US2758511A - Balanced capacitor integrator - Google Patents

Balanced capacitor integrator Download PDF

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US2758511A
US2758511A US221494A US22149451A US2758511A US 2758511 A US2758511 A US 2758511A US 221494 A US221494 A US 221494A US 22149451 A US22149451 A US 22149451A US 2758511 A US2758511 A US 2758511A
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condenser
circuit
charging
potential
contact
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William B Mclean
William L Whitson
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    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03KPULSE TECHNIQUE
    • H03K17/00Electronic switching or gating, i.e. not by contact-making and –breaking
    • H03K17/28Modifications for introducing a time delay before switching
    • H03K17/288Modifications for introducing a time delay before switching in tube switches
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S1/00Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Catching Or Destruction (AREA)

Description

Aug. 14, 1956 w. B. MCLEAN ETAL 2,758,511
BALANCED CAPACITOR INTEGRATOR Filed April 17; 1951 IIIIIIIIIE 3 Bone Rams: Chara/r INVENTORS WIN/19M a. MSLEAN B 4.4119114. VII/Mb fl.4im m (9/3 7 2,7585 ll Patented Aug. 14, 1956 2,758,5l1 BALANCED CAPACITOR INTEGRATOR William B. McLean, Inyokern, Calif., and William L. Whitson, Washington, D. C.
The present invention relates generally to electrical timing devices, and more particularly to a balanced capacitance electrical timing device especially adapted to controlling the release of bombs in a toss bombing attack.
A toss bombing attack is accomplished by the attacking plane approaching the target on a substantially level flight and then maneuvering into .a downward glide or dive course, the plane being directed for collision with the target, moving or stationary, until the attacking plane is within a desired range of the target. Whereupon, the pilot maneuvers so as to pull out of his downward glide or dive and into an upward course. During this latter maneuver, the pull-up operation, the bomb, or stick of bombs, or the like is released. The present timing device is particularly adapted to such operations for controlling the release of a bomb at the proper point on the pull-up arc to provide a hit on the target.
United States Patmt fifice 2 lision with the target if the plane were maintained on its collision course, and at that time the thyratron tube would become conductive or the trigger mechanism would be operated to release the bombs. However, the toss bombing attack is accomplished by the plane pulling out of the dive at some point before collision with the target but after traversing the timing fraction of the distance to collision. The present device is therefore provided with an acceleration responsive means, which operates in response to the pull-up acceleration at the start of the pull out maneuver as the plane course is reversed into a substantially upward course, to decrease the resistance in the second condensers charging circuit in accordance with this pull-up acceleration. Thus, the time required for the second condenser to obtain such a charge as would place thereacross a potential equal to that established on the first condenser is reduced in accordance with the magnitude of the pull-up accelera- Considering the present invention generally in its ap- I, v plication to bomb release control during a toss bombingv attack, a condenser is charged by a fixed potential source,
through a resistance during a predetermined fraction of the dive run of the toss bombing attack, and if this dive run is accomplished at a uniform velocity, the potential established across said condenser is a measure of the time required to traverse the entire distance to collision with the target. Upon the completion of the established fraction of the dive run, a second condenser is' charged from the same potential source through a resistance while the charge established on the first condenser is held thereon. Since the fraction of the above-described timing run with respect to the entire distance to collision with the target is known, the values of the second condenser and the resistance through which it is charged may be so chosen that the second condenser attains a potential difference thereacross equal to the potential across the first condenser in the remaining time required for collision with the tar et, if'the plane were to continue on its course at the same velocity until such collision occurred. Also included in this circuit is a trigger mechanism, such as a thyratron tube or the like, which operates to control a bomb release mechanism in response to the potentials of said condensers. potentials impressed on' the plate and cathode thereof are so chosen and the condensers above-mentioned are so connected to the control grid thereof that the tube is biased against conduction until the potential across the second condenser becomesequal to that across the first; whereupon, the tube becomes conductive from its cathode to its plate and operates a bomb release control mechanism in its plate circuit. Thus, if at a determined altitude on the dive run charging of the first condenser is initiated and continued during the predetermined fraction of the dive run on collision course with the target, and after traversing this fraction the first condenser is disconnected from its charging source and the second condenser is charged, the potential across the second 'condenserwould become equal to that across the first condenser upon col- In the case of a thyratron tube, the
' which releases the horn tion, and the thyratron tube becomes conductive to release the bombs at some point on the pull-up maneuver.
With the proper potentials impressed upon the plate and cathode of the thyratron tube, the proper values chosen for the several elements comprising the present circuit, and with the pull-up acceleration responsive mechanism providing the appropriate decrease in the second condensers charging resistance, the bombs are released at that point on the pull-aparc which obtains a hit on the target, provided the dive course of the plane is established for collision with the target.
It is, therefore, one object of the present invention to provide a bomb release control circuit for a toss bombing attack which releases the bomb at an appropriate point during the pull-up maneuver to obtain a hit on the target. Another object of the present invention is to provide a bomb release control circuit'f or a toss bombing attack atthe proper point during the pull-up maneuver to obtain a hit on the target, wherein the control is eflectuated by the cooperation of two buckingcondensers operating to control the action of a trigger mechanism. 7 I
Another object of the present invention is to provide a bomb release control circuit for a toss bombing attack which releases a bomb at a desired point on the pull-up maneuver to obtain a hit on the target, wherein the time of flight to collision with the target is represented by a potential across one condenser connected to bias a thyratron tube or the like against conduction, and the potential impressed across a second condenser, whose charging rate is afiected by the acceleration during the pull-up maneuver, is so applied to said first condenser and thyratron tube as to balance the potential established across the first condenser to permit the thyratron tube to become conductive at the desired point during the pull-up maneu-' ver, current flow through the plate circuit of the thyratron tube operating to release the bomb.
Still another object of the present invention is to provide a balanced capacitance timing circuit which operates substantially independently of the temperature, variations in the value of the operating voltage supply, and variations in the values'andcharacteristics of the elements comprising the circuit,.provided they are constant during .a particular operational run of the circuit.
A still, further object of thepresentinvention is to pro- ;vide abala'nced capacitance timing circuit wherein one condenser is charged to a reference potential through a charging circuit over a known timing interval, and a second condenser is charged to an equal potential through a second charging. circuit, the interval for charging said second condenser being related to the interval for charging said first condenser by a known ratio as established by the 3 resistance-capacitance values of the two condenser charging circuits.
Still another object of the present invention is to provide a balanced capacitance timing circuit wherein one condenser is charged to a reference potential over a known timing interval and a second condenser is charged during a measured interval, the interval for charging said second condenser being related to the interval for charging said first condenser in accordance with the ratio of potentials thus obtained across said condensers and the ratio of the resistance-capacitance values of the condenser charging circuits during the charging of the condensers.
Other objects and advantages of the present invention will become apparent to those skilled in the art from a consideration of the following detailed description thereof, made in conjunction with the accompanying drawing which is a wiring diagram of the present electrical timing circuit, illustrating an embodiment particularly adapted to control the release of bombs during a toss bombing attack.
Referring to the drawing, the embodiment there shown of the present timing circuit comprises a bomb release control tube 50, preferably of the gas filled or thyratron type, having the plate 51, the screen grid 52 connected to the cathode 54, and the control grid 53. The plate circuit of this tube comprises lead 21, the relay coil 23, lead 59, the switch arm 55 controlled by the relay coil 30a, the contact point 55a for said switch arm, lead 57, and a portion of lead 11 connected to the positive side of the voltage supply 10. The cathode 54 of this tube is also connected to the voltage supply through the variable tap connection 53, the potentiometer 40, and the lead 12. Thus, if the switch arm 55 is moved from its normally biased open position, as shown in the drawing, into engagement with its contact 55a, as is. accomplished by energization of the relay coil a, and if the control grid 53 of the tube 50 is biased to permit conduction through the thyratron tube for the potential difference existing between plate 51 and cathode 54, electron current flows from the cathode to the plate and through the plate circuit. Energization of relay coil 23, as results from current flow through the plate circuit, causes the switch arm 26 to move from its normally biased open position shown in the drawing into engagement with its contact 26a, thereby closing a bomb release circuit, not shown, which operates to release a bomb, or a stick of bombs, or the like upon the closure thereof.
' As previously indicated and as is apparent from the drawing, the bias on the control grid 53 of thyratron tube 50 is determined by the potentials across the condensers 24 and 25. When the switch arm 27 is in the position shown in the drawing, in engagement with its contact 27a, the condenser 24 is charged through its charging circuit comprising the voltage source 10, a portion of lead 11, lead 14, resistor 17, lead 1451, switch arm 19 when this arm is in engagement with its contact 1%, its normally biased position, lead 29, lead 22, condenser 24, lead 28, contact 27a, switch arm 27, and thence to ground. The potential thus impressed across the condenser 24 over a given time interval is a function of the R. C. value of this circuit. .However, it is to he noted that with the circuit in the condition as shown in the drawing, condenser 24 is shorted by means of leads 22, 20, and 29 and switch arm 31, shown in its normally biased position in engagement with its contact 31a, connected to ground, while the other side of condenser 24 is also connected to ground through lead 28, and switc arm 27 in engagement with contact 2701. However, upon the closure of switch 33 a current is applied to the relay coil 34, which operates to break switch arm 31 from engagement with its contact 31a and to bring it into engagement with its contact 31b, thereby breaking the ground connection across the condenser 24 and enabling the condenser to become charged through its charging circuit described above. After the lapse of a time interval, a potential is established across condenser 24 in accordance with the value of resistor 17, the value of the voltage source 10, and the capacitance of the condenser 24. Upon the subsequent closure of switch 35 relay coil 28a is energized, the flow of current therethrough being enabled by the closure of switch arm 31 to its contact 31b and its connection to ground, as effected by the operation of relay coil 34 described above. The energization of relay coil 28a causes the switch arm 27 to break from its contact 27a and to engage its contact 27b. This action traps the charge on condenser 24 and closes the charging circuit for condenser 25 comprising the voltage source It), leads 11 and 13, rheostat 15, lead 13a, switch arm 19 when in engagement with its contact 2%, lead 2%, lead 13, condenser 25, lead 36, switch arm 27 now in engagement with its contact 27b, and thence to ground. it is to be noted, however, that in the circuit condition shown in the drawing condenser 25 is shorted to ground, one side thereof being connected to ground through leads 1%, 20, and 29, contact 31a, and switch arm 31 connected to ground, and the other side also being connected to ground through lead 13a, switch arm 30 in engagement with its contact 3011, its normally biased position, lead 37, a portion of lead 29, contact 31a, and switch arm 31. Thus, in the nonoperating state of the circuit both sides of both condensers 24 and 25 are at ground potential. However, energization of relay coil 34 operates similarly on switch arm 30 as on switch arm 31, causing arm 30 to break from its contact 30a into open position to place condenser 25 in chargeable state as is done to condenser 24.
The energization of relay coil 28a affects switch arm 38 in the same manner as switch arm 27, causing it to move from its normally biased open position, as shown in the drawing, into engagementwith its contact 38a, enabling current to flow therethrough and through lead 39, relay coil 20a, and thence to ground. The resultant energization of coil 20a operates to move both switch arms 19 and 55 from their normally biased positions,
as shown in the drawing, so as to bring arm 19 into engagement with its contact 1% and arm 55 into engagement with itscontact55a, thus simultaneously operating to close the charging circuit for condenser 25 and the plate circuit of the thyratron 50, both described above. The condenser 25 charges at a rate as determined by the voltage source 10, the rheostat 15, and the capacitance of condenser 25. The charging of condenser 24 through its charging circuit and the trapping of the charge thereon by the breaking of switch 27, from engagement with its contact 27a, results in a negative potential on its grid connected plate and on the grid 53. As condenser 25 is charged through its charging circuit, with the switch arm 27 in engagement with its contact 27b, the increase in potential thereacross bucks the potential across condenser 24 and causes the reference point of the potential across the condenser 24 to become correspondingly more positive, thereby causing the control grid to become less negative or more positive in accordance therewith until such time as the potential on grid 53 attains such a value as to enable tube 50 to become conductive from its cathode 54- to its plate 51. Whereupon, the relay coil 23 in the plate circuit of tube 50 is energized to bring switch arm 26 into engagement with its contact 26a and hence close the bomb release circuit.
If, for example, the characteristics of tube 50 and the potential applied to its plate 51 and cathode 54 are so chosen that tube 50 becomes conductive when its control grid 53 is at ground potential, it is apparent that immediately upon the closure of switch 33, with switch arms 19, 27, and 55 in the positions as shown in the drawing and with switch arms 30 moved into open position and 31 moved into engagement with its contact 31b, the charging circuit for condenser 24 is closed and the control grid 53 is maintained at ground potential; but the tube 50 does not fire because its plate circuit is open, switch arm 55 being out of engagement with its contact 55a, and
the circuit may be readily modified to charge both condensers 24 and 25 through the same resistor, fixed or variable, but set to a determined value for a given operational run. By such a modification, the ratio of the timing interval, during which condenser 24 is charged to carry a reference potential thereacross, to the interval to be measured, during which condenser 25 is charged to obtain an equal potential thereacross, is equal to the ratio of the capacitance values of condenser 24 to condenser 25. Also, even when the present invention is intended to operate in response to acceleration as in the embodiment shown in the drawing, the circuit may be likewise modified to employ only one charging resistor, the rheostat 15; and resistor 17 and switch arm 19 may be eliminated. The full resistance value of rheostat 15 would then be employed in charging condenser 24 during the timing interval, and the condenser 25 would be charged through this rheostat by operation of switch arm 27 in the same manner as indicated in the abovedetailed description. Further, it is apparent that although here described in its application to toss bombing, the present invention is not limited to a downward to upward reverse acceleration but is applicable to reverse accelerations generally.
For many timing operations using the present circuit, it would not be necessary to actually provide for equal potentials across the two condensers; but the ratio of the timing interval to themeasured interval would, in general, be a function of the ratio of the potential obtained across condenser 24 to that obtained across condenser 25 and the ratio of the R. C. value of the charging circuit for condenser 24 to that of the charging circuit for condenser 25. Regardless of in which manner the circuit is employed, other trigger or voltage indicating means than the thyratron tube may be used, as may be considered suitable for the particular use and operation of the device.
Because of the balancing type operation of the present circuit, it is apparent that when the balanced potential method of operation is employed the variables which are normally difficult to control in an electrical timing device affect the voltage obtained across both condensers proportionately and are thus canceled out when the voltages are equated, provided there is no variation during an operational run or timing cycle. Variations in charging voltage except during a charging cycle do not affect the results obtained, and similarly variations in the values of resistances or capacitanccs, as may be caused by aging or cycling, are balanced out if the initial elements are matched, for ratios of the elements remain constant.
Other uses of the present invention, and other modifications thereof within the spirit and scope of the teachings herein set forth and as defined by the appended claims, will be apparent to those skilled in the art.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
What is claimed is:
1. A computing circuit for determining the proper instant for releasing a bomb from an aircraft performing a dive bombing attack compr sing a first capacitor, first 8 circuit means coupled to said first capacitor for charging said first capacitor at a known rate during a predeterminedv portion of said dive bombing attack toproduce a first voltage thereonwhich is proportional to the time required for a released bomb to reach said target, a second capacitor, second circuit means coupled to said second capacitor for charging said second capacitor to a second voltage, switch means coupling said first and second circuit means for causing said first circuit means to cease charging said first capacitor after said predetermined portion of said dive bombing attack has been made and for causing said second circuit means to cornmence charging said second capacitor upon the cessation of the charging of saidfirst capacitor whereby said second voltage has a portion thereof which has an instantaneous magnitude which is proportional to the distance traversed by the aircraft toward the target, acceleration responsive means coupled to said second circuit means for increasing the rate of charging of said second capacitor, said accel eration responsive means being responsive to the pull-up acceleration of said dive bombing aircraft when it departs from a collision course with said target whereby said second voltage has a portion thereof which is proportional to the upward velocity of said aircraft, means coupled to said first and second capacitors for producing a signal when said first and second voltages bear a predetermined relationship to each other which signifies the proper time for bomb release, and means coupled to said last mentioned means for releasing said bomb. I
2. A circuit for providing a signal at the proper instant for releasing a bomb from an aircraft performinga dive bombingattack, said circuit comprising: a first capacitor, afirst charging circuit coupled to said first capacitor and having a switch when closed for completing a circuit to cause said first capacitor to commence; charging through said first charging circuit, a second capacitor, an acceleration responsive slide Wire variable resistor, a sec' and charging circuit connectedv with said acceleration slide wire variable resistor for charging said second capacitor through said variable resistor, switch means operatively connected into said first and second charging circuits for substantially simultaneously causing said second capacitor to commence charging through said second charging circuit and for causing said first charging circuit to open and cease the charging of said first capacitor, and means responsive to the voltages on said first and second capacitors for producing a signal when the voltages on said first and second capacitors bear a predetermined relationship to each other.
References Cited in the file of this patent UNITED STATES PATENTS Kurland et al. Nov. 3, 1953
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2898809A (en) * 1955-09-15 1959-08-11 Jr John A Ryan Low altitude bombing system and apparatus
US2910916A (en) * 1956-08-30 1959-11-03 Mergenthaler Linotype Gmbh Toss bombing apparatus
US2951203A (en) * 1955-08-31 1960-08-30 Reuel Q Tillman Voltage measuring device
US2988960A (en) * 1956-07-16 1961-06-20 Gen Motors Corp Bombing navigational computer
US2995984A (en) * 1956-07-16 1961-08-15 Gen Motors Corp Multiple solution bombing computer
US3091993A (en) * 1957-07-03 1963-06-04 Paul L Brink Dive-toss air-to-ground delivery system
US3183814A (en) * 1963-03-27 1965-05-18 Keystone Camera Company Inc Camera exposure control
DE1196099B (en) * 1959-03-23 1965-07-01 Eltra Corp Bomb trigger for dive planes

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1997208A (en) * 1934-01-20 1935-04-09 Bell Telephone Labor Inc Electrical counting system
US2090224A (en) * 1936-02-20 1937-08-17 Noble Daniel Earl Control apparatus
US2177569A (en) * 1935-01-02 1939-10-24 Jorgensen Mathias Oluf Method and means for measuring voltages
US2236157A (en) * 1939-06-30 1941-03-25 Bell Telephone Labor Inc Contact chatter measuring device
US2459632A (en) * 1947-12-26 1949-01-18 Rca Corp Comparison control system
US2478670A (en) * 1943-10-09 1949-08-09 Bell Telephone Labor Inc Automatic register for echo pulses from a plurality of objects
US2545257A (en) * 1948-04-26 1951-03-13 Douglas Aircraft Co Inc Electronic control device
US2658141A (en) * 1951-01-20 1953-11-03 Jerome J Kurland Time delay circuits

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1997208A (en) * 1934-01-20 1935-04-09 Bell Telephone Labor Inc Electrical counting system
US2177569A (en) * 1935-01-02 1939-10-24 Jorgensen Mathias Oluf Method and means for measuring voltages
US2090224A (en) * 1936-02-20 1937-08-17 Noble Daniel Earl Control apparatus
US2236157A (en) * 1939-06-30 1941-03-25 Bell Telephone Labor Inc Contact chatter measuring device
US2478670A (en) * 1943-10-09 1949-08-09 Bell Telephone Labor Inc Automatic register for echo pulses from a plurality of objects
US2459632A (en) * 1947-12-26 1949-01-18 Rca Corp Comparison control system
US2545257A (en) * 1948-04-26 1951-03-13 Douglas Aircraft Co Inc Electronic control device
US2658141A (en) * 1951-01-20 1953-11-03 Jerome J Kurland Time delay circuits

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2951203A (en) * 1955-08-31 1960-08-30 Reuel Q Tillman Voltage measuring device
US2898809A (en) * 1955-09-15 1959-08-11 Jr John A Ryan Low altitude bombing system and apparatus
US2988960A (en) * 1956-07-16 1961-06-20 Gen Motors Corp Bombing navigational computer
US2995984A (en) * 1956-07-16 1961-08-15 Gen Motors Corp Multiple solution bombing computer
US2910916A (en) * 1956-08-30 1959-11-03 Mergenthaler Linotype Gmbh Toss bombing apparatus
US3091993A (en) * 1957-07-03 1963-06-04 Paul L Brink Dive-toss air-to-ground delivery system
DE1196099B (en) * 1959-03-23 1965-07-01 Eltra Corp Bomb trigger for dive planes
US3183814A (en) * 1963-03-27 1965-05-18 Keystone Camera Company Inc Camera exposure control

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