US2540728A - Condition control system with stepped response - Google Patents
Condition control system with stepped response Download PDFInfo
- Publication number
- US2540728A US2540728A US654475A US65447546A US2540728A US 2540728 A US2540728 A US 2540728A US 654475 A US654475 A US 654475A US 65447546 A US65447546 A US 65447546A US 2540728 A US2540728 A US 2540728A
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- United States
- Prior art keywords
- flag
- pointer
- control system
- condition
- coils
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B1/00—Comparing elements, i.e. elements for effecting comparison directly or indirectly between a desired value and existing or anticipated values
- G05B1/01—Comparing elements, i.e. elements for effecting comparison directly or indirectly between a desired value and existing or anticipated values electric
- G05B1/04—Comparing elements, i.e. elements for effecting comparison directly or indirectly between a desired value and existing or anticipated values electric with sensing of the position of the pointer of a measuring instrument
Definitions
- This invention relates to control systems and more particularly to electrical systems for controlling a variable condition such as temperature, pressure, flow or the like.
- One of the objects of the invention is to provide a control system which will maintain a condition in a given control range and which will effect a control operation tending to return the condition to the range upon a departure therefrom.
- Another object is to provide a control stein in which the control range can be easily and quickly adjusted throughout wide limits.
- Still another object is to provide an electrical control system having high, low and neutral control positions and inv which the range of the neutral position can easily be adjusted.
- the instrument is adapted to control the temperature of a furnace 13, although any other condition such as pressure, flow or the like could equally well be controlled.
- the furnace I is heated by fuel burners supp led with fluid fuel such as gas through valves l i and l2co'ntrolled by solenoids l3 and I4.
- Temperature of the furnace is indicated by a thermocouple [5 connected to the coil Q5 of a galvanometer to produce a movement of the coil proportional to changes in furnace temperature.
- the galvanonieter includes a pointer I! connected to the coil to be moved thereby and swinging over an arcuate scale l8 to indicate the temperature of the furnace.
- the pointer I1 carries near its free end a stepped metal flag having stepped portions l9 and 20 which are offset both vertically and horizontally with respect to each other.
- the position of the pointer is sensed by reactance elements shown as inductance coils 2! and 22 which are mounted respectively adjacent the paths of movement of the flag portions l9 and 20.
- may be connected to the input or tank circuit side of an oscillator indicated generally at 23 and which may be similar to the oscillator more particularly described and claimed in the patent to Cohen No. 2,228,163.
- the coils 22 may be similarly connected to an oscillator 24, both oscillators bein so arranged that when the flag is displaced from the coils the oscillator will be in tune, while when the flag is adjacent or between the coils, the oscillator will be detuned.
- the oscillators may be powered by a common transformer 25 and may be connected through amplifiers 26 to relays 21 and 23, respectively.
- the amplifiers 26 are preferably connected to the respective oscillators as described in Cohen Patent No. 2,228,163 so that when the oscillator plate current increases, the amplifier will cut off and the amplifier will conduct when the oscillator is oscillated and its direct plate current is at a minimum.
- the relay 2 controls a switch having a movable blade 29 which normally falls away from the relay to engage a contact 32 and which is raised into engagement with a contact 3
- the contact 32 is a dead contact, although it could, if desired, be connected to an indicator or the like.
- the switch blade 29 is connected to one side of a power input circuit 33 and the contact Si is connected through the winding l3 to the opposite side of the power input circuit.
- the relay coil 28 similarly controls a switch blade 34 which is connected to one side of the circuit 33 and which normally engages a dead contact 35. When the i coil 28 is energized it pushes the switch blade up to engage a contact 36 connected through the solenoid H! to the other side of the power circuit 33. In the position shown, both coils are deenergized to permit the valve 12 to close.
- the flag portion 20 will move away from the coils 22 tuning the oscillator 24 and energizing the relay 28. At this time the switch blade 34 will be raised to close the circuit through the solenoid [4 so that both valves will be open and the furnace temperature will increase.
- the operating range of the instrument and the width of its neutral range, when only the valve 3 H is open, may be determined by design by the spacing of the coils 2i and 22 and the horizontal lengths of the flag portions l9 and 2!].
- are preferably supported on an arm 39 pivoted coaxially with the pointer 11.
- the coils 22 are similarly supported on an arm 39 and both arms may carry pointers 40 for movement over the scale 18 to indicate the positions of the arms.
- the instrument can be set to maintain the furnace temperature at any desired value by simultaneously moving the arms 38 and 39 so that the pointers 49 indicate the value at which furnace temperature will be maintained. Since the arms are independently movable, the neutral range can easily be adjusted by separating the pointers 90 or by moving them closer together. In this way the amount of permissible movement of the pointer 11 in the neutral range to hold the valve ll open and the valve 12 closed can readilybe adjusted. Thus for some installations a neutral range of 50- or more degrees may be desirable, while for others a'relatively narrow range comprising only a few degrees change may be required. By separating' the pointers or by bringing them closer together, the width of the neutral range can be made any desired value within the limits of ad ,iustment permitted by the lengths of the flag segments l9 and 20.
- a unit responsive to a condition to be controlled, a pointer moved by the unit in proportion to changes in the condition, a flag on the pointer having stepped portions spaced in a direction transverse to the path of movement of the pointer, a pair of reactance elements whose reactance is affected by proximity of the flag mounted adjacent the paths of movement of the stepped portionsrespectively, a pair of oscillator circuits connected to the reactance elements respectively to have their tuning and consequently their output currents controlled by proximity of the flag to the reactance elements, means mounting the reactance elements for individual adjustment parallel to the path of travel of the flag, and means controlled by the output currents of the oscillators to control the condition.
- a unit responsive to a condition to be controlled, a pivotally mounted pointer swung about its pivot by the unit in proportion to changes in the condition, a flag on the pointer having stepped portions spaced in a direction transverse to the path of movement of the pointer, a pair of individuallymovable arms pivoted coaxially with the pointer, reactance elements carried by the arms adjacent the paths of movement of the stepped portions respectively, oscillators connected to the reactance elements respectively to be tuned and detuned thereby as the flag portions recede from and approach the reactance elements, and control means connected to the oscillators to control the condition.
- a unit responsive to a condition to be controlled, a pivotally mounted pointer swung about its pivot by the unit in proportion to changes in the condition, a flag on the pointer having stepped portions spaced in a direction transverse to the path .of movement of the pointer, a pair of individually movable arms pivoted coaxially with the pointer, reactance'ele ments carried by the arms adjacent thepaths'of movement of the stepped portions respectively, oscillators connected to the reactance elements respectively to be tuned and detuned thereby as the flag portions recede from and approach the reactance elements, and control devices connected to the oscillators to be controlled by their output currents.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Control Of Combustion (AREA)
- Feedback Control In General (AREA)
Description
Feb. 6, 1951 F. A HANSEN ET AL CONDITION CONTROL SYSTEM WITH STEPPED RESPONSE Filed March 14, 1946 Patented Feb. 6, 1951 UNITED STATES PATENT OFFICE CONDITION CONTROL SYSTEM WITH STEPPED RESPONSE Application March 14, 1946, Serial No. 654,475
3 Claims.
1' This invention relates to control systems and more particularly to electrical systems for controlling a variable condition such as temperature, pressure, flow or the like.
'One of the objects of the invention is to provide a control system which will maintain a condition in a given control range and which will effect a control operation tending to return the condition to the range upon a departure therefrom.
Another object is to provide a control stein in which the control range can be easily and quickly adjusted throughout wide limits.
Still another object is to provide an electrical control system having high, low and neutral control positions and inv which the range of the neutral position can easily be adjusted.
The above and other objects and advantages of the invention will be more readily apparent from the following description when read in connection with-the accompanying drawing, in which the single figure is a diagrammatic view of a control system embodying the invention.
- The instrument, as shown, is adapted to control the temperature of a furnace 13, although any other condition such as pressure, flow or the like could equally well be controlled. The furnace I is heated by fuel burners supp led with fluid fuel such as gas through valves l i and l2co'ntrolled by solenoids l3 and I4. Temperature of the furnace is indicated by a thermocouple [5 connected to the coil Q5 of a galvanometer to produce a movement of the coil proportional to changes in furnace temperature. The galvanonieter includes a pointer I! connected to the coil to be moved thereby and swinging over an arcuate scale l8 to indicate the temperature of the furnace. The pointer I1 carries near its free end a stepped metal flag having stepped portions l9 and 20 which are offset both vertically and horizontally with respect to each other.
The position of the pointer is sensed by reactance elements shown as inductance coils 2! and 22 which are mounted respectively adjacent the paths of movement of the flag portions l9 and 20. The coils 2| may be connected to the input or tank circuit side of an oscillator indicated generally at 23 and which may be similar to the oscillator more particularly described and claimed in the patent to Cohen No. 2,228,163. The coils 22 may be similarly connected to an oscillator 24, both oscillators bein so arranged that when the flag is displaced from the coils the oscillator will be in tune, while when the flag is adjacent or between the coils, the oscillator will be detuned.
The oscillators may be powered by a common transformer 25 and may be connected through amplifiers 26 to relays 21 and 23, respectively. The amplifiers 26 are preferably connected to the respective oscillators as described in Cohen Patent No. 2,228,163 so that when the oscillator plate current increases, the amplifier will cut off and the amplifier will conduct when the oscillator is oscillated and its direct plate current is at a minimum.
The relay 2] controls a switch having a movable blade 29 which normally falls away from the relay to engage a contact 32 and which is raised into engagement with a contact 3| when the relay is energized. In the circuit shown the contact 32 is a dead contact, although it could, if desired, be connected to an indicator or the like. The switch blade 29 is connected to one side of a power input circuit 33 and the contact Si is connected through the winding l3 to the opposite side of the power input circuit. The relay coil 28 similarly controls a switch blade 34 which is connected to one side of the circuit 33 and which normally engages a dead contact 35. When the i coil 28 is energized it pushes the switch blade up to engage a contact 36 connected through the solenoid H! to the other side of the power circuit 33. In the position shown, both coils are deenergized to permit the valve 12 to close.
In operation of the apparatus as so far described, when the temperature in the furnace rises, the pointer I! will swing to the right to move the flag [9 between the coils 2!, the flag remaining between the coils 22. As the flag portion [9 enters the coils 2 I, it detunes the oscillator 23 to de-energize the relay 21 so that the switch blade 29 will drop to the position shown to deenergize the solenoid l3 and close the valve ll. At this time both valves are closed so that no heat is supplied to the furnace. As the furnace temperature falls, the flag portion l9 moves away from the coils 2! to tune the oscillator 23 and close the circuit to the solenoid l3 to open the valve ll. At this time only the valve II is open which may be the normal operating condition. If the temperature should continue to fall with only the valve II open, the flag portion 20 will move away from the coils 22 tuning the oscillator 24 and energizing the relay 28. At this time the switch blade 34 will be raised to close the circuit through the solenoid [4 so that both valves will be open and the furnace temperature will increase.
The operating range of the instrument and the width of its neutral range, when only the valve 3 H is open, may be determined by design by the spacing of the coils 2i and 22 and the horizontal lengths of the flag portions l9 and 2!]. To permit easy adjustment of the neutral range, the coils 2| are preferably supported on an arm 39 pivoted coaxially with the pointer 11. The coils 22 are similarly supported on an arm 39 and both arms may carry pointers 40 for movement over the scale 18 to indicate the positions of the arms.
With this construction the instrument can be set to maintain the furnace temperature at any desired value by simultaneously moving the arms 38 and 39 so that the pointers 49 indicate the value at which furnace temperature will be maintained. Since the arms are independently movable, the neutral range can easily be adjusted by separating the pointers 90 or by moving them closer together. In this way the amount of permissible movement of the pointer 11 in the neutral range to hold the valve ll open and the valve 12 closed can readilybe adjusted. Thus for some installations a neutral range of 50- or more degrees may be desirable, while for others a'relatively narrow range comprising only a few degrees change may be required. By separating' the pointers or by bringing them closer together, the width of the neutral range can be made any desired value within the limits of ad ,iustment permitted by the lengths of the flag segments l9 and 20.
While one embodiment of the invention has been shown and described in detail herein, it will be understood that it is illustrative only and is not intended to be taken as a definition of the scope of the invention, reference being had for this purpose to the appended claims.
What is claimed is:
1. In a control system, a unit responsive to a condition to be controlled, a pointer moved by the unit in proportion to changes in the condition, a flag on the pointer having stepped portions spaced in a direction transverse to the path of movement of the pointer, a pair of reactance elements whose reactance is affected by proximity of the flag mounted adjacent the paths of movement of the stepped portionsrespectively, a pair of oscillator circuits connected to the reactance elements respectively to have their tuning and consequently their output currents controlled by proximity of the flag to the reactance elements, means mounting the reactance elements for individual adjustment parallel to the path of travel of the flag, and means controlled by the output currents of the oscillators to control the condition.
2. In a control system, a unit responsive to a condition to be controlled, a pivotally mounted pointer swung about its pivot by the unit in proportion to changes in the condition, a flag on the pointer having stepped portions spaced in a direction transverse to the path of movement of the pointer, a pair of individuallymovable arms pivoted coaxially with the pointer, reactance elements carried by the arms adjacent the paths of movement of the stepped portions respectively, oscillators connected to the reactance elements respectively to be tuned and detuned thereby as the flag portions recede from and approach the reactance elements, and control means connected to the oscillators to control the condition.
3. In a control system, a unit responsive to a condition to be controlled, a pivotally mounted pointer swung about its pivot by the unit in proportion to changes in the condition, a flag on the pointer having stepped portions spaced in a direction transverse to the path .of movement of the pointer, a pair of individually movable arms pivoted coaxially with the pointer, reactance'ele ments carried by the arms adjacent thepaths'of movement of the stepped portions respectively, oscillators connected to the reactance elements respectively to be tuned and detuned thereby as the flag portions recede from and approach the reactance elements, and control devices connected to the oscillators to be controlled by their output currents.
FRED A. HANSEN. OLAF FRYXELL.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US654475A US2540728A (en) | 1946-03-14 | 1946-03-14 | Condition control system with stepped response |
GB4982/47A GB628643A (en) | 1946-03-14 | 1947-02-20 | Improvements in or relating to control system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US628643XA | 1946-03-14 | 1946-03-14 | |
US654475A US2540728A (en) | 1946-03-14 | 1946-03-14 | Condition control system with stepped response |
Publications (1)
Publication Number | Publication Date |
---|---|
US2540728A true US2540728A (en) | 1951-02-06 |
Family
ID=26742794
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US654475A Expired - Lifetime US2540728A (en) | 1946-03-14 | 1946-03-14 | Condition control system with stepped response |
Country Status (2)
Country | Link |
---|---|
US (1) | US2540728A (en) |
GB (1) | GB628643A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2706250A (en) * | 1952-03-06 | 1955-04-12 | Illinois Testing Laboratories | Circuit control apparatus |
US2761064A (en) * | 1951-06-13 | 1956-08-28 | Western Electric Co | Electric oscillator |
US2967278A (en) * | 1957-09-30 | 1961-01-03 | Internat Instr Inc | Inductive type sensing and control system |
US3028503A (en) * | 1958-11-18 | 1962-04-03 | Ian W Stevenson | Control devices for automatically controlling physical variables |
US3032692A (en) * | 1959-12-08 | 1962-05-01 | Internat Instr Inc | Polarity discriminating control meter |
US3164755A (en) * | 1961-05-31 | 1965-01-05 | Tyer & Co Ltd | Instrument for the sensing of temperature |
US3992655A (en) * | 1974-09-16 | 1976-11-16 | Dieterich Standard Corporation | Electronic meter signalling device |
US5076583A (en) * | 1990-08-21 | 1991-12-31 | Sportstech Industries (U.S. Tech) Inc. | Racket frame with circular cross section and variable thickness |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2894179A (en) * | 1955-09-14 | 1959-07-07 | Lewis Eng Co | Instrument relay |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1650889A (en) * | 1925-11-16 | 1927-11-29 | Texas Co | System of regulation |
US1838084A (en) * | 1926-09-11 | 1931-12-29 | Sperry Gyroscope Co Inc | Follow-up system |
US1841559A (en) * | 1930-02-06 | 1932-01-19 | Uehling Fritz Frederick | Automatic temperature control device |
FR750075A (en) * | 1932-04-27 | 1933-08-03 | Cie Forges Et Acieries Marine | Electric servo device controlled by members having a very low torque |
US1944988A (en) * | 1928-07-24 | 1934-01-30 | Gen Electric | Control system |
US2154260A (en) * | 1934-05-12 | 1939-04-11 | Westinghouse Electric & Mfg Co | Electronic metering system |
US2153986A (en) * | 1937-11-15 | 1939-04-11 | Bristol Company | Electronic control system for selfbalancing measuring instruments |
US2165510A (en) * | 1936-03-27 | 1939-07-11 | Bell Telephone Labor Inc | Electrical measuring, recording, and control system |
US2218502A (en) * | 1936-11-25 | 1940-10-22 | Illinois Testing Laboratories | Temperature controller |
US2295471A (en) * | 1942-09-08 | Control device | ||
US2411247A (en) * | 1942-01-07 | 1946-11-19 | Wheelco Instr Company | Electric oscillator and oscillator controlled relay circuit |
-
1946
- 1946-03-14 US US654475A patent/US2540728A/en not_active Expired - Lifetime
-
1947
- 1947-02-20 GB GB4982/47A patent/GB628643A/en not_active Expired
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2295471A (en) * | 1942-09-08 | Control device | ||
US1650889A (en) * | 1925-11-16 | 1927-11-29 | Texas Co | System of regulation |
US1838084A (en) * | 1926-09-11 | 1931-12-29 | Sperry Gyroscope Co Inc | Follow-up system |
US1944988A (en) * | 1928-07-24 | 1934-01-30 | Gen Electric | Control system |
US1841559A (en) * | 1930-02-06 | 1932-01-19 | Uehling Fritz Frederick | Automatic temperature control device |
FR750075A (en) * | 1932-04-27 | 1933-08-03 | Cie Forges Et Acieries Marine | Electric servo device controlled by members having a very low torque |
US2154260A (en) * | 1934-05-12 | 1939-04-11 | Westinghouse Electric & Mfg Co | Electronic metering system |
US2165510A (en) * | 1936-03-27 | 1939-07-11 | Bell Telephone Labor Inc | Electrical measuring, recording, and control system |
US2218502A (en) * | 1936-11-25 | 1940-10-22 | Illinois Testing Laboratories | Temperature controller |
US2153986A (en) * | 1937-11-15 | 1939-04-11 | Bristol Company | Electronic control system for selfbalancing measuring instruments |
US2411247A (en) * | 1942-01-07 | 1946-11-19 | Wheelco Instr Company | Electric oscillator and oscillator controlled relay circuit |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2761064A (en) * | 1951-06-13 | 1956-08-28 | Western Electric Co | Electric oscillator |
US2706250A (en) * | 1952-03-06 | 1955-04-12 | Illinois Testing Laboratories | Circuit control apparatus |
US2967278A (en) * | 1957-09-30 | 1961-01-03 | Internat Instr Inc | Inductive type sensing and control system |
US3028503A (en) * | 1958-11-18 | 1962-04-03 | Ian W Stevenson | Control devices for automatically controlling physical variables |
US3032692A (en) * | 1959-12-08 | 1962-05-01 | Internat Instr Inc | Polarity discriminating control meter |
US3164755A (en) * | 1961-05-31 | 1965-01-05 | Tyer & Co Ltd | Instrument for the sensing of temperature |
US3992655A (en) * | 1974-09-16 | 1976-11-16 | Dieterich Standard Corporation | Electronic meter signalling device |
US5076583A (en) * | 1990-08-21 | 1991-12-31 | Sportstech Industries (U.S. Tech) Inc. | Racket frame with circular cross section and variable thickness |
Also Published As
Publication number | Publication date |
---|---|
GB628643A (en) | 1949-09-01 |
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