[go: up one dir, main page]

CN113389767B - Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof - Google Patents

Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof Download PDF

Info

Publication number
CN113389767B
CN113389767B CN202110833995.XA CN202110833995A CN113389767B CN 113389767 B CN113389767 B CN 113389767B CN 202110833995 A CN202110833995 A CN 202110833995A CN 113389767 B CN113389767 B CN 113389767B
Authority
CN
China
Prior art keywords
guide sleeve
cylinder cover
air inlet
air
cylinder
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.)
Active
Application number
CN202110833995.XA
Other languages
Chinese (zh)
Other versions
CN113389767A (en
Inventor
冯汉升
周亚琦
张硕
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hefei Institutes of Physical Science of CAS
Original Assignee
Hefei Institutes of Physical Science of CAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hefei Institutes of Physical Science of CAS filed Critical Hefei Institutes of Physical Science of CAS
Priority to CN202110833995.XA priority Critical patent/CN113389767B/en
Publication of CN113389767A publication Critical patent/CN113389767A/en
Application granted granted Critical
Publication of CN113389767B publication Critical patent/CN113389767B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/08Characterised by the construction of the motor unit
    • F15B15/14Characterised by the construction of the motor unit of the straight-cylinder type
    • F15B15/1423Component parts; Constructional details
    • 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
    • F15B13/021Valves for interconnecting the fluid chambers of an actuator
    • 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
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/08Characterised by the construction of the motor unit
    • F15B15/14Characterised by the construction of the motor unit of the straight-cylinder type
    • F15B15/1423Component parts; Constructional details
    • F15B15/1438Cylinder to end cap assemblies
    • 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
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/08Characterised by the construction of the motor unit
    • F15B15/14Characterised by the construction of the motor unit of the straight-cylinder type
    • F15B15/1423Component parts; Constructional details
    • F15B15/1471Guiding means other than in the end cap
    • 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
    • F15B19/00Testing; Calibrating; Fault detection or monitoring; Simulation or modelling of fluid-pressure systems or apparatus not otherwise provided for
    • 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
    • F15B21/00Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
    • F15B21/04Special measures taken in connection with the properties of the fluid
    • F15B21/041Removal or measurement of solid or liquid contamination, e.g. filtering
    • 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
    • F15B21/00Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
    • F15B21/08Servomotor systems incorporating electrically operated control means
    • F15B21/087Control strategy, e.g. with block diagram
    • 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
    • F15B2215/00Fluid-actuated devices for displacing a member from one position to another
    • F15B2215/30Constructional details thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Actuator (AREA)

Abstract

The invention relates to a double-acting pneumatic actuator with a long-stroke large-cylinder-diameter structure and a control system thereof. The pneumatic actuator comprises a front cylinder cover, a rear cylinder cover, a cylinder barrel, a front guide sleeve, a rear guide sleeve, a front throttle valve a, a rear throttle valve a, a piston, a front buffer plunger, a rear buffer plunger, a push rod guide sleeve and a push rod, wherein the cylinder barrel is arranged between the front cylinder cover and the rear cylinder cover, the front guide sleeve is arranged on the front cylinder cover, the rear guide sleeve is arranged on the rear cylinder cover, the front throttle valve a is arranged on the front guide sleeve, the rear throttle valve a is arranged on the rear guide sleeve, the piston is arranged in the cylinder barrel, and the front buffer plunger is arranged at the front end of the piston. The control system comprises an air inlet main pipeline, a first branch, a second branch, a third branch, a fourth branch and an exhaust main pipeline. The invention improves the space utilization rate of the device, ensures the running stability, the accuracy and the safety of the pneumatic actuator when the pneumatic actuator performs the high-thrust bidirectional movement, and prolongs the service life of the pneumatic system.

Description

Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof
Technical Field
The invention relates to the technical field of air and control, in particular to a double-acting pneumatic actuator with a long-stroke large-cylinder-diameter structure and a control system thereof.
Background
Large fusion devices are a major technological infrastructure project in which integrated engineering is being designed in China. The cryopump is used as one of key components of a vacuum system of a large fusion device, and is a direct place for adsorption and regeneration of discharge reaction products in a divertor chamber. During the operation of the plasma, the cryopump timely and efficiently pumps out the hydrogen, isotopes thereof, helium ash and other impurity particles in the divertor chamber, thereby providing a high vacuum environment for the stable operation of the plasma.
The opening and closing of the main valve are regulated by controlling the pneumatic actuating mechanism in the running process of the low-temperature pump, the required environment is provided for the adsorption and regeneration process of the low-temperature pump, and the pumping speed of the pump is regulated by precisely controlling the opening of the main valve. Therefore, whether the pneumatic actuator can safely and reliably operate directly affects the normal operation of the cryopump. The pneumatic actuator commonly used in commercial use is used on the main valve of the cryopump, and mainly has the following problems: (1) The main valve operates in the environment of high irradiation and strong magnetic field, and the electrical equipment contained in the pneumatic actuator is easy to fail, so that the pneumatic actuator cannot work normally; (2) The motion stroke of the main valve is longer, about 450mm, and the pretightening force required by the sealing at the main valve opening is larger, about 190kN, and the general pneumatic actuator cannot provide the larger sealing force required by the main valve under the working condition of longer stroke; (3) The motion of the main valve is horizontal reciprocating motion, and a common pneumatic actuator cannot provide bidirectional acting force.
Therefore, the double-acting pneumatic actuator with the long-stroke large-cylinder-diameter structure and the control system thereof are provided to meet the use requirement of the main valve of the low-temperature pump of the large fusion device, and are technical problems to be solved in the prior art.
Disclosure of Invention
In order to solve the technical problems, the invention aims to provide a double-acting pneumatic actuator with a long-stroke large-cylinder-diameter structure and a control system thereof, so as to realize accurate and effective opening and closing of a main valve of a low-temperature pump of a large fusion device.
In order to achieve the above purpose, the present invention provides the following technical solutions:
A double-acting pneumatic actuator with a long-stroke large-cylinder-diameter structure is characterized by comprising a front cylinder cover, a rear cylinder cover, a cylinder barrel, a front guide sleeve, a rear guide sleeve, a front throttle valve a, a rear throttle valve a, a piston, a front buffer plunger, a rear buffer plunger, a push rod guide sleeve and a push rod, wherein,
The cylinder barrel is arranged between the front cylinder cover and the rear cylinder cover, the front guide sleeve is arranged on the front cylinder cover, the rear guide sleeve is arranged on the rear cylinder cover, the front throttle valve a is arranged on the front guide sleeve, the rear throttle valve a is arranged on the rear guide sleeve, the piston is arranged in the cylinder barrel, the front buffer plunger is arranged at the front end of the piston, the rear buffer plunger is arranged at the rear end of the piston, the push rod guide sleeve is connected with the piston, the front buffer plunger and the rear buffer plunger, and the push rod is connected with the push rod guide sleeve.
Furthermore, an air inlet hole is formed in one side of the front cylinder cover, an air outlet hole is formed in the other side of the front cylinder cover, and a hanging ring is arranged on the front cylinder cover.
One side of the rear cylinder cover is provided with an air inlet hole, the air inlet hole and the air inlet hole on the front cylinder cover are positioned on the same side, the other side of the rear cylinder cover is provided with an air outlet hole, the air outlet hole and the air outlet hole on the front cylinder cover are positioned on the same side, the rear cylinder cover is provided with a lifting ring, and the lifting ring is collinear with the central line of the lifting ring on the front cylinder cover.
Furthermore, the cylinder barrel is fixedly connected with the front cylinder cover and the rear cylinder cover through stud bolts, and forms a closed cavity together with the front cylinder cover and the rear cylinder cover through sealing of a sealing element.
Further, two sealing grooves are formed in the opening of the front guide sleeve, a sealing piece is arranged between the front guide sleeve and the front cylinder cover to seal, an air inlet and an air outlet are formed in the front guide sleeve, and the opening and closing of the air inlet are controlled by adjusting the front throttle valve b.
The opening part of the rear guide sleeve is provided with two sealing grooves and bearing seat holes, a sealing piece is arranged between the rear guide sleeve and the rear cylinder cover for sealing, the rear guide sleeve is provided with an air inlet hole and an air outlet hole, and the opening and closing of the air inlet hole are controlled by adjusting the rear throttle valve b.
Further, the surfaces of the front throttle valve b and the rear throttle valve b are provided with threads and sealing grooves.
Further, a round hole is formed in the center of the piston and detachably connected with the push rod guide sleeve, and two sealing grooves e and guide ring grooves are formed in the outer side of the piston.
Further, the front buffer plunger and the rear buffer plunger are provided with damping surfaces, are detachably connected with the push rod guide sleeve, and are sealed by a sealing piece arranged between the front buffer plunger and the rear buffer plunger and the piston.
Furthermore, the push rod and the push rod guide sleeve are of tubular structures, and after being matched and installed, the central lines of the push rod and the push rod guide sleeve are collinear.
According to another aspect of the present invention, a control system using the pneumatic actuator described above is provided, comprising an intake main line, a first branch, a second branch, a third branch, a fourth branch, an exhaust main line, a gas source, a ball valve, a filter, a pressure setter, a pressure gauge, a safety valve, a three-way valve, and a muffler, wherein,
The air inlet main pipeline is connected with the air source, the first branch pipeline is connected with the air inlet main pipeline and the air inlet hole of the air cylinder cover in front of the pneumatic actuator, the second branch pipeline is connected with the air inlet main pipeline and the air inlet hole of the air cylinder cover in back of the pneumatic actuator, the third branch pipeline is connected with the air outlet hole of the air cylinder cover in front of the pneumatic actuator, the fourth branch pipeline is connected with the air outlet hole of the air cylinder cover in back of the pneumatic actuator, and the air outlet main pipeline is connected with the third branch pipeline and the fourth branch pipeline.
Further, the air inlet main pipeline is provided with a ball valve, a filter, a pressure constant value device and a pressure gauge. The first branch is provided with a pressure constant value device, a pressure gauge and a ball valve. The second branch is provided with a pressure constant value device, a pressure gauge and a ball valve. The third branch is provided with a ball valve and a pressure gauge. The fourth branch is provided with a ball valve and a pressure gauge. The exhaust main pipeline is provided with a three-way valve and a muffler.
The invention has the beneficial effects that:
The invention aims at improving the existing pneumatic actuator and a control system thereof, so that the pneumatic actuator can normally operate in the environment of high irradiation and strong magnetic field, and meets the use requirement of a main valve of a low-temperature pump of a large fusion device.
Drawings
The invention is further described below with reference to the accompanying drawings.
Fig. 1 is a schematic diagram showing a cross-sectional structure of a double-acting pneumatic actuator with a long stroke and large cylinder diameter structure.
Fig. 2 is a schematic diagram showing a cross-sectional structure of a double-acting pneumatic actuator with a long-stroke large-diameter structure.
Fig. 3 is a left side view of a double acting pneumatic actuator of a long stroke large bore configuration.
Fig. 4 is a partial enlarged view at a of fig. 1.
Fig. 5 is a partially enlarged view at B of fig. 1.
Fig. 6 is a schematic structural view of a pneumatic actuator piston.
Fig. 7 is a D-D view of fig. 6.
Fig. 8 is a partial enlarged view at C of fig. 2.
Fig. 9 is a schematic structural view of a cryopump of a large fusion device.
FIG. 10 is a schematic structural view of a control system for a pneumatic actuator.
The reference numerals include:
1-front cylinder head, 2-rear cylinder head, 3-cylinder barrel, 4-front guide sleeve, 5-rear guide sleeve, 6-front throttle valve a, 7-rear throttle valve a, 8-piston, 9-front buffer plunger, 10-rear buffer plunger, 11-push rod guide sleeve, 12-push rod, 13-front cylinder head air inlet hole, 14-rear cylinder head air inlet hole, 15-main valve, 16-front cylinder head air outlet hole, 17-rear cylinder head air outlet hole, 18-hanging ring, 19-stud, 20-seal groove a, 21-seal groove b, 22-front guide sleeve air inlet hole, 23-front guide sleeve air outlet hole, 24-front throttle valve b, 25-seal groove C, 26-sealing groove d, 27-rear guide sleeve air inlet hole, 28-rear guide sleeve exhaust hole, 29-rear throttle valve b, 30-bearing seat hole, 31-sealing groove e, 32-guide ring groove, 33-damping surface of buffer plunger, A1-pneumatic actuator, G1-air source, F1-filter, S1-muffler, V1-V5-ball valve, V6-safety valve, V7-three-way valve, C1-C3-pressure constant value device, P1-P5-pressure gauge, m 1-main air inlet pipeline, m 101-first branch, m 102-second branch, m 201-third branch, m 202-fourth branch, m 2-main air exhaust pipeline.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the present invention without making any inventive effort, are intended to fall within the scope of the present invention.
The embodiment provides a double-acting pneumatic actuator with a long-stroke large-cylinder-diameter structure and a control system thereof, which are pneumatic actuators and control systems thereof applied to a main valve of a low-temperature pump of a large fusion device. The aim of the invention can be achieved by the following technical scheme:
Referring to fig. 1 to 9, the long-stroke large-bore structure double-acting pneumatic actuator provided in this embodiment includes a front cylinder head 1, a rear cylinder head 2, a cylinder barrel 3, a front guide sleeve 4, a rear guide sleeve 5, a front throttle valve a6, a rear throttle valve a7, a piston 8, a front buffer plunger 9, a rear buffer plunger 10, a push rod guide sleeve 11, and a push rod 12. The cylinder barrel 3 is arranged between the front cylinder cover 1 and the rear cylinder cover 2, the front guide sleeve 4 is arranged on the front cylinder cover 1, the rear guide sleeve 5 is arranged on the rear cylinder cover 2, the front throttle valve a6 is arranged on the front guide sleeve 4, the rear throttle valve a7 is arranged on the rear guide sleeve 5, the piston 8 is arranged in the cylinder barrel 3, the front buffer plunger 9 is arranged at the front end of the piston 8, the rear buffer plunger 10 is arranged at the rear end of the piston 8, the push rod guide sleeve 11 is connected with the piston 8 and the front and rear buffer plungers 10, and the push rod 12 is connected with the push rod guide sleeve 11.
According to another embodiment of the invention, a control system of a pneumatic actuator is provided, which comprises an air inlet main pipeline m1, a first branch pipeline m101, a second branch pipeline m102, a third branch pipeline m201, a fourth branch pipeline m202, an air exhaust main pipeline m2, an air source G1, ball valves V1-V5, a filter F1, pressure positioners C1-C3, pressure gauges P1-P5, a safety valve V6, a three-way valve V7 and a muffler S1. The air inlet main pipeline m1 is connected with the air source, the first branch pipeline m101 is connected with the air inlet main pipeline m1 and an air inlet hole of the front cylinder cover 1 of the pneumatic actuator A1, the second branch pipeline m102 is connected with the air inlet main pipeline m1 and an air inlet hole of the rear cylinder cover 2 of the pneumatic actuator A1, the third branch pipeline m201 is connected with an air outlet hole of the front cylinder cover 1 of the pneumatic actuator A1, the fourth branch pipeline m202 is connected with an air outlet hole of the rear cylinder cover 2 of the pneumatic actuator A1, and the air outlet main pipeline is connected with the third branch pipeline m201 and the fourth branch pipeline m202, as shown in FIG. 10.
As shown in fig. 1, 2 and 3, in order to further optimize the above scheme, one side of the front cylinder head 1 of the pneumatic actuator A1 is provided with a front cylinder head air inlet hole 13, the other side is provided with a front cylinder head air outlet hole 16, one side of the rear cylinder head 2 of the pneumatic actuator A1 is provided with a rear cylinder head air inlet hole 14, which is positioned on the same side as the front cylinder head air inlet hole 13 on the front cylinder head 1, the other side is provided with a rear cylinder head air outlet hole 17, which is positioned on the same side as the front cylinder head air outlet hole 16 on the front cylinder head 1, in order to facilitate the lifting of the pneumatic actuator A1, the front cylinder head 1 and the rear cylinder head 2 are provided with lifting rings 18, and the central lines of the two lifting rings 18 are collinear.
In order to further optimize the scheme, the cylinder barrel 3 is fixedly connected with the front cylinder cover 1 and the rear cylinder cover 2 through stud bolts 19, and forms a closed cavity together with the front cylinder cover 1 and the rear cylinder cover through rubber sealing rings, and the cylinder barrel 3, the front cylinder cover 1 and the rear cylinder cover 2 are made of 304L stainless steel materials, as shown in figure 2.
In order to further optimize the scheme, the opening part of the front guide sleeve 4 is provided with two sealing grooves, a sealing groove a20 is provided with a sealing ring for sealing between the front guide sleeve 4 and the main valve 15, a sealing groove b21 is provided with a felt ring for preventing lubricating grease in a cylinder from leaking along with the movement of the main valve 15, a sealing ring is arranged between the front guide sleeve 4 and the front cylinder cover 1 for sealing, the front guide sleeve 4 is provided with a front guide sleeve air inlet hole 22 and a front guide sleeve air outlet hole 23, and the opening and closing of the air inlet hole are controlled by adjusting the front throttle valve b24, as shown in figures 1,2 and 4.
In order to further optimize the scheme, the opening part of the rear guide sleeve 5 is provided with two sealing grooves and a bearing seat hole 30, a sealing ring is arranged at the sealing groove c25 for sealing between the rear guide sleeve 5 and the push rod guide sleeve 11, a felt ring is arranged at the sealing groove d26 for preventing lubricating grease in the cylinder from leaking along with the movement of the main valve 15, a sealing piece is arranged between the rear guide sleeve 5 and the rear cylinder cover 2 for sealing, the bearing seat hole 30 is used for installing a linear motion bearing and storing lubricating grease required by the movement of the lubricating piston 8, a rear guide sleeve air inlet hole 27 and a rear guide sleeve air outlet hole 28 are arranged on the rear guide sleeve 5, and the opening and closing of the air inlet hole is controlled by adjusting the rear throttle valve b29 as shown in figures 1,2 and 5.
To further optimize the above solution, the front throttle b24 and the rear throttle b29 are provided with threads and sealing grooves on their surfaces.
In order to further optimize the scheme, the piston 8 is made of an aluminum alloy material, a round hole is formed in the center of the piston 8 and detachably connected with the push rod guide sleeve 11, two sealing grooves e31 and a guide ring groove 32 are formed in the outer side of the piston 8, a sealing ring is installed in the sealing groove e31 and used for sealing between the piston 8 and the cylinder barrel 3, a guide ring is installed in the guide ring groove 32 and used for guaranteeing stability of the piston 8 in reciprocating motion, and the guide ring is made of polytetrafluoroethylene composite materials, as shown in fig. 6 and 7.
In order to further optimize the above solution, during the operation of the piston 8, the cylinder end cover, the guide sleeve, etc. are easy to be damaged due to the impact, so that the damping surfaces 33 of the front buffer plunger 9 and the rear buffer plunger 10 are provided as buffer devices to reduce the impact, and the buffer plungers are detachably connected with the push rod guide sleeve 11, and are sealed with the piston 8 by a sealing ring.
In order to further optimize the scheme, the push rod 12 and the push rod guide sleeve 11 are of tubular structures, and after being matched and installed, the central lines of the push rod 12 and the push rod guide sleeve 11 are collinear, as shown in fig. 1.
In order to further optimize the above solution, the inlet main line m1 is provided with a ball valve V1, a filter F1, a pressure setter C1 and a pressure gauge P1. The first branch m101 is provided with a pressure setter C3, a pressure gauge P3 and a ball valve V3. The second branch m102 is provided with a pressure setter C2, a pressure gauge P2 and a ball valve V2. The third branch m201 is provided with a ball valve V5 and a pressure gauge P5. The fourth branch m202 is provided with a ball valve V4 and a pressure gauge P4. The exhaust main pipe is provided with a three-way valve V7 and a muffler S1 as shown in fig. 10.
When the main valve of the low-temperature pump of the large fusion device is required to be closed, the ball valves V1, V3, V4 and V7 are opened, the ball valves V2 and V5 are closed, so that clean and dry compressed air enters the front cylinder cover air inlet hole 13 of the front cylinder cover 1 through the air inlet main pipeline m1 and the first branch pipeline m101, the main valve 15 is driven to be closed through the piston 8, and the compressed air in the rear cavity is discharged to the environment through the fourth branch pipeline m202 and the air outlet main pipeline m 2. When the main valve 15 of the cryogenic pump of the large fusion device is required to be opened, the ball valves V3 and V4 are closed, the ball valves V1, V2, V5 and V7 are opened, so that clean and dry compressed air enters the air inlet hole 14 of the rear cylinder cover 2 through the main air inlet pipeline m1 and the second branch pipeline m102, the main valve 15 is driven to be opened through the piston 8, and the compressed air in the front cavity is discharged to the environment through the third branch pipeline m201 and the main air outlet pipeline m 2. Since the residual pressure of the discharged compressed air is high, strong noise is generated, and a muffler S1 is provided on the exhaust pipe to reduce noise pollution, thereby reducing exhaust noise. The safety valve V6 is always in operation during operation of the main valve 15, mainly to prevent the device from being damaged by the excessive pressure in the pipeline.
The foregoing is merely illustrative of the structure of this invention and many variations may be made in the specific embodiments and application scope by those skilled in the art based on the teachings herein without departing from its structure or its scope beyond the scope defined in the appended claims.

Claims (8)

1. The double-acting pneumatic actuator with the long-stroke large cylinder diameter structure is characterized by being a pneumatic actuator applied to a main valve of a low-temperature pump of a large fusion device, and comprises a front cylinder cover (1), a rear cylinder cover (2), a cylinder barrel (3), a front guide sleeve (4), a rear guide sleeve (5), a front throttle valve a (6), a rear throttle valve a (7), a piston (8), a front buffer plunger (9), a rear buffer plunger (10), a push rod guide sleeve (11) and a push rod (12),
The cylinder barrel (3) is arranged between the front cylinder cover (1) and the rear cylinder cover (2), the front guide sleeve (4) is arranged on the front cylinder cover (1), the rear guide sleeve (5) is arranged on the rear cylinder cover (2), the front throttle valve a (6) is arranged on the front guide sleeve (4), the rear throttle valve a (7) is arranged on the rear guide sleeve (5), the piston (8) is arranged in the cylinder barrel (3), the front buffer plunger (9) is arranged at the front end of the piston (8), the rear buffer plunger (10) is arranged at the rear end of the piston (8), the push rod guide sleeve (11) is connected with the piston (8) and the front buffer plunger (10), and the push rod (12) is connected with the push rod guide sleeve (11).
An air inlet hole is formed in one side of the front cylinder cover (1), an air outlet hole is formed in the other side of the front cylinder cover, and a hanging ring (18) is arranged on the front cylinder cover (1);
an air inlet hole is formed in one side of the rear cylinder cover (2), the air inlet hole of the rear cylinder cover is positioned on the same side as the air inlet hole of the front cylinder cover (1), an air outlet hole is formed in the other side of the rear cylinder cover, the air outlet hole of the rear cylinder cover is positioned on the same side as the air outlet hole of the front cylinder cover (1), a lifting ring (18) is arranged on the rear cylinder cover (2), and the lifting ring (18) is collinear with the central line of the lifting ring (18) on the front cylinder cover (1);
two sealing grooves are formed in the opening of the front guide sleeve (4), a sealing piece is arranged between the front guide sleeve (4) and the front cylinder cover (1) for sealing, an air inlet hole and an air outlet hole are formed in the front guide sleeve (4), and the opening and closing of the air inlet hole of the front guide sleeve are controlled by adjusting the front throttle valve b (24);
The opening part of the rear guide sleeve (5) is provided with two sealing grooves and bearing seat holes (30), a sealing piece is arranged between the rear guide sleeve (5) and the rear cylinder cover (2) for sealing, the rear guide sleeve (5) is provided with an air inlet hole and an air outlet hole, and the opening and closing of the air inlet hole of the rear guide sleeve are controlled by adjusting the rear throttle valve b (29).
2. A double-acting pneumatic actuator of a long-stroke large-bore structure according to claim 1, characterized in that the cylinder barrel (3) is fixedly connected with the front cylinder head (1) and the rear cylinder head (2) by stud bolts (19) and forms a closed chamber together with the front cylinder head (1) and the rear cylinder head (2) by sealing with a sealing element.
3. A double acting pneumatic actuator of long stroke large bore construction according to claim 1 wherein the front and rear throttle b (24, 29) surfaces are provided with threads and sealing grooves.
4. The double-acting pneumatic actuator with the long-stroke and large-cylinder-diameter structure according to claim 1, wherein a round hole is formed in the center of the piston (8), the piston is detachably connected with the push rod guide sleeve (11), and a sealing groove e (31) and a guiding ring groove (32) are formed in the outer side of the piston.
5. A double acting pneumatic actuator of long stroke large bore construction according to claim 1, characterized in that the front (9) and rear (10) buffer plungers are provided with damping surfaces, detachably connected to the push rod guide sleeve (11), and sealed with the piston (8) by a seal.
6. A double-acting pneumatic actuator of a long-stroke large-cylinder-diameter structure according to claim 1, characterized in that the push rod (12) and the push rod guide sleeve (11) are of tubular structures, and the central lines of the push rod (12) and the push rod guide sleeve are collinear after being matched and installed.
7. A control system for a double-acting pneumatic actuator with a long-stroke large-cylinder-diameter structure, which is applied to any one of claims 1 to 6, and is characterized by comprising an air inlet main pipeline (m 1), a first branch pipeline (m 101), a second branch pipeline (m 102), a third branch pipeline (m 201), a fourth branch pipeline (m 202), an air outlet main pipeline (m 2), an air source (G1), a ball valve, a filter (F1), a pressure constant device, a pressure gauge, a safety valve (V6), a three-way valve (V7) and a muffler (S1), wherein,
The air inlet main pipeline (m 1) is connected with the air source (G1), the first branch pipeline (m 101) is connected with an air inlet hole of the air inlet main pipeline (m 1) and an air inlet hole of the air cylinder cover (1) in front of the air actuator (A1), the second branch pipeline (m 102) is connected with the air inlet hole of the air inlet main pipeline (m 1) and an air inlet hole of the air cylinder cover (2) behind the air actuator, the third branch pipeline (m 201) is connected with an air outlet hole of the air cylinder cover (1) in front of the air actuator (A1), the fourth branch pipeline (m 202) is connected with an air outlet hole of the air cylinder cover (2) behind the air actuator (A1), and the air outlet main pipeline (m 2) is connected with the third branch pipeline (m 201) and the fourth branch pipeline (m 202).
8. The control system according to claim 7, characterized in that the inlet main line (m 1) is provided with a ball valve, a filter (F1), a pressure setter and a pressure gauge; the first branch (m 101) is provided with a pressure constant value device, a pressure gauge and a ball valve; the second branch (m 102) is provided with a pressure constant value device, a pressure gauge and a ball valve; the third branch (m 201) is provided with a ball valve and a pressure gauge; the fourth branch (m 202) is provided with a ball valve and a pressure gauge; the exhaust main pipeline (m 2) is provided with a three-way valve and a muffler (S1).
CN202110833995.XA 2021-07-23 2021-07-23 Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof Active CN113389767B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202110833995.XA CN113389767B (en) 2021-07-23 2021-07-23 Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202110833995.XA CN113389767B (en) 2021-07-23 2021-07-23 Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof

Publications (2)

Publication Number Publication Date
CN113389767A CN113389767A (en) 2021-09-14
CN113389767B true CN113389767B (en) 2024-06-21

Family

ID=77626759

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202110833995.XA Active CN113389767B (en) 2021-07-23 2021-07-23 Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof

Country Status (1)

Country Link
CN (1) CN113389767B (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204357830U (en) * 2014-10-30 2015-05-27 陈鸿宇 A kind of novel low friction single pole double-acting cylinder
CN109469662A (en) * 2017-10-13 2019-03-15 湖北江山重工有限责任公司 A kind of servo hydraulic cylinder

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB815972A (en) * 1955-04-28 1959-07-08 Renault Improvements in or relating to double-acting pneumatic jacks
CH672169A5 (en) * 1987-06-29 1989-10-31 Luciano Gubbiotti Dual action fluid actuator - operates with two degrees of freedom giving rotary and linear movement
DE19747298A1 (en) * 1997-10-25 1999-04-29 Nimak Automatisierte Schweiste Welding gun cylinder
ITMI20012137A1 (en) * 2001-10-16 2003-04-16 Luciano Migliori VARIABLE STROKE PNEUMATIC CYLINDER
KR100985469B1 (en) * 2008-07-24 2010-10-05 (주)팜코 Pneumatic low friction high speed sealless cylinder
CN101387598B (en) * 2008-10-08 2010-08-18 中国科学院武汉岩土力学研究所 Rock porosity real-time test device under action of Chemosmosis and creep coupling
CN201843740U (en) * 2010-05-05 2011-05-25 郭金阳 Automatic two-way continuous gas-liquid pressure boosting system
CN203784427U (en) * 2013-11-20 2014-08-20 无锡智能自控工程股份有限公司 Compact double-buffering piston type fast actuation mechanism
DE102016214767A1 (en) * 2016-02-16 2017-08-17 Sms Group Gmbh Synchronous cylinder for extrusion presses
CN106122169B (en) * 2016-08-31 2018-07-27 浙江金洲管道工业有限公司 A kind of pneumatic integrating device with hydraulic damping
CN206361156U (en) * 2016-12-08 2017-07-28 中国航天空气动力技术研究院 A kind of vapour-pressure type acceleration switching valve
CN106907518B (en) * 2017-04-21 2023-09-12 杭州富尚阀门有限公司 Double-acting pneumatic reset electric open type actuating mechanism
CN108050123B (en) * 2017-11-29 2019-04-12 重庆维庆液压机械有限公司 Two-way Hydraulic Cylinder
CN209078743U (en) * 2018-09-20 2019-07-09 长春工业大学 A kind of three freedom degree manipulator structure with double end effector mechanisms
CN109519274A (en) * 2018-10-23 2019-03-26 中国科学院工程热物理研究所 Miniature two-stroke reciprocating swing type free-piston engine and starting method
CN111120449A (en) * 2018-10-31 2020-05-08 泰州市宏科电气配件有限公司 Double-acting air cylinder
CN209671728U (en) * 2019-02-25 2019-11-22 常州恒立气动科技有限公司 Gate valve cylinder
CN210531308U (en) * 2019-09-27 2020-05-15 无锡市永新液压气动成套有限公司 Integrated double-piston compression cylinder
CN111486150A (en) * 2020-05-26 2020-08-04 太重集团榆次液压工业(济南)有限公司 A self-releasing hydraulic cylinder with adjustable buffer function
CN212407176U (en) * 2020-06-17 2021-01-26 新能凤凰(滕州)能源有限公司 Adjustable double-acting double-piston pneumatic actuator with spring reset

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204357830U (en) * 2014-10-30 2015-05-27 陈鸿宇 A kind of novel low friction single pole double-acting cylinder
CN109469662A (en) * 2017-10-13 2019-03-15 湖北江山重工有限责任公司 A kind of servo hydraulic cylinder

Also Published As

Publication number Publication date
CN113389767A (en) 2021-09-14

Similar Documents

Publication Publication Date Title
CN111350715B (en) A middle cylinder guide structure of a hydraulic breaker
CN107859699B (en) Brake
CN112483506B (en) High-pressure oil cylinder structure with buffer function
CN113389767B (en) Double-acting pneumatic actuator with long-stroke and large-cylinder-diameter structure and control system thereof
CN114576233B (en) Middle cylinder part of hydraulic breaking hammer
CN2924068Y (en) Hydraulic drive mechanism for two-directional production of compressed gas
CN201943918U (en) Fully oil lubrication-free oxygen compressor
CN109854482B (en) Gas-liquid booster pump
CN201925513U (en) Top mounted ball valve of inner-propped compound seal forged steel
CN213116913U (en) Multistage constant-speed oil cylinder
CN1873226A (en) Hydraulic gear of producing compressed gas in bothway
CN111502980A (en) Piston Cylinder Construction for Diaphragm Pumps
CN222254510U (en) A new type of high-speed cylinder for copper converter air eye machine
CN221401191U (en) Excavator bucket rod oil cylinder
CN220769838U (en) Locking oil cylinder with buffer cavity
CN222122247U (en) Wear-resistant RTO flat push valve
CN216447236U (en) Disordered sealing structure is prevented to sequence hydro-cylinder
CN217301101U (en) Hydraulic cylinder of gas compression tool
CN221374121U (en) Leak-proof structure for hydraulic cylinder
CN219176694U (en) Hydro-cylinder locking mechanism
CN218207309U (en) Split type hydraulic cylinder structure
CN218927672U (en) Valve bush assembly fixture
CN219888761U (en) Cut off aluminium oxide material push-pull valve device
CN220980003U (en) Lifting point longitudinally moving oil cylinder
CN114060331B (en) Column type hydraulic bidirectional propulsion locking device

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant