GB763805A - Improvements relating to radar aerial assemblies - Google Patents
Improvements relating to radar aerial assembliesInfo
- Publication number
- GB763805A GB763805A GB2222/55A GB222255A GB763805A GB 763805 A GB763805 A GB 763805A GB 2222/55 A GB2222/55 A GB 2222/55A GB 222255 A GB222255 A GB 222255A GB 763805 A GB763805 A GB 763805A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- reflector
- housing
- gear
- scan
- 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
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/12—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems
- H01Q3/16—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device
- H01Q3/20—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device wherein the primary active element is fixed and the reflecting device is movable
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/42—Simultaneous measurement of distance and other co-ordinates
- G01S13/422—Simultaneous measurement of distance and other co-ordinates sequential lobing, e.g. conical scan
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Toys (AREA)
Abstract
763,805. Aerials. METROPOLITANVICKERS ELECTRICAL CO., Ltd. (Compagnie Francaise Thomson-Houston). Jan. 25, 1955, No. 2222/55. Class 40(7) A radar aerial assembly comprises a fixed primary element radiating energy into a beam producing reflector, the reflector being pivoted about a point on its axis and capable of movement to cause the beam to scan spirally or conically. Preferably balancing means are provided for maintaining the reflector in substantial dynamic equilibrium. As shown schematically in Fig. 3 the reflector 1 may be attached to a shaft 11 pivoted at 3 in the front of a housing 9 by' means of a universal coupling allowing it to oscillate about two axes perpendicular to each other and the shaft 11. To maintain dynamic equilibrium an annular ring carrying adjustable balance weights 4 is provided inside the housing and this is mounted on a second universal coupling at 15. The balance system is coupled to shaft 11 through a sliding ball and socket joint 18 so placed that motion of the shaft causes opposite displacements of the reflector and balance ring. Springs 19 are connected between housing 9 and the reflector 1 and springs 20 between the balance system and the housing. The natural periods of vibration of the two spring systems thus obtained are arranged to be equal and the frequency of the drive is also made to he such that one rotation takes place in this period. This reduces the power required to drive the aerial. A flexible mounting may be introduced between the reflector and the housing to stiffen the system. Alternative ways of obtaining dynamic equilibrium are described with reference to Figs. 4 to 7 (not shown). The drive mechanism for-shaft 11 is described with reference to Fig. 8. Here the spiral scan drive motor 75 drives shaft 48 through gearing and this shaft in turn drives annular gear 44 which engages planet wheel 42 on shaft 62. The shaft 11 is coupled to the planet wheel through ball and socket joint 52. The movement of axis 62 of the planet wheel is also the movement of main shaft 43 which is driven from shaft 48 through pinion 50 and clutch 51. The conical scan is effected by energizing motor 53 which drives gear 44 through gear 60 and operating locking device 55 which causes a notch 63 to engage in socket 54 so that gear 44 and shaft 43 rotate together. Clutch 51 slips under these conditions and the speed and gearing of motor 53 is arranged so that the conical scan is at a higher speed than the spiral scan and wheel 47, which is constructed to " over-run " freely, will disconnect motor 75 even if this is still running. Generator 58 is arranged to provide an alternating reference voltage and switch 66 operated by cam 57 produces a changeover which can be used to resolve ambiguity in the reference signal.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1095342D FR1095342A (en) | 1953-10-09 | 1953-10-09 | Advanced radar aerial |
GB2222/55A GB763805A (en) | 1953-10-09 | 1955-01-25 | Improvements relating to radar aerial assemblies |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1095342T | 1953-10-09 | ||
GB2222/55A GB763805A (en) | 1953-10-09 | 1955-01-25 | Improvements relating to radar aerial assemblies |
Publications (1)
Publication Number | Publication Date |
---|---|
GB763805A true GB763805A (en) | 1956-12-19 |
Family
ID=52465045
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2222/55A Expired GB763805A (en) | 1953-10-09 | 1955-01-25 | Improvements relating to radar aerial assemblies |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1095342A (en) |
GB (1) | GB763805A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4043841A1 (en) * | 2021-02-12 | 2022-08-17 | Rosemount Tank Radar AB | Radar level gauge with elastic system |
-
1953
- 1953-10-09 FR FR1095342D patent/FR1095342A/en not_active Expired
-
1955
- 1955-01-25 GB GB2222/55A patent/GB763805A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4043841A1 (en) * | 2021-02-12 | 2022-08-17 | Rosemount Tank Radar AB | Radar level gauge with elastic system |
EP4043842A1 (en) * | 2021-02-12 | 2022-08-17 | Rosemount Tank Radar AB | Radar level gauge with elastic system |
Also Published As
Publication number | Publication date |
---|---|
FR1095342A (en) | 1955-06-01 |
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