GB538030A - Improvements in navigational devices - Google Patents
Improvements in navigational devicesInfo
- Publication number
- GB538030A GB538030A GB1935/40A GB193540A GB538030A GB 538030 A GB538030 A GB 538030A GB 1935/40 A GB1935/40 A GB 1935/40A GB 193540 A GB193540 A GB 193540A GB 538030 A GB538030 A GB 538030A
- Authority
- GB
- United Kingdom
- Prior art keywords
- switch
- craft
- phase
- aerial
- generator
- 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
- 238000004804 winding Methods 0.000 abstract 1
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
Landscapes
- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automatic Cycles, And Cycles In General (AREA)
Abstract
538,030. Directive wireless systems. MARCONI'S WIRELESS TELEGRAPH CO., Ltd. Jan. 31, 1940, No. 1935. Convention date, Jan. 31, 1939. [Class 40 (v)] The heading of a moving craft with respect to (a) an earth compass, (b) a radio compass, (c) the bearing of the craft with respect to a radio transmitter are separately shown on a single indicator. A frame aerial 1, a local generator 3, and an earth inductorwinding 5 are mounted in fixed relation on a common shaft, which is continuously rotated by a motor 9. Signals from the aerial 1, and from a non-directive aerial 15, are combined in a receiver 13, the output from which is fed directly to a centre terminal 14, and through a phase-shifter 16 to the lower terminal 17, of a three-position switch 19. The output from the generator 3 is connected to the upper and centre terminals of a switch 23, whilst the earth inductor 5 is connected to the'upper terminal 27 of switch 19 and to the lower terminal of switch 23. The hinge contact of switch 23 is connected through a phasesplitter 35 to the deflecting plates of a cathode ray tube 41, the other electrodes of which are connected through switches 47, 49, 51 to a potentiometer 43. The hinge contact of switch 19 is connected to a saturation transformer 31 which also feeds the control grid 57 of the cathode ray tube through the hinge contact of the switch 51. All the switches are driven through reduction gearing 61 from the aerial shaft 7. The arrangement allows the phase of the signal current to be compared (a) with that generated by the inductor 5, and (b) with the " standard " phase from the generator 5. For instance, when the craft is heading due North, there will be no phase-difference between two of these currents, and similarly when the craft is heading directly on to the distant radio transmitter. For other directions of flight, the relative phase-differences, indicating the headings and bearings, will be shown as radial traces on three concentric scales 61, 63 and 65, Fig. 2 on the screen of the cathode ray tube. The inductor winding may be replaced by a gyro compass (Fig. 3 not shown) which is connected to a small coil located in a rotating field derived from the generator of the " standard " or reference current. A " fix " of the craft's position at any time can be obtained by observing the intersecting traces formed in a double-stream indicator tube. Reference has been directed by the Comptroller to Specification 532,854.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US538030XA | 1939-01-31 | 1939-01-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB538030A true GB538030A (en) | 1941-07-17 |
Family
ID=21986641
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1935/40A Expired GB538030A (en) | 1939-01-31 | 1940-01-31 | Improvements in navigational devices |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB538030A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2502721A (en) * | 1945-07-02 | 1950-04-04 | Sperry Corp | Instrument landing indicator |
US4442609A (en) * | 1980-09-25 | 1984-04-17 | Nissan Motor Company, Limited | Vehicle orientation detecting device for an automotive vehicle or another vehicle |
-
1940
- 1940-01-31 GB GB1935/40A patent/GB538030A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2502721A (en) * | 1945-07-02 | 1950-04-04 | Sperry Corp | Instrument landing indicator |
US4442609A (en) * | 1980-09-25 | 1984-04-17 | Nissan Motor Company, Limited | Vehicle orientation detecting device for an automotive vehicle or another vehicle |
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