US2035011A - Shipboard antenna system - Google Patents
Shipboard antenna system Download PDFInfo
- Publication number
- US2035011A US2035011A US724316A US72431634A US2035011A US 2035011 A US2035011 A US 2035011A US 724316 A US724316 A US 724316A US 72431634 A US72431634 A US 72431634A US 2035011 A US2035011 A US 2035011A
- Authority
- US
- United States
- Prior art keywords
- antenna
- condenser
- pendulum
- ship
- shipboard
- 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 - Lifetime
Links
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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
- H01Q1/34—Adaptation for use in or on ships, submarines, buoys or torpedoes
Definitions
- the present invention has for its object the compensation of the effect on the control of antennas for Wireless telegraphy installed on board of ships, produced by the rolling of the ships.
- this detuning is avoided by means of a compensating organ whose functioning is controlled by the same action, the influence of which is intended to be corrected, that is to say, by the inclination of the ship.
- a compensating organ whose functioning is controlled by the same action, the influence of which is intended to be corrected, that is to say, by the inclination of the ship.
- Such action will be obtained for instance, by means of a pendulum or gyroscope.
- the compensating organ proper will be very easily obtained by means of a variable condenser or a variable self inductance connected in series or in parallel to the antenna, or by means of circuits coupled to the latter.
- Figure 2 is a section of a variable condenser wherein compensation is controlled by means of a pendulum;
- Figure 3 is a section of a variable condenser wherein the pendulum forms the movable plate element of the condenser.
- Figure 1 shows at N a ship, whose antenna A, assumed to be vertical if rolling does not occur, moves, as a result thereof, into an instantaneous inclination oz.
- the apparent antenna capacity is shown at C in dotted lines. It is obvious that this capacity is a minimum if the antenna is in a vertical position and that it increases with the inclination of the ship in accordance with a law depending upon the shape of the antenna.
- Figure 2 shows the manner in which the compensation can be obtained by means of a variable condenser controlled by a pendulum.
- l and 2 represent the two armatures of the condenser and 3 the pendulum.
- the armature l is fixedly secured to the ship thereby following the inclination a; the armature 2, on the contrary, is maintained in the vertical position by the pendulum. It will thus be readily seen that in this manner a capacity is obtained which is a maximum when the inclination is zero, and which decreases with increasing inclination.
- Figure 3 shows a preferred embodiment of the invention whereby the pendulum proper forms one of the armatures 2 of the condenser.
- the other armature I will be formed for instance by two metallic plates fastened to the Walls of a container, containing an insulating liquid, assuring the damping of the oscillations of the pendulum.
- the profile of the armatures l and 2 can be so shaped that a law of determined variation is obtained by which the variations of the antenna capacity C can be exactly compensated.
- the condenser is mounted in parallel with the antenna capacity.
- suifices that, in order to maintain the tuning of the control means, that the sum of the two capacities remains constant.
- variable condenser of Figures 2 and 3 could be placed in series to the antenna instead of being connected in parallel thereto and these elements could be placed in circuits indirectly coupled to the antenna.
- variable condenser could be replaced by a variable self inductance or other elements permitting the same result.
- the pendulum can be replaced by a gyroscope or any other suitable stabilizing element.
- a shipboard antenna circuit comprising an aerial and a variable tuning element, and means for automatically adjusting the said tuning ele- 40 ment so that the proper frequency of the antenna circuit remains constant, said means being controlled by the rolling of the ship.
- a shipboard antenna circuit comprising an aerial and a variable condenser connected therewith, and means controlled by the rolling of the ship for automatically adjusting the said condenser so that the proper frequency of the antenna circuit remains constant.
- a shipboard antenna. circuit comprising an aerial and a variable condenser connected therewith, an armature of this condenser being fixedly mounted relatively to the ship and a second armature being pivotally mounted so as to remain by the weight action in a constant position with respect to the vertical line when the ship rolls, the said armatures being so shaped that the antenna circuit capacity remains constant during, the rollmg.
- a shipboard antenna circuit comprising an aerial and a. variable condenser connected therewith, an armature of this condenser being fixedly and a second armature being pivotally mounted with respect to the ship, a pendulum attached to the said second armature, and means comprising a predetermined armature shape for maintaining the antenna circuit capacitance constant irre- 5
Landscapes
- Details Of Aerials (AREA)
- Support Of Aerials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR769245T | 1933-05-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2035011A true US2035011A (en) | 1936-03-24 |
Family
ID=9184668
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US724316A Expired - Lifetime US2035011A (en) | 1933-05-18 | 1934-05-07 | Shipboard antenna system |
Country Status (3)
Country | Link |
---|---|
US (1) | US2035011A (fr) |
BE (1) | BE402706A (fr) |
FR (1) | FR769245A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3146450A (en) * | 1961-02-01 | 1964-08-25 | Gen Bronze Corp | Capacity-compensated motor-driven antenna |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2550390B1 (fr) * | 1983-08-03 | 1985-11-29 | Legall Jean Claude | Monture d'antenne a stabilisation passive |
-
0
- BE BE402706D patent/BE402706A/xx unknown
-
1933
- 1933-05-18 FR FR769245D patent/FR769245A/fr not_active Expired
-
1934
- 1934-05-07 US US724316A patent/US2035011A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3146450A (en) * | 1961-02-01 | 1964-08-25 | Gen Bronze Corp | Capacity-compensated motor-driven antenna |
Also Published As
Publication number | Publication date |
---|---|
FR769245A (fr) | 1934-08-22 |
BE402706A (fr) |
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