US3633104A - High-stability electromagnetic resonator - Google Patents
High-stability electromagnetic resonator Download PDFInfo
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- US3633104A US3633104A US61225A US3633104DA US3633104A US 3633104 A US3633104 A US 3633104A US 61225 A US61225 A US 61225A US 3633104D A US3633104D A US 3633104DA US 3633104 A US3633104 A US 3633104A
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- dielectric layer
- dielectric
- layer
- electromagnetic resonator
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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
- H01P7/08—Strip line resonators
- H01P7/084—Triplate line resonators
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/03—Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
- G01S7/032—Constructional details for solid-state radar subsystems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/46—Indirect determination of position data
- G01S2013/466—Indirect determination of position data by Trilateration, i.e. two antennas or two sensors determine separately the distance to a target, whereby with the knowledge of the baseline length, i.e. the distance between the antennas or sensors, the position data of the target is determined
Definitions
- An electromagnetic resonator may be constructed by placing a conductor parallel to and insulated from a ground plane. If that conductor is in the shape of a disc, the resonant frequency of the structure is determined by the radius of the disc and the dielectric constant of the material between the disc and the ground plane.
- Changes in temperature can cause changesin the resonant frequency of the structure by affecting the radius of thedisc or the dielectric constant of the material between the disc and the ground plane. If the metal disc is bonded to a dielectric substrate with a lower linear thermal coefficient of expansion, then the effective linear thermal coefficient of expansion of the disc is that of the dielectric substrate. Thus, changes in resonant frequency due to changes in the radius of the disc can be reduced.
- the thermal stability of the dielectric between thedisc and the ground plane can be improved by placing between the substrate and the ground plane another dielectric which has a dielectric constant with either a lower thermal coefficient or one of opposite polarity. By reducing temperature effects on the radius of the disc and the dielectric constant of the dielectric, the frequency stability of the resonator is improved.
- FIG. 1 shows a sectional perspective view of the preferred embodiment of an electromagnetic resonator according to this invention.
- FIGS. 2-4 show sectional views of alternative embodiments of an electromagnetic resonator according to this invention.
- FIG. 5 shows an electromagnetic resonator, such as that of FIG. 1, in a doppler radar.
- an electromagnetic resonator is comprised of a metal layer or disc 12 bonded to a dielectric layer or substrate 14 mounted on a metal layer or block 16.
- Metal block 16 has a recess 17 directly below disc 12 for a dielectric layer 18 of, for example, air.
- the bottom of recess 17 forms a ground plane 20.
- Recess 17 is sufficiently larger in diameter than disc 12 that all the electric field lines from disc 12 are essentially perpendicular to ground plane 20.
- Strip lines 22 deposited on substrate 14 are used to couple signals in and out of resonator 10.
- Gaps 24 act as coupling capacitors between strip lines 22 and disc 12.
- the thermal stability of the dielectric between disc 12 and ground plane can also be improved by placing another dielectric 18 having a dielectric coefficient with either a lower thermal coefficient or one of opposite polarity (such as air) between quartz substrate 14 and ground plane 20.
- a thermal coefficient which increases with increasing temperature is said to have a positive polarity and one which decreases with increasing temperature is said to have a negative polarity.
- a dielectric with a positive dielectric constant thermal coefficient is combined with one having a negative thermal coefficient the resultant combination can be made to have a zero thermal coefficient by selecting the necessary thickness of each dielectric.
- Reduction of the effective dielectric constant thermal coefficient can also be achieved by placing a dielectric 18 between substrate 14 and ground plane 20 which has a smaller dielectric thermal coefficient than substrate 14, though of the same polarity.
- the dielectric constant thermal coefficient of quartz is +28 p.p.m./C. and that of air is essentially 0.
- the effective thermal coefficient of the totaldielectric between disc 12 and ground plane 20 can be reduced to about 6 p.p.m./C..
- a 10 gigaHertz resonator hasbeen built using the above-mentioned materials and the following dimensions are given for illustrative purposes.
- Disc 12 is 0.5 mil thick by 400 mils in diameter
- substrate is 25 mils thick
- recess 17 is 25 mils deep by 600 mils in diameter.
- Gaps 24 may be between 10 and 60 mils wide depending upon the impedance of the circuit they are coupling into.
- FIGS. 2, 3 and 4 illustrate alternative embodiments of the electromagnetic resonator.
- dielectric 18 may also be placed above disc 12 to achieve the desired results.
- FIGS. 3 and 4 show triplate rather than strip line configurations with the alternative placements of dielectrics 14 and 18 as were shown for the strip line embodiments in FIGS. 1 and 2. Transmission lines for coupling; signals into and out of the electromagnetic resonator are omitted in FIGS. 2, 3 and 4 for the purposes of illustration.
- FIG. 5 shows the use of a high stability electromagnetic resonator 10 in a doppler radar 30 including a negative resistance device 32, such as a Gunn diode, Impatt diode or tunnel diode, to excite the electromagnetic resonator at its resonant frequency.
- Electromagnetic resonator 10 is connected to a directional coupler 34 which in turn is connected to one port of a circulator 36.
- the second port of circulator 36 is connected to antenna 38 and the third port of circulator 36 is connected through directional coupler 34 to band-pass filter 42.
- Band-pass filter 42 is connected to detector 44 which in turn is connected to display 46.
- Antenna 38 radiates a microwave signal 48.
- signal 48 strikes a moving object 40, part of the signal will be reflected by the moving object and will return to antenna 38 as signal 50.
- Signal 50 will be offset in frequency (i.e., doppler shifted) from signal 48 by an amount proportional to the velocity of moving object 40 and will then pass through circulator 36 into directional coupler 34.
- directional coupler 34 a part of the signal from resonator 10, at the same frequency as signal 48, is combined with doppler shifted signal 50 and the resultant two-tone signal passes through band-pass filter 42 and is mixed in detector 44.
- the output of detector 44 is the frequency difference between signals 48 and 50. This frequency difference may be employed for driving display 46 to indicate the velocity of moving object 40, or to serve as an alarm indicating the presence of a moving object.
- the high stability electromagnetic resonator ensures that the frequency of one doppler radar set will not drift into the frequency range of another and cause erroneous readings, and it ensures a high degree of accuracy in the measurement of velocity.
- An electromagnetic resonator comprising:
- the first metallic layer being bonded to the first dielectric layer
- the first dielectric layer having a smaller linear thermal coefficient of expansion than the first metallic layer
- the first and second metallic layers being separated by at least one of the dielectric layers
- the second dielectric layer being adjacent at least one of the first and second metallic layers and having a dielectric constant thermal coefficient smaller than or of opposite polarity from that of the first dielectric layer when the second dielectric layer is adjacent the second metallic layer and having a dielectric constant thermal coefficient of opposite polarity from that of the first dielectric layer when the second dielectric layer is adjacent the first metallic layer and not the second metallic layer.
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- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Control Of Motors That Do Not Use Commutators (AREA)
- Piezo-Electric Or Mechanical Vibrators, Or Delay Or Filter Circuits (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
A metal disc is deposited on a quartz substrate to reduce the effective linear thermal coefficient of expansion of the disc, and air is contained between the quartz substrate and a ground plane to reduce the effective dielectric constant thermal coefficient to make an electromagnetic resonator which is stable in frequency with temperature.
Description
United States Patent Douglas A. Gray Portola Valley;
William W. Heinz, Palo Alto, both of Calif. 61,225
Aug. 5, 1970 Jan. 4, 1972 Hewlett-Packard Company Palo Alto, Calif.
[72] Inventors App]. No. Filed Patented Assignee HIGH-STABILITY ELECTROMAGNETI RESONATOR 6 Claims, 5 Drawing Figs.
U.S. Cl 325/18, 325/105, 325/29, 331/115, 333/83 T Int. Cl H04b l/38 Field of Search 325/484, 485, 104, 105,15, 24, 18; 330/45, 56,143;
[5 6] References Cited UNITED STATES PATENTS 3,544,920 12/1970 Konishi 333/83 T 3,034,078 5/1962 McCoubrey 333/83 T 3,504,303 3/1970 Konishi 333/83 T 3,454,946 7/1969 Warren et a1. 331/107 G Primary Examiner-Benedict V. Safourek Assistant ExaminerAlbert J. Mayer Attorney-Roland l. Griffin ABSTRACT: A metal disc is deposited on a quartz substrate to reduce the effective linear thermal coefficient of expansion of the disc, and air is contained between the quartz substrate and a ground plane to reduce the effective dielectric constant thermal coefficient to make an electromagnetic resonator which is stable in frequency with temperature.
PAIEIITEDJIII 4:972
NEGATIVE RESISTANCE DEVICE DIRECTIONAL COUPLER BANDP ss DISPLAY -DETECTOR HUAER i9ure 5 CIRCULATOR INVENTUPE DOUGLAS A. GFLY WILLIAM W. HEINZ 1 HIGH-STABILITY ELECTROMAGNETIC RESONATOR SUMMARY OF THE INVENTION An electromagnetic resonator may be constructed by placing a conductor parallel to and insulated from a ground plane. If that conductor is in the shape of a disc, the resonant frequency of the structure is determined by the radius of the disc and the dielectric constant of the material between the disc and the ground plane. Changes in temperature can cause changesin the resonant frequency of the structure by affecting the radius of thedisc or the dielectric constant of the material between the disc and the ground plane. If the metal disc is bonded to a dielectric substrate with a lower linear thermal coefficient of expansion, then the effective linear thermal coefficient of expansion of the disc is that of the dielectric substrate. Thus, changes in resonant frequency due to changes in the radius of the disc can be reduced. The thermal stability of the dielectric between thedisc and the ground plane can be improved by placing between the substrate and the ground plane another dielectric which has a dielectric constant with either a lower thermal coefficient or one of opposite polarity. By reducing temperature effects on the radius of the disc and the dielectric constant of the dielectric, the frequency stability of the resonator is improved.
DESCRIPTION OF THE DRAWINGS FIG. 1 shows a sectional perspective view of the preferred embodiment of an electromagnetic resonator according to this invention.
FIGS. 2-4 show sectional views of alternative embodiments of an electromagnetic resonator according to this invention.
FIG. 5 shows an electromagnetic resonator, such as that of FIG. 1, in a doppler radar.
DESCRIPTION OF THE PREFERRED EMBODIMENT As shown in FIG. 1 an electromagnetic resonator is comprised of a metal layer or disc 12 bonded to a dielectric layer or substrate 14 mounted on a metal layer or block 16. Metal block 16 has a recess 17 directly below disc 12 for a dielectric layer 18 of, for example, air. The bottom of recess 17 forms a ground plane 20. Recess 17 is sufficiently larger in diameter than disc 12 that all the electric field lines from disc 12 are essentially perpendicular to ground plane 20. Strip lines 22 deposited on substrate 14 are used to couple signals in and out of resonator 10. Gaps 24 act as coupling capacitors between strip lines 22 and disc 12.
If, for example, gold is used for disc 12 and it is vacuum deposited on a quartz substrate 14, then the linear thermal coefficient of expansion of disc 12 will change from 14 parts per million per centigrade degree (p.p.m./C.) to 0.5 p.p.m./C.. Thus, changes in resonant frequency due to changes in the radius of disc 12 can be greatly reduced.
The thermal stability of the dielectric between disc 12 and ground plane can also be improved by placing another dielectric 18 having a dielectric coefficient with either a lower thermal coefficient or one of opposite polarity (such as air) between quartz substrate 14 and ground plane 20. A thermal coefficient which increases with increasing temperature is said to have a positive polarity and one which decreases with increasing temperature is said to have a negative polarity. If a dielectric with a positive dielectric constant thermal coefficient is combined with one having a negative thermal coefficient the resultant combination can be made to have a zero thermal coefficient by selecting the necessary thickness of each dielectric. Reduction of the effective dielectric constant thermal coefficient can also be achieved by placing a dielectric 18 between substrate 14 and ground plane 20 which has a smaller dielectric thermal coefficient than substrate 14, though of the same polarity. For example, the dielectric constant thermal coefficient of quartz is +28 p.p.m./C. and that of air is essentially 0. By using an air layer with a thickness approximately equal to the thickness of substrate 14 for dielectric 18 the effective thermal coefficient of the totaldielectric between disc 12 and ground plane 20 can be reduced to about 6 p.p.m./C.. A 10 gigaHertz resonator hasbeen built using the above-mentioned materials and the following dimensions are given for illustrative purposes. Disc 12 is 0.5 mil thick by 400 mils in diameter, substrate is 25 mils thick and recess 17 is 25 mils deep by 600 mils in diameter. Gaps 24 may be between 10 and 60 mils wide depending upon the impedance of the circuit they are coupling into.
FIGS. 2, 3 and 4 illustrate alternative embodiments of the electromagnetic resonator. As shown in FIG. 2, dielectric 18 may also be placed above disc 12 to achieve the desired results. FIGS. 3 and 4 show triplate rather than strip line configurations with the alternative placements of dielectrics 14 and 18 as were shown for the strip line embodiments in FIGS. 1 and 2. Transmission lines for coupling; signals into and out of the electromagnetic resonator are omitted in FIGS. 2, 3 and 4 for the purposes of illustration.
FIG. 5 shows the use of a high stability electromagnetic resonator 10 in a doppler radar 30 including a negative resistance device 32, such as a Gunn diode, Impatt diode or tunnel diode, to excite the electromagnetic resonator at its resonant frequency. Electromagnetic resonator 10 is connected to a directional coupler 34 which in turn is connected to one port of a circulator 36. The second port of circulator 36 is connected to antenna 38 and the third port of circulator 36 is connected through directional coupler 34 to band-pass filter 42. Band-pass filter 42 is connected to detector 44 which in turn is connected to display 46. Antenna 38 radiates a microwave signal 48. If signal 48 strikes a moving object 40, part of the signal will be reflected by the moving object and will return to antenna 38 as signal 50. Signal 50 will be offset in frequency (i.e., doppler shifted) from signal 48 by an amount proportional to the velocity of moving object 40 and will then pass through circulator 36 into directional coupler 34. In directional coupler 34 a part of the signal from resonator 10, at the same frequency as signal 48, is combined with doppler shifted signal 50 and the resultant two-tone signal passes through band-pass filter 42 and is mixed in detector 44. The output of detector 44 is the frequency difference between signals 48 and 50. This frequency difference may be employed for driving display 46 to indicate the velocity of moving object 40, or to serve as an alarm indicating the presence of a moving object. The high stability electromagnetic resonator ensures that the frequency of one doppler radar set will not drift into the frequency range of another and cause erroneous readings, and it ensures a high degree of accuracy in the measurement of velocity.
lclaim:
1. An electromagnetic resonator comprising:
first and second dielectric layers;
first and second metallic layers;
the first metallic layer being bonded to the first dielectric layer;
the first dielectric layer having a smaller linear thermal coefficient of expansion than the first metallic layer;
the first and second metallic layers being separated by at least one of the dielectric layers; and
the second dielectric layer being adjacent at least one of the first and second metallic layers and having a dielectric constant thermal coefficient smaller than or of opposite polarity from that of the first dielectric layer when the second dielectric layer is adjacent the second metallic layer and having a dielectric constant thermal coefficient of opposite polarity from that of the first dielectric layer when the second dielectric layer is adjacent the first metallic layer and not the second metallic layer.
2. An electromagnetic resonator as in claim I wherein the second metallic layer is adjacent to the second dielectric layer and the first dielectric layer is adjacent to the second dielec' tric layer.
3. An electromagnetic resonator as in claim 1 wherein the second metallic layer is adjacent to the first dielectric layer 6. An electromagnetic resonator as in claim 2 wherein the electromagnetic resonator is part of a microwave transceiver, the electromagnetic resonator being connected to a negative resistance device and a directional coupler, the directional coupler being connected to a circulator, a detector being connected to the directional coupler through a band-pass filter, and output means being connected to the detector.
Claims (6)
1. An electromagnetic resonator comprising: first and second dieLectric layers; first and second metallic layers; the first metallic layer being bonded to the first dielectric layer; the first dielectric layer having a smaller linear thermal coefficient of expansion than the first metallic layer; the first and second metallic layers being separated by at least one of the dielectric layers; and the second dielectric layer being adjacent at least one of the first and second metallic layers and having a dielectric constant thermal coefficient smaller than or of opposite polarity from that of the first dielectric layer when the second dielectric layer is adjacent the second metallic layer and having a dielectric constant thermal coefficient of opposite polarity from that of the first dielectric layer when the second dielectric layer is adjacent the first metallic layer and not the second metallic layer.
2. An electromagnetic resonator as in claim 1 wherein the second metallic layer is adjacent to the second dielectric layer and the first dielectric layer is adjacent to the second dielectric layer.
3. An electromagnetic resonator as in claim 1 wherein the second metallic layer is adjacent to the first dielectric layer and the second dielectric layer is adjacent to the first metallic layer.
4. An electromagnetic resonator as in claim 2 wherein the first dielectric layer is quartz, the second dielectric layer is air and the first metallic layer is a metal disc vacuum deposited on the first dielectric layer.
5. An electromagnetic resonator as in claim 4 including strip line means to couple signals into and out of the electromagnetic resonator.
6. An electromagnetic resonator as in claim 2 wherein the electromagnetic resonator is part of a microwave transceiver, the electromagnetic resonator being connected to a negative resistance device and a directional coupler, the directional coupler being connected to a circulator, a detector being connected to the directional coupler through a band-pass filter, and output means being connected to the detector.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US6122570A | 1970-08-05 | 1970-08-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3633104A true US3633104A (en) | 1972-01-04 |
Family
ID=22034442
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US61225A Expired - Lifetime US3633104A (en) | 1970-08-05 | 1970-08-05 | High-stability electromagnetic resonator |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3633104A (en) |
| JP (1) | JPS5316660B1 (en) |
| DE (1) | DE2135566B2 (en) |
| FR (1) | FR2101239B1 (en) |
| GB (1) | GB1321493A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3798578A (en) * | 1970-11-26 | 1974-03-19 | Japan Broadcasting Corp | Temperature compensated frequency stabilized composite dielectric resonator |
| US4646038A (en) * | 1986-04-07 | 1987-02-24 | Motorola, Inc. | Ceramic resonator filter with electromagnetic shielding |
| US4661790A (en) * | 1983-12-19 | 1987-04-28 | Motorola, Inc. | Radio frequency filter having a temperature compensated ceramic resonator |
| US4667172A (en) * | 1986-04-07 | 1987-05-19 | Motorola, Inc. | Ceramic transmitter combiner with variable electrical length tuning stub and coupling loop interface |
| EP0434847A1 (en) * | 1989-07-07 | 1991-07-03 | NGK Spark Plug Co. Ltd. | Microwave strip line filter of temperature compensation type |
| EP0519085A1 (en) * | 1990-12-26 | 1992-12-23 | TDK Corporation | High-frequency device |
| WO1997045889A2 (en) * | 1996-05-31 | 1997-12-04 | Get Technology, Inc. | Improved transmission line |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6152064U (en) * | 1984-09-11 | 1986-04-08 | ||
| GB2222315B (en) * | 1988-08-24 | 1993-04-07 | Murata Manufacturing Co | Dielectric resonator |
| FR3119582B1 (en) | 2021-02-10 | 2022-12-23 | Psa Automobiles Sa | Bodywork element comprising an electrical current dissipation surface. |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3034078A (en) * | 1959-06-29 | 1962-05-08 | Nat Company Inc | Temperature compensated microwave cavity |
| US3454946A (en) * | 1967-01-25 | 1969-07-08 | Marconi Co Ltd | Pulsed doppler radar systems |
| US3504303A (en) * | 1967-05-04 | 1970-03-31 | Japan Broadcasting Corp | Reentrant cavity type circulator |
| US3544920A (en) * | 1967-04-27 | 1970-12-01 | Broadcasting Corp | Wide frequency band circulator |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE67921C (en) * | H. EHRHARDT in Düsseldorf | Process for punching and simultaneously shaping iron and steel blocks in a heated state |
-
1970
- 1970-08-05 US US61225A patent/US3633104A/en not_active Expired - Lifetime
-
1971
- 1971-07-06 GB GB3155971A patent/GB1321493A/en not_active Expired
- 1971-07-16 DE DE19712135566 patent/DE2135566B2/en active Pending
- 1971-08-03 FR FR7128395A patent/FR2101239B1/fr not_active Expired
- 1971-08-05 JP JP5926071A patent/JPS5316660B1/ja active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3034078A (en) * | 1959-06-29 | 1962-05-08 | Nat Company Inc | Temperature compensated microwave cavity |
| US3454946A (en) * | 1967-01-25 | 1969-07-08 | Marconi Co Ltd | Pulsed doppler radar systems |
| US3544920A (en) * | 1967-04-27 | 1970-12-01 | Broadcasting Corp | Wide frequency band circulator |
| US3504303A (en) * | 1967-05-04 | 1970-03-31 | Japan Broadcasting Corp | Reentrant cavity type circulator |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3798578A (en) * | 1970-11-26 | 1974-03-19 | Japan Broadcasting Corp | Temperature compensated frequency stabilized composite dielectric resonator |
| US4661790A (en) * | 1983-12-19 | 1987-04-28 | Motorola, Inc. | Radio frequency filter having a temperature compensated ceramic resonator |
| US4646038A (en) * | 1986-04-07 | 1987-02-24 | Motorola, Inc. | Ceramic resonator filter with electromagnetic shielding |
| US4667172A (en) * | 1986-04-07 | 1987-05-19 | Motorola, Inc. | Ceramic transmitter combiner with variable electrical length tuning stub and coupling loop interface |
| EP0434847A1 (en) * | 1989-07-07 | 1991-07-03 | NGK Spark Plug Co. Ltd. | Microwave strip line filter of temperature compensation type |
| EP0434847A4 (en) * | 1989-07-07 | 1991-12-04 | Ngk Spark Plug Co. Ltd. | Microwave strip line filter of temperature compensation type |
| EP0519085A1 (en) * | 1990-12-26 | 1992-12-23 | TDK Corporation | High-frequency device |
| EP0519085A4 (en) * | 1990-12-26 | 1993-05-26 | Tdk Corporation | High-frequency device |
| WO1997045889A2 (en) * | 1996-05-31 | 1997-12-04 | Get Technology, Inc. | Improved transmission line |
| WO1997045889A3 (en) * | 1996-05-31 | 1998-02-26 | Get Technology Inc | Improved transmission line |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2101239B1 (en) | 1976-12-03 |
| JPS5316660B1 (en) | 1978-06-02 |
| DE2135566B2 (en) | 1972-11-23 |
| GB1321493A (en) | 1973-06-27 |
| DE2135566A1 (en) | 1972-02-10 |
| FR2101239A1 (en) | 1972-03-31 |
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