US2428793A - Antenna system - Google Patents
Antenna system Download PDFInfo
- Publication number
- US2428793A US2428793A US490367A US49036743A US2428793A US 2428793 A US2428793 A US 2428793A US 490367 A US490367 A US 490367A US 49036743 A US49036743 A US 49036743A US 2428793 A US2428793 A US 2428793A
- Authority
- US
- United States
- Prior art keywords
- antenna
- reflector
- loop
- high frequency
- signal
- 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
Links
- 229910052754 neon Inorganic materials 0.000 description 4
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 description 4
- 239000004020 conductor Substances 0.000 description 2
- 230000011664 signaling Effects 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/04—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
- H01Q19/108—Combination of a dipole with a plane reflecting surface
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q5/00—Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
- H01Q5/40—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q7/00—Loop antennas with a substantially uniform current distribution around the loop and having a directional radiation pattern in a plane perpendicular to the plane of the loop
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
- H01Q9/04—Resonant antennas
- H01Q9/16—Resonant antennas with feed intermediate between the extremities of the antenna, e.g. centre-fed dipole
Definitions
- the present invention relates to signalling by means of radio waves and in particular to means for measuring distance and determining direction of an object adapted to reflect ultra high frequency radio waves in combination with an identifying means where the reflecting body also acts as a signal transmitting source.
- Range and distance measurement by means of electromagnetic waves have been usefully employed for detecting the presence of objects but these means as a whole have not been applied for the purpose of distinguishing the reflecting objects and identifying means.
- One of the objects in the present invention is a combination of means whereby a signaling station may be both identified by means of its code signal and its distance and direction determined by the use of ultra high frequency reflected impulses, for instance, by the time-of-travel method in which distance is measured as a function of the time interval required for an electromagnetic impulse to travel to the wave reflecting object and return to the position of the measuring source.
- the receiving unit of the system combined a semi-directive loop circuit with a suitable ultra high frequency directive antenna which preferably employs a reflector and a doublet antenna pickup unit.
- Transmitting station may be identified on the ultra high frequency indicator in relation to the direction determination by a semi-directive loop and also by means of an audible signal.
- An advantage of the system in accordance with the present application is that it may be used for navigational purposes as a vessel is approaching a lightship or directive radio station, and serve as a means for clearly making known what might otherwise be unknown objects as picked up by the ultra high frequency directional range indicator.
- FIG. 3 shows diagrammatically a circuit arrangement and elements of the system.
- a system as set forth in Fig. 3 comprises, in combination, a radio receiving loop I, and a high frequency doublet antenna 2 which may be used with a reflector 3 (see Fig. l).
- the ultra high frequency antenna and the loop are rotated by a proper motor 4 which may be of the synchronous type and which is positioned in the base 5 of the antenna unit.
- an indicator disc 5 Rotating in synchronism with the antenna unit as driven by the motor 4 is an indicator disc 5 which is rotated by motor 6 turning the shaft 1 on which the indicator disc 5' is mounted.
- a neon tube indicator 8 or other equivalent device may be mounted on the disc and energized by the indicator control 9 in accordance with the intensity of the signal in the receiver Iii.
- the indicator control 9 may be so biassed that it will not produce a flash on the neon tube 8 when the signal received is at its lowest intensity. In accordance with this arrangement, therefore, as the loop approaches a null position, the indicator 8 will go out so that this will determin the direction of the bearing of the transmitted signal picked up by the loop I.
- a loud speaker II may also be connected to the output of the receiver so that the code signal of the transmitting station may be picked up.
- the ultra high frequency system has as its pickup unit the doublet antenna 2 which is centered in a reflector 3 made of conductive material. This reflector may be cut radially in sectors with slots I2 extending part way to the center of the reflector, in order to increase the reflector impedance to the circulatory current induced in the loop antenna I.
- the loop antenna may be mounted at the edge of the reflector as indicated in Figs. 1 and 2. This mounting may be made by placing the antenna loop or coil I within a conductive or non-conductive annular tube or torus I3.
- the torus I3 is made of conductive material, it should be slotted as indicated at M and I 5, and the ring should also preferably be insulatedly supported and spaced slightly away from the outer edge or rim of the reflector 3. This may be accomplished by using a pair of insulating sleeves I6 and I1.
- the antenna pickup element is rotated or spun synchronously with the indicating disc 5 by means of the motor 4.
- An ultra high frequency radio impulse or wave train is periodically emitted by means of the transmitter II. This emission is controlled by a keying control of any In the present In the operation of the system, therefore, the ultra high frequency signal will be transmitted by the transmitter and received by the cathode ray tube in such a manner as to indicate the distance and direction of the reflecting object. If this reflecting object is also able'to transmit a signal, this signal will give a directional indication arrangement, it is controlled by means of coil mounted on a ring 2 I, surrounding the neck of the cathode ray tube 50.
- Proper brush connections are shown to conducting rings 22 and 23 on the ring 20 illustratively in Fig. 3 by the brushes 24 and 25 which are energized from the cathode beam circuit over the conducting lines 26 and 21, respectively.
- the indicator 8 and a code indication over the loud speaker ll so that in this manner a spot corresponding to the transmitting station will be easily identified.
- the cathode ray tube indicator, disc 5 and the indicator 8 together with the loud speaker may be incorporated in'a single unitary structure 5
- the keying circuit l8 provides a variable energization of the coil 20 to bend the cathode beam from its center out to the edge of the tube.
- the coil 20 mounted on the ring 21 is rotated by means of a ring gear 28 meshing with the gear 29 which is driven by the motor 30 in synchronous operation with the motors d and 6 through the same supply source 3!.
- the time intervals are of a the order of microseconds, a comparatively slow continuous rotation of the coil 20 at, for instance, 20 RP. S. will hardly affect the sweep of the cathode beam which must sweep from the center of the tube radially to the circumference in intervals of the order of microseconds.
- the circuit arrangement may be to suppress the beam except at the instant that a reflecting signal is received, in which case when a signal is received, a spot will appear on the luminescent face of the cathode ray tube.
- the distance of this spot from the center of the tube indicates the distance of the reflecting object from the observing station, and the radial direction of the spot from the center of the tube indicates the direction that the reflecting object appears to the observing station.
- the neon light 8' will produce the same relative indication "that the spot on the cathode ray tube will produce. .
- the spot may, therefore, be made to correspond to the point at which the neon light indicator goes out.
- means including a reflector having a doublet ultra-high frequency antenna and a loop antenna surrounding said reflector.
- means including a reflector having a symmetry about a point and having a doublet ultrahigh'frequency antenna and a loop antenna surrounding said reflector, said reflector being slotted radially towards the point of symmetry and said loop surrounding said reflector at its rim.
- means including a reflector having a symmetry about a point and having a doublet ultrahigh frequency antenna and a loop antenna surrounding said reflector, said reflector being slotted radially towards the point of symmetry and said loop surrounding said reflector at its rim, said loop having a conductive case surrounding the same and means insulating sections of said conductive case from each other.
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- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Radar Systems Or Details Thereof (AREA)
Description
Oct. 14,1947. I H. J. w. FAY 2,428,793
ANTENNA SYSTEM Filed June 10, 1945 2 Sheets-Sheet 1 I l l I I l I l I I l I I I I FIG.1 I I INVBVTOR.
' HAROLD J.W. FAY
Oct; 14, 1947.
H. J. W. FAY
ANTENNA SYSTEM 1943 2 Sheets-Sheet 2 Filed June 10 KEYING CONTROL FOR TRANSMITTER AND CATHUDE 1 55AM SWEEP CATHODE BEAM SWEEP SUPPLY SYNCHEONOUS POWER CI ECUIT' 2 w W mi M M Ru \MU W0 O l Nm ED M um T R Y MRA- 3 WWW m M D 2 1 m y 5 H F u Patented Oct. 14, 1947 OFFICE ANTENNA SYSTEM Harold J. W. Fay, Westboro, Mass., assignor, by
mesne assignments, to Submarine Signal Company, Boston, Mass., a corporation of Delaware Application June 10, 1943, SerialNo. 490,367
3 Claims.
The present invention relates to signalling by means of radio waves and in particular to means for measuring distance and determining direction of an object adapted to reflect ultra high frequency radio waves in combination with an identifying means where the reflecting body also acts as a signal transmitting source.
Range and distance measurement by means of electromagnetic waves have been usefully employed for detecting the presence of objects but these means as a whole have not been applied for the purpose of distinguishing the reflecting objects and identifying means.
One of the objects in the present invention-is a combination of means whereby a signaling station may be both identified by means of its code signal and its distance and direction determined by the use of ultra high frequency reflected impulses, for instance, by the time-of-travel method in which distance is measured as a function of the time interval required for an electromagnetic impulse to travel to the wave reflecting object and return to the position of the measuring source. In the present invention, the receiving unit of the system combined a semi-directive loop circuit with a suitable ultra high frequency directive antenna which preferably employs a reflector and a doublet antenna pickup unit. By this means the code signal picked up from a transmitting station and the reflected beam picked up from it also may be made to operate associated indicated device.
Transmitting station may be identified on the ultra high frequency indicator in relation to the direction determination by a semi-directive loop and also by means of an audible signal. An advantage of the system in accordance with the present application is that it may be used for navigational purposes as a vessel is approaching a lightship or directive radio station, and serve as a means for clearly making known what might otherwise be unknown objects as picked up by the ultra high frequency directional range indicator.
Further advantages and merits of the present invention will be more fully understood from a description of the invention set forth in the speci- Fig. 3 shows diagrammatically a circuit arrangement and elements of the system.
A system as set forth in Fig. 3 comprises, in combination, a radio receiving loop I, and a high frequency doublet antenna 2 which may be used with a reflector 3 (see Fig. l). The ultra high frequency antenna and the loop are rotated by a proper motor 4 which may be of the synchronous type and which is positioned in the base 5 of the antenna unit.
Rotating in synchronism with the antenna unit as driven by the motor 4 is an indicator disc 5 which is rotated by motor 6 turning the shaft 1 on which the indicator disc 5' is mounted. A neon tube indicator 8 or other equivalent device may be mounted on the disc and energized by the indicator control 9 in accordance with the intensity of the signal in the receiver Iii. The indicator control 9 may be so biassed that it will not produce a flash on the neon tube 8 when the signal received is at its lowest intensity. In accordance with this arrangement, therefore, as the loop approaches a null position, the indicator 8 will go out so that this will determin the direction of the bearing of the transmitted signal picked up by the loop I. If desired, a loud speaker II may also be connected to the output of the receiver so that the code signal of the transmitting station may be picked up. The ultra high frequency system has as its pickup unit the doublet antenna 2 which is centered in a reflector 3 made of conductive material. This reflector may be cut radially in sectors with slots I2 extending part way to the center of the reflector, in order to increase the reflector impedance to the circulatory current induced in the loop antenna I. The loop antenna may be mounted at the edge of the reflector as indicated in Figs. 1 and 2. This mounting may be made by placing the antenna loop or coil I within a conductive or non-conductive annular tube or torus I3. If the torus I3 is made of conductive material, it should be slotted as indicated at M and I 5, and the ring should also preferably be insulatedly supported and spaced slightly away from the outer edge or rim of the reflector 3. This may be accomplished by using a pair of insulating sleeves I6 and I1.
As indicated by the diagram in Fig. 3, the antenna pickup element is rotated or spun synchronously with the indicating disc 5 by means of the motor 4. An ultra high frequency radio impulse or wave train is periodically emitted by means of the transmitter II. This emission is controlled by a keying control of any In the present In the operation of the system, therefore, the ultra high frequency signal will be transmitted by the transmitter and received by the cathode ray tube in such a manner as to indicate the distance and direction of the reflecting object. If this reflecting object is also able'to transmit a signal, this signal will give a directional indication arrangement, it is controlled by means of coil mounted on a ring 2 I, surrounding the neck of the cathode ray tube 50. Proper brush connections are shown to conducting rings 22 and 23 on the ring 20 illustratively in Fig. 3 by the brushes 24 and 25 which are energized from the cathode beam circuit over the conducting lines 26 and 21, respectively.
by the indicator 8 and a code indication over the loud speaker ll so that in this manner a spot corresponding to the transmitting station will be easily identified. For this purpose the cathode ray tube indicator, disc 5 and the indicator 8 together with the loud speaker may be incorporated in'a single unitary structure 5|.
Having now described my invention, I claim: 1. In a combination for distance ranging by the use of ultra-high frequency electromagnetic For each transmitted impulse, the keying circuit l8 provides a variable energization of the coil 20 to bend the cathode beam from its center out to the edge of the tube. The coil 20 mounted on the ring 21 is rotated by means of a ring gear 28 meshing with the gear 29 which is driven by the motor 30 in synchronous operation with the motors d and 6 through the same supply source 3!. Since in measuring distance by means of electromagnetic waves, the time intervals are of a the order of microseconds, a comparatively slow continuous rotation of the coil 20 at, for instance, 20 RP. S. will hardly affect the sweep of the cathode beam which must sweep from the center of the tube radially to the circumference in intervals of the order of microseconds.
The impulse, after it has been reflected, and picked up by the antenna 2, is impressed upon the receiving amplifier 33 of the ultra high radio frequency, the output of which is impressed upon the control grid (not shown) of the cathode ray tube over the line 34. In accordance with the known practice, the circuit arrangement may be to suppress the beam except at the instant that a reflecting signal is received, in which case when a signal is received, a spot will appear on the luminescent face of the cathode ray tube. The distance of this spot from the center of the tube indicates the distance of the reflecting object from the observing station, and the radial direction of the spot from the center of the tube indicates the direction that the reflecting object appears to the observing station. In the event that theobject producing the indication also is transmitting a signal of its own, the neon light 8'will produce the same relative indication "that the spot on the cathode ray tube will produce. .The spot may, therefore, be made to correspond to the point at which the neon light indicator goes out. I
'waves, means including a reflector having a doublet ultra-high frequency antenna and a loop antenna surrounding said reflector.
"2. In a combination for distance ranging by the use of ultra-high frequency electromagnetic waves, means including a reflector having a symmetry about a point and having a doublet ultrahigh'frequency antenna and a loop antenna surrounding said reflector, said reflector being slotted radially towards the point of symmetry and said loop surrounding said reflector at its rim.
3. In a combination for distance ranging by the use of ultra-high frequency electromagnetic waves, means including a reflector having a symmetry about a point and having a doublet ultrahigh frequency antenna and a loop antenna surrounding said reflector, said reflector being slotted radially towards the point of symmetry and said loop surrounding said reflector at its rim, said loop having a conductive case surrounding the same and means insulating sections of said conductive case from each other.
HAROLD J. W. FAY.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATEN'IS
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US490367A US2428793A (en) | 1943-06-10 | 1943-06-10 | Antenna system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US490367A US2428793A (en) | 1943-06-10 | 1943-06-10 | Antenna system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2428793A true US2428793A (en) | 1947-10-14 |
Family
ID=23947742
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US490367A Expired - Lifetime US2428793A (en) | 1943-06-10 | 1943-06-10 | Antenna system |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2428793A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2569758A (en) * | 1939-12-06 | 1951-10-02 | Csf | Radar system |
| US2597895A (en) * | 1944-09-23 | 1952-05-27 | Joseph F Novy | Remote location and identification system |
| US2659075A (en) * | 1949-06-15 | 1953-11-10 | Cole E K Ltd | Radio ground control equipment for aircraft |
| US2691161A (en) * | 1947-10-03 | 1954-10-05 | Cossor Ltd A C | Navigation system, including radio direction-finding equipment |
| US2814038A (en) * | 1953-07-29 | 1957-11-19 | Westinghouse Electric Corp | Lightweight antennas |
| US2922154A (en) * | 1952-10-06 | 1960-01-19 | Granqvist Carl-Erik | Arrangement in constructions for automatic radio direction finding |
| US3131249A (en) * | 1958-01-27 | 1964-04-28 | Karolus E Kunze | Stellar compass |
| US20160084935A1 (en) * | 2014-09-22 | 2016-03-24 | Symbol Technologies, Inc. | Co-located locationing techniologies |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB497147A (en) * | 1936-04-09 | 1938-12-09 | British Thomson Houston Co Ltd | Improvements in and relating to radio direction and range finding apparatus |
| US2257319A (en) * | 1936-06-06 | 1941-09-30 | Charles E Williams | Radiant energy system |
| GB542634A (en) * | 1939-10-16 | 1942-01-21 | Helge Fabian Rost | Apparatus for simultaneously measuring distances and directions of invisible objects from a movable or stationary spot |
| US2327641A (en) * | 1936-02-12 | 1943-08-24 | Rca Corp | Radio compass |
-
1943
- 1943-06-10 US US490367A patent/US2428793A/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2327641A (en) * | 1936-02-12 | 1943-08-24 | Rca Corp | Radio compass |
| GB497147A (en) * | 1936-04-09 | 1938-12-09 | British Thomson Houston Co Ltd | Improvements in and relating to radio direction and range finding apparatus |
| US2257319A (en) * | 1936-06-06 | 1941-09-30 | Charles E Williams | Radiant energy system |
| GB542634A (en) * | 1939-10-16 | 1942-01-21 | Helge Fabian Rost | Apparatus for simultaneously measuring distances and directions of invisible objects from a movable or stationary spot |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2569758A (en) * | 1939-12-06 | 1951-10-02 | Csf | Radar system |
| US2597895A (en) * | 1944-09-23 | 1952-05-27 | Joseph F Novy | Remote location and identification system |
| US2691161A (en) * | 1947-10-03 | 1954-10-05 | Cossor Ltd A C | Navigation system, including radio direction-finding equipment |
| US2659075A (en) * | 1949-06-15 | 1953-11-10 | Cole E K Ltd | Radio ground control equipment for aircraft |
| US2922154A (en) * | 1952-10-06 | 1960-01-19 | Granqvist Carl-Erik | Arrangement in constructions for automatic radio direction finding |
| US2814038A (en) * | 1953-07-29 | 1957-11-19 | Westinghouse Electric Corp | Lightweight antennas |
| US3131249A (en) * | 1958-01-27 | 1964-04-28 | Karolus E Kunze | Stellar compass |
| US20160084935A1 (en) * | 2014-09-22 | 2016-03-24 | Symbol Technologies, Inc. | Co-located locationing techniologies |
| US10261167B2 (en) * | 2014-09-22 | 2019-04-16 | Symbol Technologies, Llc | Co-located locationing technologies |
| US11262431B2 (en) | 2014-09-22 | 2022-03-01 | Symbol Technologies, Llc | Co-located locationing technologies |
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