US2293112A - Compact high frequency dipole - Google Patents

Compact high frequency dipole Download PDF

Info

Publication number
US2293112A
US2293112A US292773A US29277339A US2293112A US 2293112 A US2293112 A US 2293112A US 292773 A US292773 A US 292773A US 29277339 A US29277339 A US 29277339A US 2293112 A US2293112 A US 2293112A
Authority
US
United States
Prior art keywords
dipole
conductors
transmission line
tuning
pair
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US292773A
Inventor
Wendell L Carlson
Vernon D Landon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RCA Corp
Original Assignee
RCA Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by RCA Corp filed Critical RCA Corp
Priority to US292773A priority Critical patent/US2293112A/en
Priority to GB13699/40A priority patent/GB543376A/en
Application granted granted Critical
Publication of US2293112A publication Critical patent/US2293112A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/28Adaptation for use in or on aircraft, missiles, satellites, or balloons

Definitions

  • This invention relates to a compact high frequency dipole antenna of a design which is especially useful for aircraft direction finders.
  • Direction finding with dipole antennas is old but the use of high frequency horizontally polarized Waves has presented new problems.
  • a dipole which is fixed in space and which is fixedly tuned is not especially difiicult to design. When the dipole is dirigible, is tunable and is limited to a small streamline housing, a conventional design is impractical.
  • Another object is to provide a compact dirigible and tunable dipole. Another object is to provide a compact dirigible dipole with tuning means so constructed and arranged that the symmetrical properties of the antenna are not altered substantially by the tuning.
  • Figure 1 is a schematic diagram of one embodiment of the invention
  • Figure 2 is an elevational view, partly in section, of an antenna designed in accordance with the invention. Similar reference numerals will be used to indicate similar elements in the figures.
  • the arms I of a dipole antenna 3 are connected to the conductors 5 of a tunable transmission line.
  • the resonant transmission line includes a bulged section I which is formed by oppositely extending arcs formed by bending the conductors 5.
  • a tuning disc 9 is mounted within the bulged section I so that the transmission line may be tuned by rotating the disc about an axispassing through its diameter.
  • a conventional transmission line H is connected to the tunable line 5 at points where a suitable impedance match is found.
  • the second line is terminated at shielded transformer [3, having a symmetrical primary relative to the shield.
  • the secondary of the transformer is connected to a radio receiver [5 and hence to an indicator N.
  • the dipole were made of the conventional length for receiving waves of the order of 125 megacycles it would be approximately 1.2 meters long. While this length would not be a factor in installations where space is not at a premium or where the drag due to the airspeed was not an important element, the length does not lend itself to the small streamline antenna housings used on modern aircraft.
  • the solution of this difficulty is to reduce the length of the dipole to about six inches, tune the line connected thereto, and mount copper discs E3 on the ends of the dipole.
  • the discs may be of copper about four inches in diameter and one thirty second of an inch in thickness. The dimensions are determined by the practical operating conditions.
  • the dipole length is thus reduced to A; of the normal length; nevertheless, the effectiveness is percent of a full length dipole because the radiation resistance is reduced and the Q of the circuit is increased.
  • the antenna resonant circuit includes the arms i, discs i8, conductors 5, and tuning disc 9. Of these the unshielded parts are the effective reception or radiation elements.
  • Fig. 2. illustraterates one practical embodiment of the invention.
  • the lower portion E9 of the transmission line is mounted within a shield member 2
  • Insulation members 23 support the line at the ends of the shield.
  • the shield is mounted within bearings 25 and held in position by collars 21.
  • the dipole 3 is rotated within an insulated streamline housing 29 by means of the handle 3
  • the bulged portion 1 of the transmission line is housed within a second shield member 33.
  • the tuning disc 9 is suitably connected to a tuning knob 35 which rotates with the dipole. Tuning and dipole azimuth scales may be associated with the controls.
  • the invention has been described as a dipole which has been shortened from a half wave to a sixteenth of a wave length.
  • the dipole is made dirigible within a compact streamline housing.
  • the resonant transmission line connected to the dipole includes a bulged section within which is positioned a tuning disc.
  • the line and disc are shielded.
  • the symmetry of the device is not affected by tuning or azimuth position.
  • the disc members either for the dipole or tuning may be made of any desired geometric form instead of circular.
  • the antenna is preferably symmetrically balanced so that in phase voltages reaching the transmission line do not induce voltages on the receiver.
  • a dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured respectively to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member located within said bulged section and consisting of a movable member mutually coupled to said bulged section for varying the effective length of said line.
  • a dipole antenna including in combination a pair of dipole conductors having an overall length substantially less than half the operating Wave length, a pair of conductive members secured respectively to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member located within said bulged section and consisting of a movable metal member mutually coupled to said bulged section.
  • a dipole antenna including in combination a pair of dipole conductors, a pair of conductive discs having diameters equal to a substantial portion of the dipole length secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member consisting of a metal disc mutually coupled to and rotatably mounted Within said bulged section.
  • a dipole antenna including in combination a pair of dipole conductors having an overall length substantially less than half the operating wave length, a pair of conductive discs having diameters of the order of said dipole length secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member consisting of a member mutually coupled to and rotatably mounted within said bulged section.
  • a dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, a tuning member consisting of a movable metal member mutually coupled to and located within said bulged section, and means shielding said transmission line.
  • a dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, a tuning member consisting of a movable metal disc mutually coupled to and located within said bulged section, means shielding said transmission line and said tuning member.
  • a dipole antenna including in combination a pair of dipole conductors having an overall length substantiallyless than the operating wave length, a pair of conductive discs having diameters of the order of two-thirds of said dipole length secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, a tuning member rotatably mounted within said bulged section, means shielding said transmission line and said tuning member, and an insulated streamline housing enclosing said dipole antenna.
  • a dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured to the outer ends of said conductors, a transmission line connected to said dipole conductors, and a tuning member consisting of a movable member mutually coupled to and located within said transmission line.

Description

g- 1942- w. L. CARLSON ET AL 2,293,112
COMPACT HIGH F'REQUEIIQY DIPOLE Filed Aug. 31, 1939 N 7 z WM 0 WW w H m t 6 .1 L0. M M/ 5 W M 8 t & M a 00% W M 4 Patenteol Aug. 18, 1942 UNETE SA 2.1
Parser orrlcis CGMPACT men FREQUENCY DIPOLE Application August 31, 1939, Serial No. 292,773
(Cl. 25fi33) 8 Claims.
This invention relates to a compact high frequency dipole antenna of a design which is especially useful for aircraft direction finders.
Direction finding with dipole antennas is old but the use of high frequency horizontally polarized Waves has presented new problems. A dipole which is fixed in space and which is fixedly tuned is not especially difiicult to design. When the dipole is dirigible, is tunable and is limited to a small streamline housing, a conventional design is impractical.
Therefore, it is one of the objects of this invention to provide a dipole of suitable design for use on aircraft. Another object is to provide a compact dirigible and tunable dipole. Another object is to provide a compact dirigible dipole with tuning means so constructed and arranged that the symmetrical properties of the antenna are not altered substantially by the tuning.
The invention will be described by reference to the accompanying drawing in which Figure 1 is a schematic diagram of one embodiment of the invention; and Figure 2 is an elevational view, partly in section, of an antenna designed in accordance with the invention. Similar reference numerals will be used to indicate similar elements in the figures.
Referring to Figure 1, the arms I of a dipole antenna 3 are connected to the conductors 5 of a tunable transmission line. The resonant transmission line includes a bulged section I which is formed by oppositely extending arcs formed by bending the conductors 5. A tuning disc 9 is mounted within the bulged section I so that the transmission line may be tuned by rotating the disc about an axispassing through its diameter. A conventional transmission line H is connected to the tunable line 5 at points where a suitable impedance match is found. The second line is terminated at shielded transformer [3, having a symmetrical primary relative to the shield. The secondary of the transformer is connected to a radio receiver [5 and hence to an indicator N.
If the dipole were made of the conventional length for receiving waves of the order of 125 megacycles it would be approximately 1.2 meters long. While this length would not be a factor in installations where space is not at a premium or where the drag due to the airspeed was not an important element, the length does not lend itself to the small streamline antenna housings used on modern aircraft. The solution of this difficulty, for the chosen example in accordance with the present invention, is to reduce the length of the dipole to about six inches, tune the line connected thereto, and mount copper discs E3 on the ends of the dipole. The discs may be of copper about four inches in diameter and one thirty second of an inch in thickness. The dimensions are determined by the practical operating conditions. The dipole length is thus reduced to A; of the normal length; nevertheless, the effectiveness is percent of a full length dipole because the radiation resistance is reduced and the Q of the circuit is increased. These factors increasing the efiiciency are offset by the lower induced voltage. It should be understood that the antenna resonant circuit includes the arms i, discs i8, conductors 5, and tuning disc 9. Of these the unshielded parts are the effective reception or radiation elements.
By way of example, Fig. 2.illustrates one practical embodiment of the invention. The lower portion E9 of the transmission line is mounted within a shield member 2|. Insulation members 23 support the line at the ends of the shield. The shield is mounted within bearings 25 and held in position by collars 21. The dipole 3 is rotated within an insulated streamline housing 29 by means of the handle 3| mounted on the disc 33 which terminates the transmission line. The bulged portion 1 of the transmission line is housed within a second shield member 33. The tuning disc 9 is suitably connected to a tuning knob 35 which rotates with the dipole. Tuning and dipole azimuth scales may be associated with the controls.
Thus the invention has been described as a dipole which has been shortened from a half wave to a sixteenth of a wave length. The dipole is made dirigible within a compact streamline housing. The resonant transmission line connected to the dipole includes a bulged section within which is positioned a tuning disc. The line and disc are shielded. The symmetry of the device is not affected by tuning or azimuth position. The disc members either for the dipole or tuning may be made of any desired geometric form instead of circular. The antenna is preferably symmetrically balanced so that in phase voltages reaching the transmission line do not induce voltages on the receiver.
What is claimed is:
l. A dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured respectively to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member located within said bulged section and consisting of a movable member mutually coupled to said bulged section for varying the effective length of said line.
2. A dipole antenna including in combination a pair of dipole conductors having an overall length substantially less than half the operating Wave length, a pair of conductive members secured respectively to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member located within said bulged section and consisting of a movable metal member mutually coupled to said bulged section.
3. A dipole antenna including in combination a pair of dipole conductors, a pair of conductive discs having diameters equal to a substantial portion of the dipole length secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member consisting of a metal disc mutually coupled to and rotatably mounted Within said bulged section.
4. A dipole antenna including in combination a pair of dipole conductors having an overall length substantially less than half the operating wave length, a pair of conductive discs having diameters of the order of said dipole length secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, and a tuning member consisting of a member mutually coupled to and rotatably mounted within said bulged section.
5. A dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, a tuning member consisting of a movable metal member mutually coupled to and located within said bulged section, and means shielding said transmission line.
6. A dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, a tuning member consisting of a movable metal disc mutually coupled to and located within said bulged section, means shielding said transmission line and said tuning member.
7. A dipole antenna including in combination a pair of dipole conductors having an overall length substantiallyless than the operating wave length, a pair of conductive discs having diameters of the order of two-thirds of said dipole length secured to the outer ends of said conductors, a transmission line connected to said dipole conductors and including a bulged section, a tuning member rotatably mounted within said bulged section, means shielding said transmission line and said tuning member, and an insulated streamline housing enclosing said dipole antenna.
8. A dipole antenna including in combination a pair of dipole conductors, a pair of conductive members secured to the outer ends of said conductors, a transmission line connected to said dipole conductors, and a tuning member consisting of a movable member mutually coupled to and located within said transmission line.
WENDELL L. CARLSON. VERNON D. LANDON.
US292773A 1939-08-31 1939-08-31 Compact high frequency dipole Expired - Lifetime US2293112A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US292773A US2293112A (en) 1939-08-31 1939-08-31 Compact high frequency dipole
GB13699/40A GB543376A (en) 1939-08-31 1940-08-31 Improvements in dipole aerial systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US292773A US2293112A (en) 1939-08-31 1939-08-31 Compact high frequency dipole

Publications (1)

Publication Number Publication Date
US2293112A true US2293112A (en) 1942-08-18

Family

ID=23126134

Family Applications (1)

Application Number Title Priority Date Filing Date
US292773A Expired - Lifetime US2293112A (en) 1939-08-31 1939-08-31 Compact high frequency dipole

Country Status (2)

Country Link
US (1) US2293112A (en)
GB (1) GB543376A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2501072A (en) * 1945-08-30 1950-03-21 Us Sec War Antenna housing
US2505115A (en) * 1944-09-11 1950-04-25 Belmont Radio Corp Dipole antenna system
US2558145A (en) * 1948-05-20 1951-06-26 Jr Wesley C Mock Antenna
US2563243A (en) * 1949-05-10 1951-08-07 Joseph N Marks Indoor television antenna
US2566491A (en) * 1946-03-15 1951-09-04 Belmont Radio Corp Antenna construction
US2611869A (en) * 1944-04-21 1952-09-23 Int Standard Electric Corp Aerial system
US2624843A (en) * 1945-06-07 1953-01-06 Redheffer Raymond Radio wave radiating system
US2642528A (en) * 1949-06-17 1953-06-16 Philco Corp Antenna for television receivers
US2838755A (en) * 1952-07-03 1958-06-10 Philco Corp Cabinet antenna system
US3056925A (en) * 1959-06-29 1962-10-02 Empire Devices Inc Radio power density probe

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2611869A (en) * 1944-04-21 1952-09-23 Int Standard Electric Corp Aerial system
US2505115A (en) * 1944-09-11 1950-04-25 Belmont Radio Corp Dipole antenna system
US2624843A (en) * 1945-06-07 1953-01-06 Redheffer Raymond Radio wave radiating system
US2501072A (en) * 1945-08-30 1950-03-21 Us Sec War Antenna housing
US2566491A (en) * 1946-03-15 1951-09-04 Belmont Radio Corp Antenna construction
US2558145A (en) * 1948-05-20 1951-06-26 Jr Wesley C Mock Antenna
US2563243A (en) * 1949-05-10 1951-08-07 Joseph N Marks Indoor television antenna
US2642528A (en) * 1949-06-17 1953-06-16 Philco Corp Antenna for television receivers
US2838755A (en) * 1952-07-03 1958-06-10 Philco Corp Cabinet antenna system
US3056925A (en) * 1959-06-29 1962-10-02 Empire Devices Inc Radio power density probe

Also Published As

Publication number Publication date
GB543376A (en) 1942-02-23

Similar Documents

Publication Publication Date Title
US3474453A (en) Whip antenna with adjustable tuning
US2338134A (en) Variable tuning system
US2293112A (en) Compact high frequency dipole
US2359620A (en) Short wave antenna
US2966678A (en) Multifrequency resonant antenna
US2425585A (en) Wave-signal antenna
US2274389A (en) Asymmetrical antenna with shielded feed line
US2465381A (en) Loop antenna system
US4379298A (en) Tunable citizen band antenna
US2255520A (en) Directional antenna system
US2143658A (en) Ultra short wave system
US2426226A (en) Rotatable coupler
US2086615A (en) High frequency wave meter
US3594805A (en) Ferrite rod antenna with longitudinally split sleeve
GB614419A (en) Improvements in radio antennas
US2991355A (en) Power cord type antenna system for a wave-signal receiver
US3290601A (en) Line cord and monopole antenna system
US2498350A (en) Shock mount for collapsible antennas
US2972146A (en) Folded dipole antenna with internally mounted loading means
US2963704A (en) Antenna
US2939130A (en) Dipole radio sonde
Donn A new helical antenna design for better on-and off-boresight axial ratio performance
US2805414A (en) Antenna structure
US1889568A (en) Universally adjustable radio apparatus for aircraft
US2201807A (en) Direction finder loop