US2475445A - Servomotor with rotary input and rectilinear output - Google Patents

Servomotor with rotary input and rectilinear output Download PDF

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US2475445A
US2475445A US710361A US71036146A US2475445A US 2475445 A US2475445 A US 2475445A US 710361 A US710361 A US 710361A US 71036146 A US71036146 A US 71036146A US 2475445 A US2475445 A US 2475445A
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piston
cylinder
inlet
servo
ports
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Charles D Chidgey
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Vickers Inc
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Vickers Inc
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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

  • 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 pump and another as a fluid motor.
  • the invention is particularly concerned with servo-motors of the reciprocating piston type and controls therefor.
  • the general practice in designing servo-motor control circuits is to provide any standard type directional valve for selectively porting operating fluid to either end of the servo-cylinder.
  • the general object of this invention is to provide a servo-motor in which the directional valve is an integral part of the servo-motor elements.
  • valves One of the common types of directional valves employed is the spool or sleeve valve. Such valves are controlled by axial movement of the spool or sleeve.
  • An object of the proposed invention is to provide a combination spool and sleeve valve in which the valve is controlled by rotary movement of the sleeve.
  • Servo-circuits employing directional valves normally provide for full strokes of the servo-piston in either direction.
  • a follow-up control is necessary.
  • the piston travel is initiated by rotation of the sleeve a predetermined distance.
  • the porting of operating fluid to or from the cylinder is blocked and the piston stops.
  • Another object of the invention is to provide a servo-valve in which ports and passages in the sleeve and piston cooperate to control the direction and distance of travel of the servo-piston.
  • Still another object is to provide a servo-valve in which the piston operates to perform a follow-up function and terminate its own travel at any selected position.
  • the proposed valving device includes a rotatable cylinder or sleeve provided with inlet and outlet ports in combination with a piston containing helical passages adapted to -be brought into register with the inlet and outlet ports by rotation of the sleeve.
  • the ports are blocked by the piston body as the helical groove is moved axially out of register with the ports.
  • the limitations of such a valve requires that the piston length be greater than the length of stroke and the cylinder length approximately equal to the sum of the piston and stroke length. In the proposed design, the piston length is less than the length of the stroke and the cylinder length is considerably more than the sum of the two.
  • Another object of the invention is to provide a valve of the type described wherein the piston may be shorter than the length of stroke.
  • inlet and outlet ports are required and have been located on the internal bore of the cylinder along a helical line similar in form to the passage or groove in the piston.
  • separate valving means are provided between the cylinder and the body.
  • Another object of the invention is to provide multiple inlet and outlet ports in the cylinder progressivelycooperating with the helical piston groove and blocked by separate valving means when the piston moves out of contact with the por s.
  • Figure 1 is a top plan View of a servo-motor incorporating a preferred form of the invention.
  • Figure 2 is a section on line 2-2 of Figure 1.
  • Figure 3 is an end elevation and Figure 4 a plan view of the cylinder or valve sleeve.
  • Figure 5 is a section on line 5-5 of Figure 2.
  • Figure 6 is a section on line 66 of Figure 2.
  • Figure 7 is a section on line l-'l of Figure 2.
  • Figure 8 is a section on line 8-8 of Figure 2.
  • Figure 9 is a schematic view of a servo-controlled variable displacement pump.
  • Figure 10 is a developed view of the internal and external surfaces of the cylinder showing the ports in relation to the piston groove in its central position.
  • Figures 11 and 12 are similar to Figure 10, but
  • Figure 13 is a diagrammatic view of the method employed in developing the illustration in Figures 10, 11 and 12.
  • the servo-motor I 4 comprises a piston l6 re- 3 ciprocably mounted in a sleeve or cylinder I8 which in turn is rotatably mounted in the body 20.
  • a cap 22, carrying the control lever 24, is fastened to the sleeve I8 by screws 26.
  • the piston I6 is mechanically coupled by rod 28 and link 30, to the yoke 32 of pump 34 ( Figure 9).
  • the pump 34 is driven by a prime mover 36 through shaft 88 and is provided with pressure and return conduits 40 and 42 connected to a power transmission not shown. Hydraulic pressure fluid for operating servo I4 is supplied by the auxiliary pump 44 through conduit 46 when driven by belt 48 from the shaft 36.
  • Hydraulic fluid is supplied to pump 44 through suction conduit 50 from tank 52 and excess delivery is relieved through conduit 54 and relief valve 56.
  • the conduit 58 serves as a drain line for the easing 60 of pump 34 and as a discharge or outlet conduit for servo I4 which discharges directly into the pump casing 60.
  • variable displacement pumps of the rotary cylinder type employing axially reciprocable pistons mounted in a swinging yoke 32
  • the position of the yoke 32 determines the direction of flow through the conduits 40 and 62.
  • the degree of deflection either side of the central position, controls the amount of displacement.
  • the pump is operating maximum capacity and pressure fluid is delivered through conduit 32 and suction is obtained through conduit ee.
  • the servo-piston I6 is'a differential reciprocating piston type having a rod end 62 and head end 64 exposed to pressure in working chambers 66 and 68, respectively, of the cylinder I8.
  • Pressure conduit 46 communicates with servo-body 20 at connection which is further connected by means of passages I2 and 14 to pressure ports 16 and I8 on the internal bore 80 on body ( Figure 2).
  • Port 16 communicates with annular groove 82 in cylinder I8 which in turn connects by means of radial passage 84 to axial passage 86.
  • Axial passage 88 communicates at one end with the working chamber 66 and the rod end of servo-piston I6 by means of radial passage 88 and at the other end with inlet port 90 of cylinder I8.
  • Tank slot 94 may be rotated into communication with outlet port 86 of body 20 (see Figure 6) and thereby connected by passage 98 to slot I00 ( Figure 7).
  • Slot I00 opens into annular tank groove I02 which is connected to the pump case and tank 52 by means of radial passage I04 and axial passage I08 in the sleeve I8.
  • Axial tank passage 98 extends beyond slot I00 to connect with tank port H0 in body 20.
  • a second set of control ports is located in cylinder I8 at a point nearer the head end working chamber 68. It comprises the inlet or pressure port H2 and the outlet or tank port H4 ( Figure 8).
  • Inlet port II2 connects through peripheral slot II8 which in turn is connected by passage II8 ( Figure 4) to annular groove I20 and to pressure balancing slot I22 through passage I24.
  • Outlet port I I4 is connected to peripheral slot I26 by means of diagonal slot I28 ( Figure l0).
  • Servo-piston I6 is provided with two identical helical grooves I30 and I32 interconnected by radial passage-I34.
  • the helical grooves extend from a point in the piston periphery adjacent the rod end 62 to the head end 64 and communicate with the head end working chamber 68 of cylinder I8.
  • The-body 20 is drilled and plugged at I36 and I38 in order to form outlet ports 86 and H0, respectively, connected with axial passage 88.
  • a set screw I40 is threaded through body 20 and adapted to bottom against the annular groove I02 ( Figure 1) for the purpose of locking the cylinder I8 in rotation and fixing the servo position thereby maintaining constant pump delivery.
  • Sealing ring I08 ( Figure 2) is fixed to the cylinder I8 by machine screw I42 and supports the bearing I44 in the retainer I45.
  • the servo-motor Iii is fastened to the pump casing 60 by means of bolts through flange I46. Between the cap 22 and body 28, a suitable hydraulic packing I48 is provided which is urged into position by spring I50.
  • the helical groove I30 is diagrammatically shown positioned between the inlet ports and land the outlet ports 92 and H4 in Figure 10.
  • the cross-sectional view shown in Figures 6 and 8 illustrate the same condition. If the inlet ports and H2 in Figure 10 were moved upwardly into communication with helical groove I30 (similar to rotating cylinder I8 counterlockwise in Figures 6 and 8) then pressure fluid would be directed to working chamber 68 against the head of the piston I8. At the same time, operating pressure fluid is constantly present in the rod end 82 or working chamber 66 as communicated thereto by passage 12, port 16, annular groove 82, passages 84, 86 and 88. However, piston I6 being provided with differential areas, equal pressure in both chambers 66 and 68 will move the piston I8 to the left.
  • the helical groove I30 is shown adjacent both sets of inlet and outlet ports.
  • the piston I8 travels to the left as described above, it will reach a point where the head end 64 moves beyond the inlet and outlet ports H2 and H4. If ports H2 and H4 were the only ports used, the piston travel would stop as soon as the ports were out of contact with the helical groove I30. Therefore, it would be necessary to increase the length of the piston or as has been done in this invention, an additional set of ports was provided separated axially from the first set.
  • the multiple inlet ports or multiple outlet ports are located along a helical line parallel to the helical groove in the piston.
  • the working chamber 68 is thus drained by means of hellcal groove I30, port 92, slot 94, passage 98, passage 9B ( Figure 6), passage I00, annular groove Hi2, radial passage I04, axial passage I06 ( Figure '2), pump casing 60, and conduit 58 to tank 52.
  • the above described communication to tank is employed when the servo-piston i8 is in its left position ( Figure 11).
  • discharge is accomplished by means of helical groove I30, outlet port H4, slots tit and H26, tank port ill! in the body 20 to axial passage 98 and then by passage it"), etc., to tank as described in the preceding sentence.
  • Helical grooves i3! and H32 in piston 96 are diametrically opposite each other and since they are interconnected by passage ltd, pressure in both grooves is equal thereby providing pressure balance.
  • the flow of pressure fluid from or to the chamber 68 may be directly via groove E30 (the shortest and the usual path of flow) or indirectly via groove H30, passage I34, and groove 63%.
  • a graduated rotary operating means may control and axially position the ion-- gitudinal movement of a servo-piston with a short length of servo-cylinder. This is accomplished by means of helical grooves in the servopiston in cooperation with a multiple ported rotatable servo-cylinder Provided with passages adapted to be blocked by the servo-motor body at predetermined points.
  • a servo-motor control comprising a cylinder provided with a set of inlet and outlet ports on its internal bore, a piston reciprocably mounted in the cylinder and providedwith a helical groove in the surface of the piston and adapted to communicate with the cylinder at one end of the piston, means for rotating and angularly displacing the cylinder and piston and selectively connecting the helical groove with the inlet or outlet ports, whereby the piston will travel until the groove is moved axially out of contact with the port, and a second set of inlet and outlet ports in the cylinder axially displaced from the first set for providing a set of ports adjacent the helical groove regardless of the position of the piston in the cylinder.
  • a stroke. control for a servo-motor comprising a. cylinder rotatively mounted in a housing, a dverentlal servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the differential piston to a pressure fluid source, inlet and outlet ports on the internal bore of the cylinder in combination with a helical groove in the piston surface communicating with the opposite end of the differential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the groove whereby the piston will travel axially and block communication with th port, and additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston during its entire travel.
  • a stroke control for a, servo-motor comprising a cylinder rotatively mounted in a housing, a differential servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the differential piston to a pressure fiuid source,
  • inlet and outlet ports on the internal bore of the cylinder in combination with a helical groove in the piston surface communicating with the opposite end of the differential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the. groove whereby the piston will travel axially and block communication with the port, and additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston during its entire travel, the inlet ports and the outlet ports bein angularly and axially disposed along a path on the internal 'bore of the cylinder having a helical form and of the same magnitude as the helical groove.
  • a stroke control for a servo-motor comprising a cylinder rotatively mounted in a housing, a diiferential servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the difierential piston to a pressure fluid source, inlet and outlet ports on the internal bore of the cylinder in combination with a helical groove in the piston surface communicating with the opposite end of the diflerential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the groove whereby the piston will travel axially and block communication with the port, additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston during its entire travel, and means for blocking the inlet and outlet ports not adjacent the piston when the piston has traveled to a point beyond the ports.
  • a stroke control for a servo-motor comprising a cylinder rotatively mounted in a housing, a differential servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the differential piston to a pressure fluid source, inlet and outlet ports on the internal bore of the cylinder in combination 'with a helical 7 groove in the piston surface communicating with the opposite end of the diilerential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the groove whereby .the piston will travel axially and block communication with the port, additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston durin its entire travel, and inlet and outlet passages in the housing positioned for communicating with their respective inlet and outlet ports of the cylinder only during that phase of the servo operation during which the respective inlet and outlet ports are in contact with the piston.
  • a valving device comprising a helical groove communicating with an operating chamber and located in the surface of one of the elements in combination with a plurality of inlet and outlet ports dispersed along a helical path parallel to the groove in the other element whereby the relative rotation of the elements will selectively connect the operating chamber to at least one of the inlet or outlet ports for driving the piston axially through the cylinder, and valving means for blocking the inlet and outlet ports connected to the operating chamber by means other than the helical groove.
  • a servo-motor employing a, cylinder rotatively positioned in a housing and a reciprocating piston mounted therein and requiring a piston stroke greater than the length of the piston, a plurality of inlet ports located along a helical path on the internal bore of the cylinder, a plurality of outlet ports along a parallel helical path but circumferentially separated from the inlet ports a predetermined distance to form a land therebetween, a helical groove in the surface of the piston extending to one end thereof and having a width approximately equal, to the circumferential distance separating the inlet and outlet ports and normally positioned against the 8 land between the inlet and outlet ports when the servo-piston is stopped, and means for rotatively adjusting the relative position of the cylinder and piston to port pressure fluid along the groove to the cylinder.
  • a servo-motor employing a cylinder rotatively positioned in a housing and a reciprocating piston mounted therein and requiring a piston stroke greater than the length of the piston, a plurality of inlet ports located along a helical path on the internal bore of the cylinder, a plurality of outlet ports along a parallel helical path but circumferentially separated from the inlet ports a predetermined distance to form a land therebetween, a helical groove in the surface of the piston extending to one end thereof and having a width approximately equal to the circumierential distance separating the inlet and outlet ports and normally positioned against the land between the inlet and outlet ports when the servo-piston is stopped, and means for rotatively adjusting the relative position of the cylinder and piston to port pressure fluid along the groove to the cylinder, inlet and outlet ports in the housing adapted to be rotated into communication with the inlet and outlet ports in the cylinder only during the period the cylinder ports are ad- Jacent the piston and capable of

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
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  • General Engineering & Computer Science (AREA)
  • Reciprocating Pumps (AREA)

Description

ZAYEJMS July 5, WM. 0. D. CHIDGEY SERVOMOTOR WITH ROTARY INPUT AND RECTILINEAR OUTPUT 3 Sheets-Sheet 1 Filed NOV. 16, 1946 Fl 6. 4 INVENTOR.
CHARLES 0. CH DGEY C. D. CHIDGEY SERVOMOTOR WITH ROTARY I 2,475A45 mu? AND RECTILINEAR OUTPUT Filed NOV. 1G, 194% INVENTOR. CHARLES D. CHID GEY 3 Sheets-Sheet 2 3 Shasta-Sheet D. CHIDGEY SERVOMOTOR WITH ROTARY INPUT AND RECTILINEAB OUTPUT IL. T
mmvroza. CHARLES E). CHIDGEY HTTURNELH Filed Nov. 16, 1
a... July 5, 1949 SERVOMOTOR WITH ROTARY INPUT AND RECTILINEAR OUTPUT Charles D. Chidgey, Detroit, Mich., assignor to Vickers Incorporated, Detroit, Mich., a corporation of Michigan Application November 16, 1946, Serial No. 710,361
8 Claims.
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 pump and another as a fluid motor.
The invention is particularly concerned with servo-motors of the reciprocating piston type and controls therefor. The general practice in designing servo-motor control circuits is to provide any standard type directional valve for selectively porting operating fluid to either end of the servo-cylinder.
The general object of this invention is to provide a servo-motor in which the directional valve is an integral part of the servo-motor elements.
One of the common types of directional valves employed is the spool or sleeve valve. Such valves are controlled by axial movement of the spool or sleeve.
An object of the proposed invention is to provide a combination spool and sleeve valve in which the valve is controlled by rotary movement of the sleeve.
Servo-circuits employing directional valves normally provide for full strokes of the servo-piston in either direction. When partial movement of the piston is desired, a follow-up control is necessary. In the proposed valve device, the piston travel is initiated by rotation of the sleeve a predetermined distance. When the piston has traveled the selected distance in accordance with the setting of the sleeve, the porting of operating fluid to or from the cylinder is blocked and the piston stops. v
Therefore, another object of the invention is to provide a servo-valve in which ports and passages in the sleeve and piston cooperate to control the direction and distance of travel of the servo-piston.
Still another object is to provide a servo-valve in which the piston operates to perform a follow-up function and terminate its own travel at any selected position.
The proposed valving device includes a rotatable cylinder or sleeve provided with inlet and outlet ports in combination with a piston containing helical passages adapted to -be brought into register with the inlet and outlet ports by rotation of the sleeve. The ports are blocked by the piston body as the helical groove is moved axially out of register with the ports. To carry out the above principle, it is necessary that the ports be adjacent the piston at all times, otherwise, the ports would be in direct communication with the cylinder when the piston moved beyond the ports. Therefore, the limitation of such a valve requires that the piston length be greater than the length of stroke and the cylinder length approximately equal to the sum of the piston and stroke length. In the proposed design, the piston length is less than the length of the stroke and the cylinder length is considerably more than the sum of the two.
Therefore, another object of the invention is to provide a valve of the type described wherein the piston may be shorter than the length of stroke.
To accomplish this, multiple inlet and outlet ports are required and have been located on the internal bore of the cylinder along a helical line similar in form to the passage or groove in the piston. In order to block the inlet and outlet port as the piston moves beyond their location, separate valving means are provided between the cylinder and the body.
Another object of the invention is to provide multiple inlet and outlet ports in the cylinder progressivelycooperating with the helical piston groove and blocked by separate valving means when the piston moves out of contact with the por s.
Further objects and advantages of the present invention will be apparent from the following description, reference being had to the accompanying drawings wherein a preferred form of the present invention is clearly shown.
In the drawings:
Figure 1 is a top plan View of a servo-motor incorporating a preferred form of the invention.
Figure 2 is a section on line 2-2 of Figure 1.
Figure 3 is an end elevation and Figure 4 a plan view of the cylinder or valve sleeve.
Figure 5 is a section on line 5-5 of Figure 2.
Figure 6 is a section on line 66 of Figure 2.
Figure 7 is a section on line l-'l of Figure 2.
Figure 8 is a section on line 8-8 of Figure 2.
Figure 9 is a schematic view of a servo-controlled variable displacement pump.
Figure 10 is a developed view of the internal and external surfaces of the cylinder showing the ports in relation to the piston groove in its central position.
. Figures 11 and 12 are similar to Figure 10, but
illustrating the helical piston groove in its extreme left and extreme right position, respectively.
Figure 13 is a diagrammatic view of the method employed in developing the illustration in Figures 10, 11 and 12.
The servo-motor I 4 comprises a piston l6 re- 3 ciprocably mounted in a sleeve or cylinder I8 which in turn is rotatably mounted in the body 20. A cap 22, carrying the control lever 24, is fastened to the sleeve I8 by screws 26. The piston I6 is mechanically coupled by rod 28 and link 30, to the yoke 32 of pump 34 (Figure 9). The pump 34 is driven by a prime mover 36 through shaft 88 and is provided with pressure and return conduits 40 and 42 connected to a power transmission not shown. Hydraulic pressure fluid for operating servo I4 is supplied by the auxiliary pump 44 through conduit 46 when driven by belt 48 from the shaft 36. Hydraulic fluid is supplied to pump 44 through suction conduit 50 from tank 52 and excess delivery is relieved through conduit 54 and relief valve 56. The conduit 58 serves as a drain line for the easing 60 of pump 34 and as a discharge or outlet conduit for servo I4 which discharges directly into the pump casing 60.
In variable displacement pumps of the rotary cylinder type employing axially reciprocable pistons mounted in a swinging yoke 32, the position of the yoke 32, either side of the neutral or central position (as illustrated by 32 in dotted line of Figure 9), determines the direction of flow through the conduits 40 and 62. The degree of deflection, either side of the central position, controls the amount of displacement. In other words, with yoke 32 in its extreme left position as shown in dotted lines in Figure 9, the pump is operating maximum capacity and pressure fluid is delivered through conduit 32 and suction is obtained through conduit ee. When the yoke 32 is in its extreme right-hand position as shown in dotted line, it is delivering at maximum capacity, but conduit 42 has become the suction conduit and 40 the pressure conduit of power transmission. When the yoke 32 is in its central or neutral position as shown in Figure 9, the displacement of pump 38 is zero. Therefore, by controlling the position of servo-motor piston I8, the displacement of pump 34 may be selectively varied.
The servo-piston I6 is'a differential reciprocating piston type having a rod end 62 and head end 64 exposed to pressure in working chambers 66 and 68, respectively, of the cylinder I8. Pressure conduit 46 communicates with servo-body 20 at connection which is further connected by means of passages I2 and 14 to pressure ports 16 and I8 on the internal bore 80 on body (Figure 2). Port 16 communicates with annular groove 82 in cylinder I8 which in turn connects by means of radial passage 84 to axial passage 86. Axial passage 88 communicates at one end with the working chamber 66 and the rod end of servo-piston I6 by means of radial passage 88 and at the other end with inlet port 90 of cylinder I8.
Adjacent the inlet port 80 is an outlet or discharge port 92 which is connected to the peripheral slot 94 in cylinder I8. Tank slot 94 may be rotated into communication with outlet port 86 of body 20 (see Figure 6) and thereby connected by passage 98 to slot I00 (Figure 7). Slot I00 opens into annular tank groove I02 which is connected to the pump case and tank 52 by means of radial passage I04 and axial passage I08 in the sleeve I8. Axial tank passage 98 extends beyond slot I00 to connect with tank port H0 in body 20.
A second set of control ports is located in cylinder I8 at a point nearer the head end working chamber 68. It comprises the inlet or pressure port H2 and the outlet or tank port H4 (Figure 8). Inlet port II2 connects through peripheral slot II8 which in turn is connected by passage II8 (Figure 4) to annular groove I20 and to pressure balancing slot I22 through passage I24. Outlet port I I4 is connected to peripheral slot I26 by means of diagonal slot I28 (Figure l0).
Servo-piston I6 is provided with two identical helical grooves I30 and I32 interconnected by radial passage-I34. The helical grooves extend from a point in the piston periphery adjacent the rod end 62 to the head end 64 and communicate with the head end working chamber 68 of cylinder I8.
The-body 20 is drilled and plugged at I36 and I38 in order to form outlet ports 86 and H0, respectively, connected with axial passage 88. A set screw I40 is threaded through body 20 and adapted to bottom against the annular groove I02 (Figure 1) for the purpose of locking the cylinder I8 in rotation and fixing the servo position thereby maintaining constant pump delivery. Sealing ring I08 (Figure 2) is fixed to the cylinder I8 by machine screw I42 and supports the bearing I44 in the retainer I45. The servo-motor Iii is fastened to the pump casing 60 by means of bolts through flange I46. Between the cap 22 and body 28, a suitable hydraulic packing I48 is provided which is urged into position by spring I50.
In operation, the starting position is illustrated in Figures 1 to 10 inclusive. The pump yoke is shown in its neutral position in Figure 9 and the relative position of cylinder IE3 and piston to together with the porting arrangement are illustrated in the other figures.
The helical groove I30 is diagrammatically shown positioned between the inlet ports and land the outlet ports 92 and H4 in Figure 10. The cross-sectional view shown in Figures 6 and 8 illustrate the same condition. If the inlet ports and H2 in Figure 10 were moved upwardly into communication with helical groove I30 (similar to rotating cylinder I8 counterlockwise in Figures 6 and 8) then pressure fluid would be directed to working chamber 68 against the head of the piston I8. At the same time, operating pressure fluid is constantly present in the rod end 82 or working chamber 66 as communicated thereto by passage 12, port 16, annular groove 82, passages 84, 86 and 88. However, piston I6 being provided with differential areas, equal pressure in both chambers 66 and 68 will move the piston I8 to the left.
As the piston moves to the left, the helical groove will tend to move away from inlet ports 90 and I I2. When the travel is sufficient to block communication between the pressure ports 90 and H2 and the helical groove I30, no further travel of the piston will be permitted. However, if the sleeve or cylinder I8 is rotated still further, the piston I6 will continue its travel in the same direction so long as the inlet ports 90 and H2 are in communication with the helical groove.
In Figure 10, the helical groove I30 is shown adjacent both sets of inlet and outlet ports. When the piston I8 travels to the left as described above, it will reach a point where the head end 64 moves beyond the inlet and outlet ports H2 and H4. If ports H2 and H4 were the only ports used, the piston travel would stop as soon as the ports were out of contact with the helical groove I30. Therefore, it would be necessary to increase the length of the piston or as has been done in this invention, an additional set of ports was provided separated axially from the first set.
The multiple inlet ports or multiple outlet ports are located along a helical line parallel to the helical groove in the piston.
By duplicating the ports, a further difilculty arises for as the piston travels beyond the ports, they would be out of control of the helical groove and provide direct communication to pressure and to tank. In the present design, slots H8 and lit (Figure 8) have been provided which are rotated out of communication with pressure and tank port 18 and H0, respectively, in the body and thereby block inlet port H2 and outlet port lit when piston it has moved beyond the location as illustrated in Figure 11. When the cylinder or sleeve valve 20 is rotated clockwise, the tank ports 92 and ill are shifted into communication with the helical groove I30. The working chamber 68 is thus drained by means of hellcal groove I30, port 92, slot 94, passage 98, passage 9B (Figure 6), passage I00, annular groove Hi2, radial passage I04, axial passage I06 (Figure '2), pump casing 60, and conduit 58 to tank 52. The above described communication to tank is employed when the servo-piston i8 is in its left position (Figure 11). When in the right end of the cylinder i8, discharge is accomplished by means of helical groove I30, outlet port H4, slots tit and H26, tank port ill! in the body 20 to axial passage 98 and then by passage it"), etc., to tank as described in the preceding sentence.
When the pressure in working chamber 63 has been relieved to tank, the force on the rod end iii of piston it drives the servo-motor to the right. When the piston has traveled sufilciently to the right to have moved out of contact with inlet and outlet ports 90 and 9'2, respectively, then the outlet or tank port 92 must'be blocked by separate valving means. Since working chamber 66 is constantly under full operating pressure, the uncovering of port 90 by the axial piston travel makes no difierence. As to the tank port 92, cylinder it with groove 94 is rotated clockwise until tank port 95 in body 20 is blocked (Figure 6).
Helical grooves i3! and H32 in piston 96 are diametrically opposite each other and since they are interconnected by passage ltd, pressure in both grooves is equal thereby providing pressure balance. The flow of pressure fluid from or to the chamber 68 may be directly via groove E30 (the shortest and the usual path of flow) or indirectly via groove H30, passage I34, and groove 63%.
It will thus be seen that the present invention has provided a servo-motor and follow-up control system in which a graduated rotary operating means may control and axially position the ion-- gitudinal movement of a servo-piston with a short length of servo-cylinder. This is accomplished by means of helical grooves in the servopiston in cooperation with a multiple ported rotatable servo-cylinder Provided with passages adapted to be blocked by the servo-motor body at predetermined points.
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: a
1. A servo-motor control comprising a cylinder provided with a set of inlet and outlet ports on its internal bore, a piston reciprocably mounted in the cylinder and providedwith a helical groove in the surface of the piston and adapted to communicate with the cylinder at one end of the piston, means for rotating and angularly displacing the cylinder and piston and selectively connecting the helical groove with the inlet or outlet ports, whereby the piston will travel until the groove is moved axially out of contact with the port, and a second set of inlet and outlet ports in the cylinder axially displaced from the first set for providing a set of ports adjacent the helical groove regardless of the position of the piston in the cylinder.
2. A stroke. control for a servo-motorcomprising a. cylinder rotatively mounted in a housing, a diilerentlal servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the differential piston to a pressure fluid source, inlet and outlet ports on the internal bore of the cylinder in combination with a helical groove in the piston surface communicating with the opposite end of the differential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the groove whereby the piston will travel axially and block communication with th port, and additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston during its entire travel.
3. A stroke control for a, servo-motor comprising a cylinder rotatively mounted in a housing, a differential servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the differential piston to a pressure fiuid source,
inlet and outlet ports on the internal bore of the cylinder in combination with a helical groove in the piston surface communicating with the opposite end of the differential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the. groove whereby the piston will travel axially and block communication with the port, and additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston during its entire travel, the inlet ports and the outlet ports bein angularly and axially disposed along a path on the internal 'bore of the cylinder having a helical form and of the same magnitude as the helical groove.
4. A stroke control for a servo-motor comprising a cylinder rotatively mounted in a housing, a diiferential servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the difierential piston to a pressure fluid source, inlet and outlet ports on the internal bore of the cylinder in combination with a helical groove in the piston surface communicating with the opposite end of the diflerential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the groove whereby the piston will travel axially and block communication with the port, additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston during its entire travel, and means for blocking the inlet and outlet ports not adjacent the piston when the piston has traveled to a point beyond the ports.
5. A stroke control for a servo-motor comprising a cylinder rotatively mounted in a housing, a differential servo-piston reciprocably mounted in the cylinder, passages connecting the rod end of the differential piston to a pressure fluid source, inlet and outlet ports on the internal bore of the cylinder in combination 'with a helical 7 groove in the piston surface communicating with the opposite end of the diilerential piston, means for rotating the cylinder thereby moving the inlet or outlet port into communication with the groove whereby .the piston will travel axially and block communication with the port, additional inlet and outlet ports spaced axially along the internal bore of the cylinder to provide at least one inlet and one outlet port adjacent the helical groove of the piston durin its entire travel, and inlet and outlet passages in the housing positioned for communicating with their respective inlet and outlet ports of the cylinder only during that phase of the servo operation during which the respective inlet and outlet ports are in contact with the piston.
6. In a servo-motor, a cylinder element and a piston element reciprocably mounted therein, means for angularly displacing the cylinder and piston by relative rotation, a valving device comprising a helical groove communicating with an operating chamber and located in the surface of one of the elements in combination with a plurality of inlet and outlet ports dispersed along a helical path parallel to the groove in the other element whereby the relative rotation of the elements will selectively connect the operating chamber to at least one of the inlet or outlet ports for driving the piston axially through the cylinder, and valving means for blocking the inlet and outlet ports connected to the operating chamber by means other than the helical groove. '7. In a servo-motor employing a, cylinder rotatively positioned in a housing and a reciprocating piston mounted therein and requiring a piston stroke greater than the length of the piston, a plurality of inlet ports located along a helical path on the internal bore of the cylinder, a plurality of outlet ports along a parallel helical path but circumferentially separated from the inlet ports a predetermined distance to form a land therebetween, a helical groove in the surface of the piston extending to one end thereof and having a width approximately equal, to the circumferential distance separating the inlet and outlet ports and normally positioned against the 8 land between the inlet and outlet ports when the servo-piston is stopped, and means for rotatively adjusting the relative position of the cylinder and piston to port pressure fluid along the groove to the cylinder.
8. In a servo-motor employing a cylinder rotatively positioned in a housing and a reciprocating piston mounted therein and requiring a piston stroke greater than the length of the piston, a plurality of inlet ports located along a helical path on the internal bore of the cylinder, a plurality of outlet ports along a parallel helical path but circumferentially separated from the inlet ports a predetermined distance to form a land therebetween, a helical groove in the surface of the piston extending to one end thereof and having a width approximately equal to the circumierential distance separating the inlet and outlet ports and normally positioned against the land between the inlet and outlet ports when the servo-piston is stopped, and means for rotatively adjusting the relative position of the cylinder and piston to port pressure fluid along the groove to the cylinder, inlet and outlet ports in the housing adapted to be rotated into communication with the inlet and outlet ports in the cylinder only during the period the cylinder ports are ad- Jacent the piston and capable of porting operating fluid into or out of the helical groove.
CHARLES D. CHIDGEY.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 788,006 Wilkinson Apr, 25, 1905 840,877 Steedman Jan. 8, 1907 1,484,030 Kitchen Feb. 19, 192% 1,848,698 Curtis Mar. 8, 1932 2,244,296 Heinrich June 3, 1941 FOREIGN PATENTS Number Country Date 464,891 Great Britain Apr. 27, 1937
US710361A 1946-11-16 1946-11-16 Servomotor with rotary input and rectilinear output Expired - Lifetime US2475445A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1101963B (en) * 1957-06-28 1961-03-09 Kloeckner Humboldt Deutz Ag Hydraulic booster
DE1262777B (en) * 1962-09-12 1968-03-07 Boelkow Gmbh Hydraulic amplifier, in particular a hydraulically power-amplified actuator
FR2203943A1 (en) * 1972-10-21 1974-05-17 Mitsubishi Metal Mining Co Ltd

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US788006A (en) * 1904-08-24 1905-04-25 Wilkinson Turbine Company Compound marine turbine.
US840877A (en) * 1905-12-04 1907-01-08 George F Steedman Fluid-actuated cushioned hoist.
US1484030A (en) * 1923-01-30 1924-02-19 Kitchen John George Aulsebrook Means for controlling motion in fluid-pressure apparatus
US1848698A (en) * 1932-03-08 curtis
GB464891A (en) * 1935-08-22 1937-04-27 Messerschmitt Boelkow Blohm Improved arrangements for actuating a power member in accordance with the movement of a control member
US2244296A (en) * 1937-07-22 1941-06-03 Bosch Gmbh Robert Servomotor

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1848698A (en) * 1932-03-08 curtis
US788006A (en) * 1904-08-24 1905-04-25 Wilkinson Turbine Company Compound marine turbine.
US840877A (en) * 1905-12-04 1907-01-08 George F Steedman Fluid-actuated cushioned hoist.
US1484030A (en) * 1923-01-30 1924-02-19 Kitchen John George Aulsebrook Means for controlling motion in fluid-pressure apparatus
GB464891A (en) * 1935-08-22 1937-04-27 Messerschmitt Boelkow Blohm Improved arrangements for actuating a power member in accordance with the movement of a control member
US2244296A (en) * 1937-07-22 1941-06-03 Bosch Gmbh Robert Servomotor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1101963B (en) * 1957-06-28 1961-03-09 Kloeckner Humboldt Deutz Ag Hydraulic booster
DE1262777B (en) * 1962-09-12 1968-03-07 Boelkow Gmbh Hydraulic amplifier, in particular a hydraulically power-amplified actuator
FR2203943A1 (en) * 1972-10-21 1974-05-17 Mitsubishi Metal Mining Co Ltd

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