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US3621880A - Jet pipe servo valve - Google Patents

Jet pipe servo valve Download PDF

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Publication number
US3621880A
US3621880A US3621880DA US3621880A US 3621880 A US3621880 A US 3621880A US 3621880D A US3621880D A US 3621880DA US 3621880 A US3621880 A US 3621880A
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United States
Prior art keywords
feed tube
fluid
end portion
jet pipe
body portion
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
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Inventor
James M Jessee
Ernest Niederer
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HR TEXTRON Inc A CORP OF DE
Bell Aerospace Corp
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Bell Aerospace Corp
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Publication of US3621880A publication Critical patent/US3621880A/en
Assigned to HR TEXTRON INC., A CORP. OF DE. reassignment HR TEXTRON INC., A CORP. OF DE. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: TEXTRON, INC.,
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/04Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
    • F15B13/042Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure
    • F15B13/043Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure with electrically-controlled pilot valves
    • F15B13/0436Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure with electrically-controlled pilot valves the pilot valves being of the steerable jet type
    • 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
    • Y10T137/2278Pressure modulating relays or followers
    • Y10T137/2322Jet control type
    • 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
    • Y10T137/8593Systems
    • Y10T137/86493Multi-way valve unit
    • Y10T137/86574Supply and exhaust
    • Y10T137/86582Pilot-actuated
    • Y10T137/86606Common to plural valve motor chambers
    • 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
    • Y10T137/8593Systems
    • Y10T137/86493Multi-way valve unit
    • Y10T137/86574Supply and exhaust
    • Y10T137/86582Pilot-actuated
    • Y10T137/86614Electric

Definitions

  • JET PIPE SERVO VALVE ABSTRACT Disclosed is a jet pipe-type servo valve wherein 1 Claim, 4 Drawing Figs.
  • the feed tube is disposed angularly with respect to a flapper to which it is affixed and which is movable by a torque motor the armature of which is connected to the flapper.
  • the feed tube has one end thereof affixed rigidly to the housing and the other end thereof terminating in a nozzle which is positioned adjacent a receiver,
  • the output ports of the receiver are connected to the end chambers of a cylinder within which a power control valve is slidably positioned so as to control the flow of References Cited fluid under pressure from a source thereof to an apparatus to UNITED STATES PATENTS be positioned such as an actuator.
  • 962 Gordon power control valve stage are isolated from each other.
  • Jet pipe servovalves have long been known and typical examples of such apparatus are shown in U.S. Pat. Nos. 2,884,906; 2,884,907; 2,996,072 and 3,017,864.
  • typical jet pipe servovalves are constructed in such a manner that the feed tube and the armature of the torque motor are an integral unit or at the most the feed tube is axially an extension of the torque motor armature.
  • the degree of movement of the nozzle tip, which terminates the feed tube is limited by the amount of movement of the armature in the torque motor.
  • alignment between the jet pipe nozzle orifice and the receiver ports is somewhat difficult to obtain and there is little or no adjustment available.
  • FIG. 1 is a schematic diagram shown in perspective of a jet pipe servovalve constructed in accordance with the present invention
  • FIG. 2 is a cross-sectional view of the servovalve illustrated in FIG. 1, taken about the line 2-2;
  • FIG. 3 is a fragmentary cross-sectional view taken about the line 3-3 ofFIG. 2;
  • FIG. 4 is a cross-sectional view taken about the line 44 of F IG. 2.
  • FIG. 1 there is illustrated a jet pipe servovalve which includes a torque motor 11 having pole pieces 12 and 13 with an armature 14 disposed therebetween.
  • a pair of coils 15 and 16 are disposed to received an input signal upon leads 17 thereby to provide movement of the armature and, as indicated by the arrow 18, which is proportional to the magnitude of the input signal.
  • a flapper 21 is rigidly connected to the armature 14 so as to move as indicated by the arrow 20 in response to movement of the armature 14.
  • the flapper 21 is suspended within a torque tube 22 so as to provide a seal between the fluid sections of the servovalve and the torque motor.
  • Such a suspension is well known and, for example, is illustrated in U.S. Pat. No. 3,221,760.
  • a feed tube 23 has one end thereof rigidly affixed to a retainer member 24 which in turn is rigidly affixed to the body portion 25 of the housing.
  • the feed tube 23 is constructed of a hollow flexure tube which is movable with respect to the housing.
  • Movement is imparted to the tube 23 by way of a flexible connection such as the link or spring clip 26 which is rigidly affixed to the flapper 21, but is releasably attached to the tube 23 by being inserted through an opening 27 defined by the clip 26.
  • a flexible connection such as the link or spring clip 26 which is rigidly affixed to the flapper 21, but is releasably attached to the tube 23 by being inserted through an opening 27 defined by the clip 26.
  • the feed tube 23 also is caused to move as indicated by the arrow 28.
  • the mechanical interconnection provides amplification of movement of the nozzle tip as compared to the flapper 21.
  • small armature movement results in larger nozzle tip movement.
  • the feed tube terminates in an ejector end having a nozzle 29 which is positioned adjacent openings 31 in a receiver port means 32.
  • Fluid under pressure is provided from a source thereof (not shown) through conduits 33 and 34 to the fixed or receiving end portion of the feed tube 23.
  • differential pressure is applied through conduits 35 and 36 to the end chambers 37 and 38, respectively, of the power control valve spool shown generally at 40.
  • the structure of a flow control valve spool is well known in the prior art and, for example, detailed description thereof may be found in the above referenced patents.
  • Generally movement of the valve spool 41 in response to differential pressure thereacross in the end chambers 37 and 38 as indicated by the arrow 42, causes fluid under pressure to flow through the conduits 33, and 43 or 44 to an actuator connected to cylinder ports 45 and 46 depending upon the direction of movement of the valve 41.
  • a feedback spring 47 which is affixed to the armature 14.
  • the manner in which the feed tube is rigidly affixed to the body 25 is illustrated.
  • the end 51 of the feed tube is rigidly affixed as by brazing or the like to an opening 52 provided in the retainer 24.
  • the retainer 24 defines a bevelled surface 53 which mates with a bevelled shoulder 54 defined by the bore 55 into which the retainer 24 is inserted.
  • the retainer 24 defines a reentrant bore 56 which receives a cup-shaped member 57 defining a restriction orifice 58, the function of which is well known in the art.
  • a plug 59 is also received within the bore 55 and is utilized to force the surface 53 into engagement with the shoulder 54 thereby effecting a metal-to-metal seal against the leakage of fluid under pressure. This function is accomplished through the shoulder 62 which abuts the end edge 63 of the retainer 24. A lock screw 64 is then threaded into the bore 55 and urges the plug 59 against the retainer 24 thereby causing the entire assembly to firmly seat in place. A wire screen filter 65 is seated within a reduced diameter area of the retainer 24 and is also held in place by the plug 59.
  • Fluid under pressure enters the body 25 through an opening 66 provided therein.
  • An auxiliary opening 67 is also provided in the body and communicates between the opening 66 and the reentrant bore 56 provided in the retainer 24 through the openings 68 formed in the rear edge 63 of the retainer 24.
  • valve spool 41 is slidably disposed within a sleeve 71 which is seated within a bore 72 provided in the body 25.
  • the sleeve 71 is provided with a land 73 which provides a seal about an opening 74 defined by the body 25 and through which the feedback spring 47 passes.
  • the land 73 is relieved to provide an opening 75 through which the feedback spring 47 also passes.
  • the feedback spring 47 terminates in a ball 76 which is disposed within an opening 77 provided in the spool valve 41.
  • the feed tube is positioned solely within the body of the housing thus eliminating the usual external plumbing to provide fluid under pressure to the feed tube.
  • the spring clip 26 comprises a body section 81 terminating in one end portion 82 which is wrapped around the flapper 21 and is rigidly affixed thereto as by brazing or the like.
  • the body 81 terminates in a second end portion 83 which is bent so as to provide a V-shaped section with the body portion 81.
  • the body 81 and the end portion 83 each define axially aligned openings therethrough and through which the feed tube 23 is disposed.
  • the end portion 83 may be compressed toward the body section 81 to align the various portions of the apparatus.
  • the end portion 83 may be released and the spring tension of the body portion 81 and the end portion 83 moving outwardly causes the spring clip 26 to grip the feed tube 23 and holds it firmly in place with respect to the flapper 21.
  • the axes of the feed tube 23 and the flapper 21 are offset and nonintersecting.
  • valve spool 41 is shown to have a central land 91 having sealing edges 92 and 93 which engage the sleeve 71 to provide the isolation between the jet pipe stage and the power valve stage as above described. It should also be particularly noted that the axes of the flapper 21 and feedback spring 47 are aligned.
  • the receiver port means 32 is received within a bore 94 defined in the body portion 25 of the housing.
  • the receiver port means 32 maybe rotated about its axis 95 as shown by arrow 96.
  • the receiver port means may be moved axially within the bore 94.
  • Ajet pipe servovalve comprising:
  • a housing having a body portion
  • a torque motor mounted on said body portion and including a movable member adapted for pivotal movement in response to electrical signals applied thereto, said member defining a first longitudinal axis;
  • a feed tube mounted in said body portion, separate from said movable member, adapted to receive fluid under pressure, having a receiving end portion and an ejecting end portion and defining a second longitudinal axis, said second axis being angularly positioned with respect to said first axis and offset therefrom so that said axes do not intersect;
  • receiver port means positioned adjacent said ejector end portion of said feed tube for receiving fluid ejected therefrom, said receiver port means being rotatable to effect adjustment;
  • control valve connected to receive fluid pressure from said receiver port means and to move responsively thereto to control the flow of fluid from a source thereof to a load;

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Servomotors (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Automatic Assembly (AREA)

Abstract

Disclosed is a jet pipe-type servo valve wherein the feed tube is disposed angularly with respect to a flapper to which it is affixed and which is movable by a torque motor the armature of which is connected to the flapper. The feed tube has one end thereof affixed rigidly to the housing and the other end thereof terminating in a nozzle which is positioned adjacent a receiver. The output ports of the receiver are connected to the end chambers of a cylinder within which a power control valve is slidably positioned so as to control the flow of fluid under pressure from a source thereof to an apparatus to be positioned such as an actuator. The jet pipe stage and the power control valve stage are isolated from each other.

Description

l nited States Patent 33 emu 771 UB5 2 6 7 3 n av. a T h nnfl w i 8W0 n FSC a 789 A 666 999 w MUM .m m a 1 1 v\. 7204 I U 4276 m 2638 n 334 3333 P.
Attorney-Nilsson, Robbins. Wills & Berliner [73] Assignee Bell Aerospace Corporation [54] JET PIPE SERVO VALVE ABSTRACT: Disclosed is a jet pipe-type servo valve wherein 1 Claim, 4 Drawing Figs.
the feed tube is disposed angularly with respect to a flapper to which it is affixed and which is movable by a torque motor the armature of which is connected to the flapper. The feed tube has one end thereof affixed rigidly to the housing and the other end thereof terminating in a nozzle which is positioned adjacent a receiver, The output ports of the receiver are connected to the end chambers of a cylinder within which a power control valve is slidably positioned so as to control the flow of References Cited fluid under pressure from a source thereof to an apparatus to UNITED STATES PATENTS be positioned such as an actuator. The jet pipe stage and the 2/|962 Gordon power control valve stage are isolated from each other.
JET PIPE SERVO VALVE BACKGROUND OF THE INVENTION Jet pipe servovalves have long been known and typical examples of such apparatus are shown in U.S. Pat. Nos. 2,884,906; 2,884,907; 2,996,072 and 3,017,864. As can be seen from these prior art patents, typical jet pipe servovalves are constructed in such a manner that the feed tube and the armature of the torque motor are an integral unit or at the most the feed tube is axially an extension of the torque motor armature. As a result the degree of movement of the nozzle tip, which terminates the feed tube, is limited by the amount of movement of the armature in the torque motor. Furthermore, alignment between the jet pipe nozzle orifice and the receiver ports is somewhat difficult to obtain and there is little or no adjustment available.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic diagram shown in perspective of a jet pipe servovalve constructed in accordance with the present invention;
FIG. 2 is a cross-sectional view of the servovalve illustrated in FIG. 1, taken about the line 2-2;
FIG. 3 is a fragmentary cross-sectional view taken about the line 3-3 ofFIG. 2; and
FIG. 4 is a cross-sectional view taken about the line 44 of F IG. 2.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to FIG. 1 there is illustrated a jet pipe servovalve which includes a torque motor 11 having pole pieces 12 and 13 with an armature 14 disposed therebetween. A pair of coils 15 and 16 are disposed to received an input signal upon leads 17 thereby to provide movement of the armature and, as indicated by the arrow 18, which is proportional to the magnitude of the input signal.
A flapper 21 is rigidly connected to the armature 14 so as to move as indicated by the arrow 20 in response to movement of the armature 14. The flapper 21 is suspended within a torque tube 22 so as to provide a seal between the fluid sections of the servovalve and the torque motor. Such a suspension is well known and, for example, is illustrated in U.S. Pat. No. 3,221,760. A feed tube 23 has one end thereof rigidly affixed to a retainer member 24 which in turn is rigidly affixed to the body portion 25 of the housing. The feed tube 23 is constructed of a hollow flexure tube which is movable with respect to the housing. Movement is imparted to the tube 23 by way of a flexible connection such as the link or spring clip 26 which is rigidly affixed to the flapper 21, but is releasably attached to the tube 23 by being inserted through an opening 27 defined by the clip 26. Thus, as the flapper 21 moves the feed tube 23 also is caused to move as indicated by the arrow 28. As is illustrated by the difference in arrows 20 and 28, the mechanical interconnection provides amplification of movement of the nozzle tip as compared to the flapper 21. Thus, small armature movement results in larger nozzle tip movement. The feed tube terminates in an ejector end having a nozzle 29 which is positioned adjacent openings 31 in a receiver port means 32.
Fluid under pressure is provided from a source thereof (not shown) through conduits 33 and 34 to the fixed or receiving end portion of the feed tube 23. As the nozzle 29 moves with respect to the receiver ports 31, differential pressure is applied through conduits 35 and 36 to the end chambers 37 and 38, respectively, of the power control valve spool shown generally at 40. The structure ofa flow control valve spool is well known in the prior art and, for example, detailed description thereof may be found in the above referenced patents. Generally movement of the valve spool 41 in response to differential pressure thereacross in the end chambers 37 and 38 as indicated by the arrow 42, causes fluid under pressure to flow through the conduits 33, and 43 or 44 to an actuator connected to cylinder ports 45 and 46 depending upon the direction of movement of the valve 41. As the valve 41 thusly moves, such movement is transmitted by way of a feedback spring 47 which is affixed to the armature 14.
Referring now more particularly to FIG. 2, the manner in which the feed tube is rigidly affixed to the body 25 is illustrated. As is therein illustrated, the end 51 of the feed tube is rigidly affixed as by brazing or the like to an opening 52 provided in the retainer 24. The retainer 24 defines a bevelled surface 53 which mates with a bevelled shoulder 54 defined by the bore 55 into which the retainer 24 is inserted. The retainer 24 defines a reentrant bore 56 which receives a cup-shaped member 57 defining a restriction orifice 58, the function of which is well known in the art. It should be understood that the restriction orifice is used only in instances of high fluid pressure where it is deemed desirable to drop some pressure prior to the fluid reaching the nozzle orifice. A plug 59 is also received within the bore 55 and is utilized to force the surface 53 into engagement with the shoulder 54 thereby effecting a metal-to-metal seal against the leakage of fluid under pressure. This function is accomplished through the shoulder 62 which abuts the end edge 63 of the retainer 24. A lock screw 64 is then threaded into the bore 55 and urges the plug 59 against the retainer 24 thereby causing the entire assembly to firmly seat in place. A wire screen filter 65 is seated within a reduced diameter area of the retainer 24 and is also held in place by the plug 59. Fluid under pressure enters the body 25 through an opening 66 provided therein. An auxiliary opening 67 is also provided in the body and communicates between the opening 66 and the reentrant bore 56 provided in the retainer 24 through the openings 68 formed in the rear edge 63 of the retainer 24.
As is also illustrated in FIG. 2, the valve spool 41 is slidably disposed within a sleeve 71 which is seated within a bore 72 provided in the body 25. The sleeve 71 is provided with a land 73 which provides a seal about an opening 74 defined by the body 25 and through which the feedback spring 47 passes. The land 73 is relieved to provide an opening 75 through which the feedback spring 47 also passes. As is illustrated, the feedback spring 47 terminates in a ball 76 which is disposed within an opening 77 provided in the spool valve 41. As is clear from FIGS. 1 and 2, the feed tube is positioned solely within the body of the housing thus eliminating the usual external plumbing to provide fluid under pressure to the feed tube.
By reference to FIG. 3, a more detailed understanding in the manner which the feed tube 23 is connected to the flapper 21 can be had. As is therein shown, the spring clip 26 comprises a body section 81 terminating in one end portion 82 which is wrapped around the flapper 21 and is rigidly affixed thereto as by brazing or the like. The body 81 terminates in a second end portion 83 which is bent so as to provide a V-shaped section with the body portion 81. The body 81 and the end portion 83 each define axially aligned openings therethrough and through which the feed tube 23 is disposed. The end portion 83 may be compressed toward the body section 81 to align the various portions of the apparatus. Once such alignment has occurred, the end portion 83 may be released and the spring tension of the body portion 81 and the end portion 83 moving outwardly causes the spring clip 26 to grip the feed tube 23 and holds it firmly in place with respect to the flapper 21. As can clearly be seen the axes of the feed tube 23 and the flapper 21 are offset and nonintersecting.
Referring now more particularly to FIG. 4, various details, as above described, are further illustrated and particularly the valve spool 41 is shown to have a central land 91 having sealing edges 92 and 93 which engage the sleeve 71 to provide the isolation between the jet pipe stage and the power valve stage as above described. It should also be particularly noted that the axes of the flapper 21 and feedback spring 47 are aligned.
As is illustrated, particularly in FIGS. 1 and 2, the receiver port means 32 is received within a bore 94 defined in the body portion 25 of the housing. To accomplish alignment between the receiver ports 31 and the nozzle 29 orifice the receiver port means 32 maybe rotated about its axis 95 as shown by arrow 96. Also the receiver port means may be moved axially within the bore 94. Thus, once the feed tube is positioned within the body portion 25 of the housing and afflxed to the flapper 21, the receiver ports may be adjusted to effect the desired null balance relationship (assuming no input signal to the torque motor).
What is claimed is:
1. Ajet pipe servovalve comprising:
a housing having a body portion;
a torque motor mounted on said body portion and including a movable member adapted for pivotal movement in response to electrical signals applied thereto, said member defining a first longitudinal axis;
a feed tube mounted in said body portion, separate from said movable member, adapted to receive fluid under pressure, having a receiving end portion and an ejecting end portion and defining a second longitudinal axis, said second axis being angularly positioned with respect to said first axis and offset therefrom so that said axes do not intersect;
means fixedly securing said receiving end portion of said feed tube to said body portion;
flexible link means securing said feed tube to said member thereby to cause said ejection and portion of said feed tube to move responsive to pivotal movement of said member;
receiver port means positioned adjacent said ejector end portion of said feed tube for receiving fluid ejected therefrom, said receiver port means being rotatable to effect adjustment;
a control valve connected to receive fluid pressure from said receiver port means and to move responsively thereto to control the flow of fluid from a source thereof to a load; and
means isolating the fluid in said control valve area from the fluid in said ejection-receiver port area.

Claims (1)

1. A jet pipe servovalve comprising: a housing having a body portion; a torque motor mounted on said body portion and including a movable member adapted for pivotal movement in response to electrical signals applied thereto, said member defining a first longitudinal axis; a feed tube mounted in said body portion, separate from said movable member, adapted to receive fluid under pressure, having a receiving end portion and an ejecting end portion and defining a second longitudinal axis, said second axis being angularly positioned with respect to said first axis and offset therefrom so that said axes do not intersect; means fixedly securing said receiving end portion of said feed tube to said body portion; flexible link means securing said feed tube to said member thereby to cause said ejection and portion of said feed tube to move responsive to pivotal movement of said member; receiver port means positioned adjacent said ejector end portion of said feed tube for receiving fluid ejected therefrom, said receiver port means being rotatable to effect adjustment; a control valve connected to receive fluid pressure from said receiver port means and to move responsively thereto to control the flow of fluid from a source thereof to a load; and means isolating the fluid in said control valve area from the fluid in said ejection-receiver port area.
US3621880D 1969-06-13 1969-06-13 Jet pipe servo valve Expired - Lifetime US3621880A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US83304269A 1969-06-13 1969-06-13

Publications (1)

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US3621880A true US3621880A (en) 1971-11-23

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Application Number Title Priority Date Filing Date
US3621880D Expired - Lifetime US3621880A (en) 1969-06-13 1969-06-13 Jet pipe servo valve

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US (1) US3621880A (en)
JP (1) JPS505793B1 (en)
DE (1) DE2026089B2 (en)
FR (1) FR2052513A5 (en)
GB (1) GB1286378A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3701365A (en) * 1971-05-24 1972-10-31 Joseph T Abdo Slide valve
US5573036A (en) * 1996-01-11 1996-11-12 Sargent Controls & Aerospace/Dover Diversified Inc. Electro-hydraulic servovalve having mechanical feedback
US20130206260A1 (en) * 2010-07-29 2013-08-15 In-Lhc Servo-valve pilot stage and a two-stage servo-valve including such a stage
US8997624B1 (en) 2010-04-02 2015-04-07 Jansen's Aircraft Systems Controls, Inc. Jet pipe servo with flexure pivot
US20160033052A1 (en) * 2014-07-31 2016-02-04 Zodiac Hydraulics Servo valve with double mobile assembly
EP3098456A1 (en) * 2015-05-26 2016-11-30 Zodiac Hydraulics Servovale with pilot stage of the jet type

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3019805A (en) * 1960-09-06 1962-02-06 William F Stoesser Electro-hydraulic servo valve
US3324871A (en) * 1965-04-05 1967-06-13 Sperry Rand Corp Jet pipe regulator with null position adjustment
US3362423A (en) * 1964-06-29 1968-01-09 Pneumo Dynamics Corp Control valve with fluid diverter
US3386343A (en) * 1965-08-20 1968-06-04 Bell Aerospace Corp Dynamically constantly variable gain servocontrol system
US3437101A (en) * 1966-03-01 1969-04-08 Abex Corp Servovalve construction

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3019805A (en) * 1960-09-06 1962-02-06 William F Stoesser Electro-hydraulic servo valve
US3362423A (en) * 1964-06-29 1968-01-09 Pneumo Dynamics Corp Control valve with fluid diverter
US3324871A (en) * 1965-04-05 1967-06-13 Sperry Rand Corp Jet pipe regulator with null position adjustment
US3386343A (en) * 1965-08-20 1968-06-04 Bell Aerospace Corp Dynamically constantly variable gain servocontrol system
US3437101A (en) * 1966-03-01 1969-04-08 Abex Corp Servovalve construction

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3701365A (en) * 1971-05-24 1972-10-31 Joseph T Abdo Slide valve
US5573036A (en) * 1996-01-11 1996-11-12 Sargent Controls & Aerospace/Dover Diversified Inc. Electro-hydraulic servovalve having mechanical feedback
US8997624B1 (en) 2010-04-02 2015-04-07 Jansen's Aircraft Systems Controls, Inc. Jet pipe servo with flexure pivot
US20130206260A1 (en) * 2010-07-29 2013-08-15 In-Lhc Servo-valve pilot stage and a two-stage servo-valve including such a stage
US8967179B2 (en) * 2010-07-29 2015-03-03 Zodiac Hydraulics, Societe Par Actions Simplifiee Servo-valve pilot stage and a two-stage servo-valve including such a stage
US20160033052A1 (en) * 2014-07-31 2016-02-04 Zodiac Hydraulics Servo valve with double mobile assembly
US9677682B2 (en) * 2014-07-31 2017-06-13 Zodiac Hydraulics Servo valve with double mobile assembly
EP3098456A1 (en) * 2015-05-26 2016-11-30 Zodiac Hydraulics Servovale with pilot stage of the jet type
US20160348805A1 (en) * 2015-05-26 2016-12-01 Zodiac Hydraulics Enhanced pilot stage servovalve
FR3036765A1 (en) * 2015-05-26 2016-12-02 Zodiac Hydraulics SERVOVALVE PILOTAGE STAGE, WHICH CAN SERVE AS A FIRST FLOOR IN A SERVOVALVE WITH TWO FLOORS.
US10145490B2 (en) * 2015-05-26 2018-12-04 Zodiac Hydraulics Enhanced pilot stage servovalve

Also Published As

Publication number Publication date
DE2026089A1 (en) 1970-12-23
JPS505793B1 (en) 1975-03-07
GB1286378A (en) 1972-08-23
DE2026089B2 (en) 1974-04-04
DE2026089C3 (en) 1974-10-31
FR2052513A5 (en) 1971-04-09

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Owner name: HR TEXTRON INC., 25200 WEST RYE CANYON RD. VALENCI

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Effective date: 19820222