US1360235A - Electric relay - Google Patents

Electric relay Download PDF

Info

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
Authority
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
Application number
US343903A
Inventor
Mcalpine Gustavus
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US343903A priority Critical patent/US1360235A/en
Application granted granted Critical
Publication of US1360235A publication Critical patent/US1360235A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting 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.

Landscapes

  • 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
US343903A 1919-12-10 1919-12-10 Electric relay Expired - Lifetime US1360235A (en)

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
US (1) US1360235A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
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

Cited By (3)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
US1958258A (en) Automatic steering system
US2137974A (en) Aileron control for airplanes
US2387795A (en) Aircraft control apparatus
US2464629A (en) Maneuvering automatic control
US1703280A (en) Directional stabilizer
US2162862A (en) Attitude control means for aircraft
US2570905A (en) Automatic pilot
US2446180A (en) Gyroscope controlling means
US1360235A (en) Electric relay
US1958259A (en) Automatic steering equipment
US1679354A (en) Gyroscopic control of cameras and other optical devices
US2542975A (en) Erecting mechanism for reducing turn errors in vertical gyroscopes
US1869840A (en) Stabilizing apparatus
US3292269A (en) Gyroscopic compasses
US2830160A (en) Control switches
US2824710A (en) Control system for guided missiles
US2146620A (en) Gyroscopic apparatus
US1335055A (en) Controlling and stabilizing device
US2454161A (en) Electrical relay system
US2252338A (en) alkan
US1015837A (en) Automatic stabilizer for aeroplanes and the like.
US2835861A (en) Automatic pilot motor control system
US2429605A (en) Presetting means for long period gyroscopes
US2175631A (en) Gyroscopic apparatus for determining the inclination of an airplane
US1360259A (en) Horizontal steering-gear for torpedoes