GB616369A - Radio direction finder - Google Patents
Radio direction finderInfo
- Publication number
- GB616369A GB616369A GB16623/46A GB1662346A GB616369A GB 616369 A GB616369 A GB 616369A GB 16623/46 A GB16623/46 A GB 16623/46A GB 1662346 A GB1662346 A GB 1662346A GB 616369 A GB616369 A GB 616369A
- Authority
- GB
- United Kingdom
- Prior art keywords
- reception
- aerials
- pulses
- aerial
- pulse
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
Abstract
616,369. Radio direction finding. SPAN DARD TELEPHONES & CABLES, Ltd. May 31, 1946, No. 16623. Convention date, June 27, 1945. [Class 40 (vii)] A radio direction-finder for use in the reception of single pulses comprises a plurality of differently directed aerials 1, 2, 3, 4, the outputs from which are applied respectively through the delay units 14, 15, 16, 17. each of which has a different delay time, to the receiver 13 so that upon the reception of a single pulse a train of pulses of different amplitudes is applied to the receiver. The aerials which are rendered unidirectional by mounting reflecting shields behind them are so arranged that a signal received from any direction energizes at least one, but not more than two of the aerials. An omnidirectional aerial is also provided. the undelayed output from this aerial being used to trigger the circuit 21 which generates the linear time-base of the cathode-ray tube indicator and to apply a brightening pulse to the grid 26 of the tube when a signal is received. The signals received by the directional aerials are consequently displayed in succession on the cathode-ray tube trace, their relative amplitudes being indicative of the direction of reception. The Specification as open to inspection under Sect. 91 describes a system comprising an aerial system as previously described so that a train of pulses is delivered for each pulse received, wherein means are provided at the receiver for directing the pulses of each train into different channels corresponding to the appropriate receiving aerial, these channels being connected to separate plates of a cathoderay tube so that the direction of deflection of the spot corresponds to the direction of reception of the pulse signal. This subjectmatter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US616369XA | 1945-06-27 | 1945-06-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB616369A true GB616369A (en) | 1949-01-20 |
Family
ID=22037095
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16623/46A Expired GB616369A (en) | 1945-06-27 | 1946-05-31 | Radio direction finder |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB616369A (en) |
-
1946
- 1946-05-31 GB GB16623/46A patent/GB616369A/en not_active Expired
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