[go: up one dir, main page]

US3521654A - Fluidic device - Google Patents

Fluidic device Download PDF

Info

Publication number
US3521654A
US3521654A US697082A US3521654DA US3521654A US 3521654 A US3521654 A US 3521654A US 697082 A US697082 A US 697082A US 3521654D A US3521654D A US 3521654DA US 3521654 A US3521654 A US 3521654A
Authority
US
United States
Prior art keywords
fluid
control
jet
flapper
interaction chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US697082A
Inventor
Knut Brautaset
Arthur H Delmege
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vickers Inc
Original Assignee
Sperry Rand Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sperry Rand Corp filed Critical Sperry Rand Corp
Application granted granted Critical
Publication of US3521654A publication Critical patent/US3521654A/en
Assigned to SPERRY CORPORATION reassignment SPERRY CORPORATION CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SPERRY RAND CORPORATION
Assigned to VICKERS, INCORPORATED reassignment VICKERS, INCORPORATED ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: SPERRY CORPORATION A DE CORP.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F15C1/02Details, e.g. special constructional devices for circuits with fluid elements, such as resistances, capacitive circuit elements; devices preventing reaction coupling in composite elements ; Switch boards; Programme devices
    • F15C1/04Means for controlling fluid streams to fluid devices, e.g. by electric signals or other signals, no mixing taking place between the signal and the flow to be controlled
    • 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]
    • Y10T137/218Means to regulate or vary operation of device
    • Y10T137/2202By movable element
    • Y10T137/2213Electrically-actuated element [e.g., electro-mechanical transducer]
    • 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]
    • Y10T137/218Means to regulate or vary operation of device
    • Y10T137/2202By movable element
    • Y10T137/2218Means [e.g., valve] in control input

Definitions

  • a fluid amplifier having an interaction chamber therein and a plurality of fluid outputs extending therefrom and a plurality of control nozzles for directing fluid to said interaction chamber with means for selectively connect; ing the working pressure to one nozzle while restricting said pressure to the other nozzle for controlling the fluid output of the amplifier.
  • This invention relates to power transmissions, particularly to those of the type comprising two or more fluid pressure energy translating devices, one of which may function as a fluid pump and another as a fluid motor.
  • This invention is generally concerned with pure fluid devices for controlling the direction of fluid in such transmission systems, and, in particular, to fluid amplifiers.
  • Fluid amplifiers are currently finding wide application in various fields due primarily to their reliability, temperature insensitivity, shock resistance, and ease of fabrication. These devices may be employed as digital or analog computing elements and also can be utilized as power devices to operate pistons and the like. Fluid amplifiers may be operated equally as well as pneumatic devices employing a compressible fluid, such as gas or air, or as hydraulic devices utilizing incompressible fluids, such as water or oil.
  • Fluidic amplifiers can be employed as power devices to drive comparatively large loads such as spool type valves and the like, which are operatively connected to the fluid receivers.
  • loads such as spool type valves and the like, which are operatively connected to the fluid receivers.
  • the load be operated in response to an application of a very low level input signal from an electronic or magnetic control system. It is further desirable in such devices that provision be made for supplying the fluid amplifier with fluid derived from the working fluid introduced into the load cylinder so that the fluid amplifier is selfenergized.
  • Such a device includes a fluid amplifier section having a nozzle for generating a main jet of fluid, such as oil, the axis of the nozzle extending along a path midway between two fluid receiving load passages.
  • a main jet of fluid such as oil
  • the point of intersection of the nozzle and load passages is generally referred to as an interaction chamber.
  • the jet of fluid is directed to one of the load passages by injecting a control jet into the interaction chamber from either of two control nozzles which are generally perpendicular to the main jet of fluid.
  • control of the control jet has been accomplished in such devices by connecting each of the control jet nozzles to the working fluid supplied to the device and to a reservoir through a control passage.
  • Control of the control jet is readily obtained by alternately opening and restricting communication between the control passage and the reservoir. When communication to the reservoir is restricted, the working fluid is directed to the control nozzle and into the interaction chamber to control the direction of the main jet of fluid. If the communication between the reservoir and the control passage is open, working fluid will be directed to the reservoir and thus the direction of the main jet is not effected.
  • Such restric- 3,521,654 Patented July 28, 1970 ice tion and opening of the control passage may be obtained by using an electrically actuated servo leaf type flapper.
  • control jet since the control jet must be discharged into the reservoir when control of the main jet of fluid is not required, the total system leakage is unnecessarily increased.
  • This invention comprises a combination of a fluid amplifier and an electrically actuated flapper element in which a portion of the working fluid is directed to the interaction of the fluid amplifier by selectively connecting one of a plurality of control nozzles to the working fluid while restricting said working fluid from the other control nozzle by means of the flapper element.
  • the single figure is a diagrammatic view of a fluid amplifier incorporating a preferred form of the present invention.
  • a pure fluid device 12 having a power stream input channel 14 connecting an inlet chamber 16 to an interaction chamber 18 by means of sonic venturi 20 which defines a fluid power stream emanating from venturi 20 into the interaction chamber 18.
  • the other extremity of the inlet chamber 16 is connected to a pressure fluid source such as pressure energy translating device, not shown.
  • First and second diverging output channels 22 and 24 also communicate with the interaction chamber 18 and define first and second output paths of fluid flow respectively.
  • the output channels 22 and 24 diverge from a common wedge 26 disposed therebetween which is preferably truncated and forms one wall of the interaction chamber 18.
  • the other Walls of the interaction chamber 18 may be formed by extensions of the exterior walls of the output channels 22 and 24.
  • the device 12 has a left control jet nozzle 28 and a right control jet nozzle 30 which communicate with the interaction chamber 18 at one extremity, and are connected respectively to left and right feedback control ports 32 and 34 in a servo valve chamber 36 by means of conduits 38 and 40, respectively.
  • the servo valve chamber 36 is connected to the inlet chamber 16 by means of conduit 41, thus, both chambers are substantially at the same pressure.
  • the pressure fluid in chamber 36 may be selectively directed to either left and right feedback control ports 32 and 34 by means of a leaf type flapper 42 which is mechanically linked and actuated by solenoids 44 and 46.
  • solenoids 44 and 46 When the solenoids are actuated so as to shift the flapper 42 rightwardly, as illustrated by the letter A, the pressure fluid entering the right feedback control port 34 is substantially restricted, thus, pressure fluid in chamber 36 will exit through the left feedback control port 32 and be directed to the interaction chamber 18 via conduit 38 and left nozzle 28.
  • Pure fluid device 12 may be constructed according to any of the methods known to those skilled in the art.
  • the device 12 may be of the momentum exchange type wherein the power stream is deflected by one of the control jet nozzles which directs pressure fluid laterally at the stream.
  • This device is accordingly referred to as a proportional, or analog, device.
  • a second type of device which may be used is generally known as a boundary layer, or Coanda effect, device.
  • the power jet is deflected by the action of side walls of an interaction chamber which are shaped in such a way that the power stream will attach to one or the oiher of the walls of the output channels, but not both of the walls.
  • This type of a device is basically a two position device, and for this reason, is referred to as a digital device. Either the analog or the digital type of device can be employed in combination with the subject invention.
  • the power stream When pressure fluid is directed through the left control jet nozzle 28 into the interaction chamber 18, the power stream -will be directed through the flow path defined by channel 22, and when pressure fluid is directed through the right control nozzle 30 into the interaction chamber 18, the power stream will be directed through the flow path defined by the channel 24.
  • the power stream may be selectively directed to either output channel 22 or 24 by means of positioning flapper 42.
  • fluid outlets 48 and 50 Associated with the output channels 22 and 24 are fluid outlets 48 and 50, respectively.
  • the flapper 42 is actuated so as to cause the power stream to be directed into the flow path associated with output channel 22 in a manner herebefore described, the power stream will exit through the fluid outlet 48' and may be directed to a pressure energy translating device, not shown, for use by the same.
  • the flapper 42 When the flapper 42 is actuated so as to cause the power stream to be directed into the flow path associated with the output channel 24 in a manner herebefore described, the power stream will exit through the fluid outlet 50 and be directed to the said pressure energy translating device for use by the same.
  • the present invention provides an electrically actuated fluidic device capable of directing fluid selectively to a plurality of outlets, which has a minimum of electrical power consumption, in which its construction provides for the collection and utilization of the control working fluid and which is eflicient and reliable in operation and has a long life.
  • a fluid amplifier device comprising:
  • a flapper element for selectively restricting fluid communication between said connecting means and one of said opposed fluid ports while permitting fluid communication between said connecting means and the other of said fluid ports whereby said pressure fluid is directed to said interaction chamber and utilized in the output of the device;

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Jet Pumps And Other Pumps (AREA)

Description

July 28; 1970 BRAUTASET ET AL 3,521,654
FLUIDIC DEVICE Filed Jan. 11, 1968 \'VENTOR. KNUT BRAUTASETQS ARTHUR H. DELMEGE ATTORNEYS United States Patent 3,521,654 FLUIDIC DEVICE Knut .Brautaset, Royal Oak, and Arthur H. Delmege, Grosse Pointe Woods, Mich, assignors to Sperry Rand Corporation, Troy, Mich., a corporation of Delaware Filed Jan. 11, 1968, Ser. No. 697,082 Int. Cl. F15c 1/04, 3/00 U.S. Cl. 137--81.5 2 Claims ABSTRACT OF THE DISCLOSURE A fluid amplifier having an interaction chamber therein and a plurality of fluid outputs extending therefrom and a plurality of control nozzles for directing fluid to said interaction chamber with means for selectively connect; ing the working pressure to one nozzle while restricting said pressure to the other nozzle for controlling the fluid output of the amplifier.
BACKGROUND OF THE INVENTION This invention relates to power transmissions, particularly to those of the type comprising two or more fluid pressure energy translating devices, one of which may function as a fluid pump and another as a fluid motor.
This invention is generally concerned with pure fluid devices for controlling the direction of fluid in such transmission systems, and, in particular, to fluid amplifiers.
Fluid amplifiers are currently finding wide application in various fields due primarily to their reliability, temperature insensitivity, shock resistance, and ease of fabrication. These devices may be employed as digital or analog computing elements and also can be utilized as power devices to operate pistons and the like. Fluid amplifiers may be operated equally as well as pneumatic devices employing a compressible fluid, such as gas or air, or as hydraulic devices utilizing incompressible fluids, such as water or oil.
Fluidic amplifiers can be employed as power devices to drive comparatively large loads such as spool type valves and the like, which are operatively connected to the fluid receivers. In such power applications, it is very desirable that the load be operated in response to an application of a very low level input signal from an electronic or magnetic control system. It is further desirable in such devices that provision be made for supplying the fluid amplifier with fluid derived from the working fluid introduced into the load cylinder so that the fluid amplifier is selfenergized.
Such a device includes a fluid amplifier section having a nozzle for generating a main jet of fluid, such as oil, the axis of the nozzle extending along a path midway between two fluid receiving load passages. The point of intersection of the nozzle and load passages is generally referred to as an interaction chamber. The jet of fluid is directed to one of the load passages by injecting a control jet into the interaction chamber from either of two control nozzles which are generally perpendicular to the main jet of fluid.
In the past, the control of the control jet has been accomplished in such devices by connecting each of the control jet nozzles to the working fluid supplied to the device and to a reservoir through a control passage. Control of the control jet is readily obtained by alternately opening and restricting communication between the control passage and the reservoir. When communication to the reservoir is restricted, the working fluid is directed to the control nozzle and into the interaction chamber to control the direction of the main jet of fluid. If the communication between the reservoir and the control passage is open, working fluid will be directed to the reservoir and thus the direction of the main jet is not effected. Such restric- 3,521,654 Patented July 28, 1970 ice tion and opening of the control passage may be obtained by using an electrically actuated servo leaf type flapper.
Such systems require a high level of input signal to the electrically actuating means since the flapper must act against the force created by the pressure of the working fluid in order to create the necessary restriction. Further, such forces tend to fatigue the flapper leading to a premature failure of the control device.
Further, since the control jet must be discharged into the reservoir when control of the main jet of fluid is not required, the total system leakage is unnecessarily increased.
SUMMARY OF THE INVENTION This invention comprises a combination of a fluid amplifier and an electrically actuated flapper element in which a portion of the working fluid is directed to the interaction of the fluid amplifier by selectively connecting one of a plurality of control nozzles to the working fluid while restricting said working fluid from the other control nozzle by means of the flapper element.
It is therefore an object of this invention to provide a novel and improved input means for controlling the position of a fluid jet in a fluid amplifier.
It is another object of this invention to provide a novel and improved input means for controlling the position of a fluid jet in a fluid amplifier in which all control flow is collected and utilized for the output.
It is also an object of this invention to provide a novel and improved input means for controlling the position of a fluid jet in a fluid amplifier which is electrically actuated and has a minimum electrical power consumption.
It is a further object of this invention to provide a novel and improved input means for controlling the position of a fluid jet in a fluid amplifier which is compact and economical to manufacture and which is efficient and reliable in operation and has a long life.
Further objects and advantages of the present invention will be apparent from the following description, reference being made to the accompanying drawing wherein a preferred form of the present invention is clearly shown.
In the drawing, the single figure is a diagrammatic view of a fluid amplifier incorporating a preferred form of the present invention.
Referring now to the drawing, there is illustrated a pure fluid device 12 having a power stream input channel 14 connecting an inlet chamber 16 to an interaction chamber 18 by means of sonic venturi 20 which defines a fluid power stream emanating from venturi 20 into the interaction chamber 18. The other extremity of the inlet chamber 16 is connected to a pressure fluid source such as pressure energy translating device, not shown. First and second diverging output channels 22 and 24 also communicate with the interaction chamber 18 and define first and second output paths of fluid flow respectively. The output channels 22 and 24 diverge from a common wedge 26 disposed therebetween which is preferably truncated and forms one wall of the interaction chamber 18. The other Walls of the interaction chamber 18 may be formed by extensions of the exterior walls of the output channels 22 and 24. The device 12 has a left control jet nozzle 28 and a right control jet nozzle 30 which communicate with the interaction chamber 18 at one extremity, and are connected respectively to left and right feedback control ports 32 and 34 in a servo valve chamber 36 by means of conduits 38 and 40, respectively.
The servo valve chamber 36 is connected to the inlet chamber 16 by means of conduit 41, thus, both chambers are substantially at the same pressure.
The pressure fluid in chamber 36 may be selectively directed to either left and right feedback control ports 32 and 34 by means of a leaf type flapper 42 which is mechanically linked and actuated by solenoids 44 and 46. When the solenoids are actuated so as to shift the flapper 42 rightwardly, as illustrated by the letter A, the pressure fluid entering the right feedback control port 34 is substantially restricted, thus, pressure fluid in chamber 36 will exit through the left feedback control port 32 and be directed to the interaction chamber 18 via conduit 38 and left nozzle 28. When the solenoids are actuated so as to shift the flapper 42 leftwardly, as illustrated by the letter B, the pressure fluid entering the left feedback control port 32 is substantially restricted, thus, pressure fluid in the chamber 36 will exit through the right feedback control port 34 and be directed to the interaction chamber 18 via conduit 40 and right jet nozzle 30.
Pure fluid device 12 may be constructed according to any of the methods known to those skilled in the art. The device 12 may be of the momentum exchange type wherein the power stream is deflected by one of the control jet nozzles which directs pressure fluid laterally at the stream.
This device is accordingly referred to as a proportional, or analog, device. A second type of device which may be used is generally known as a boundary layer, or Coanda effect, device. In this latter device, the power jet is deflected by the action of side walls of an interaction chamber which are shaped in such a way that the power stream will attach to one or the oiher of the walls of the output channels, but not both of the walls. This type of a device is basically a two position device, and for this reason, is referred to as a digital device. Either the analog or the digital type of device can be employed in combination with the subject invention.
When pressure fluid is directed through the left control jet nozzle 28 into the interaction chamber 18, the power stream -will be directed through the flow path defined by channel 22, and when pressure fluid is directed through the right control nozzle 30 into the interaction chamber 18, the power stream will be directed through the flow path defined by the channel 24. Thus, the power stream may be selectively directed to either output channel 22 or 24 by means of positioning flapper 42.
Associated with the output channels 22 and 24 are fluid outlets 48 and 50, respectively.
If the flapper 42 is actuated so as to cause the power stream to be directed into the flow path associated with output channel 22 in a manner herebefore described, the power stream will exit through the fluid outlet 48' and may be directed to a pressure energy translating device, not shown, for use by the same.
When the flapper 42 is actuated so as to cause the power stream to be directed into the flow path associated with the output channel 24 in a manner herebefore described, the power stream will exit through the fluid outlet 50 and be directed to the said pressure energy translating device for use by the same.
It should be noted that that portion of the working fluid which flows from the inlet to either the feedback ports is collected in the interaction chamber and is utilized in the output of the device, thus, there is no leakage due to the present pilot control. Further, the flapper 42 in restricting the flow to a feedback port does not act against a large force as in the hereinbefore described devices used in the past, thus, the flapper is not highly stressed nor subject to fatigue and is therefore assured a long life. Since the flapper does not have to overcome a force of great magnitude, as in past devices, the level of input power to the solenoids will be substantially decreased relative to the aforementioned past devices.
It can thus be seen that the present invention provides an electrically actuated fluidic device capable of directing fluid selectively to a plurality of outlets, which has a minimum of electrical power consumption, in which its construction provides for the collection and utilization of the control working fluid and which is eflicient and reliable in operation and has a long life.
While the form of embodiment of the invention as herein disclosed constitutes a preferred form, it is to be understood that other forms might be adopted, all coming Within the scope of the claims which follow.
What is claimed is as follows:
1. A fluid amplifier device comprising:
(a) a pure fluid element having an inlet connected to a power stream input channel for defining a power stream, first and second output channels each defining a path of fluid flow, and an interaction chamber d'isposed between and communicating with said channels;
(b) means forming first and second jet nozzles associated with said interaction chamber, one of said jet nozzles being adapted to direct pressure fluid into said interaction chamber for directing said power stream to said first output channel flow path, the other being adapted to direct pressure fluid into said interaction chamber for directing said power stream to said second output channel flow path;
(c) a fluid chamber having diametrically opposed fluid ports, one of which is connected to said first jet nozzle, the other being connected to the said second jet nozzle;
((1) means connecting said inlet to said chamber for providing pressure fluid from said inlet to said jet nozzle via said fluid ports;
(e) a flapper element for selectively restricting fluid communication between said connecting means and one of said opposed fluid ports while permitting fluid communication between said connecting means and the other of said fluid ports whereby said pressure fluid is directed to said interaction chamber and utilized in the output of the device; and,
(f) means for actuating said flapper element from one opposed fluid port to the other opposed fluid port.
2. The combination as in claim 1, wherein said actuating means comprises:
(a) a pair of electrically operated elements mechanically linked to said flapper and adapted to shift said flapper between said opposed fluid ports to selectively restrict the pressure fluid flowing therethrough.
References Cited UNITED STATES PATENTS 2,984,218 5/1961 Christianson 137596.15
3,152,612 10/1964 Avery 137625.62 XR 3,153,934 10/1964 Reilly.
3,171,421 3/1965 Joesting l3781.5 3,187,763 6/1965 Adams l3781.5 3,239,150 3/1966 Chisel 13781.5 XR
3,285,262 11/1966 Ernst et al 137-815 3,420,255 l/1969 Wilkerson 13781.5
SAMUEL SCOTT, Primary Examiner
US697082A 1968-01-11 1968-01-11 Fluidic device Expired - Lifetime US3521654A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US69708268A 1968-01-11 1968-01-11

Publications (1)

Publication Number Publication Date
US3521654A true US3521654A (en) 1970-07-28

Family

ID=24799709

Family Applications (1)

Application Number Title Priority Date Filing Date
US697082A Expired - Lifetime US3521654A (en) 1968-01-11 1968-01-11 Fluidic device

Country Status (1)

Country Link
US (1) US3521654A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762441A (en) * 1971-08-20 1973-10-02 Philco Ford Corp Jet coupled four-way valve
US4407186A (en) * 1980-04-07 1983-10-04 Nissan Motor Company, Ltd. Flow outlet structure for automotive air conditioner
US4413795A (en) * 1980-09-05 1983-11-08 The Garrett Corporation Fluidic thruster control and method
US7080664B1 (en) * 2005-05-20 2006-07-25 Crystal Fountains Inc. Fluid amplifier with media isolation control valve
US20120186682A1 (en) * 2009-07-23 2012-07-26 Airbus Operations Gmbh Fluid actuator for producing a pulsed outlet flow in the flow around an aerodynamic body, and discharge device and aerodynamic body equipped therewith

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2984218A (en) * 1958-07-29 1961-05-16 Gen Electric Fluid pressure modulating servo valve
US3152612A (en) * 1956-09-28 1964-10-13 Gen Electric Piezoelectric crystal transducer for controlling fluid flow
US3153934A (en) * 1962-07-20 1964-10-27 Honeywell Inc Pressure responsive device
US3171421A (en) * 1961-12-07 1965-03-02 Honeywell Inc Fluid amplifier control system
US3187763A (en) * 1962-12-17 1965-06-08 Moore Products Co Control apparatus
US3239150A (en) * 1961-11-29 1966-03-08 Continental Aviat & Eng Corp Thrust vector control
US3285262A (en) * 1962-08-07 1966-11-15 Snecma Aerodynamic or hydrodynamic servovalve, especially for use for the guidance and stabilisation of rockets
US3420255A (en) * 1965-09-01 1969-01-07 Gen Electric Fluid control devices

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3152612A (en) * 1956-09-28 1964-10-13 Gen Electric Piezoelectric crystal transducer for controlling fluid flow
US2984218A (en) * 1958-07-29 1961-05-16 Gen Electric Fluid pressure modulating servo valve
US3239150A (en) * 1961-11-29 1966-03-08 Continental Aviat & Eng Corp Thrust vector control
US3171421A (en) * 1961-12-07 1965-03-02 Honeywell Inc Fluid amplifier control system
US3153934A (en) * 1962-07-20 1964-10-27 Honeywell Inc Pressure responsive device
US3285262A (en) * 1962-08-07 1966-11-15 Snecma Aerodynamic or hydrodynamic servovalve, especially for use for the guidance and stabilisation of rockets
US3187763A (en) * 1962-12-17 1965-06-08 Moore Products Co Control apparatus
US3420255A (en) * 1965-09-01 1969-01-07 Gen Electric Fluid control devices

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762441A (en) * 1971-08-20 1973-10-02 Philco Ford Corp Jet coupled four-way valve
US4407186A (en) * 1980-04-07 1983-10-04 Nissan Motor Company, Ltd. Flow outlet structure for automotive air conditioner
US4413795A (en) * 1980-09-05 1983-11-08 The Garrett Corporation Fluidic thruster control and method
US7080664B1 (en) * 2005-05-20 2006-07-25 Crystal Fountains Inc. Fluid amplifier with media isolation control valve
US20120186682A1 (en) * 2009-07-23 2012-07-26 Airbus Operations Gmbh Fluid actuator for producing a pulsed outlet flow in the flow around an aerodynamic body, and discharge device and aerodynamic body equipped therewith
US8844571B2 (en) * 2009-07-23 2014-09-30 Airbus Operations Gmbh Fluid actuator for producing a pulsed outlet flow in the flow around an aerodynamic body, and discharge device and aerodynamic body equipped therewith

Similar Documents

Publication Publication Date Title
US3148691A (en) Fluid controlled device
US3521653A (en) Power transmission
US3537466A (en) Fluidic multiplier
US3470894A (en) Fluid jet devices
US3318329A (en) Fluid-operated logic devices
US3417770A (en) Fluid amplifier system
US3536085A (en) Fluid actuated valve assembly
US3285265A (en) Fluid amplifier devices
US3340896A (en) Fluid amplifier-driven oscillator
US3211182A (en) Servo valve with rotary first stage
US3521654A (en) Fluidic device
US3279323A (en) Electrohydraulic actuator
GB1181243A (en) Improvements in or relating to Fluid Control Switching Arrangements
US3174497A (en) Fluid power amplifier not-gate
US3270758A (en) Fluid amplifiers
US3028880A (en) Fluid flow control valve
US3405727A (en) Fluid control valve with feedback
US3331382A (en) Pure fluid amplifier
US3261372A (en) Fluid control element
US3176703A (en) Pulsed fluid amplifier
US3486520A (en) Deflector fluidic amplifier
USRE27712E (en) Power transmission
US4265272A (en) Transient start-up eliminator for pressure piloted valve
US2904055A (en) Hydraulic amplifier valve with feedback
US3381698A (en) Adjustable pressure gain control servo valve system

Legal Events

Date Code Title Description
AS Assignment

Owner name: SPERRY CORPORATION

Free format text: CHANGE OF NAME;ASSIGNOR:SPERRY RAND CORPORATION;REEL/FRAME:003794/0122

Effective date: 19790824

AS Assignment

Owner name: VICKERS, INCORPORATED TROY, MI A DE CORP

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST. EFFECTIVE NOVEMBER 2, 1983;ASSIGNOR:SPERRY CORPORATION A DE CORP.;REEL/FRAME:004337/0889

Effective date: 19831102

Owner name: VICKERS, INCORPORATED,MICHIGAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SPERRY CORPORATION A DE CORP.;REEL/FRAME:004337/0889

Effective date: 19831102