US1315539A - carson - Google Patents
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- US1315539A US1315539A US1315539DA US1315539A US 1315539 A US1315539 A US 1315539A US 1315539D A US1315539D A US 1315539DA US 1315539 A US1315539 A US 1315539A
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- 230000001939 inductive effect Effects 0.000 description 18
- 230000000875 corresponding Effects 0.000 description 12
- 230000000694 effects Effects 0.000 description 6
- 230000004048 modification Effects 0.000 description 6
- 238000006011 modification reaction Methods 0.000 description 6
- 230000002459 sustained Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 230000011664 signaling Effects 0.000 description 4
- 241001112285 Berta Species 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000001419 dependent Effects 0.000 description 2
- 238000002407 reforming Methods 0.000 description 2
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- H—ELECTRICITY
- H03—ELECTRONIC CIRCUITRY
- H03K—PULSE TECHNIQUE
- H03K3/00—Circuits for generating electric pulses; Monostable, bistable or multistable circuits
- H03K3/02—Generators characterised by the type of circuit or by the means used for producing pulses
- H03K3/26—Generators characterised by the type of circuit or by the means used for producing pulses by the use, as active elements, of bipolar transistors with internal or external positive feedback
- H03K3/30—Generators characterised by the type of circuit or by the means used for producing pulses by the use, as active elements, of bipolar transistors with internal or external positive feedback using a transformer for feedback, e.g. blocking oscillator
Definitions
- transmitting electrical energy and is especially applicable to signaling systems in which it is desired to correct the wave form of signaling impulses which has been destroyed by the distorting effect of the transmission line.
- the transmitting voltage at the sending end mav be represented by a curve of rectangular square topped form while the wave received atv the distant end is a very flattened curve which requires a relatively long time to build up to its steady value.
- the transmitting voltage at the sending end mav be represented by a curve of rectangular square topped form while the wave received atv the distant end is a very flattened curve which requires a relatively long time to build up to its steady value.
- FIG. 1 illustrates diagrammatically one embodiment thereof
- Fig. 2 is a detail of the amplifier circuits represented by the rectangles in Figs. 1 and 5;
- Fig. 3 is a set of curves representing a typical arrival curve and its derivatives;
- Fig. 4 is a curve indicating the form of arrival curve which may be derived by the employment of this invention and
- Fig. 5 illustrates a modification of the arrangement shown in Fig. 1.
- the invention includes an arrangement embodying correcting networks per 86 and amplifiers, preferably of the thermionic type, which may be arranged to introduce no distortion of their own.
- the amplifiers in the present case, perform. the very important function of separating the different sections of correcting network so-that one does not react upon itsvneighbor and the value of the elements in the networks may,
- the secondary of transformer 13 is to all intents and purposes open circuited, and the voltage developed across its terminals unaffected by the presence of the amplifiers. Under such conditions it may be shown that the voltage developed across the terminals of either primary or secondary of the transformer 13 approximates the first derivative of the arrival curve of the cable itself, provided the inductance of the primary is relatively small, this first derivative being of the form illustrated in age impressedin the input circuits of amtional to the first derivative of the arrlval curve itself.
- the input circuit of amplifier A is connected by circuit-17 to'the-high side ofautocircuit of amplifier A retain the arrangement as shown since a substantial voltage step u is, obtained by the inductive action of t e autotransformer.
- This is particularly advantageous because the inductance in the output circuit of amplifier A should be very small compared with the internal resistance of the tube if the voltage drop across said inductance is to closely approximate the second derivative of the arrival-curve.
- the system shown may be extended to provide derivatives of higher orders than the fourth by adding additional derived circuits.
- the number of derived circuits required will depend upon, and increase with, the distortion intransformer 16 whose low side is connected in series with the output circuit of amplifier (1 With this arrangement.
- the voltage drop across the input circuit of amplifier'A is substantially the second derivative of the arrival curve since the voltage impressed on the input circuit of amplifier a is the first derivative thereof. Consequently the voltage drop across resistance r is proportional to the second derivative of the arrival curve and its magnitude is controllable by either adjusting the amplifier A or adjusting the value of the resistance T
- the autotransformer may be replaced by an inductance coil if desired; it is practically preferable to troduced by the line and the desired speed of signaling.
- the branch circuit 21 leading from the transformer 13 to the amplifier b with its associated apparatus supplies this voltage.
- Its output circuit is connected to a distortion network comprising the resistance 2-2 and'the capacity 23 in parallel. The effect of these is to convert the wave form of the voltage existing across the terminals of trans- As already indicated the amplifier I).
- the amplifiers A, A, like A, are each connected to a resistance (r and r respectively) in the circuit 11-12.
- the aggregate effect of the voltages across resistances r, r and r will then be to add a voltage to those across resistances r to r, substantially like that indicated by curve 1 in Fig. 5, which when combined with voltages having wave forms corresponding'to the several derivatives as above described will give the desired wave form for recording.
- the results obtained by the system are dependent upon proper relations among the constants of the apparatus, as will be readil understood, and these must be chosen with ue regard to the wave form to be received and the wave form it is deslred to produce.
- the amplifying devices have been indicated merely by rectangles in Fig. 1, Fig. 2, however, lllustrates the circuit" represented by the :rectangle in each instance. It comprises thewell known form of thermionic amplifier 26 having a high resistance 27 connected across its input circuit and acondenser 28 in series. It will be observed that the capacity 28 and the resistance 27 will, in practice, be metallicallyconnected with the distortion networks with Which the amplifiers are associated but they do not constitute any part thereof and inorder'that they may not interfere with the operation of the netpreceding circuit.
- Fig. 1 may be adjusted to give practically any desired form of voltage or current in circuit 11-12 by changing the relative valuesof the difierent components, of the voltage drops across the resistances in said circuit. This may be, done partially by adjusting the amplifiers A to A to give varying values to the components transmitted through them respectively.
- the modification shown in Fig. 5 differs from that shown in Fig. 1 in that the circuits for obtaining the successive deriva tives are connected in series instead of in parallel and a series arrangement for the integral branch of the circuit is also used in place of the parallel arrangement of Fig.
- the current applied to the resistance r in the circuit 11-12 is a combination of the first, second,' third and fourth derivatives of the arrival current.
- the arrangement is simpler than that shown in'Fig. 1 and requires fewer amplifiers but it does not have the flexibility of the more elaborate circuit.
- a wave-form correcting device means for producmg from the arrival current separate currents having wave forms corresponding substantially to the arrival current itself and one or more of its derivatives respectively, a single .circuit for receiving the several currents so produced, and
- a Wave-form correcting device means for producing from-the arrival current separate currents having wave forms corresponding substantially to the arrival current itself and one or more of .its derivatives respectively, means for amplifying separately thecurrents so produced, and connections for superlmposing sald amplified currents upon a single output circuit in desired proportions.
- a wave-form correctlng device means for producing fromthe arrival current a plurality of currents having wave forms of varying. degrees of abruptness and duration, separate circuits into which the several currents are respectively introduced, means in each separate circuit for amplifying the current therein, and means for superimposing the separate amplified currents upon a single outputcircuit.
- the method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality varying degrees of abruptness and duration, separating the several currents into distinct circuits, and applying the separate currents to a single output circuit in desired proportions.
- he method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality of currents having wave forms of of currents having wave forms ofvarying degrees of abruptness and duration separating the several currents into 'dlStlIlCt circuits, amplifying the currents separately and applying the separate currents to a single output circuit in desired proportions.
- the method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality of separate currents corresponding substantially in wave form to the successive derivatives of the arrival current, and combining in a single output circuit the currents so produced with a current whose wave form corresponds substantially with the arrival current itself.
- the method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality of currents of varying wave forms, separating each of the currents from the others to prevent reaction of one upon another, amplifying the produced currents separately to desired strength, and superimposing the separate currents in a single output circuit in a proportion to give the desired resulting wave form.
- an inductive device in which t e arriving impulses are received, parallel circuits connected to said inductive device one of which is provided with means for producing a current having awave form approximatin the wave form of the arrival current, an another of which is provided with means for producing currents having wave forms corresponding substantially to derivatives of said arrival current, and means forimposing the currents in said parallel circuits upon a single output circuit in desired proportions.
- an inductive device in which the arriving impulses are received, parallel circuits connected to said inductive device, means located in certain of said parallel circuits for producing in them separately, current impulses of different slopes and duration but all more sustained than the impulses taken from the inductive device, and means in the other parallel circuits for producin in them separately current impulses of different slopes and duration but all more abrupt than the impulses taken from the inductive device, and means for imposing currents from the parallel'circuits and said inductive device upon a single output circuit in desired proportions.
Description
J. R. CARSON.
DISTORTION CORRECTING CIRCUIT.
APPLICATION man JULY 3.19 s.
Patented Sept. 9, 1919.
3 SHEETSSHEET 1.
IN VEN TOR.
A TTORNEY J. R. CARSGN.
DISTORTION CORRECTING CIRCUIT.
APPLICATION FILED JULY 3.!913.
mmmww Patentedsept. 9,1919.
3 SHEETS-SHEET 2.
IN V EN TOR.
@[MWRWMW BY Z 5 A TTORNE Y J. R. CARSON. DISTORTION CORRECTING CIRCUIT.-
APPLICATION FILED JULY 3.191s.
1,1 11; PatentedSept. 9,1919
3 SHEETS-SHEET s.
ATTORNEY UNITED STATES PATENT OFFICE.
JOHN R. CARSON, OF- NEW YORK, N. Y., ASSIGNOR TO AMERICAN TELEPHONE AND TELEGRAPH COMPANY, A CORPORATION OF NEW YORK.
DISTOETION OORRECTING CIRCUIT.
. transmitting electrical energy and is especially applicable to signaling systems in which it is desired to correct the wave form of signaling impulses which has been destroyed by the distorting effect of the transmission line. lln ocean cables, for instance, the transmitting voltage at the sending end mav be represented by a curve of rectangular square topped form while the wave received atv the distant end is a very flattened curve which requires a relatively long time to build up to its steady value. For receiving purposes it is important to have an arrival curve whose wave form approximates that of the voltage impressed on the sending end. It is the purpose of the present invention to provide "a distortion correcting network capable of reforming the arrival curve in cases of the kind above indicated. The invention will be more fully described in connection with the accompanying drawings in which Figure 1 illustrates diagrammatically one embodiment thereof; Fig. 2 is a detail of the amplifier circuits represented by the rectangles in Figs. 1 and 5;. Fig. 3 is a set of curves representing a typical arrival curve and its derivatives; Fig. 4 is a curve indicating the form of arrival curve which may be derived by the employment of this invention and Fig. 5 illustrates a modification of the arrangement shown in Fig. 1.
The invention, includes an arrangement embodying correcting networks per 86 and amplifiers, preferably of the thermionic type, which may be arranged to introduce no distortion of their own. The amplifiers, in the present case, perform. the very important function of separating the different sections of correcting network so-that one does not react upon itsvneighbor and the value of the elements in the networks may,
therefore, be readily calculated to give the desired result without having to estimate I the modifying efiect of one network upon another. n the process of distortion correction is'attended by diminution in the strength of the received signal or when it is desired to increase the intensity thereof Specification of LcttcraPatent. Patented Sept, 9, 1919, Application filed July a, me. Berta! no. am.
cause of its slow rate 0 building up. If a current of this form flows through an inductive device such as the windings of a transformer or a. plain inductance coil, the voltage developed in said device will be the first derivative of the arrival current which wlll have a wave form approximately as indicated at 2 in Fig. 3,-the derivative representing the time rate of change of the arrival curve. Similarly if a current of the form of derivative 2 flow through an inductance coil the voltage across the terminals of said coil will be the second derivative of the arrival current which has a wave form indicated at 3* in Fig. 3. Continuing by the same process successive derivatives may be obtained, the third and fourth being indicated at 4 and 5 respectively in Fig. 3. It Will be observed that the derivatives have a sharper and sharper rise in value which is one of the" characteristics essential for good recording. 0n the other hand the curves of the successive derivatives fall ofi' more and more rapidly asindicated in the drawing and the best current for receiving purposes should have not only a sharp rise but a sustained tail. It will be understood that the successive derivatives do not normally all have the same maximum value as shown but are so indicated merely to compare their characteristics conveniently. It
1s possible, however, by the use of amplifiers to give any particular derivative any desired value and it will be obvious from a consideration of the curves shown in Fig. 3
that by giving the various derivatives the proper value and combining them in a sinlot A curve 2 of Fig. 5. Consequently the voltnecesslty of a metallic connection between K the line and said amplifiers. Owin to the fact that the input circuits of amplifiers of the vacuum tube type are of substantially.
infinite impedance, the secondary of transformer 13 is to all intents and purposes open circuited, and the voltage developed across its terminals unaffected by the presence of the amplifiers. Under such conditions it may be shown that the voltage developed across the terminals of either primary or secondary of the transformer 13 approximates the first derivative of the arrival curve of the cable itself, provided the inductance of the primary is relatively small, this first derivative being of the form illustrated in age impressedin the input circuits of amtional to the first derivative of the arrlval curve itself.
Across the circuit 11, ,12 is connected a 5 series of resistances 1' 1", 1' 1', '1", 0", and
. voltage drop across resistance 1" is similarly proportional to said first derivative.
The input circuit of amplifier A is connected by circuit-17 to'the-high side ofautocircuit of amplifier A retain the arrangement as shown since a substantial voltage step u is, obtained by the inductive action of t e autotransformer. This is particularly advantageous because the inductance in the output circuit of amplifier A should be very small compared with the internal resistance of the tube if the voltage drop across said inductance is to closely approximate the second derivative of the arrival-curve. T
Connected in parallel with the input circuit of amplifier A is that of amplifier a the low side of autotransformer 18. Across the .highside of said transformer is connected the input circuit of am lifier A throughcircuit 19; consequently it will be readily seen in the light of the foregoing explanation that the voltage dro across resistance 1' is proportional to t e third derivative of the arrival curve.
Connected in parallel with the in ut circuit of amplifier A is that of amp ifier a. in the output circuit of which is connected the low side of autotransformer 20, to the high side of which is connected the input Consequently the voltage drop across resistance r is proportional to the fourth derivative of the arrival curve. plifiers a, A and b is substantially propor- The resultant voltage drop across resistances 7*, 1' 1' and 1' is thus made sip of the sum'pf individual voltage" drops whose respectlve waveforms are those of the second, fourth, thlrd and first derivatives ofthe arrival curve in predeterminate readily adj ustable proportion.
It is obvious that the system shown may be extended to provide derivatives of higher orders than the fourth by adding additional derived circuits. In practice the number of derived circuits required will depend upon, and increase with, the distortion intransformer 16 whose low side is connected in series with the output circuit of amplifier (1 With this arrangement. the voltage drop across the input circuit of amplifier'A is substantially the second derivative of the arrival curve since the voltage impressed on the input circuit of amplifier a is the first derivative thereof. Consequently the voltage drop across resistance r is proportional to the second derivative of the arrival curve and its magnitude is controllable by either adjusting the amplifier A or adjusting the value of the resistance T The autotransformer may be replaced by an inductance coil if desired; it is practically preferable to troduced by the line and the desired speed of signaling.
Without addition of a voltage correspondin to the arrival curve itself or a substantia equivalent thereof, the combination of the derivatives 'will give a wave which is not sufficiently sustained. This will be obvious from a consideration of the curves shown in Fig. 3. The branch circuit 21 leading from the transformer 13 to the amplifier b with its associated apparatus supplies this voltage. has a voltagecorresponding approximately to the first derivative applied to its input circuit. Its output circuit is connected to a distortion network comprising the resistance 2-2 and'the capacity 23 in parallel. The effect of these is to convert the wave form of the voltage existing across the terminals of trans- As already indicated the amplifier I).
'in the output circuit of whichis connected as h former 13 into a voltage across said parallel "elements approximating the integral of this same as the arrival current itself. This voltage is impressed on the input circuit of an amplifier A in whose output circuit is connected a resistance r. Theoretically ne section of such a network could be designed to provide a voltage drop across resistance r of practically the form desired but a more convenient and exact way of securing the desired result is to provide successive stages of a network as indicated on the drawing, applying the output from the successive stages to separate resistances in circuit -11-12. Thus there are shown in addition, amplifiers b and b feeding networks 24 and 25 respectively, which latter feed the input circuits of amplifiers A and A respectively. The amplifiers A, A, like A, are each connected to a resistance (r and r respectively) in the circuit 11-12. The aggregate effect of the voltages across resistances r, r and r will then be to add a voltage to those across resistances r to r, substantially like that indicated by curve 1 in Fig. 5, which when combined with voltages having wave forms corresponding'to the several derivatives as above described will give the desired wave form for recording. The results obtained by the system are dependent upon proper relations among the constants of the apparatus, as will be readil understood, and these must be chosen with ue regard to the wave form to be received and the wave form it is deslred to produce. In order that the output from the amphfiel's A to A inclusive, may affect the en'- cuit 11--12 in just the proportions represented by the values assigned to the reslstances r to 1" inclusive, it is important that the circuit represented 'by 11-12 be of high till impedance. A long transmission line of high impedance would substantially "satlsfy the requirements. The result may be perfectly attained, however, if the circuit 1-1--12 is connected to the input side of a thermionic amplifier (not shown) since no appreciable current will then flow in circuit and the current emanating from one of the amplifiers A -A cannot affect the potential drop across the resistances connected to the other amplifiers.
For the sake of simplicity the amplifying devices have been indicated merely by rectangles in Fig. 1, Fig. 2, however, lllustrates the circuit" represented by the :rectangle in each instance. It comprises thewell known form of thermionic amplifier 26 having a high resistance 27 connected across its input circuit and acondenser 28 in series. It will be observed that the capacity 28 and the resistance 27 will, in practice, be metallicallyconnected with the distortion networks with Which the amplifiers are associated but they do not constitute any part thereof and inorder'that they may not interfere with the operation of the netpreceding circuit.
be large, especially in the circuits dealing.
with t e arrival current or its lower derivatives, in order not to shorten the time period of the applied voltages in these components of the signaling current.
In operation the system shown in Fig. 1 may be adjusted to give practically any desired form of voltage or current in circuit 11-12 by changing the relative valuesof the difierent components, of the voltage drops across the resistances in said circuit. This may be, done partially by adjusting the amplifiers A to A to give varying values to the components transmitted through them respectively. A very simple method of adjusting the wave form, however, is aiforded by the resistances 1' to 1" since upon the value of any one of these depends the amount of the corresponding voltage component which is impressed 11-12L It is to be observed that the amplifiers in the circuits shown serve not only to compensate for the loss in amplitude due to the correcting networks and the attenuation in the line 10, but they separate each of the correcting networks from all of the others and this Without disturbing its modifying efl'ect upon the Wave form. This is by reason of the fact that the thermionic amplifier is essentially a one-Way device which consumes no appreciable energy in its input circuit. This makes it possible to calculate and adjust the. form of the network for giving any one'of the various components as above described without the complications introduced when one network reacts upon its neighbor.
The modification shown in Fig. 5 differs from that shown in Fig. 1 in that the circuits for obtaining the successive deriva tives are connected in series instead of in parallel and a series arrangement for the integral branch of the circuit is also used in place of the parallel arrangement of Fig.
upon the line 18' and 20' each includes a resistance 26 inseries with the inductance. The effect of this resistance is to preserve in the succeeding circuit the component introduced by the The result is that the current applied to the resistance r in the circuit 11-12 is a combination of the first, second,' third and fourth derivatives of the arrival current.
The arrangement is simpler than that shown in'Fig. 1 and requires fewer amplifiers but it does not have the flexibility of the more elaborate circuit.
The invention is not' to be regarded as limited to the particular forms herein illustrated and described as it is obvious that various modifications may be made without 1. In this case the distortion networks 16,
. departing from the spirit of the invention as 2. In a wave-form correcting device, means for producmg from the arrival current separate currents having wave forms corresponding substantially to the arrival current itself and one or more of its derivatives respectively, a single .circuit for receiving the several currents so produced, and
, means for determining the relative values of said currents applied to said circuit.
3. In a Wave-form correcting device, means for producing from-the arrival current separate currents having wave forms corresponding substantially to the arrival current itself and one or more of .its derivatives respectively, means for amplifying separately thecurrents so produced, and connections for superlmposing sald amplified currents upon a single output circuit in desired proportions.
a. In a wave-form. correcting device,
means for producing from the arrival current a plurality of currents having wave forms 0 varying degrees of abruptness and 1 duration, separate circuits into which the .several currents are respectlvely introduced, a single outpu t c1rcu1t, and means for 1mposing the several separatecurrents upon the output circuit in desired proportions.
5.. In, a wave-form correctlng device, means for producing fromthe arrival current a plurality of currents having wave forms of varying. degrees of abruptness and duration, separate circuits into which the several currents are respectively introduced, means in each separate circuit for amplifying the current therein, and means for superimposing the separate amplified currents upon a single outputcircuit.
6. The method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality varying degrees of abruptness and duration, separating the several currents into distinct circuits, and applying the separate currents to a single output circuit in desired proportions.
7. he method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality of currents having wave forms of of currents having wave forms ofvarying degrees of abruptness and duration separating the several currents into 'dlStlIlCt circuits, amplifying the currents separately and applying the separate currents to a single output circuit in desired proportions.
8. The method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality of separate currents corresponding substantially in wave form to the successive derivatives of the arrival current, and combining in a single output circuit the currents so produced with a current whose wave form corresponds substantially with the arrival current itself.
9. The method of correcting the wave form of current impulses which consists in producing from the arrival current a plurality of currents of varying wave forms, separating each of the currents from the others to prevent reaction of one upon another, amplifying the produced currents separately to desired strength, and superimposing the separate currents in a single output circuit in a proportion to give the desired resulting wave form.
'10. In a signal receivin circuit, an inductive device in which t e arriving impulses are received, parallel circuits connected to said inductive device one of which is provided with means for producing a current having awave form approximatin the wave form of the arrival current, an another of which is provided with means for producing currents having wave forms corresponding substantially to derivatives of said arrival current, and means forimposing the currents in said parallel circuits upon a single output circuit in desired proportions.
'11. In a signal receiving circuit, an inductive device in which the arriving impulses are received, parallel circuits connected to said inductive device, means located in certain of said parallel circuits for producing in them separately, current impulses of different slopes and duration but all more sustained than the impulses taken from the inductive device, and means in the other parallel circuits for producin in them separately current impulses of different slopes and duration but all more abrupt than the impulses taken from the inductive device, and means for imposing currents from the parallel'circuits and said inductive device upon a single output circuit in desired proportions.
In testimony whereof, I have signed my name to this specification this 2nd day of July, 1918.
JOHN R. CARSON.
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US1315539A true US1315539A (en) | 1919-09-09 |
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US2446567A (en) * | 1941-12-30 | 1948-08-10 | Sperry Corp | Alternating current rate circuits |
US2462095A (en) * | 1941-08-19 | 1949-02-22 | Sperry Corp | Rate circuits |
US2472611A (en) * | 1945-06-02 | 1949-06-07 | Bell Telephone Labor Inc | Motor control circuit |
US2494036A (en) * | 1947-09-20 | 1950-01-10 | Bell Telephone Labor Inc | Differential analyzer |
US2499413A (en) * | 1944-05-17 | 1950-03-07 | Sperry Corp | Pulse generator |
US2525496A (en) * | 1946-09-28 | 1950-10-10 | Westinghouse Electric Corp | Analyzer |
US2533587A (en) * | 1944-09-11 | 1950-12-12 | Reconstruction Finance Corp | Controller |
US2577506A (en) * | 1945-07-09 | 1951-12-04 | Logan M Belleville | Amplifier |
US2611126A (en) * | 1944-12-29 | 1952-09-16 | Jack H Irving | Radio object locating system having a hyperbolic sweep |
US2613351A (en) * | 1948-05-18 | 1952-10-07 | Sperry Corp | Radio navigation device |
US2621292A (en) * | 1947-02-11 | 1952-12-09 | Emi Ltd | Electrical integrating circuit arrangement |
US2654882A (en) * | 1945-10-15 | 1953-10-06 | Honeywell Regulator Co | Aircraft radio apparatus |
US2678388A (en) * | 1950-08-14 | 1954-05-11 | Hazeltine Research Inc | Signal-translating system for television receivers |
US2678389A (en) * | 1950-08-14 | 1954-05-11 | Hazeltine Research Inc | Signal-translating system for television receivers |
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US2689345A (en) * | 1949-06-25 | 1954-09-14 | Int Standard Electric Corp | Automatic approach control |
US2692333A (en) * | 1951-08-02 | 1954-10-19 | Rca Corp | Wave shaping circuit |
US2697168A (en) * | 1946-02-20 | 1954-12-14 | Carl P Spaulding | Sweep circuit |
US2703203A (en) * | 1946-02-21 | 1955-03-01 | Amasa S Bishop | Computer |
US2718638A (en) * | 1950-01-20 | 1955-09-20 | Itt | Signal correlation radio receiver |
US2727988A (en) * | 1949-08-08 | 1955-12-20 | Nat Res Dev | Electrical signal detecting and amplifying systems |
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US2836894A (en) * | 1954-04-19 | 1958-06-03 | H A Wagner Company | Optical tracking recording system |
US2856525A (en) * | 1954-07-09 | 1958-10-14 | Underwood Corp | Pulse shaper |
US2863999A (en) * | 1953-04-21 | 1958-12-09 | Rca Corp | Wave shaper |
US2867752A (en) * | 1954-08-11 | 1959-01-06 | Baird Atomic Inc | Pulse forming networks |
US2873067A (en) * | 1954-02-26 | 1959-02-10 | Sperry Rand Corp | Fuze setting order computer |
US2907878A (en) * | 1955-12-12 | 1959-10-06 | Research Corp | Electronic interpolator |
DE1108346B (en) * | 1956-10-25 | 1961-06-08 | Telefunken Patent | Circuit arrangement for equalizing the frequency-dependent amplitude response of a four-pole transmission for signals of a wide frequency band |
US3030502A (en) * | 1947-03-14 | 1962-04-17 | Otto H Schmitt | Automatic radio spectrum monitor |
US3038069A (en) * | 1949-06-24 | 1962-06-05 | Melpar Inc | Spectrum analyzers |
US3040988A (en) * | 1953-07-17 | 1962-06-26 | Emi Ltd | Apparatus for evaluating the rate of change of a variable |
US3073524A (en) * | 1959-05-25 | 1963-01-15 | North American Aviation Inc | Compensator for system of plural degrees of freedom |
US3081457A (en) * | 1949-03-03 | 1963-03-12 | Int Standard Electric Corp | Decade method of noise reduction |
US3153207A (en) * | 1961-10-31 | 1964-10-13 | Bell Telephone Labor Inc | Means for improving the quality of received television images |
US3162756A (en) * | 1959-01-19 | 1964-12-22 | Socony Mobil Oil Co Inc | Seismic frequency band restoration |
US3178595A (en) * | 1962-10-15 | 1965-04-13 | Bunker Ramo | Pulse peak detector circuit |
US3181075A (en) * | 1962-08-27 | 1965-04-27 | Klaas Edward Charles | Signal reproducing system |
US3231819A (en) * | 1961-09-07 | 1966-01-25 | Bell Telephone Labor Inc | Intermodulation distortion correction of angle modulated transmission system by use of nonlinear cancellation circuit |
US3450840A (en) * | 1965-11-19 | 1969-06-17 | Ibm | Multiplex data transmission system using orthogonal transmission waveforms |
US3492606A (en) * | 1966-07-14 | 1970-01-27 | Bell Telephone Labor Inc | Transversal filters |
US6525579B1 (en) * | 1954-01-12 | 2003-02-25 | The United States Of America As Represented By The Attorney General | Pulse translational circuits |
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0
- US US1315539D patent/US1315539A/en not_active Expired - Lifetime
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