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US3926221A - Laminar fluidic multiplier - Google Patents

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US3926221A
US3926221A US497412A US49741274A US3926221A US 3926221 A US3926221 A US 3926221A US 497412 A US497412 A US 497412A US 49741274 A US49741274 A US 49741274A US 3926221 A US3926221 A US 3926221A
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amplifier
fluidic
multiplier
gain
supply pressure
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Robert L Woods
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United States Department of the Army
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United States Department of the Army
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15CFLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
    • F15C1/00Circuit elements having no moving parts
    • F15C1/14Stream-interaction devices; Momentum-exchange devices, e.g. operating by exchange between two orthogonal fluid jets ; Proportional amplifiers
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/206Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/212System comprising plural fluidic devices or stages
    • Y10T137/2125Plural power inputs [e.g., parallel inputs]
    • Y10T137/2147To cascaded plural devices
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/206Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/2229Device including passages having V over T configuration

Definitions

  • ABSTRACT CCII.2 137/812,;2763 A fluidic multiplier which comprises a proportional 58 Field of Search 37/567519 819, 834, amplifier P i in T gain of the amplifier is proportional to the power et 137/836 pressure, thereby prov1d1ng an output s1gnal wh1ch is [561 Cited 311 ii gficfiiiiiofifig"aiii ilifingiiififi'is iflil UNITED. STATES PATENTS disclosed for linearizing and isolating the multiplier 3,468,324 9/1969 Schrader 137/818 X from other circuitry. 3,499,460 3/1970 Rainer 137/818 X 3,530,870 9/1970 Hoglund 137/818 2 Claims, 10 Drawing Figures U.S. Patent Dec.16,1975 Sheet 1 015 3,926,221
  • FIG. 3 A k" APO 1a APO 20 0 PS PS 1.4 kPa 1 04 /10 12 AP (kP0) P (kPa)
  • FIG. 3 A k" APO 1a APO 20 0 PS PS 1.4 kPa 1 04 /10 12 AP (kP0) P (kPa)
  • FIG. 3 A k" APO 1a APO 20 0 PS PS 1.4 kPa 1 04 /10 12 AP (kP0) P (kPa)
  • LAMINAR FLUIDIC MULTIPLIER RIGHTS OF THE GOVERNMENT The invention described herein may be manufactured, used, and licensed by or for the United States Government for governmental purposes without the payment to me of any royalty thereon.
  • the present invention relates to fluidic amplifiers and, more particularly, to a fluidic amplifier operated as a gain changer or multiplier.
  • Multiplication or gain change is a function often required in fluidic computation and control circuits.
  • Applications include the straight multiplication of two signals for computation purposes; the division of one signal by another which may be accomplished, for example, by placing a multiplier in the feedback loop of a high gain amplifier; function generation such as,-for example, squaring; and gain change, i.e., varying the system gain for control purposes.
  • Another object of the present invention is to provide a fluidic multiplier which has a greatly improved range over prior art devices and in which the gain is linearly proportional to the input supply pressure.
  • An additional object of the present invention is to provide a fluidic multiplier circuit having preconditioned inputs and a buffered output which-increases the performance of the multiplier and isolates the same from the environment in which it is utilized.
  • a fluidic'multiplier which comprises a proportional fluidic amplifier operated in the laminar region. It is shown that such an amplifier has an output signal which is theproduct of its input signal and the supply pressure, thereby allowing operation as a gain changer or multiplier.
  • a fluidic multiplier circuit is provided in which the fluidic multiplier has a pair of fluid amplifiers operating as signal preconditioners and an output fluid amplifier operating as a buffer by means of which improved performance and isolation may be achieved.
  • FIG. 1 is a graph illustrating the output pressure versus the input pressure for a proportional amplifier
  • FIG. 2 is a graph illustrating the gain versus the supply pressure for the proportional amplifier illustrated in FIG. 1;
  • FIG. 3 is a graph illustrating the transfer characteristics of the proportional fluid amplifier of the present invention for various supply pressures
  • FIG. 4 is a' graph illustrating experimental results of the gain obtained for various supply pressures according to the present invention.
  • FIG. 5 illustrates preconditioning circuitry utilized in connection with the present invention and a graph helpful in understanding the operation thereof;
  • FIG. 6 illustrates a preferred embodiment of a fluidic multiplier circuit having preconditioning and output buffering in accordance with the present invention
  • FIGS. 7 and 8 are graphs of the transfer characte ristics of the circuitry of FIG. 6;
  • FIGS. 9 and 10 are graphs which illustrate the gain dependence of the circuitry illustrated in FIG. 6.
  • FIG. l there is illustrated at 10 a proportional fluidic amplifier having a power supply nozzle input 12, a pair of signal inputs 14 and 16, and output channels 18 and 20.
  • the graph illustrates the input pressure AP, versus the output pressure AP the slope of the curve representing the gain G and generally being linear.
  • FIG. 2 illustrates for the amplifier 10 the gain dependence upon the supply pressure P It is seen from FIG. 2 that when the amplifier 10 is operated in the turbulent region, the gain is constant. However, in the laminar region, the gain falls off to zero in an approximate straight line curve having a slope K.
  • the gain dependence upon the supply pressure of proportional amplifier 10 when operated in the laminar region is a generally undesirable characteristic, such characteristic forms the basis of the present invention.
  • the primary input referred to hereinafter as signal A
  • the secondary input referred to hereinafter as signal B
  • the proportional amplifier 10 operated in the laminar region according to the present invention may be utilized as either a multiplier or a gain changer.
  • a porportional amplifier 10 is operated in the laminar region when its supply pressure P has a Reynolds number R defined as follows:
  • P is the power supply pressure
  • p is the fluid density
  • w is the power nozzle width of amplifier 10
  • V is the kinematic viscosity
  • FIG. 3 illustrates the transfer characteristics for various supply pressures obtained from a commercially available proportional amplifier l operated in the laminar region according to the present invention.
  • the best mode of operation resulted from a center-vented proportional amplifier having a power nozzle width of 0.5 millimeters (0.020 inches) and as aspect ratio of 0.5.
  • the transfer characteristics illustrated in FIG. 3 attest to the linearity, low noise, and data consistency achieved according to the present invention.
  • FIG. 4 is a further graph of the small signal gain versus supply pressure of the device described in connection with FIG. 3.
  • the curve depicted in FIG. 4 can be best characterized by a straight line having a slight offset.
  • the points at which the curve deviate more than plus or minus 10 percent from the straight line (with offset) are designated P, min and P, max.
  • the device described above in connection with FIGS. 3 and 4 serves well as a multiplier or as an excellent gain changer with no further modifications. It is possible, however to enhance the linearity and performance of the basic proportional amplifier in accordance with another aspect of the present invention.
  • the fluidic multiplier according to the present invention the following three conditions should be met:
  • the gain versus power supply pressure curve (FIG. 4) should be offset to allow the gain curve to pass through zero;
  • the mean output level of the multiplier (which varies with supply pressure) should be held constant to avoid level sensitivity problems in suceeding stages.
  • the input and output signal levels should be consistent with the fluidic circuitry in which the multiplier will be utilized.
  • the offsetting of the gain versus the power supply pressure curve may be accomplished by using a biased fluid amplifier 30 having single-sided transfer charac teristics as seen in FIG. 5.
  • One. output 34 of preconditioning amplifier 30 is biased off, while the other output 32 is utilized as the supply pressure input to multiplier 10.
  • the supply pressure P, of amplifier 30 is selected such that its output pressure P,,,, at saturation is slightly greater than P max.
  • the input bias signal P,-,, of amplifier 30 is selected such that P equals P min at a null input signal P
  • the supply pressure P to the multiplier 10 ranges from P, min to P, max as the input signal P varies from zero, thereby allowing the gain of multiplier 10 to be linearized with respect to P
  • the connection of biased fluid amplifier 30 to the multiplier 10 of the present invention via line 32 is shown again in FIG. 6, which also illustrates a second preconditioning amplifier 34 which includes a pair of inputs 40 and 42 and a pair of outputs 36 and 38 which are respectively fed to the inputs of multiplier 10.
  • Preconditioning amplifier 34 is required to provide a predictable, low mean input level to multiplier 10 in order to isolate multiplier 10 from an arbitrary driving signal.
  • Amplifier 34 operates with the same supply pressure as amplifier 30 and is also provided, by means of fluid resistors 44 and 46, with a large attentuation of the output signal in order to match signal levels to the multiplier 10.
  • an output buffer amplifier 50 is provided to receive the output from multiplier 10 via lines 48 and 49.
  • the supply pressure and power nozzle of buffer amplifier 50 should be selected so that the maximum output signal from multiplier 10 is below saturation of buffer amplifier 50 in order to provide a low mean input level.
  • the mean output level of buffer amplifier 50 will thus be constant, and normal staging techniques may be utilized to other circuitry.
  • FIG. 6 The circuitry depicted in FIG. 6 has been tested experimentally and in a best mode utilizes amplifiers having 0.5 millimeter power nozzle widths with an aspect ratio of 0.5.
  • the supply pressures, bias offset, and attenuation were selected in accordance with the above-mentioned-criteria.
  • the transfer characteristics of such a circuit for input channels A and B are shown respectively in FIGS. 7 and 8. It is seen from FIGS. 7 and 8 that the circuitry described in FIG. 6 can be used as a true multiplier since the circuit has zero gain with zero input in both channels A and B, while the gain increases linearly with respect to both inputs, better seen with reference to FIGS. 9 and 10.
  • FIGS. 9 and 10 illustrate the experimental performance of the circuitry of FIG.
  • the input range (range being the ratio of maximum signal to minimum signal in which there is less than 10 percent deviation from the linear approximation) of the A-channel (amplifier inputs) is greater than 50:1 while the B-channel (power supply) range is 20:1. Since all amplifiers were operated with laminar flow, signal noise was several hundred below the maximum signals.
  • a fluidic multiplier circuit which comprises: a proportional fluidic amplifier operated in the laminar region having a supply pressure input and a pair of signal inputs and a pair of outputs;
  • a preconditioning fluid amplifier having a supply pressure equal to that of said biased fluid amplifier and an output connected to said pair of signal inputs of said proportional fluidic amplifier.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Amplifiers (AREA)

Abstract

A fluidic multiplier which comprises a proportional fluidic amplifier operated in the laminar region. The gain of the amplifier is proportional to the power jet pressure, thereby providing an output signal which is the product of the input signal and the supply pressure. A preconditioning and buffering circuit is also disclosed for linearizing and isolating the multiplier from other circuitry.

Description

' United States Patent Woods Dec. 16, 1975 1 LAMINAR FLUIDIC MULTIPLIER 3,667,491 6/1972 Hasbrouck 137/818 3,687,150 8/1972 Hoglund 137/818 [75] lnvemor- Wwds, Kensmgtom 3,752,171 8/1973 Ayre 137/819 x [73] A i The United States of America as 3,785,390 l/1974 Taylor 137/836 X represented by the Secretary of the Army, Washington, DC. Primary Examiner-William R. Cline Attorney, Agent, 0rv FirmNathan Edelberg; Robert P. [22] Filed. Aug. 14, 1974 Gibson; Saul Elbaum [21] Appl. No.: 497,412
[57] ABSTRACT CCII.2 137/812,;2763: A fluidic multiplier which comprises a proportional 58 Field of Search 37/567519 819, 834, amplifier P i in T gain of the amplifier is proportional to the power et 137/836 pressure, thereby prov1d1ng an output s1gnal wh1ch is [561 Cited 311 ii gficfiiiiiiofifig"aiii ilifingiiififi'is iflil UNITED. STATES PATENTS disclosed for linearizing and isolating the multiplier 3,468,324 9/1969 Schrader 137/818 X from other circuitry. 3,499,460 3/1970 Rainer 137/818 X 3,530,870 9/1970 Hoglund 137/818 2 Claims, 10 Drawing Figures U.S. Patent Dec.16,1975 Sheet 1 015 3,926,221
1o APi 14 A k" APO 1a APO 20 0 PS PS 1.4 kPa 1 04 /10 12 AP (kP0) P (kPa) FIG. 3
LAMINAR TURBULENT GAIN, e K
SUPPLY PRESSURE Ps FIG. 2
GAIN
FIG. 4
US. Patent Dec. 16,1975 Sheet50f5 3,926,221
b bAPm Pu(kP0) FIG. 10
LAMINAR FLUIDIC MULTIPLIER RIGHTS OF THE GOVERNMENT The invention described herein may be manufactured, used, and licensed by or for the United States Government for governmental purposes without the payment to me of any royalty thereon.
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to fluidic amplifiers and, more particularly, to a fluidic amplifier operated as a gain changer or multiplier.
2. Description of the Prior Art Multiplication or gain change is a function often required in fluidic computation and control circuits. Applications include the straight multiplication of two signals for computation purposes; the division of one signal by another which may be accomplished, for example, by placing a multiplier in the feedback loop of a high gain amplifier; function generation such as,-for example, squaring; and gain change, i.e., varying the system gain for control purposes.
In spite of the great need for fluidic multipliers as evidenced by the foregoing requirements, prior art fluidic multipliers are lacking in performance, simplicity, and availability. Prior art approaches in the development of suitable fluidic multipliers have been to utilize inherent device characteristics or to build circuits which accomplish the desired effect. Most of the prior art devices fall into the category of gain changers since the second input decreases the gain of the device with increasing input. A true multiplier, however, increases gain with both inputs and has zero gain at zero input. Thus, a nonlinear inversion of the second input is generally required to convert gain changers into true multipliers.
One prior art approach as described in US. Pat. No. 3,638,671 achieves multiplication with the aid of moving parts. In this device, the differential output pressure is a function of the supply pressure and the position of a pin located in the interaction region. A pair of bellows are utilized to convert pressure to position. Such an arrangement, while generally sound, is disadvantageous when no moving parts are required. A quartersquare multiplier circuit is also known in the art (see, for example, US. Pat. No. 3,495,774) which again is generally workable, but is complex and lacking in linear range. Other prior art approaches to fluidic multipliers include U.S. Pat. Nos. 3,499,460; 3,530,870; and 3,687,150 in which a dual-differencing amplifier circuit is utilized in which the offset on nonlinear transfer curves determines the circuit gain. Such circuits reduce the gain to zero in an inverse manner, but also lack linearity and range.
OBJECTS AND SUMMARY OF THE INVENTION It is accordingly a primary object of the present invention to provide a novel and unique fluidic amplifier which may be utilized as a gain changer or multiplier which overcomes the above-mentioned disadvantages of prior art fluidic multipliers.
Another object of the present invention is to provide a fluidic multiplier which has a greatly improved range over prior art devices and in which the gain is linearly proportional to the input supply pressure.
An additional object of the present invention is to provide a fluidic multiplier circuit having preconditioned inputs and a buffered output which-increases the performance of the multiplier and isolates the same from the environment in which it is utilized.
The foregoing and other objects are achieved in accordance with one aspect of the present invention through the provision of a fluidic'multiplier which comprises a proportional fluidic amplifier operated in the laminar region. It is shown that such an amplifier has an output signal which is theproduct of its input signal and the supply pressure, thereby allowing operation as a gain changer or multiplier. In accordance with another aspect "of the present invention, a fluidic multiplier circuit is provided in which the fluidic multiplier has a pair of fluid amplifiers operating as signal preconditioners and an output fluid amplifier operating as a buffer by means of which improved performance and isolation may be achieved.
BRIEF DESCRIPTION OF THE DRAWINGS Various objects, features and attendant advantages of the present invention will be more fully appreciated as the same becomes better understood from the following detailed description of the present invention when considered in connection .with the accompanying drawings, in which:
FIG. 1 is a graph illustrating the output pressure versus the input pressure for a proportional amplifier;
FIG. 2 is a graph illustrating the gain versus the supply pressure for the proportional amplifier illustrated in FIG. 1; I
FIG. 3 is a graph illustrating the transfer characteristics of the proportional fluid amplifier of the present invention for various supply pressures;
FIG. 4 is a' graph illustrating experimental results of the gain obtained for various supply pressures according to the present invention;
FIG. 5 illustrates preconditioning circuitry utilized in connection with the present invention and a graph helpful in understanding the operation thereof;
FIG. 6 illustrates a preferred embodiment of a fluidic multiplier circuit having preconditioning and output buffering in accordance with the present invention;
FIGS. 7 and 8 are graphs of the transfer characte ristics of the circuitry of FIG. 6; and
FIGS. 9 and 10 are graphs which illustrate the gain dependence of the circuitry illustrated in FIG. 6.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring now to FIG. l, there is illustrated at 10 a proportional fluidic amplifier having a power supply nozzle input 12, a pair of signal inputs 14 and 16, and output channels 18 and 20. The graph illustrates the input pressure AP, versus the output pressure AP the slope of the curve representing the gain G and generally being linear. FIG. 2 illustrates for the amplifier 10 the gain dependence upon the supply pressure P It is seen from FIG. 2 that when the amplifier 10 is operated in the turbulent region, the gain is constant. However, in the laminar region, the gain falls off to zero in an approximate straight line curve having a slope K. Although the gain dependence upon the supply pressure of proportional amplifier 10 when operated in the laminar region is a generally undesirable characteristic, such characteristic forms the basis of the present invention.
3 It may be observed from FIG. 1 that from the transfer characteristic AP, r; a P,-. and, from FIG. 2, thegain-supply pressure characteristic c= KP,,. I 7 that the output signal AP is the product of the input signal AP,- and the supply pressure P i.e.,
AP, KP, an. v The primary input, referred to hereinafter as signal A, comprises the, input. signal to the amplifier, while the secondary input, referred to hereinafter as signal B, comprises the amplifiers supply pressure. It is seen from FIG. 2 that in the laminar region the transfer gain can be changed almost linearly from zero to a maximum value with increasing supply pressure; thus, the proportional amplifier 10 operated in the laminar region according to the present invention may be utilized as either a multiplier or a gain changer. Mathematically speaking, a porportional amplifier 10 is operated in the laminar region when its supply pressure P has a Reynolds number R defined as follows:
wherein P, is the power supply pressure; p is the fluid density; w is the power nozzle width of amplifier 10;
and V is the kinematic viscosity.
FIG. 3 illustrates the transfer characteristics for various supply pressures obtained from a commercially available proportional amplifier l operated in the laminar region according to the present invention. The best mode of operation resulted from a center-vented proportional amplifier having a power nozzle width of 0.5 millimeters (0.020 inches) and as aspect ratio of 0.5. The transfer characteristics illustrated in FIG. 3 attest to the linearity, low noise, and data consistency achieved according to the present invention.
FIG. 4 is a further graph of the small signal gain versus supply pressure of the device described in connection with FIG. 3. The curve depicted in FIG. 4 can be best characterized by a straight line having a slight offset. The points at which the curve deviate more than plus or minus 10 percent from the straight line (with offset) are designated P, min and P, max.
If precise computation is not required, the device described above in connection with FIGS. 3 and 4 serves well as a multiplier or as an excellent gain changer with no further modifications. It is possible, however to enhance the linearity and performance of the basic proportional amplifier in accordance with another aspect of the present invention. For optimum operation of the fluidic multiplier according to the present invention, the following three conditions should be met:
1. The gain versus power supply pressure curve (FIG. 4) should be offset to allow the gain curve to pass through zero;
2. The mean input level to the multiplier should be carefully staged to avoid unexpected gain degradation of the multiplier; and
3. The mean output level of the multiplier (which varies with supply pressure) should be held constant to avoid level sensitivity problems in suceeding stages.
4 Further, the input and output signal levels should be consistent with the fluidic circuitry in which the multiplier will be utilized.
The offsetting of the gain versus the power supply pressure curve may be accomplished by using a biased fluid amplifier 30 having single-sided transfer charac teristics as seen in FIG. 5. One. output 34 of preconditioning amplifier 30 is biased off, while the other output 32 is utilized as the supply pressure input to multiplier 10. The supply pressure P, of amplifier 30 is selected such that its output pressure P,,,, at saturation is slightly greater than P max. The input bias signal P,-,, of amplifier 30 is selected such that P equals P min at a null input signal P In this manner, the supply pressure P to the multiplier 10 ranges from P, min to P, max as the input signal P varies from zero, thereby allowing the gain of multiplier 10 to be linearized with respect to P The connection of biased fluid amplifier 30 to the multiplier 10 of the present invention via line 32 is shown again in FIG. 6, which also illustrates a second preconditioning amplifier 34 which includes a pair of inputs 40 and 42 and a pair of outputs 36 and 38 which are respectively fed to the inputs of multiplier 10. Preconditioning amplifier 34 is required to provide a predictable, low mean input level to multiplier 10 in order to isolate multiplier 10 from an arbitrary driving signal. Amplifier 34 operates with the same supply pressure as amplifier 30 and is also provided, by means of fluid resistors 44 and 46, with a large attentuation of the output signal in order to match signal levels to the multiplier 10.
Since the supply pressure via line 32 to multiplier 10 varies, the mean output level of the multiplier varies. Such a variation in mean output level may affect the gain of a succeeding stage. For proper staging, an output buffer amplifier 50 is provided to receive the output from multiplier 10 via lines 48 and 49. The supply pressure and power nozzle of buffer amplifier 50 should be selected so that the maximum output signal from multiplier 10 is below saturation of buffer amplifier 50 in order to provide a low mean input level. The mean output level of buffer amplifier 50 will thus be constant, and normal staging techniques may be utilized to other circuitry.
The circuitry depicted in FIG. 6 has been tested experimentally and in a best mode utilizes amplifiers having 0.5 millimeter power nozzle widths with an aspect ratio of 0.5. The supply pressures, bias offset, and attenuation were selected in accordance with the above-mentioned-criteria. The transfer characteristics of such a circuit for input channels A and B are shown respectively in FIGS. 7 and 8. It is seen from FIGS. 7 and 8 that the circuitry described in FIG. 6 can be used as a true multiplier since the circuit has zero gain with zero input in both channels A and B, while the gain increases linearly with respect to both inputs, better seen with reference to FIGS. 9 and 10. FIGS. 9 and 10 illustrate the experimental performance of the circuitry of FIG. 6 wherein the input range (range being the ratio of maximum signal to minimum signal in which there is less than 10 percent deviation from the linear approximation) of the A-channel (amplifier inputs) is greater than 50:1 while the B-channel (power supply) range is 20:1. Since all amplifiers were operated with laminar flow, signal noise was several hundred below the maximum signals.
It is seen that l have provided an extremely simple fluidic multiplier which utilizes the laminar flow characteristics of a proportional amplifier to provide gain change or multiplication. The prior art disadvantages such as component nonlinearities, input signal inversion, and limited functional range have been overcome.
Obviously, numerous modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understoodthat within the scope of the appended claims the invention may be practiced otherwise than as specifically described herein. I
What is claimed as new and desired to be secured by Letters Patent of the United States is:
l. A fluidic multiplier circuit, which comprises: a proportional fluidic amplifier operated in the laminar region having a supply pressure input and a pair of signal inputs and a pair of outputs;
a biased fluid amplifier having a supply pressure, an
I output and a single-sided transfer characteristic, said output connected to said supply pressure input of said proportional fluidic amplifier; and
a preconditioning fluid amplifier having a supply pressure equal to that of said biased fluid amplifier and an output connected to said pair of signal inputs of said proportional fluidic amplifier.
2. The fluidic multiplierzcircuit according to claim 1, further comprising a buffer amplifier having a pair of inputs connected to said pair of outputs of said proportional fluidic amplifier, said buffer amplifier including means for providing a constant mean output level therefrom

Claims (2)

1. A fluidic multiplier circuit, which comprises: a proportional fluidic amplifier operated in the laminar region having a supply pressure input and a pair of signal inputs and a pair of outputs; a biased fluid amplifier having a supply pressure, an output and a single-sided transfer characteristic, said output connected to said supply pressure input of said proportional fluidic amplifier; and a preconditioning fluid amplifier having a supply pressure equal to that of said biased fluid amplifier and an output connected to said pair of signal inputs of said proportional fluidic amplifier.
2. The fluidic multiplier circuit accordinG to claim 1, further comprising a buffer amplifier having a pair of inputs connected to said pair of outputs of said proportional fluidic amplifier, said buffer amplifier including means for providing a constant mean output level therefrom.
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3986527A (en) * 1975-11-06 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Laminar flow digital logic elements with feedback
US4369811A (en) * 1978-10-20 1983-01-25 The United States Of America As Represented By The Secretary Of The Army Null balancing for fluidic sensors and amplifiers
US4678009A (en) * 1986-10-03 1987-07-07 The United States Of America As Represented By The Secretary Of The Army Fluidic complementary gain changing circuit
US11231055B1 (en) * 2019-06-05 2022-01-25 Facebook Technologies, Llc Apparatus and methods for fluidic amplification

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3468324A (en) * 1965-10-23 1969-09-23 Bowles Eng Corp Limiting amplifier
US3499460A (en) * 1967-08-11 1970-03-10 Honeywell Inc Fluid circuit
US3530870A (en) * 1967-12-14 1970-09-29 Honeywell Inc Fluid circuit
US3667491A (en) * 1970-05-04 1972-06-06 United Aircraft Corp Function generator using fluid amplifiers
US3687150A (en) * 1970-08-10 1972-08-29 Honeywell Inc Proportional fluidic gain changer
US3752171A (en) * 1971-06-25 1973-08-14 Us Army Fluid gain change circuit
US3785390A (en) * 1967-03-09 1974-01-15 Powers Regulator Co Pure fluid amplifier

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3468324A (en) * 1965-10-23 1969-09-23 Bowles Eng Corp Limiting amplifier
US3785390A (en) * 1967-03-09 1974-01-15 Powers Regulator Co Pure fluid amplifier
US3499460A (en) * 1967-08-11 1970-03-10 Honeywell Inc Fluid circuit
US3530870A (en) * 1967-12-14 1970-09-29 Honeywell Inc Fluid circuit
US3667491A (en) * 1970-05-04 1972-06-06 United Aircraft Corp Function generator using fluid amplifiers
US3687150A (en) * 1970-08-10 1972-08-29 Honeywell Inc Proportional fluidic gain changer
US3752171A (en) * 1971-06-25 1973-08-14 Us Army Fluid gain change circuit

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3986527A (en) * 1975-11-06 1976-10-19 The United States Of America As Represented By The Secretary Of The Army Laminar flow digital logic elements with feedback
US4369811A (en) * 1978-10-20 1983-01-25 The United States Of America As Represented By The Secretary Of The Army Null balancing for fluidic sensors and amplifiers
US4678009A (en) * 1986-10-03 1987-07-07 The United States Of America As Represented By The Secretary Of The Army Fluidic complementary gain changing circuit
US11231055B1 (en) * 2019-06-05 2022-01-25 Facebook Technologies, Llc Apparatus and methods for fluidic amplification

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