GB646357A - Short wave directive radio antennae - Google Patents
Short wave directive radio antennaeInfo
- Publication number
- GB646357A GB646357A GB13491/45A GB1349145A GB646357A GB 646357 A GB646357 A GB 646357A GB 13491/45 A GB13491/45 A GB 13491/45A GB 1349145 A GB1349145 A GB 1349145A GB 646357 A GB646357 A GB 646357A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flap
- edge
- antenna
- sheet
- angle
- 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
- 238000003491 array Methods 0.000 abstract 1
- 230000035559 beat frequency Effects 0.000 abstract 1
- 239000004020 conductor Substances 0.000 abstract 1
- 239000003989 dielectric material Substances 0.000 abstract 1
- 230000005855 radiation Effects 0.000 abstract 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/10—Resonant slot antennas
-
- 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
-
- 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
- H01Q19/06—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 refracting or diffracting devices, e.g. lens
-
- 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
- H01Q19/22—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 a secondary device in the form of a single substantially straight conductive element
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
646,357. Aerials;radio navigation. MARCONI'S WIRELESS TELEGRAPH CO., Ltd. Mav 29, 1945, No. 13491. Convention date, May 26, 1943. [Class 40 (vii)] A short wave directive antenna is formed by attaching a conductive rectangular flap 12 along one edge to a conductive base sheet 10 so that there is a small angle between them. The base sheet may be large, e.g. the side of an aircraft fuselage. The triangular ends of the antenna are preferably closed and a curve (Fig. 15, not shown) relating width to length for an antenna with ends closed is given. To prevent ingress of dirt and moisture, the open bottom edge may be filled with dielectric material. Connection to the antenna can be made by means of a coaxial feeder 15, the outer sheath being connected to the sheet 10 and the inner conductor to a point mid-way along the flap. The vertical distance of the connection from the edge of the flap may be chosen to give a particular terminal impedance. Maximum radiation occurs downwards along a line making an angle of 45 degrees with the sheet 10 and at right angles to the line of attachment of the flap; to increase the directivity a second reflector flap 22 may be mounted above the radiator with its open edge just overlapping the latter's attached edge. The units may be tuned either by U-shaped adjustable attachments 13 and 23, or by using a capacity plate mounted on a threaded rod screwed through a boss on the lower edge of the reflector, Fig. 11 (not shown). The antennae may be mounted in arrays, an array of four antennµ with reflectors and fed in phase by branched feeders tuned by stubs is described with reference to Figs. 8 and 12 (not shown). Radio navigation.-In order to estimate drift an aircraft 1, Fig. 2, fitted with the antennµ described, radiates two lobes of energy Pb and Sb of the same frequency downwards at an angle of 45 degrees. After diffuse reflection by the land or sea surface S, energy is received by the same aerials and the signals from the port and starboard sides are compared in frequency, the beat frequency being proportional to the craft's rate of drift.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US488584A US2425303A (en) | 1943-05-26 | 1943-05-26 | Antenna system for radio drift indication |
Publications (1)
Publication Number | Publication Date |
---|---|
GB646357A true GB646357A (en) | 1950-11-22 |
Family
ID=23940266
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13491/45A Expired GB646357A (en) | 1943-05-26 | 1945-05-29 | Short wave directive radio antennae |
Country Status (2)
Country | Link |
---|---|
US (1) | US2425303A (en) |
GB (1) | GB646357A (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2573460A (en) * | 1945-08-25 | 1951-10-30 | Rca Corp | Antenna |
US2604595A (en) * | 1945-09-25 | 1952-07-22 | Standard Telephones Cables Ltd | Antenna reflector |
US2516500A (en) * | 1946-03-26 | 1950-07-25 | Alford Andrew | Electrical apparatus |
US2573401A (en) * | 1947-11-13 | 1951-10-30 | Rca Corp | Louver antenna |
US2661422A (en) * | 1949-02-21 | 1953-12-01 | Johnson William Arthur | Slotted antenna system |
US2908000A (en) * | 1949-04-08 | 1959-10-06 | John S Lacey | Notch antenna |
US2589664A (en) * | 1949-08-30 | 1952-03-18 | Airborne Instr Lab Inc | Antenna system |
US2996713A (en) * | 1956-11-05 | 1961-08-15 | Antenna Engineering Lab | Radial waveguide antenna |
US2990546A (en) * | 1957-04-30 | 1961-06-27 | Herbert W Haas | Quadraloop antenna |
US3096515A (en) * | 1958-08-29 | 1963-07-02 | Raytheon Co | Antenna systems |
US3683281A (en) * | 1969-10-13 | 1972-08-08 | Scanwell Lab Inc | Crab angle sensing system |
DE102009019995A1 (en) * | 2009-05-05 | 2010-11-11 | Airbus Deutschland Gmbh | Method for directional digital data transmission between an aircraft and a ground station |
US9705185B2 (en) * | 2013-04-11 | 2017-07-11 | Raytheon Company | Integrated antenna and antenna component |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1670553A (en) * | 1927-01-07 | 1928-05-22 | Sharp And Combs Inc | Wireless antenna |
GB462466A (en) * | 1935-09-10 | 1937-03-10 | Castle Fuse & Engineering Comp | Improvements in aerial and earth connections for wireless apparatus |
-
1943
- 1943-05-26 US US488584A patent/US2425303A/en not_active Expired - Lifetime
-
1945
- 1945-05-29 GB GB13491/45A patent/GB646357A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US2425303A (en) | 1947-08-12 |
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