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US3578009A - Distributed control flueric amplifier - Google Patents

Distributed control flueric amplifier Download PDF

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Publication number
US3578009A
US3578009A US770184A US3578009DA US3578009A US 3578009 A US3578009 A US 3578009A US 770184 A US770184 A US 770184A US 3578009D A US3578009D A US 3578009DA US 3578009 A US3578009 A US 3578009A
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Prior art keywords
control
chamber
ports
attachment
fluid
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US770184A
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Chris E Spyropoulos
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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
    • F15C1/08Boundary-layer devices, e.g. wall-attachment amplifiers coanda effect
    • 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
    • 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
    • Y10T137/224With particular characteristics of control input
    • Y10T137/2245Multiple control-input passages

Definitions

  • One of the control ports comprises an entrainment control port for introducing positive pressure control fluid to the attachment bubble existing along the attachment wall, and the other one of the control ports constitutes a momentum exchange control port for creating a momentum impact force on the power stream.
  • This invention is a flueric amplifier in which each control flow is split and applied to the power jet through at least two separate control ports. This separate application is called distributed control and results in greater flow recovery and pressure recovery and improved switching time.
  • FIGURE is a top view of a flueric amplifier according to the present invention.
  • the FIGURE represents a flueric amplifier, especially a bistable amplifier.
  • the power jet flow is applied through a DESCRIPTION OF THE PREFERRED EMBODIMENT and enters an interaction chamber 2 through ajet nozzle area 3.
  • the fluid from the power jet leaves the chamber through either a left output channel 4 or a right output channel 5, which are separated by a splitter 6.
  • a control stream is being applied to the chamber from a left primary control channel 7.
  • Channel 7 is split into secondary channels 8 and 9 by a splitter 10.
  • Valves 11 and 12 which may be variable, are located respectively in channels 8 and 9 to control the flueric impedance of the channels 8 and 9 for proper proportioning of flow between the two channels.
  • Elements 7a through 14a from the right side of the amplifier respectively correspond in description and function to elements 7 through 14 from the left side of the amplifier.
  • the distance from jet nozzle 3 to power jet splitter 6 is preferably kept to a minimum for optimum pressure and flow recovery.
  • Iclaimi l. ln a flueric amplifier of the wall attachment type having tachment walls, the improvement comprising:
  • At least one upstream control port on each side of said chamber comprising an entrainment control port for introducing positive pressure control fluid to the attachment bubble existing along the attachment wall and at least one control port on the same side of said chamber and downstream of said entrainment control port constituting a momentum exchange control port for creating a momentum impact force on the same side of said power stream,
  • a common primary control channel for independently supplying control fluid and secondary control channels separately connecting the control ports for each group to its primary control channel to simultaneously supply control fluid to said chamber through said entrainment control port and said momentum exchange control .port.
  • each of the secondary control channels includes a variable flueric impedance for control of the amounts of fluid flow in each secondary channel.

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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)
  • Control Of Fluid Pressure (AREA)

Abstract

A flueric amplifier with two control ports for each control channel. Each control channel is split to operate both ports. The control flow is split and applied to the power jet through the two separate control ports. This separate application is called distributed control and results in greater flow recovery and pressure recovery as well as improved switching time. One of the control ports comprises an entrainment control port for introducing positive pressure control fluid to the attachment bubble existing along the attachment wall, and the other one of the control ports constitutes a momentum exchange control port for creating a momentum impact force on the power stream.

Description

United States Patent [72] Inventor Chris E. Spyropoulos Washington, D.C. [21] Appl. No. 770,184 [22] Filed Oct. 24, 1968 [45] Patented May 11. 1971 Assignee The United States of America as represented by the Secretary of the Army [54] DISTRIBUTED CONTROL FLUERIC AMPLIFIER 4 Claims, 1 Drawing Fig.
[52] US. Cl l37/81.5 [51] Int. Cl FlSc 1/08,
F15c 1/14 [50] Field of Search 137/815 [56] References Cited UNITED STATES PATENTS 3,124,160 3/1964 Zilberfarb l37/8l.5 3,186,422 6/1965 Boothe..... 137/81.5 3,272,214 9/1966 Warren 137/815 3,405,725 10/1968 Fox 137/815 LEFT OUTPUT CONTROL Primary ExaminerSamuel Scott Att0rneysI-Iarry M. Saragovitz, Edward .1. Kelly, Herbert Berl and John D. Edgerton ABSTRACT: A flueric amplifier with two control ports for each control channel. Each control channel is split'to operate both ports. The control flow is split and applied to the power jet through the two separate control ports. This separate application is called distributed control and results in greater flow recovery and pressure recovery as well as improved switching time. One of the control ports comprises an entrainment control port for introducing positive pressure control fluid to the attachment bubble existing along the attachment wall, and the other one of the control ports constitutes a momentum exchange control port for creating a momentum impact force on the power stream.
RIGHT OUTPUT 90 RIGHT CONTROL PATENTEU m1 1 12m LEFT OUTPUT RIGHT OUTPUT 7 WRIGHT CONTROL INVENTOR cums E. SP Y ROPOULOS DISTRIBUTED CONTROL FLUERIC AMPLIFIER BACKGROUND OF THE INVENTION SUMMARY OF THE INVENTION This invention is a flueric amplifier in which each control flow is split and applied to the power jet through at least two separate control ports. This separate application is called distributed control and results in greater flow recovery and pressure recovery and improved switching time.
BRIEF DESCRIPTION OF THE DRAWING The sole FIGURE is a top view of a flueric amplifier according to the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT The FIGURE represents a flueric amplifier, especially a bistable amplifier. The power jet flow is applied through a DESCRIPTION OF THE PREFERRED EMBODIMENT and enters an interaction chamber 2 through ajet nozzle area 3.
After deflection, accomplished in a manner described below, the fluid from the power jet leaves the chamber through either a left output channel 4 or a right output channel 5, which are separated by a splitter 6.
As illustrated, a control stream is being applied to the chamber from a left primary control channel 7. Channel 7 is split into secondary channels 8 and 9 by a splitter 10.
Valves 11 and 12, which may be variable, are located respectively in channels 8 and 9 to control the flueric impedance of the channels 8 and 9 for proper proportioning of flow between the two channels.
The control flows from channels 8 and 9 enter the interaction chamber through control ports 13 and 14 respectively.
Elements 7a through 14a from the right side of the amplifier respectively correspond in description and function to elements 7 through 14 from the left side of the amplifier.
The distance from jet nozzle 3 to power jet splitter 6 is preferably kept to a minimum for optimum pressure and flow recovery.
In the operation of the amplifier, assume that the power jet is locked onto the left wall of the interaction chamber. This configuration of the jet causes a low-pressure region, sometimes called an attachment bubble, to form along the left wall. The low-pressure region holds the jet to the wall by maintaining a pressure differential across the jet.
When'it is desired to move the jet away from the left wall, fluid must be introduced from the left control to build up pres sure in the bubble region, supply the entrainment needs of the jet on the bubble side, and thus destroy the bubble. In the place of the bubble is left a region of higher pressure which tends to deflect the jet to the right. The control fluid for this ports on each side of the interaction chamber. Three or more ports could be used. However, the preferred embodiment uses two ports for relative ease of construction.
Although the preferred use of the improved control is in a bistable amplifier, it would be obvious to use it in a proportional flueric amplifier.
Although the invention has been described in terms of an amplifier having left and right sides and two output channels, the invention would also be useful in a three-dimensional amplifier having more than two sides.
While the invention has been particularly shown and described with reference to a preferred embodiment thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention.
Iclaimi l. ln a flueric amplifier of the wall attachment type having tachment walls, the improvement comprising:
groups of longitudinally aligned control ports opening up into said chamber upstream of said attachment wall on opposite sides of the power stream with each output channel lying on diametrically opposite sides of the power stream from respective group of control ports effecting movement of said power stream into the same,
at least one upstream control port on each side of said chamber comprising an entrainment control port for introducing positive pressure control fluid to the attachment bubble existing along the attachment wall and at least one control port on the same side of said chamber and downstream of said entrainment control port constituting a momentum exchange control port for creating a momentum impact force on the same side of said power stream,
a common primary control channel for independently supplying control fluid and secondary control channels separately connecting the control ports for each group to its primary control channel to simultaneously supply control fluid to said chamber through said entrainment control port and said momentum exchange control .port.
2. An amplifier according to claim I wherein said groups of control ports number two and open up into said chamber on diametrically opposite sides thereof.
3. An amplifier according to claim I wherein each of the secondary control channels includes a variable flueric impedance for control of the amounts of fluid flow in each secondary channel.
4. An amplifier according to claim 3 wherein said groups of control ports are two in number and said groups of control ports and said output channels are diametrically opposite each other.

Claims (4)

1. In a flueric amplifier of the wall attachment type having input means for admitting a fluid input power stream into an interaction chamber, attachment walls downstream of said inlet and on opposite sides of said chamber and separate output channels leading from the chamber downstream of said attachment walls, the improvement comprising: groups of longitudinally aligned control ports opening up into said chamber upstream of said attachment wall on opposite sides of the power stream with each output channel lying on diametrically opposite sides of the power stream from respective group of control ports effecting movement of said power stream into the same, at least one upstream control port on each side of said chamber comprising an entrainment control port for introducing positive pressure control fluid to the attachment bubble existing along the attachment wall and at least one control port on the same side of said chamber and downstream of said entrainment control port constituting a momentum exchange control port for creating a momentum impact force on the same side of said power stream, a common primary control channel for independently supplying control fluid and secondary control channels separately connecting the control ports for each group to its primary control channel to simultaneously supply control fluid to said chamber through said entrainment control port and said momentum exchange control port.
2. An amplifier according to claim 1 wherein said groups of control ports number two and open up into said chamber on diametrically opposite sides thereof.
3. An amplifier according to claim 1 wherein each of the secondary control channels includes a variable flueric impedance for control of the amounts of fluid flow in each secondary channel.
4. An amplifier according to claim 3 wherein said groups of control ports are two in number and said groups of control ports and said output channels are diametrically opposite each oTher.
US770184A 1968-10-24 1968-10-24 Distributed control flueric amplifier Expired - Lifetime US3578009A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3760706A (en) * 1970-04-01 1973-09-25 Daimler Benz Ag Control installation for air or gas streams of ventilation systems
US3786839A (en) * 1971-03-15 1974-01-22 Us Army High input impedance flueric amplifier
US3873164A (en) * 1973-07-06 1975-03-25 Us Agriculture Pneumatic valve for airborne materials
FR2400632A1 (en) * 1977-08-16 1979-03-16 Continental Group PNEUMATIC DEVICE FOR SWITCHING A POWDER CURRENT
US4393897A (en) * 1979-11-20 1983-07-19 Nissan Motor Co., Ltd. Fluid outlet structure
US4770344A (en) * 1986-12-08 1988-09-13 Nordson Corporation Powder spraying system
US4860669A (en) * 1988-05-18 1989-08-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Energy efficient continuous flow ash lockhoper
US20090211224A1 (en) * 2004-11-05 2009-08-27 Volvo Aero Corporation Outlet device for a jet engine and a craft comprising such an outlet device

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3016063A (en) * 1960-07-05 1962-01-09 United Aircraft Corp Fluid valve
US3124160A (en) * 1964-03-10 zilberfarb
US3186422A (en) * 1962-12-31 1965-06-01 Gen Electric Fluid amplifier
US3272214A (en) * 1963-10-02 1966-09-13 Raymond W Warren Self-matching fluid elements
US3405725A (en) * 1964-03-24 1968-10-15 Sperry Rand Corp Fluid flow dividing means for fluid control devices
US3416487A (en) * 1966-03-22 1968-12-17 Green Eng Co Method and apparatus for generating and applying sonic energy
US3420255A (en) * 1965-09-01 1969-01-07 Gen Electric Fluid control devices
US3442278A (en) * 1966-02-28 1969-05-06 Sanders Associates Inc Temperature sensitive switch
US3460556A (en) * 1966-02-28 1969-08-12 Sanders Associates Inc Multiple mode fluid amplifier
US3511256A (en) * 1968-03-06 1970-05-12 Aro Corp Fluid logic element

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3124160A (en) * 1964-03-10 zilberfarb
US3016063A (en) * 1960-07-05 1962-01-09 United Aircraft Corp Fluid valve
US3186422A (en) * 1962-12-31 1965-06-01 Gen Electric Fluid amplifier
US3272214A (en) * 1963-10-02 1966-09-13 Raymond W Warren Self-matching fluid elements
US3405725A (en) * 1964-03-24 1968-10-15 Sperry Rand Corp Fluid flow dividing means for fluid control devices
US3420255A (en) * 1965-09-01 1969-01-07 Gen Electric Fluid control devices
US3442278A (en) * 1966-02-28 1969-05-06 Sanders Associates Inc Temperature sensitive switch
US3460556A (en) * 1966-02-28 1969-08-12 Sanders Associates Inc Multiple mode fluid amplifier
US3416487A (en) * 1966-03-22 1968-12-17 Green Eng Co Method and apparatus for generating and applying sonic energy
US3511256A (en) * 1968-03-06 1970-05-12 Aro Corp Fluid logic element

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3760706A (en) * 1970-04-01 1973-09-25 Daimler Benz Ag Control installation for air or gas streams of ventilation systems
US3786839A (en) * 1971-03-15 1974-01-22 Us Army High input impedance flueric amplifier
US3873164A (en) * 1973-07-06 1975-03-25 Us Agriculture Pneumatic valve for airborne materials
FR2400632A1 (en) * 1977-08-16 1979-03-16 Continental Group PNEUMATIC DEVICE FOR SWITCHING A POWDER CURRENT
US4165134A (en) * 1977-08-16 1979-08-21 The Continental Group, Inc. Pneumatic powder flow diverting device
US4393897A (en) * 1979-11-20 1983-07-19 Nissan Motor Co., Ltd. Fluid outlet structure
US4770344A (en) * 1986-12-08 1988-09-13 Nordson Corporation Powder spraying system
US4860669A (en) * 1988-05-18 1989-08-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Energy efficient continuous flow ash lockhoper
US20090211224A1 (en) * 2004-11-05 2009-08-27 Volvo Aero Corporation Outlet device for a jet engine and a craft comprising such an outlet device
US8215096B2 (en) * 2004-11-05 2012-07-10 Volvo Aero Corporation Outlet device for a jet engine and a craft comprising such an outlet device

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