US3416409A - Pneumatic double-acting control devices - Google Patents

Pneumatic double-acting control devices Download PDF

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Publication number
US3416409A
US3416409A US602369A US60236966A US3416409A US 3416409 A US3416409 A US 3416409A US 602369 A US602369 A US 602369A US 60236966 A US60236966 A US 60236966A US 3416409 A US3416409 A US 3416409A
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Prior art keywords
piston
chamber
housing
compartments
acting control
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US602369A
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Labat Pierre
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Societe Anonime de Vehicules Industriels et dEquipements SA SAVIEM
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Societe Anonime de Vehicules Industriels et dEquipements SA SAVIEM
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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
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/06Servomotor systems without provision for follow-up action; Circuits therefor involving features specific to the use of a compressible medium, e.g. air, steam
    • F15B11/072Combined pneumatic-hydraulic systems
    • F15B11/076Combined pneumatic-hydraulic systems with pneumatic drive or displacement and speed control or stopping by hydraulic braking

Definitions

  • a double-acting control device for use in such devices as pneumatic actuators comprising a double-acting hollow piston having opposite ends which are respectively acted upon by pressure conditions in opposite ends of a chamber, the piston cavity in turn being subdivided into two axially opposite sealed compartments by a rigid stationary partition connected "to the chamber housing, said piston cavity being defined by a rigid wall at one end of the piston and a flexible wall at its other end, damped flow being permitted between both piston compartments.
  • This invention is concerned with a double-acting control device and has specific reference to a pneumatic control piston-cylinder unit or actuator of which the primary characteristic is that it comprises a hydraulic damper incorporated in the control piston.
  • the device comprises a bell-shaped case 1 having at its open end a flanged edge to which a cover 2 is secured in a fluidtight manner.
  • the sealed chamber thus obtained is divided into two portions 3 and 4 by a double-acting piston 5 adapted to be actuated by compressed air at the proper time either from port 6 or from port 7.
  • This piston 5 has a particular design in that it is rigid with a rod 8 adapted to transmit the piston movements to the device to be actuated.
  • This rod 8 is slidably mounted through a suitable aperture 10 provided with a rod packing 9 in the end of said bellshaped member 1 which is opposite to the cover 2.
  • a skirt 11 of piston 5 Opposite to said piston rod 8 is a skirt 11 of piston 5 which slides with its outerfperiphery in a cylinderforming portion of the bell-shaped member 1, the inner portion of said skirt 11 sliding along a fixed piston 12 rigid with said cover 2.
  • the movable piston 5 is provided with a piston packing 13 and the fixed piston 12 with a piston packing 14.
  • a gauged orifice 16 is formed in the flange of the fixed piston 12.
  • a diaphragm has its central annular portion clamped between said fixed piston and the cover 2, and its outer peripheral portion is clamped between a ring and the edge of said skirt 11 which is opposite to the rod 8.
  • the fixed piston 12 constitutes a partition between chambers A and B filled with noncompressible hydraulic fluid, such as oil, any trace of gas being removed from these chambers.
  • This actuator operates as follows:
  • Air pressure will thus move the piston 5 in the direction of the arrow 17 and force liquid from chamber A to chamber B through the aforesaid gauged orifice 16, thus damping the resulting piston movement.
  • a double-acting control device for use in such devices as pneumatic actuators, comprising a housing defining a chamber having opposite axial ends, a doubleacting hollow piston slidably mounted within said chamber and dividing same into respective opposite end compartments sealed from each other, said piston being defined by a rigid wall at one end thereof defining one of said end compartments with said housing, and a flexible wall at the other end thereof defining the other of said end compartments with said housing, a rigid partition attached to said housing and being located within said piston between the end walls thereof and thereby dividing the piston cavity into separate sealed compartments, damping means providing restricted intercommunication in either direction between said piston compartments.
  • said damping means comprising an open bore of relatively small size extending through said partition between said piston compartments.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Damping Devices (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)

Description

Dec, 17, 1968 P. LABAT I PNEUMATIC DOUBLE-ACTING CONTROLIv DEVICES Filed Dec. 16, 1966 INVENTOR.
Wanna Lnsn r BTTOR M575 United States Patent Office 3,416,409 Patented Dec. 17, 1968 3,416,409 PNEUMATIC DOUBLE-ACTING CONTROL DEVICES Pierre Labat, Suresnes, France,fiassignor to Societe Anonyme de Vehicules Industriels et dEquipements Mecaniques Saviem, Suresnes, Hauts-de-Seine, France, a
corporation of France Filed Dec. 16, 1966, Ser. No. 602,369 Claims priority, application France, Jan. 27, 1966,
Claims. c1. 92-s ABSTRACT OF THE DISCLOSURE A double-acting control device for use in such devices as pneumatic actuators, comprising a double-acting hollow piston having opposite ends which are respectively acted upon by pressure conditions in opposite ends of a chamber, the piston cavity in turn being subdivided into two axially opposite sealed compartments by a rigid stationary partition connected "to the chamber housing, said piston cavity being defined by a rigid wall at one end of the piston and a flexible wall at its other end, damped flow being permitted between both piston compartments.
This invention is concerned with a double-acting control device and has specific reference to a pneumatic control piston-cylinder unit or actuator of which the primary characteristic is that it comprises a hydraulic damper incorporated in the control piston.
In the single figure of the attached drawing an axial section of the apparatus according to this invention is illustrated.
In thisspecific form of embodiment the device comprises a bell-shaped case 1 having at its open end a flanged edge to which a cover 2 is secured in a fluidtight manner.
The sealed chamber thus obtained is divided into two portions 3 and 4 by a double-acting piston 5 adapted to be actuated by compressed air at the proper time either from port 6 or from port 7. This piston 5 has a particular design in that it is rigid with a rod 8 adapted to transmit the piston movements to the device to be actuated. This rod 8 is slidably mounted through a suitable aperture 10 provided with a rod packing 9 in the end of said bellshaped member 1 which is opposite to the cover 2.
Opposite to said piston rod 8 is a skirt 11 of piston 5 which slides with its outerfperiphery in a cylinderforming portion of the bell-shaped member 1, the inner portion of said skirt 11 sliding along a fixed piston 12 rigid with said cover 2.
The movable piston 5 is provided with a piston packing 13 and the fixed piston 12 with a piston packing 14. A gauged orifice 16 is formed in the flange of the fixed piston 12.
A diaphragm has its central annular portion clamped between said fixed piston and the cover 2, and its outer peripheral portion is clamped between a ring and the edge of said skirt 11 which is opposite to the rod 8.
It will be noted that the fixed piston 12 constitutes a partition between chambers A and B filled with noncompressible hydraulic fluid, such as oil, any trace of gas being removed from these chambers.
This actuator operates as follows:
Assuming that the pressure in chamber 4 is p, compressed air is introduced through port 6 into chamber 3 at a pressure p, greater than p.
Air pressure will thus move the piston 5 in the direction of the arrow 17 and force liquid from chamber A to chamber B through the aforesaid gauged orifice 16, thus damping the resulting piston movement.
The liquid flowing from chamber A to chamber B causes the volume of this chamber B to increase and this increment is permitted by the possible displacement and distortion of diaphragm 15.
During the reverse movement, that is, in the direction of the arrow 18, assuming that chamber 3 is at a pressure p, compressed air is introduced through port 7 into chamber 4 at a pressure p' greater than p; this pressure p is exerted against the diaphragm 15 and thereby transmitted to the liquid contained in chamber B. Thus, the liquid in this chamber B flows back into chamber A through the gauged orifice 16 by damping the movement of the piston 5 which travels (in the direction of the arrow 18) as the volume of liquid increases in chamber A.
From the foregoing it will be noted that:
(a) No contact between the gas and liquid media can take place, thus avoiding any risk of emulsion.
In this respect, it will be seen that the provision of a diaphragm 15 ensures a perfect fluid-tightness between the fixed portion 12 and the movable portion 5 of the device. The permissible movement and distortion of this diaphragm avoid the use of sliding or rotary packings.
(-b) The liquid can expand freely in its cavity and the complete device is definitely fluid-tight.
(c) The absolute fluid-tightness of the device permits of dispensing with the use of an overflow reservoir, since the absence of leakages makes it unnecessary to make up for fluid losses.
Of course, the specific form of embodiment illustrated in the drawing and described hereinabove should not be construed as limiting the present invention since many modifications and variations may be brought thereto without departing from the spirit and scope of the invention.
Thus, notably, the surface area of piston 12 may be equal, superior or inferior to that of piston 5 in order to vary the magnitude of the damping action according to the direction of operation of the device.
I claim:
1. A double-acting control device for use in such devices as pneumatic actuators, comprising a housing defining a chamber having opposite axial ends, a doubleacting hollow piston slidably mounted within said chamber and dividing same into respective opposite end compartments sealed from each other, said piston being defined by a rigid wall at one end thereof defining one of said end compartments with said housing, and a flexible wall at the other end thereof defining the other of said end compartments with said housing, a rigid partition attached to said housing and being located within said piston between the end walls thereof and thereby dividing the piston cavity into separate sealed compartments, damping means providing restricted intercommunication in either direction between said piston compartments.
2. The double-acting control device of claim 1, wherein said housing has inner wall means defining said chamber, said partition being fixedly attached to said housing within said chamber and positioned at a point intermediate the ends thereof, said partition having an outer peripheral edge radially spaced inwards from said housing inner wall means, said double-acting hollow piston being axially slidable within said chamber, said piston having an outer wall portion slidable in sealed manner along said housing inner wall means and said piston having an inner wall portion slidable in sealed manner along the outer peripheral edge of said partition, said piston defining a cavity between said rigid and flexiable walls, said partition being positioned within said piston cavity between said piston rigid and flexible walls and thereby dividing said piston cavity into two axially opposed compartments, said flexible wall being formed by a flexible diaphragm having an inner radial peripheral end sealingly attached to said housing and an outer radial peripheral end sealingly attached to said piston, said piston dividing said housing chamber into respective axially opposed compartments, port means leading through said housing into each of said housing compartments.
3. The control device of claim 2, said partition comprising a radial wall portion and an axially protruding central hub portion, said hub portion being rigidly secured to said housing and defining therewith an annular space, said inner radial peripheral end of said diaphragm being sealingly gripped between said housing and hub portion in said space.
4. The control device of claim 2, said compartments in said piston cavity being adapted to hold hydraulic fluid therein in sealed manner relative to said housing chamber, and said housing chamber compartments being adapted to hold pressurized gas therein in sealed manner relative to each other.
5. The control device of claim 2, said damping means comprising an open bore of relatively small size extending through said partition between said piston compartments.
References Cited UNITED STATES PATENTS 2,081,921 6/1937 Gartin 92-9 X 2,601,511 6/1952 Gaflney 929 X 2,860,608 11/1958 Hardy et al 928 X 3,081,743 3/1963 Bishop et a1. 92-9 FOREIGN PATENTS 548,272 9/ 1956 Italy.
MARTIN P. SCHWADRON, Primary Examiner.
I. C. COHEN, Assistant Examiner.
US. Cl. X.R.
US602369A 1966-01-27 1966-12-16 Pneumatic double-acting control devices Expired - Lifetime US3416409A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR47460A FR1474052A (en) 1966-01-27 1966-01-27 Double acting pneumatic control

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DE (1) DE1601756B2 (en)
FR (1) FR1474052A (en)
GB (1) GB1166819A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3750920A (en) * 1971-04-05 1973-08-07 Gilbert & Nash Co Inc Web guide

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2081921A (en) * 1934-08-22 1937-06-01 Sullivan Machinery Co Rock drill feeding mechanism
US2601511A (en) * 1948-08-17 1952-06-24 Fisher Governor Co Pneumatically operated diaphragm motor
US2860608A (en) * 1957-12-30 1958-11-18 Gen Electric Hydraulic reciprocating motion device
US3081743A (en) * 1961-04-12 1963-03-19 Akron Standard Mold Co Air actuated motor unit

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2081921A (en) * 1934-08-22 1937-06-01 Sullivan Machinery Co Rock drill feeding mechanism
US2601511A (en) * 1948-08-17 1952-06-24 Fisher Governor Co Pneumatically operated diaphragm motor
US2860608A (en) * 1957-12-30 1958-11-18 Gen Electric Hydraulic reciprocating motion device
US3081743A (en) * 1961-04-12 1963-03-19 Akron Standard Mold Co Air actuated motor unit

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3750920A (en) * 1971-04-05 1973-08-07 Gilbert & Nash Co Inc Web guide

Also Published As

Publication number Publication date
GB1166819A (en) 1969-10-08
DE1601756A1 (en) 1970-08-13
FR1474052A (en) 1967-03-24
DE1601756B2 (en) 1972-04-06

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