US1360235A - Electric relay - Google Patents
Electric relay Download PDFInfo
- Publication number
- US1360235A US1360235A US343903A US34390319A US1360235A US 1360235 A US1360235 A US 1360235A US 343903 A US343903 A US 343903A US 34390319 A US34390319 A US 34390319A US 1360235 A US1360235 A US 1360235A
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- US
- United States
- Prior art keywords
- electric
- valve
- anode
- cathode
- needle
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
Definitions
- his invention relates to electric relays and has for its primary objects to obtain increased sensitiveness and to avoid time lag.
- the improved relay is constructed with a thermionic valve having a, fixed cathode and anode system wherein a control element or screen movable relative to the cathode and anode of the valve is adapted to render the valve conductive or not, by allowing or interfering with the flow of current between the heated cathode and the anode from an electric source of current which controls a part to be operated as hereinafter described.
- Figure 1 is a'transverse section on line 1--1, in Fig. 2, of the valve and shows some of the electric connections; and Fig. 2 is a longitudinal section, and shows other electric connections.
- the valve comprises a glass vacuum tube 3, a heated cathode or filament .5, and anodes 6, 7, the cathode and anodes being fixed relatively toeach other, that'is to say, that the operation of the control hereinafter described is not dependent upon an relative movement of the elements.
- the filament is connected by a conductor 8 with the negative terminal, and the anodes are connected by parallel conductors 9, 10 with the positive terminal of a source of electric current 11, and 12, 13 are two elec tromagnets in the conductors 9, 10.
- the filament is further connected through conductors 14, 15 with a source of alternating current by which the filament is heated.
- 16 is a compass needle pivoted at 17 and connected by a conductor 18 with the source of electric current 11 in such a mannerthat its potential may be adjusted.
- 19 is a switch.
- the filament is mounted vertically above one end of the compass needle Specification of Letters Patent.
- the anodes are mounted below and one on each side of the compass needle end and lie at such an angle to the needle and to one another when the latter is in its zero or neutral position,
- the shielding influence of the needle is adjusted to be suthcient to produce a sensible diminution of the normal current between the filament and the anodes.
- the needle has a relative deflection to either side so that it lies closer to one anode than the other, the balance of electrostatic forces is upset and the valve becomes more conductive between the filament and the anode farthest from the needle, and the current from the electric source operates the electromagnet in known manner.
- the invention is particularly suitable in ts application to aerial navigation, where- 1n, for example, the relay can be used to automatically control a rudder for steering a craft.
- the valve may be rota tably mounted on a suitable support so that while traveling on a set course it may be turned until the anodes and compass needle are in the relative positions above referred to as the Zero position with the N pole point ing to the north. Under these conditions, any deviation of the craft from the course will result in relative movement so that the compass needle will be closer to one anode and farther from the other. This will permit the fiow of current to operate one or other of the electromagnets, which in turn will appropriately operate the rudder through an electric or other type of motor, not shown, until the course is regained and the electrostatic balance is restored. Gimbal or equivalent bearings may be used to support the valve in a horizontal plane.
- the valve for controlling lateral or longitudinal flying angles of aircraft,jthe valve is arranged upright and the compass needle is replaced by a pendulum which is in its zero position when the craft is flying in correct trim, and when there is angular variation in the trim, acts like the compass needle to control the flow of current to the electromagnets which directly or indirectly give the necessary correcting movement to the ailerons, elevators or the like.
- the member 16 may be moved by an outside magnet.
- valve may be rotatably mounted on the compass frame above the compass card, and a magnet may be mounted on the compass card or part which is controlled by the rotor to move the member 16, above it, by means of the magnetic coupling.
- An electric relay comprising a thermionic valve having a cathode system and an anode system fixed with respect to each,
- control element consists of a pivoted magnet adapted to allow or interfere with the How of electrons between the heated cathode and the anode, substantially as described.
- An electric relay comprising a thermionic valve having a cathode system and a anode system fixed with respect to each other, and a control element movable about a pivot to render said valve more or less conductive, said anode. system consisting of a plurality of members arranged on opposite sides of the. pivot of the control element.
- an electric relay comprising a thermionic valve having cathode and anode members, of a movable elementmounted within the valve, and controlling the conductance thereof, an electric circuit including a source of electric current and the cathode and anode members, and electromagnetic mechanism controlled by the circuit, substantially as described.
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- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electrically Driven Valve-Operating Means (AREA)
Description
G. McALPlNE.
ELECTRIC RELAY.
APPLICATION FILED DEC, 10. 1919.
1 ,360,235, Patented Nov. 23, 1920.
W WW;
PATENT OFFICE.
GUSTAVUS MCALPINE, OF LONDON, ENGLAND.
ELECTRIC RELAY.
To all whom it may concern B it known that I, (JrUs'rAvUs MoALrmE, a subject of the Kin r of Great Britain, residin in London, ngland, have invented certain new and useful Improvements in Electric Relays, of which the following is a s ecification.
his invention relates to electric relays and has for its primary objects to obtain increased sensitiveness and to avoid time lag.
To this end, the improved relay is constructed with a thermionic valve having a, fixed cathode and anode system wherein a control element or screen movable relative to the cathode and anode of the valve is adapted to render the valve conductive or not, by allowing or interfering with the flow of current between the heated cathode and the anode from an electric source of current which controls a part to be operated as hereinafter described.
The invention is illustrated diagrammatically in the accompanying drawings, in a form of construction embodying a compass needle as the control element, and the application of other forms of control element will be obvious therefrom.
In the drawings Figure 1 is a'transverse section on line 1--1, in Fig. 2, of the valve and shows some of the electric connections; and Fig. 2 is a longitudinal section, and shows other electric connections.
As shown, the valve comprises a glass vacuum tube 3, a heated cathode or filament .5, and anodes 6, 7, the cathode and anodes being fixed relatively toeach other, that'is to say, that the operation of the control hereinafter described is not dependent upon an relative movement of the elements.
The filament is connected by a conductor 8 with the negative terminal, and the anodes are connected by parallel conductors 9, 10 with the positive terminal of a source of electric current 11, and 12, 13 are two elec tromagnets in the conductors 9, 10.
The filament is further connected through conductors 14, 15 with a source of alternating current by which the filament is heated.
16 is a compass needle pivoted at 17 and connected by a conductor 18 with the source of electric current 11 in such a mannerthat its potential may be adjusted. 19 is a switch.
As shown, the filament is mounted vertically above one end of the compass needle Specification of Letters Patent.
Patented Nov. 23, 1920.
Application filed December 10, 1919. Serial No. 343,903.
and lies parallel thereto when the latter is in its zero or neutral position. The anodes are mounted below and one on each side of the compass needle end and lie at such an angle to the needle and to one another when the latter is in its zero or neutral position,
that a small deflection say of 10 to either midway between the anodes, the shielding influence of the needle is adjusted to be suthcient to produce a sensible diminution of the normal current between the filament and the anodes. When the needle has a relative deflection to either side so that it lies closer to one anode than the other, the balance of electrostatic forces is upset and the valve becomes more conductive between the filament and the anode farthest from the needle, and the current from the electric source operates the electromagnet in known manner.
The invention is particularly suitable in ts application to aerial navigation, where- 1n, for example, the relay can be used to automatically control a rudder for steering a craft.
For example, the valve may be rota tably mounted on a suitable support so that while traveling on a set course it may be turned until the anodes and compass needle are in the relative positions above referred to as the Zero position with the N pole point ing to the north. Under these conditions, any deviation of the craft from the course will result in relative movement so that the compass needle will be closer to one anode and farther from the other. This will permit the fiow of current to operate one or other of the electromagnets, which in turn will appropriately operate the rudder through an electric or other type of motor, not shown, until the course is regained and the electrostatic balance is restored. Gimbal or equivalent bearings may be used to support the valve in a horizontal plane.
As a further example, for controlling lateral or longitudinal flying angles of aircraft,jthe valve is arranged upright and the compass needle is replaced by a pendulum which is in its zero position when the craft is flying in correct trim, and when there is angular variation in the trim, acts like the compass needle to control the flow of current to the electromagnets which directly or indirectly give the necessary correcting movement to the ailerons, elevators or the like.
It will be understood that the invention is not limited to the constructions herein described, and may be modified in details as will be obvious to those skilled in the art.
In lieu of being automatically movable by reason of its magnetism, the member 16 may be moved by an outside magnet.
Such a construction, for example, is suitable for using the invention in conjunction with a gyro-compass In this case, the valve may be rotatably mounted on the compass frame above the compass card, and a magnet may be mounted on the compass card or part which is controlled by the rotor to move the member 16, above it, by means of the magnetic coupling.
Having thus described the nature of the said invention and the best means I know of carrying th same into practical effect, I claim 1; An electric relay comprising a thermionic valve having a cathode system and an anode system fixed with respect to each,
other in which is mounted a movable control element adapted to render it more or less conductive, substantially as described.
2. An electric relay according to claim 1,
wherein the control element consists of a pivoted magnet adapted to allow or interfere with the How of electrons between the heated cathode and the anode, substantially as described.
3. An electric relay "omprising a thermionic valve having a cathode system and a anode system fixed with respect to each other, and a control element movable about a pivot to render said valve more or less conductive, said anode. system consisting of a plurality of members arranged on opposite sides of the. pivot of the control element.
4. The combination with a relay according to claim 1, of a source of electromotive force connected with the control element, substantially as described.
The combination with an electric relay comprising a thermionic valve having cathode and anode members, of a movable elementmounted within the valve, and controlling the conductance thereof, an electric circuit including a source of electric current and the cathode and anode members, and electromagnetic mechanism controlled by the circuit, substantially as described.
In testimony whereof I have signed my name to this specification.
GUSTAVUS MoALPINE
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US343903A US1360235A (en) | 1919-12-10 | 1919-12-10 | Electric relay |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US343903A US1360235A (en) | 1919-12-10 | 1919-12-10 | Electric relay |
Publications (1)
Publication Number | Publication Date |
---|---|
US1360235A true US1360235A (en) | 1920-11-23 |
Family
ID=23348168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US343903A Expired - Lifetime US1360235A (en) | 1919-12-10 | 1919-12-10 | Electric relay |
Country Status (1)
Country | Link |
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US (1) | US1360235A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2416678A (en) * | 1947-03-04 | borsum | ||
US2756346A (en) * | 1950-10-06 | 1956-07-24 | Victoreen Instr Company | Pocket ionization chamber |
US2787839A (en) * | 1951-05-11 | 1957-04-09 | Edward E Taylor | Combination pivotal electrode vacuum tube and magnetic actuating devices |
-
1919
- 1919-12-10 US US343903A patent/US1360235A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2416678A (en) * | 1947-03-04 | borsum | ||
US2756346A (en) * | 1950-10-06 | 1956-07-24 | Victoreen Instr Company | Pocket ionization chamber |
US2787839A (en) * | 1951-05-11 | 1957-04-09 | Edward E Taylor | Combination pivotal electrode vacuum tube and magnetic actuating devices |
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