US1972852A - Power amplifying positioning device - Google Patents

Power amplifying positioning device Download PDF

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Publication number
US1972852A
US1972852A US581131A US58113131A US1972852A US 1972852 A US1972852 A US 1972852A US 581131 A US581131 A US 581131A US 58113131 A US58113131 A US 58113131A US 1972852 A US1972852 A US 1972852A
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United States
Prior art keywords
pilot
piston
sleeve
passage
cylinder
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Expired - Lifetime
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US581131A
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Joseph C Albright
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Elsag Bailey Inc
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Bailey Meter Co
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Publication date
Priority claimed from US498374A external-priority patent/US1922834A/en
Application filed by Bailey Meter Co filed Critical Bailey Meter Co
Priority to US581131A priority Critical patent/US1972852A/en
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    • 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
    • F15B9/00Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/02Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
    • F15B9/08Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
    • F15B9/10Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor in which the controlling element and the servomotor each controls a separate member, these members influencing different fluid passages or the same passage

Definitions

  • Fig. 3 is a section in plan along the line 3 3; in the direction of the arrows, of Fig. 2.
  • a casing 1 has cooperating therein a piston 2 which in turn encasesa sleevev member-3 carrying at its lower end the rotor 4 of a pump for providing hydraulicfluid under pressure.
  • a pilot 5 Within the sleeve member 3 and axially movable therein is a pilot 5 having lands spaced along the length of the pilot, cooperating with ports or passages through the sleeve member.

Description

Sept. 11, 1934. J c ALBmGHT 1,972,852
POWER AMPLIFYING POSITIONING DEVICE Original FiledNov. 26, 1930 3 V g i 4 k w l9 v I r 3 3 INVENTOR Joseph QAlbTight. 2 BY ATTO EY Patented Sept. 11, 1934 UNITED STATES PATENT. OFFICE.
POWER AMPLIFYING POSITIONING DEVICE Joseph C. Albright, Teaneck, N. J., assignor to Bailey Meter Company, a corporation of Dela- 3 Claims. '(Cl. 60-52) This invention relates in general to devices wherein the positioning of a member by a relatively weaker control force results in' the positioning of another member by an amplified or 5 relatively greater force to accomplish a useful position; but in any event the second member'is caused to move or to be positioned as the resultof a change in position of the first member, and with a force relatively greater than the force imparted to the first member.
The first member may be positioned or caused to depart from a given position through various causes; for example, by variations in pressure,
differential pressure, temperature, rate of fluid fiow, or in fact any variable factor or relation whose force is desirably magnified to position a second member requiring a .relatively greater force for such positioning. The second member so positioned may move an indicator or can be used to move a damper or valve or desirable regulable mechanism whose movement may or may 'not resultin a change in value of the factor which caused the initial movement of the first member. v
My invention resides in certain improvements and arrangement of parts, in such devices wherein many advantages are obtained.
One object'is to provide such a torque or power amplifier utilizing hydraulic power.
Another object is to arrange the hydraulic power producing and controlling parts in a single unit.
A further object is to provide means wherein the movement of the secondary member may bear a desirable relation to the movement of the primary member.
I A still 'further object is to provide a construction wherein the pilot'controlling the passage of hy2lraulic fluid moves axially relative 'to and .rotor 4, and capable of axial positioning through within the amplified power piston.
Another object is to provide a construction wherein the pump for providing hydraulic fluid. is located in and axially mo ved with the ampli-' 'fied power-piston.
,A' still further object are have the jmovma;
of the second member result in shuttingofl oi? the amplified power effective in causing such a movement.
With these and further objects in view I will now describe a preferred embodiment of my invention.
In the drawing:
Fig. 1 is an arrangement, partly diagrammatic and partly in sectional elevation of an embodiment of the invention wherein is shown a certain preferred arrangement of parts.
Fig. 2 is a sectional elevation along theline 2-2, in the direction of the arrows, of Fig. 1.
Fig. 3 is a section in plan along the line 3 3; in the direction of the arrows, of Fig. 2.
I have illustrated an arrangement wherein an amplified power piston is located concentric with and movable axially relativeto a pilot, and wherein means for providing hydraulic fluid under pressure for positioning the power piston is located in and axially positioned with the power piston.
A casing 1 has cooperating therein a piston 2 which in turn encasesa sleevev member-3 carrying at its lower end the rotor 4 of a pump for providing hydraulicfluid under pressure. Within the sleeve member 3 and axially movable therein is a pilot 5 having lands spaced along the length of the pilot, cooperating with ports or passages through the sleeve member. I
I have shown the pilot 5 capable of being positioned axially in the assembly by variations in pressure of a fluid in a duct 6 effective at the pipe 7 upon a Bourdon tube 8 and through the intermediary of a linkage 9. The link 9, pivotally connected to the pilot 5 for positioning the same, further carries an extension forming a pointer 9A cooperating withan index 9B, for advising the value of the fluid pressure and/or of the position axially of the pilot 5.
To overcome a tendency toward resistance to axial positioning of the pilot 5 I preferably rotate the sleeve 3, and in so doing eifect an operation of the pump rotor 4. Such rotation is obtained from a motor shown at 10, driving through suitable gearing a shaft 11 carrying thereon a worm 12 meshing with and driving a worm wheel 13 splihedto the sleeve 3 at 14. The sleeve member 3 is thus continually rotated, driving the pump the medium of the spline 14.
Thepump as shown'more in detail in Fig. 3
hasa stationary part 15 of the piston 2 forming ashield between the rotor'4 and a rotor 16, the
between its ends and moves in effect relative to the cylinder 1 as the piston is vertically positioned in the cylinder. A passage 19 permits hydraulic fluid, preferably oil, to enter the pump from the reservoir v18. The oil is'then discharged, when needed, through a passage 20 to an annular channel 21 around the sleeve member 3, said channel having an opening at one or more points through the sleeve to the interior of the sleeve and between the lands of the pilot 5.
A passage 22communicates between the interior of the sleeve member 3 and that part of the cylinder 1 below the piston 2, while a passage 23 communicates between the interior of the sleeve member 3 and that part of the cylinder 1 lying abovethe piston 2. A drain is provided from the interior. of the sleeve 3 through a passage 24 to the reservoir 18 from below the pilot 5, while a drain from above the lands of the pilot 5 is provided through the passage 25 down through the pilot, to communicate to the space below the pilot and the drain connection 24.
Vertical motion or positioning of the piston 2 within the cylinder 1 is transmitted external of the cylinder through a rack 26 driving a pinion '27, the pinion having a shaft 28 extending through suitable fluid tight bushings externally to position an indicator 28A relative to an index 28B, or as shown in Fig. 1, through proper gearing, position a damper 29to control the pressure effective at the pipe 7. I d
In operation, a change in pressure within the duct 6 results in a movement of the Bourdon tube '8, and assuming that the pressure has increased, then the Bourdon tube tends to move counterclockwise and po'sitionsthe pilot downwardly so that the lands move downwardly out of alignment with the ports in the'sleeve'3. If the pump rotor 4 is being rotated byithe motor 10, then hydraulic fluid under pressure is available through the passage 20 and the annular chamber 21 at the interior of the sleeve 3 between the lands of the pilot 5 Immediately upon movement of the lands downwardly 'out of alignment with the ports, there will be a flow of hydraulic fluid through the passageway 23 to the upperside of the piston 2, and simultaneously a drainage of fluid from below the piston 2 through the passage 22, the opening 25 and the drain passage 24, all resulting in a downward movement of the piston 2 an amount proportional to the displacement of the pilot from its original position, The downward motion of the piston 2 results in a positioning of the ports opposite the lands to shut off flow of hydraulic fluid, as. well as rotation of the externally extending shaft 28 which may position an indicator 28A of the pressure effective at the pipe '7, or position a damper or valve means 29 to control such pressure. In any event, the shaft extension 28 is positioned to a definite point for each pressure within the range of operation, and with a power amplified over that available to position the pilot 5 through the linkage 9.
So long as the lands of the pilot 5 are aligned with the ports of the sleeve 3, no hydraulic fluid passes through the ports from the pump rotor 4, and assuming that the rotor is in continued rotation, then pressure developed thereby is relieved from passage 20 to reservoir 18 through a ballv valve 30 spring backed by a spring 31.
I have provided an amplified power positioning device wherein a relatively weaker control force positions a member to result in the positioning of a second member with greater force, thereby indie cating the positioning or movement of the first member as an indication of the position or variation in position or amount of a factor whose variation results in the relatively weaker control force; or the motion of the second member having rela tively greater power may accomplish useful work such as controlling the factor, or some other factor.
I preferably provide that a self-contained, compact unit is formed wherein the controlling pilot is surrounded by the amplified power piston which further carries the pump for supplying hydraulic fluid under pressure. It will 'be understood that I have illustrated and described a certain pre-. ferred embodiment of my invention, but that I am not to be limited thereby other than as claimed in view of prior art.
What I claim as new anddesire to secure by Letters Patent of the United States, is:
1. In a power amplifying mechanism, in combination, an axially movable pilot-capable of being positioned by a relatively weak control force, a rotatable and axially movable sleeve surrounding the pilot and having ports for the passage of hydraulic fluid, rotating means for said sleeve, a fluid pump fastened to said sleeve and operated thereby, an axially movable piston defining a casing for the sleeve and the pump and cooperating in a'cylinder, fluid passages in the piston, the i pilot arranged upon axial positioning to control passage of hydraulic fluid from the pump to the 1115 cylinder at one end or the other of the piston to cause a movement thereof, said movement effecting a closing of passage to said cylinder, the wall of said piston intermediate its ends defining with the wall of said cylinder a fluid storage space, and means extending external of the cylinder posi-' tioned by the piston.
2. In a power amplifying mechanism, in combination, a source of hydraulic fluid, a cylinder, a pilot for controlling passage of the hydraulic fluid to the cylinder, a piston positioned in the cylinder by the hydraulic fluid, the piston surrounding the pilot and capable of being positioned axially relative to the pilot, a pilot sleeve surrounding the pilot and adapted for axialmovement relative to the pilot, a fluid pump carried by the sleeve, and rotatingv means for the pilot sleeve. X
3. In combination, a member capable of, being positioned by a relatively weaker control force and comprising a pilot, fluid means controlled by the pilot to provide an amplified force, a piston positioned in a cylinder by said fluid means, the piston concentric with the pilot, a pilot "sleeve surrounding the pilot forming a casing therefor and adapted for axial movement relative thereto, a fluidpump carried by the sleeve, and rotating means for the sleeve.
JOSEPH C. ALBRIGH'I'.
US581131A 1930-11-26 1931-12-15 Power amplifying positioning device Expired - Lifetime US1972852A (en)

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US581131A US1972852A (en) 1930-11-26 1931-12-15 Power amplifying positioning device

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US498374A US1922834A (en) 1930-11-26 1930-11-26 Pressure measuring device
US581131A US1972852A (en) 1930-11-26 1931-12-15 Power amplifying positioning device

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE741199C (en) * 1939-01-08 1943-11-06 Aeg Control slide for hydraulic power amplifier
US2420649A (en) * 1944-06-14 1947-05-20 Harry B Breedlove Hydraulic torque amplifier
US2456211A (en) * 1940-10-22 1948-12-14 Bendix Aviat Corp Fluid pressure servomotor
US2466041A (en) * 1943-03-30 1949-04-05 Sperry Corp Servo system and control thereof
US2505887A (en) * 1944-12-11 1950-05-02 Lockheed Aircraft Corp Control for fluid-pressure actuated devices
US2769660A (en) * 1951-09-15 1956-11-06 Gen Motors Corp Thermostat
US2904075A (en) * 1953-07-13 1959-09-15 Hagan Chemicals & Controls Inc Pilot assemblies including a low pressure valve and a high pressure valve actuated by a piston in the low pressure valve

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE741199C (en) * 1939-01-08 1943-11-06 Aeg Control slide for hydraulic power amplifier
US2456211A (en) * 1940-10-22 1948-12-14 Bendix Aviat Corp Fluid pressure servomotor
US2466041A (en) * 1943-03-30 1949-04-05 Sperry Corp Servo system and control thereof
US2420649A (en) * 1944-06-14 1947-05-20 Harry B Breedlove Hydraulic torque amplifier
US2505887A (en) * 1944-12-11 1950-05-02 Lockheed Aircraft Corp Control for fluid-pressure actuated devices
US2769660A (en) * 1951-09-15 1956-11-06 Gen Motors Corp Thermostat
US2904075A (en) * 1953-07-13 1959-09-15 Hagan Chemicals & Controls Inc Pilot assemblies including a low pressure valve and a high pressure valve actuated by a piston in the low pressure valve

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