inserts providing axially extending exposed surfaces in the cylindrical surface of the piston adjacent one end thereof.
3. A tunable cavity comprising a cylindrical conductive shell having first and second conductive ends, a conductive cylindrical piston having a portion thereof extending axially a distance of the order of a quarter wavelength, said portion having a slightly smaller diameter than the inner diameter of the shell, the piston being longitudinally movable within the shell, one end of the shell and the adjacent end of the piston combining with the shell to define a cavity resonator, the end of the piston opposite the end defining the resonant cavity having a plurality of radially extending slots therein that extend through the outer cylindrical surface of the piston, the slots having an appreciable depth as measured parallel to the longitudinal axis of the piston, and inserts of high-loss material positioned in the slots, the inserts providing axially extending exposed surfaces in the cylindrical surface of the piston adjacent one end thereof.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,106,771 Southworth Feb. 1, 1938 2,434,560 Gunter Jan. 13, 1948 2,439,388 Hansen Apr. 13, 1948 2,471,419 Edson et a1 May 31, 1949 2,503,256 Ginzton, et al Apr. 11, 1950 2,543,721 Collard et a1 Feb. 27, 1951 2,605,459 Cook July 29, 1952
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US212991A US2692977A (en) | 1951-02-27 | 1951-02-27 | Resonant cavity wavemeter for microwave energy |
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US212991A US2692977A (en) | 1951-02-27 | 1951-02-27 | Resonant cavity wavemeter for microwave energy |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2924797A (en) * | 1955-11-29 | 1960-02-09 | Bell Telephone Labor Inc | Finline coupler |
US2944234A (en) * | 1956-07-11 | 1960-07-05 | Philips Corp | Adjustable impedance for use in waveguides |
US2944233A (en) * | 1958-10-16 | 1960-07-05 | Hewlett Packard Co | Cavity resonator and oscillation generator |
US2996686A (en) * | 1959-02-02 | 1961-08-15 | Okaya Akira | Adjustable wave guide reflection end |
US3008105A (en) * | 1959-03-05 | 1961-11-07 | D S Kennedy & Co | Tuning piston for waveguides |
US3157818A (en) * | 1961-10-18 | 1964-11-17 | Bell Telephone Labor Inc | Coaxial cavity magnetron tuning ring |
US3263118A (en) * | 1963-07-30 | 1966-07-26 | Westinghouse Electric Corp | Magnetron having concentric annular tunable resonator utilizing axial plunger and vacuum sealing bellows mounted inside principal envelope wall |
US3274513A (en) * | 1963-10-30 | 1966-09-20 | Trak Micrownve Corp | Broad band tunable microwave oscillator with substantially constant output power characteristics |
US3706910A (en) * | 1971-05-28 | 1972-12-19 | Raytheon Co | Coaxial magnetron slot mode suppressor |
WO1987002186A1 (en) * | 1985-10-03 | 1987-04-09 | Hughes Aircraft Company | Non-reactive radial line power divider/combiner with integral mode filters |
WO2016184965A1 (en) * | 2015-05-20 | 2016-11-24 | Mician Global Engineering Gbr | Bandpass filter comprising a cavity resonator and method for operating, adjusting or producing a bandpass filter of this type |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2106771A (en) * | 1935-09-11 | 1938-02-01 | American Telephone & Telegraph | Ultrahigh frequency signaling |
US2434560A (en) * | 1943-10-07 | 1948-01-13 | Westinghouse Electric Corp | Termination for transmission lines |
US2439388A (en) * | 1941-12-12 | 1948-04-13 | Sperry Corp | Resonator wave meter |
US2471419A (en) * | 1944-07-07 | 1949-05-31 | Bell Telephone Labor Inc | Tunable resonant cavity with adjustable walls |
US2503256A (en) * | 1943-01-29 | 1950-04-11 | Sperry Corp | Ultra high frequency wavemeter |
US2543721A (en) * | 1944-02-09 | 1951-02-27 | Emi Ltd | High-frequency electrical transmission line and wave guide |
US2605459A (en) * | 1943-10-23 | 1952-07-29 | Jackson H Cook | Monitoring apparatus for radio pulse transmission systems |
-
1951
- 1951-02-27 US US212991A patent/US2692977A/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2106771A (en) * | 1935-09-11 | 1938-02-01 | American Telephone & Telegraph | Ultrahigh frequency signaling |
US2439388A (en) * | 1941-12-12 | 1948-04-13 | Sperry Corp | Resonator wave meter |
US2503256A (en) * | 1943-01-29 | 1950-04-11 | Sperry Corp | Ultra high frequency wavemeter |
US2434560A (en) * | 1943-10-07 | 1948-01-13 | Westinghouse Electric Corp | Termination for transmission lines |
US2605459A (en) * | 1943-10-23 | 1952-07-29 | Jackson H Cook | Monitoring apparatus for radio pulse transmission systems |
US2543721A (en) * | 1944-02-09 | 1951-02-27 | Emi Ltd | High-frequency electrical transmission line and wave guide |
US2471419A (en) * | 1944-07-07 | 1949-05-31 | Bell Telephone Labor Inc | Tunable resonant cavity with adjustable walls |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2924797A (en) * | 1955-11-29 | 1960-02-09 | Bell Telephone Labor Inc | Finline coupler |
US2944234A (en) * | 1956-07-11 | 1960-07-05 | Philips Corp | Adjustable impedance for use in waveguides |
US2944233A (en) * | 1958-10-16 | 1960-07-05 | Hewlett Packard Co | Cavity resonator and oscillation generator |
US2996686A (en) * | 1959-02-02 | 1961-08-15 | Okaya Akira | Adjustable wave guide reflection end |
US3008105A (en) * | 1959-03-05 | 1961-11-07 | D S Kennedy & Co | Tuning piston for waveguides |
US3157818A (en) * | 1961-10-18 | 1964-11-17 | Bell Telephone Labor Inc | Coaxial cavity magnetron tuning ring |
US3263118A (en) * | 1963-07-30 | 1966-07-26 | Westinghouse Electric Corp | Magnetron having concentric annular tunable resonator utilizing axial plunger and vacuum sealing bellows mounted inside principal envelope wall |
US3274513A (en) * | 1963-10-30 | 1966-09-20 | Trak Micrownve Corp | Broad band tunable microwave oscillator with substantially constant output power characteristics |
US3706910A (en) * | 1971-05-28 | 1972-12-19 | Raytheon Co | Coaxial magnetron slot mode suppressor |
WO1987002186A1 (en) * | 1985-10-03 | 1987-04-09 | Hughes Aircraft Company | Non-reactive radial line power divider/combiner with integral mode filters |
US4812782A (en) * | 1985-10-03 | 1989-03-14 | Hughes Aircraft Company | Non-reactive radial line power divider/combiner with integral mode filters |
WO2016184965A1 (en) * | 2015-05-20 | 2016-11-24 | Mician Global Engineering Gbr | Bandpass filter comprising a cavity resonator and method for operating, adjusting or producing a bandpass filter of this type |
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