GB650592A - Improvements in or relating to radio aerial arrangements for use on aircraft - Google Patents
Improvements in or relating to radio aerial arrangements for use on aircraftInfo
- Publication number
- GB650592A GB650592A GB925748A GB925748A GB650592A GB 650592 A GB650592 A GB 650592A GB 925748 A GB925748 A GB 925748A GB 925748 A GB925748 A GB 925748A GB 650592 A GB650592 A GB 650592A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerial
- open
- depression
- feeder
- aircraft
- 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
- 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
- H01Q1/286—Adaptation for use in or on aircraft, missiles, satellites, or balloons substantially flush mounted with the skin of the craft
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Waveguide Connection Structure (AREA)
Abstract
650,592. Aerials. MARCONI'S WIRELESS TELEGRAPH CO., Ltd. April 1, 1948, No. 9257. [Class 40 (vii)] Relates to aircraft open aerials which are substantially in or sunk below the level of the aircraft skin. When such an aerial is coupled to a receiver through a long feeder the signal pick-up is reduced due to the capacity of the feeder and according to the present invention this effect is prevented by coupling the aerial to the feeder by a valve buffer stage. The invention is described as applied to a rotatable loop D.F. system in which the open aerial constitutes the sense aerial, the buffer stage also serving to decouple the two aerials. As shown, a flattened iron cored loop L rotatable by a motor (not shown) is mounted in a depression K formed in the conductive skin A of the aircraft which is covered by a removable insulating lid so as to maintain a smooth surface and the open aerial comprises a folded conductor O mounted by insulators S on the floor of the depression. One end of the conductor O is coupled to the grid of a buffer valve, Fig. 2 (not shown), mounted on the back of the floor' of the depression, Fig. 4 (not shown), and the valve anode is coupled by a toroidal matching transformer to a coaxial feeder. The other end of the open aerial is earthed and a 5 megohm resistor is connected across the two ends to disperse any static charges which may accumulate on the aerial. At the receiver end of the feeder the inner conductor is coupled to the receiver input through a capacitor which is adjusted so that the reactance presented to the receiver and hence the phasing of the input signal is the same as that produced by a conventional open aerial. If the reactance of the capacitor is high enough the buffer valve may be a cathode follower. Alternatively the open aerial may be carried by the lid or embedded in the insulating material thereof. If the depression is rectangular or square the open aerial may comprise a plurality of parallel spaced wires lying in a plane or curved surface and joined together by a cross-wire at one end or with a circular or annular depression it may comprise a central ring with a plurality of evely-spaced radial wires.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB925748A GB650592A (en) | 1948-04-01 | 1948-04-01 | Improvements in or relating to radio aerial arrangements for use on aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB925748A GB650592A (en) | 1948-04-01 | 1948-04-01 | Improvements in or relating to radio aerial arrangements for use on aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB650592A true GB650592A (en) | 1951-02-28 |
Family
ID=9868486
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB925748A Expired GB650592A (en) | 1948-04-01 | 1948-04-01 | Improvements in or relating to radio aerial arrangements for use on aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB650592A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4183027A (en) * | 1977-10-07 | 1980-01-08 | Ehrenspeck Hermann W | Dual frequency band directional antenna system |
CN103029825A (en) * | 2012-12-11 | 2013-04-10 | 江西洪都航空工业集团有限责任公司 | Embedded antenna installation mouth frame |
-
1948
- 1948-04-01 GB GB925748A patent/GB650592A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4183027A (en) * | 1977-10-07 | 1980-01-08 | Ehrenspeck Hermann W | Dual frequency band directional antenna system |
CN103029825A (en) * | 2012-12-11 | 2013-04-10 | 江西洪都航空工业集团有限责任公司 | Embedded antenna installation mouth frame |
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