GB1390009A - Method and apparatus for radiating low-frequency radio waves - Google Patents
Method and apparatus for radiating low-frequency radio wavesInfo
- Publication number
- GB1390009A GB1390009A GB5591073A GB5591073A GB1390009A GB 1390009 A GB1390009 A GB 1390009A GB 5591073 A GB5591073 A GB 5591073A GB 5591073 A GB5591073 A GB 5591073A GB 1390009 A GB1390009 A GB 1390009A
- Authority
- GB
- United Kingdom
- Prior art keywords
- helicopter
- aerial
- terminal
- shell
- drogue
- 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
Links
Classifications
-
- 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
- H01Q9/30—Resonant antennas with feed to end of elongated active element, e.g. unipole
- H01Q9/32—Vertical arrangement of element
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Details Of Aerials (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
1390009 Aerials WESTINGHOUSE ELECTRIC CORP 3 Dec 1973 [12 Dec 1972] 55910/73 Heading H4A In propagating radio waves of a frequency not exceeding 300 kHz from an aerial which is adapted to be deployed from an aircraft and to be connected toward its upper end to a transmitter, said aerial has length substantially equal to one-fourth of the operating wavelength of the transmitter, and at least part of it is suspended vertically from the aircraft. At the lower end of the aerial are means for providing a lowresistance path to a body of water having a conductivity at least equivalent to the presence therein of 1 part per 1000 of NaCl, whereby it acts as a ground plane. In one embodiment an aerial element 18, Fig. 2B, extends from a helicopter 10 to the sea 21 where it terminates in a drogue 20, which provides a good electrical connection. The aerial element 18 may have a diameter of # to ¢ inch and be made of a mechanically strong material such as steel or fibreglass, with a conductive coating of copper or aluminium. It is lowered from the helicopter by means of a winch, and passes through an insulating bushing 22. One terminal of a radio generator 26 is connected through a coupling unit 24 to the element 18, and the other terminal thereof is connected to the shell of the helicopter. A counterpoise 32, which enables the length of the element 18 to be reduced below #/4, is deployed from the helicopter, one end being connected to the shell thereof, and the other end being terminated in a conductive shell 34 of greater diameter, to reduce corona effects. In another embodiment, the counterpoise is omitted (Fig. 2A, not shown) and in another it is passed through an insulating bushing to one terminal of the radio generator, the other terminal of said generator being connected via the coupling unit to the helicopter shell, to which the aerial element is also connected (Fig. 2C, not shown). The drogue 20, Fig. 4, has a lightweight housing 44 in which is a solenoidoperated door 54 controlled by radio signals from the helicopter for admitting water when the drogue is lowered and for releasing water when it is raised. A conductive coating 62 is provided on the outside of the body 44, and the element 18 is attached via a universal connector 40.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00314486A US3823402A (en) | 1972-12-12 | 1972-12-12 | Antenna deployed from aircraft to contact a body of water for length reduction |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1390009A true GB1390009A (en) | 1975-04-09 |
Family
ID=23220152
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5591073A Expired GB1390009A (en) | 1972-12-12 | 1973-12-03 | Method and apparatus for radiating low-frequency radio waves |
Country Status (4)
Country | Link |
---|---|
US (1) | US3823402A (en) |
JP (1) | JPS4990470A (en) |
DE (1) | DE2360786A1 (en) |
GB (1) | GB1390009A (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7154430B1 (en) | 1981-01-16 | 2006-12-26 | The Boeing Company | Ventriloqual jamming using a towed transmission line |
CA1223339A (en) * | 1983-09-23 | 1987-06-23 | James Hadzoglou | Cellular mobile communications antenna |
JPS60189112U (en) * | 1984-05-24 | 1985-12-14 | 旭硝子株式会社 | automotive glass antenna |
US4730194A (en) * | 1985-06-20 | 1988-03-08 | Westinghouse Electric Corp. | Airborne transmitting antenna and method for deploying same |
FR2605805B1 (en) * | 1986-10-24 | 1989-02-24 | Thomson Csf | ELECTROMAGNETIC IMPULSE AGGRESSION SIMULATOR |
US5242376A (en) * | 1990-10-09 | 1993-09-07 | 21St Century Holdings, Inc. | Relaxation device and method |
FR2743198B1 (en) * | 1995-12-27 | 1998-02-27 | Eurocopter France | METHOD FOR COMPENSATING ATTENUATION OF THE RADIATION OF A HIGH FREQUENCY ANTENNA MOUNTED ON A STRUCTURE THUS IMPROVED |
CN114389059B (en) * | 2021-12-31 | 2024-05-07 | 国核电力规划设计研究院有限公司 | External-lead-in sea grounding device for offshore power plant and transformer substation |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE232257C (en) * | ||||
US1372658A (en) * | 1919-04-11 | 1921-03-22 | Jones Edward Thomas | Underground or underwater antenna system |
US1708071A (en) * | 1919-10-31 | 1929-04-09 | John A Willoughby | Radio signal apparatus |
US1858336A (en) * | 1930-01-09 | 1932-05-17 | Nat Electrical Supply Company | Antenna lead-out insulator |
US1953071A (en) * | 1931-08-28 | 1934-04-03 | Nat Electrical Supply Company | Aircraft antenna weight |
FR1604503A (en) * | 1960-05-31 | 1971-11-29 | ||
US3181158A (en) * | 1961-12-07 | 1965-04-27 | Kenneth W Grinde | Water-borne distress unit |
-
1972
- 1972-12-12 US US00314486A patent/US3823402A/en not_active Expired - Lifetime
-
1973
- 1973-12-03 GB GB5591073A patent/GB1390009A/en not_active Expired
- 1973-12-06 DE DE2360786A patent/DE2360786A1/en active Pending
- 1973-12-10 JP JP48136918A patent/JPS4990470A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
DE2360786A1 (en) | 1974-06-20 |
US3823402A (en) | 1974-07-09 |
JPS4990470A (en) | 1974-08-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |