CN111706484A - Gas compression driving device for pneumatic liquid conveying mechanism - Google Patents
Gas compression driving device for pneumatic liquid conveying mechanism Download PDFInfo
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- CN111706484A CN111706484A CN202010561635.4A CN202010561635A CN111706484A CN 111706484 A CN111706484 A CN 111706484A CN 202010561635 A CN202010561635 A CN 202010561635A CN 111706484 A CN111706484 A CN 111706484A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B9/00—Piston machines or pumps characterised by the driving or driven means to or from their working members
- F04B9/08—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being fluid
- F04B9/12—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being fluid the fluid being elastic, e.g. steam or air
- F04B9/123—Piston machines or pumps characterised by the driving or driven means to or from their working members the means being fluid the fluid being elastic, e.g. steam or air having only one pumping chamber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B53/00—Component parts, details or accessories not provided for in, or of interest apart from, groups F04B1/00 - F04B23/00 or F04B39/00 - F04B47/00
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- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Fluid Pressure (AREA)
Abstract
The invention discloses a gas compression driving device for a pneumatic liquid conveying mechanism, which comprises a main hollow shell, wherein an air storage space is arranged on one side in the main hollow shell. The invention combines the piston compressor and the turbine compressor, utilizes the piston compressor to convey aerodynamic force to the next machine, and can recycle the high-pressure air after working in the previous machine, thereby realizing the secondary working of the air, reducing the energy consumed by the driving motor when collecting the high-pressure air, reducing the loss of electric power, improving the utilization rate of the air, providing effective piston air compression function, and combining the air with the turbine structure, thereby providing more effective conveying distance and conveying strength.
Description
Technical Field
The invention relates to the technical field of compression devices, in particular to a gas compression driving device for a pneumatic liquid conveying mechanism.
Background
At present, when liquid is conveyed for a long distance, a compression mechanism is mostly adopted, the existing compression mechanism is not a piston type compressor or a turbine type compressor, and the structures of the two are mutually independent, so that the pressure of only one mechanism can be output during working, and the defect of short pressure conveying distance exists in the actual pressure conveying process.
Disclosure of Invention
The present invention is directed to a gas compression driving device for a pneumatic liquid conveying mechanism to solve the above problems.
In order to achieve the purpose, the invention provides the following technical scheme: a gas compression driving device for a pneumatic liquid conveying mechanism comprises a main hollow shell, wherein an air storage space is arranged on one side inside the main hollow shell, a component rotating space is arranged at the top end of one side of the air storage space, an air compression space is arranged at the bottom of the component rotating space, a driving motor installation shell is installed at the top of the outer side of the main hollow shell, a component installation space is arranged inside the driving motor installation shell, a driving motor is installed inside the component installation space, an annular array type maximum rotating strength control mechanism is installed at the end part of a motor spindle in the driving motor, a main first rotating shaft is installed at a connecting position of the annular array type maximum rotating strength control mechanism, a shaft body of the main first rotating shaft penetrates through one side of the main hollow shell, and two ends of the main first rotating shaft extend to the component rotating space and the inside of the component installation space, a rotatory plectane is installed to the tip that is located the inside main first rotation axis of part rotation space, a terminal surface edge installation column spinner of rotatory plectane, through a bearing installation main shaft cover on the cylinder of column spinner, a movable rod is fixed at the outside middle part of main shaft cover, a movable rod is at the one end installation master piston board that is located the inside air compression space, and the inside exhaust hole that communicates external space and air storage space that is equipped with in one side of main hollow shell, the biggest atmospheric pressure control mechanism of an interior mounting coil spring formula in exhaust hole, the inside of main hollow shell are equipped with the main first air vent of intercommunication external space and air storage space, just main hollow shell is lieing in the tip of the main first air vent is equipped with the main connecting plate, the inside of main hollow shell is equipped with the main second air vent of intercommunication air compression space bottom and air storage space bottom, the inside of main hollow shell is equipped with the main third air vent of intercommunication air compression space bottom and external space The hole, main hollow shell's inside is equipped with the main fourth vent hole of intercommunication external space and main third vent hole middle part side, inside, main third vent hole bottom segment of main second vent hole middle section and main fourth vent hole middle section are inside installs main first air check valve, main second air check valve and main third air check valve respectively, and the bottom of main third vent hole is equipped with vice connecting plate, main first air check valve inlet port and main second air check valve exhaust port all face air compression space, the exhaust port of main fourth vent hole is towards main third vent hole.
Further, the ring array type maximum rotation intensity control mechanism includes a main hollow housing for the ring array type maximum rotation intensity control mechanism, a main hollow section for the ring array type maximum rotation intensity control mechanism, a rotary column for the ring array type maximum rotation intensity control mechanism, a semicircular groove structure for the ring array type maximum rotation intensity control mechanism, an auxiliary hollow section for the ring array type maximum rotation intensity control mechanism, a movable plate for the ring array type maximum rotation intensity control mechanism, a coil spring for the ring array type maximum rotation intensity control mechanism, and a push rod for the ring array type maximum rotation intensity control mechanism; the center of one end face of the main hollow shell for the annular array type maximum rotation strength control mechanism is fixedly connected with the end part of a motor spindle, the center of the inside of the main hollow shell for the annular array type maximum rotation strength control mechanism is a main hollow interval for the annular array type maximum rotation strength control mechanism, the main hollow shell for the annular array type maximum rotation strength control mechanism is sleeved with a rotating column for the annular array type maximum rotation strength control mechanism inside the main hollow interval for the annular array type maximum rotation strength control mechanism, the inside of the main hollow shell for the annular array type maximum rotation strength control mechanism is an auxiliary hollow interval for the annular array type maximum rotation strength control mechanism, and the inside of the auxiliary hollow interval for the annular array type maximum rotation strength control mechanism is provided with an annular array type maximum rotation strength control mechanism on one end face of the main hollow interval for the annular array type maximum rotation strength control mechanism A movable plate for a rotation control mechanism, the secondary hollow section for the ring-arrayed maximum rotation strength control mechanism fixing a coil spring for the ring-arrayed maximum rotation strength control mechanism between one ends of the movable plates for the ring-arrayed maximum rotation strength control mechanism, one end face of the movable plate for the ring-arrayed maximum rotation strength control mechanism being provided with a push rod for the ring-arrayed maximum rotation strength control mechanism of an integrated structure therewith, and the push rod for the ring-arrayed maximum rotation strength control mechanism penetrating the main hollow housing for the ring-arrayed maximum rotation strength control mechanism and being located inside the main hollow section for the ring-arrayed maximum rotation strength control mechanism, the push rod for the ring-arrayed maximum rotation strength control mechanism being of a semicircular structure at one end of the main hollow section for the ring-arrayed maximum rotation strength control mechanism, the side surface of the rotating column for the annular array type maximum rotation strength control mechanism is provided with a semicircular groove structure for the annular array type maximum rotation strength control mechanism, the semicircular groove structure is used for placing the end part of the push rod for the annular array type maximum rotation strength control mechanism, and one end of the rotating column for the annular array type maximum rotation strength control mechanism is fixed with the end part of the main first rotating shaft.
Further, the initial length of the coil spring for the ring array type maximum rotation intensity control mechanism is larger than the length of the auxiliary hollow section for the ring array type maximum rotation intensity control mechanism.
Further, the structural shape of the end part of the push rod for the annular array type maximum rotation strength control mechanism is consistent with the structural shape of the semicircular groove structure for the annular array type maximum rotation strength control mechanism.
Further, the coil spring type maximum liquid pressure control mechanism comprises a hollow housing for the coil spring type maximum liquid pressure control mechanism, a hollow seal ring for the coil spring type maximum liquid pressure control mechanism, a hollow structure for the coil spring type maximum liquid pressure control mechanism, a liquid discharge hole for the coil spring type maximum liquid pressure control mechanism, a valve plate insertion space for the coil spring type maximum liquid pressure control mechanism, a liquid inlet hole for the coil spring type maximum liquid pressure control mechanism, a moving plate for the coil spring type maximum liquid pressure control mechanism, a valve plate for the coil spring type maximum liquid pressure control mechanism, a liquid through hole for the coil spring type maximum liquid pressure control mechanism, and a coil spring for the coil spring type maximum liquid pressure control mechanism; the side surface of the hollow shell for the coil spring type maximum liquid pressure control mechanism is sleeved with a coil spring type air-liquid sealing ring for the maximum liquid pressure control mechanism, the center inside the hollow shell for the coil spring type maximum liquid pressure control mechanism is provided with a hollow structure for the coil spring type maximum liquid pressure control mechanism, one side of the hollow shell for the coil spring type maximum liquid pressure control mechanism, which is positioned in the hollow structure for the coil spring type maximum liquid pressure control mechanism, is provided with a coil spring type liquid discharge hole for the maximum liquid pressure control mechanism, one end of the coil spring type liquid discharge hole for the maximum liquid pressure control mechanism is communicated with one end of the hollow shell for the coil spring type maximum liquid pressure control mechanism, and the other side of the hollow shell for the coil spring type maximum liquid pressure control mechanism, which is positioned in the hollow structure for the coil spring type maximum liquid pressure control mechanism, is provided with a coil spring The valve plate inserting space for the control mechanism is provided with a coil spring type liquid inlet hole for the maximum liquid pressure control mechanism at one side of the valve plate inserting space for the coil spring type maximum liquid pressure control mechanism, the coil spring type liquid inlet hole for the maximum liquid pressure control mechanism is communicated with the other side of the hollow shell for the maximum liquid pressure control mechanism, the hollow shell for the maximum liquid pressure control mechanism is positioned at the inside of the hollow structure for the coil spring type maximum liquid pressure control mechanism, a coil spring type movable plate for the maximum liquid pressure control mechanism is arranged in the hollow structure for the coil spring type maximum liquid pressure control mechanism, and the coil spring type movable plate for the maximum liquid pressure control mechanism is arranged at the center of the end face at one side of the valve plate inserting space for the coil spring type maximum liquid pressure control mechanism and is of an integrated structure with the coil spring type maximum liquid pressure control mechanism And a valve plate for mechanism, wherein a coil spring type liquid through hole for maximum liquid pressure control mechanism communicating both end faces is provided on a side face of the movable plate for coil spring type maximum liquid pressure control mechanism, and a coil spring for coil spring type maximum liquid pressure control mechanism is attached to the other end face of the movable plate for coil spring type maximum liquid pressure control mechanism.
Furthermore, the coil spring type air-liquid sealing ring for the maximum liquid pressure control mechanism is clamped inside the exhaust hole, and one end of the liquid inlet hole for the maximum liquid pressure control mechanism is communicated with the inside of the air storage space.
Further, the initial length of the coil spring type coil spring for the maximum liquid pressure control mechanism is larger than the lateral length of the coil spring type hollow structure for the maximum liquid pressure control mechanism.
Compared with the prior art, the invention has the beneficial effects that: the invention combines the piston compressor and the turbine compressor, utilizes the piston compressor to convey aerodynamic force to the next machine, and can recycle the high-pressure air after working in the previous machine, thereby realizing the secondary working of the air, reducing the energy consumed by the driving motor when collecting the high-pressure air, reducing the loss of electric power, improving the utilization rate of the air, providing effective piston air compression function, and combining the air with the turbine structure, thereby providing more effective conveying distance and conveying strength.
Drawings
FIG. 1 is a schematic view of a gas compression driving device for a pneumatic liquid conveying mechanism according to the present invention;
FIG. 2 is a schematic structural diagram of a ring array maximum rotation strength control mechanism in a gas compression driving device for a pneumatic liquid conveying mechanism according to the present invention;
FIG. 3 is a schematic structural diagram of a coil spring type maximum air pressure control mechanism in a gas compression driving device for an air pressure type liquid conveying mechanism according to the present invention;
in the figure: 1, a main hollow housing, 2, an air storage space, 3, a part rotation space, 4, an air compression space, 5, a main first air vent, 6, a main connecting plate, 7, a main second air vent, 8, a main first air check valve, 10, a main third air vent, 11, a main second air check valve, 12, an auxiliary connecting plate, 13, a main fourth air vent, 14, a main third air check valve, 15, a main piston plate, 16, a movable rod, 17, a driving motor mounting housing, 18, a part mounting space, 19, a driving motor, 20, a motor spindle, 21, a ring array maximum rotation strength control mechanism, 211, a main hollow housing for the ring array maximum rotation strength control mechanism, 212, a main hollow section for the ring array maximum rotation strength control mechanism, 213, a rotating column for the ring array maximum rotation strength control mechanism, 214, a semicircular groove structure for the ring array maximum rotation strength control mechanism, 215, secondary hollow space for ring-array maximum rotation strength control mechanism, 216, movable plate for ring-array maximum rotation strength control mechanism, 217, coil spring for ring-array maximum rotation strength control mechanism, 218, push rod for ring-array maximum rotation strength control mechanism, 22, main first rotating shaft, 23, rotating circular plate, 24, rotating column, 25, spindle cover, 26, exhaust hole, 27, coil spring type maximum air pressure control mechanism, 271, hollow housing for coil spring type maximum liquid pressure control mechanism, 272, air liquid seal ring for coil spring type maximum liquid pressure control mechanism, 273, hollow structure for coil spring type maximum liquid pressure control mechanism, 274, liquid discharge hole for coil spring type maximum liquid pressure control mechanism, 275, valve plate insertion space for coil spring type maximum liquid pressure control mechanism, 276, a liquid inlet hole for coil spring type maximum liquid pressure control mechanism, 277, a moving plate for coil spring type maximum liquid pressure control mechanism, 278, a valve plate for coil spring type maximum liquid pressure control mechanism, 279, a liquid through hole for coil spring type maximum liquid pressure control mechanism, 2710, and a coil spring for coil spring type maximum liquid pressure control mechanism.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, an embodiment of the present invention: the air compressor comprises a main hollow shell 1, wherein an air storage space 2 is arranged on one side inside the main hollow shell 1, a component rotating space 3 is arranged on the top end of one side of the air storage space 3, an air compression space 4 is arranged at the bottom of the component rotating space 3, a driving motor installation shell 17 is installed at the top of the outer side of the main hollow shell 1, a component installation space 18 is arranged inside the driving motor installation shell 17, a driving motor 19 is installed inside the component installation space 18, an annular array type maximum rotating strength control mechanism 21 is installed at the end part of a motor spindle 20 in the driving motor 19, a main first rotating shaft 22 is installed at one connecting part of the annular array type maximum rotating strength control mechanism 21, the shaft body of the main first rotating shaft 22 penetrates through one side of the main hollow shell 1, and the two ends of the main first rotating shaft 22 extend to the inside of the component rotating space 3 and the component installation space 18, a rotary circular plate 23 is arranged at the end part of a main first rotary shaft 22 in the part rotary space 3, a rotary column 24 is arranged at the edge of one end face of the rotary circular plate 23, a spindle sleeve 25 is arranged on the cylinder of the rotary column 24 through a bearing, a movable rod 16 is fixed at the middle part of the outer side of the spindle sleeve 25, a main piston plate 15 is arranged at one end in the air compression space 4 of the movable rod 16, an exhaust hole 26 communicated with the external space and the air storage space 2 is arranged in one side of a main hollow shell 1, a coil spring type maximum air pressure control mechanism 27 is arranged in the exhaust hole 26, a main first vent hole 5 communicated with the external space and the air storage space 2 is arranged in the main hollow shell 1, a main connecting plate 6 is arranged at the end part of the main first vent hole 5 of the main hollow shell 1, a main second vent hole 7 communicated with the bottom end of the air compression space 4 and the bottom end of the air storage space 2 is arranged in the main hollow, the inside of main hollow shell 1 is equipped with the main third air vent 10 of intercommunication air compression space 4 bottom and external space, the inside of main hollow shell 1 is equipped with the main fourth air vent 13 of intercommunication external space and main third air vent 10 middle part side, inside 7 middle sections of main second air vent, inside 10 bottom sections of main third air vent and the inside main fourth air vent 13 middle section of main second air vent install main first air check valve 8, main second air check valve 11 and main third air check valve 14 respectively, and the bottom of main third air vent 10 is equipped with vice connecting plate 12, main first air check valve 8 inlet port and main second air check valve 11 exhaust port all face air compression space 4, the exhaust port of main fourth air vent 13 is towards main third air vent 10.
Referring to fig. 2, the ring array type maximum rotation strength control mechanism 21 includes a main hollow housing 211 for the ring array type maximum rotation strength control mechanism, a main hollow section 212 for the ring array type maximum rotation strength control mechanism, a rotary column 213 for the ring array type maximum rotation strength control mechanism, a semicircular groove structure 214 for the ring array type maximum rotation strength control mechanism, an auxiliary hollow section 215 for the ring array type maximum rotation strength control mechanism, a movable plate 216 for the ring array type maximum rotation strength control mechanism, a coil spring 217 for the ring array type maximum rotation strength control mechanism, and a push rod 218 for the ring array type maximum rotation strength control mechanism; the center of one end surface of the main hollow housing 211 for the ring array type maximum rotation strength control mechanism is fixedly connected with the end portion of a motor spindle 20, the center of the inside of the main hollow housing 211 for the ring array type maximum rotation strength control mechanism is a main hollow section 212 for the ring array type maximum rotation strength control mechanism, the main hollow housing 211 for the ring array type maximum rotation strength control mechanism is sleeved with a rotating column 213 for the ring array type maximum rotation strength control mechanism inside the main hollow section 212 for the ring array type maximum rotation strength control mechanism, the inside of the main hollow housing 211 for the ring array type maximum rotation strength control mechanism is an auxiliary hollow section 215 for the ring array type maximum rotation strength control mechanism, the inside of the auxiliary hollow section 215 for the ring array type maximum rotation strength control mechanism is placed on one end surface of the main hollow section 212 for the ring array type maximum rotation strength control mechanism A movable plate 216 for a ring-array maximum rotation intensity control mechanism, wherein a coil spring 217 for the ring-array maximum rotation intensity control mechanism is fixed between the auxiliary hollow sections 215 for the ring-array maximum rotation intensity control mechanism and one end of the movable plate 216 for the ring-array maximum rotation intensity control mechanism, a push rod 218 for the ring-array maximum rotation intensity control mechanism is provided at one end surface of the movable plate 216 for the ring-array maximum rotation intensity control mechanism, the push rod 218 for the ring-array maximum rotation intensity control mechanism penetrates the main hollow housing 211 for the ring-array maximum rotation intensity control mechanism and is located inside the main hollow section 212 for the ring-array maximum rotation intensity control mechanism, and the push rod 218 for the ring-array maximum rotation intensity control mechanism is located at one end of the main hollow section 212 for the ring-array maximum rotation intensity control mechanism A semicircular groove structure 214 for the circular array maximum rotation intensity control mechanism is arranged on the side surface of the circular array maximum rotation intensity control mechanism rotating column 213 for placing the end part of the circular array maximum rotation intensity control mechanism push rod 218, and one end of the circular array maximum rotation intensity control mechanism rotating column 213 is fixed with the end part of the main first rotating shaft 22; the initial length of the spiral spring 217 for the ring array type maximum rotation intensity control mechanism is larger than the length of the auxiliary hollow space 215 for the ring array type maximum rotation intensity control mechanism; the configuration of the end of the push rod 218 for the ring array type maximum rotation strength controlling means is identical to the configuration of the semicircular groove structure 214 for the ring array type maximum rotation strength controlling means.
Referring to fig. 3, the coil spring type maximum hydraulic pressure control mechanism 27 includes a coil spring type hollow case 271 for maximum liquid pressure control mechanism, a coil spring type hollow seal 272 for maximum liquid pressure control mechanism, a coil spring type hollow structure 273 for maximum liquid pressure control mechanism, a coil spring type liquid discharge hole 274 for maximum liquid pressure control mechanism, a coil spring type valve plate insertion space 121 for maximum liquid pressure control mechanism, a coil spring type liquid inlet hole 276 for maximum liquid pressure control mechanism, a coil spring type moving plate 277 for maximum liquid pressure control mechanism, a coil spring type valve plate 278 for maximum liquid pressure control mechanism, a coil spring type liquid through hole 279 for maximum liquid pressure control mechanism, and a coil spring type coil spring 2710 for maximum liquid pressure control mechanism; a coil spring type hollow seal ring 272 for the maximum liquid pressure control mechanism is fitted to a side surface of the coil spring type hollow case 271 for the maximum liquid pressure control mechanism, a coil spring type hollow structure 273 for the maximum liquid pressure control mechanism is provided at the center inside the coil spring type hollow case 271 for the maximum liquid pressure control mechanism, a coil spring type liquid discharge hole 274 is provided at one side of the coil spring type hollow structure 273 for the maximum liquid pressure control mechanism, one end of the coil spring type liquid discharge hole 274 is communicated with one end of the coil spring type hollow case 271 for the maximum liquid pressure control mechanism, and the other side of the coil spring type hollow case 273 for the maximum liquid pressure control mechanism is provided with a coil spring type liquid discharge hole 274 A valve plate insertion space 121 for a coil spring type maximum liquid pressure control mechanism, a coil spring type liquid inlet hole 276 for the maximum liquid pressure control mechanism being provided on one side of the valve plate insertion space 121 for the coil spring type hollow case 271, the coil spring type liquid inlet hole 276 communicating with the coil spring type maximum liquid pressure control mechanism on the other side of the coil spring type hollow case 271, a coil spring type moving plate 277 for the maximum liquid pressure control mechanism being installed inside the coil spring type hollow structure 273 for the maximum liquid pressure control mechanism, the coil spring type moving plate 277 for the maximum liquid pressure control mechanism being provided at an end surface center on the side of the valve plate insertion space 121 for the coil spring type maximum liquid pressure control mechanism A coil spring type maximum liquid pressure control mechanism valve plate 278 of an integral structure, the side surface of the coil spring type maximum liquid pressure control mechanism moving plate 277 being provided with a coil spring type maximum liquid pressure control mechanism liquid passage hole 279 communicating both end surfaces thereof, the other end surface of the coil spring type maximum liquid pressure control mechanism moving plate 277 being provided with a coil spring type maximum liquid pressure control mechanism coil spring 2710; the coil spring type air-liquid sealing ring 272 for the maximum liquid pressure control mechanism is clamped in the exhaust hole 26, and one end of the liquid inlet hole 276 for the maximum liquid pressure control mechanism is communicated with the inside of the air storage space 2; the initial length of the coil spring type coil spring 2710 for the maximum liquid pressure control mechanism is longer than the lateral length of the hollow structure 273 for the maximum liquid pressure control mechanism.
Certain attention must be paid to: the one-way pulling speed of the one-way driver in the pneumatic driven liquid flowing device is integral multiple of the one-circle rotation speed of the driving motor.
The specific use mode is as follows: in the work of the invention, the main connecting plate 6 and the auxiliary connecting plate 12 are respectively and fixedly connected with the main connecting plate and the auxiliary connecting plate in the pneumatic driven liquid flowing device of the pneumatic liquid conveying mechanism, the driving motor 19 is turned on, the rotating circular plate 23 also rotates under the rotating action of the driving motor, the main piston plate 15 reciprocates under the action of the connecting rod in the rotating process, and when the main piston plate 15 moves upwards, the air inlet mode is as follows: one is as follows: air is introduced from the direction of the fourth vent hole 13, and the air comes from the air in the external environment; the second step is as follows: the high pressure air from the pneumatic driven liquid flowing device for the pneumatic liquid conveying mechanism is compressed into the air compression space 2 when the main piston plate 15 moves downwards, and the speed of one-way pulling of the one-way driver in the pneumatic driven liquid flowing device for the pneumatic liquid conveying mechanism is integral multiple of the speed of one-circle rotation of the driving motor, so that after the air is compressed for a certain number of times, the high pressure air is formed, and when the high pressure air is specific, the high pressure air can be injected into the pneumatic driven liquid flowing device for the pneumatic liquid conveying mechanism to provide high pressure aerodynamic force.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (7)
1. The utility model provides a vapour-pressure type is gas compression drive arrangement for liquid conveying mechanism, includes main hollow shell (1), its characterized in that: the air compressor is characterized in that an air storage space (2) is arranged on one side inside the main hollow shell (1), a component rotating space (3) is arranged on the top end of one side of the air storage space (3), an air compression space (4) is arranged at the bottom of the component rotating space (3), a driving motor installation shell (17) is installed at the top of the outer side of the main hollow shell (1), a component installation space (18) is arranged inside the driving motor installation shell (17), a driving motor (19) is installed inside the component installation space (18), an annular array type maximum rotating strength control mechanism (21) is installed at the end part of a motor spindle (20) in the driving motor (19), a main first rotating shaft (22) is installed at a connecting position of the annular array type maximum rotating strength control mechanism (21), and a shaft body of the main first rotating shaft (22) penetrates through one side of the main hollow shell (1), and both ends of the main first rotating shaft (22) extend to the interior of the component rotating space (3) and the component mounting space (18), a rotating circular plate (23) is arranged at the end part of the main first rotating shaft (22) positioned in the component rotating space (3), a rotating column (24) is arranged at one end surface edge of the rotating circular plate (23), a spindle sleeve (25) is arranged on the column body of the rotating column (24) through a bearing, a movable rod (16) is fixed at the middle part of the outer side of the spindle sleeve (25), a main piston plate (15) is arranged at one end of the movable rod (16) positioned in the air compression space (4), an exhaust hole (26) communicated with the external space and the air storage space (2) is arranged in one side of the main hollow shell (1), a helical spring type maximum air pressure control mechanism (27) is arranged in the exhaust hole (26), and a main first vent hole (5) communicated with the external space and the air storage space (2) is arranged in the main hollow shell (1), and the end part of the main hollow shell (1) positioned at the main first air vent (5) is provided with a main connecting plate (6), the inside of the main hollow shell (1) is provided with a main second air vent (7) communicated with the bottom end of the air compression space (4) and the bottom end of the air storage space (2), the inside of the main hollow shell (1) is provided with a main third air vent (10) communicated with the bottom end of the air compression space (4) and the external space, the inside of the main hollow shell (1) is provided with a main fourth air vent (13) communicated with the external space and the side surface of the middle part of the main third air vent (10), the inside of the middle section of the main second air vent (7), the inside of the bottom section of the main third air vent (10) and the inside of the main fourth air vent (13) are respectively provided with a main first air one-way valve (8), a main second air one-way valve (11) and a main third, and the bottom of main third air vent (10) is equipped with vice connecting plate (12), main first air check valve (8) inlet port and main second air check valve (11) exhaust port all face air compression space (4), the exhaust port of main fourth air vent (13) is towards main third air vent (10).
2. The gas compression driving device for a pneumatic liquid transporting mechanism according to claim 1, wherein: the ring-shaped array type maximum rotation intensity control mechanism (21) comprises a main hollow shell (211) for the ring-shaped array type maximum rotation intensity control mechanism, a main hollow interval (212) for the ring-shaped array type maximum rotation intensity control mechanism, a rotating column (213) for the ring-shaped array type maximum rotation intensity control mechanism, a semicircular groove structure (214) for the ring-shaped array type maximum rotation intensity control mechanism, an auxiliary hollow interval (215) for the ring-shaped array type maximum rotation intensity control mechanism, a movable plate (216) for the ring-shaped array type maximum rotation intensity control mechanism, a spiral spring (217) for the ring-shaped array type maximum rotation intensity control mechanism and a push rod (218) for the ring-shaped array type maximum rotation intensity control mechanism; the center of one end face of a main hollow shell (211) for the annular array type maximum rotation strength control mechanism is fixedly connected with the end part of a motor spindle (20), the center inside the main hollow shell (211) for the annular array type maximum rotation strength control mechanism is a main hollow section (212) for the annular array type maximum rotation strength control mechanism, a rotating column (213) for the annular array type maximum rotation strength control mechanism is sleeved inside the main hollow section (212) for the annular array type maximum rotation strength control mechanism, the inside of the main hollow shell (211) for the annular array type maximum rotation strength control mechanism is an auxiliary hollow section (215) for the annular array type maximum rotation strength control mechanism, and the inside of the auxiliary hollow section (215) for the annular array type maximum rotation strength control mechanism is positioned inside the annular array type maximum rotation strength control mechanism A movable plate (216) for a ring array maximum rotation strength control mechanism is placed on one end face of a main hollow space (212) for a rotation strength control mechanism, a coil spring (217) for a ring array maximum rotation strength control mechanism is fixed between one ends of the movable plates (216) for the ring array maximum rotation strength control mechanism by a secondary hollow space (215), a push rod (218) for a ring array maximum rotation strength control mechanism of an integrated structure with the movable plate (216) for the ring array maximum rotation strength control mechanism is arranged on one end face of the movable plate (216) for the ring array maximum rotation strength control mechanism, and the push rod (218) for the ring array maximum rotation strength control mechanism penetrates through the main hollow housing (211) for the ring array maximum rotation strength control mechanism and is located inside the main hollow space (212) for the ring array maximum rotation strength control mechanism, the annular array type maximum rotation intensity control mechanism push rod (218) is of a semicircular structure at one end of the main hollow section (212) located in the annular array type maximum rotation intensity control mechanism, a semicircular groove structure (214) used for placing the end portion of the annular array type maximum rotation intensity control mechanism push rod (218) is arranged on the side face of the annular array type maximum rotation intensity control mechanism rotating column (213), and one end of the annular array type maximum rotation intensity control mechanism rotating column (213) is fixed with the end portion of the main first rotating shaft (22).
3. The gas compression driving device for a pneumatic liquid transporting mechanism according to claim 2, wherein: the initial length of the spiral spring (217) for the ring array type maximum rotation intensity control mechanism is larger than the length of the auxiliary hollow section (215) for the ring array type maximum rotation intensity control mechanism.
4. The gas compression driving device for a pneumatic liquid transporting mechanism according to claim 2, wherein: the structural shape of the end part of the push rod (218) for the ring array type maximum rotation intensity control mechanism is consistent with the structural shape of the semicircular groove structure (214) for the ring array type maximum rotation intensity control mechanism.
5. The gas compression driving device for a pneumatic liquid transporting mechanism according to claim 1, wherein: the coil spring type maximum air pressure control mechanism (27) comprises a coil spring type hollow shell (271) for the maximum liquid pressure control mechanism, a coil spring type hollow sealing ring (272) for the maximum liquid pressure control mechanism, a coil spring type hollow structure (273) for the maximum liquid pressure control mechanism, a coil spring type liquid discharge hole (274) for the maximum liquid pressure control mechanism, and a valve plate insertion space (121) for the coil spring type maximum liquid pressure control mechanism, a liquid inlet hole (276) for a coil spring type maximum liquid pressure control mechanism, a moving plate (277) for a coil spring type maximum liquid pressure control mechanism, a valve plate (278) for a coil spring type maximum liquid pressure control mechanism, a liquid through hole (279) for a coil spring type maximum liquid pressure control mechanism, and a coil spring (2710) for a coil spring type maximum liquid pressure control mechanism; a coil spring type hollow seal ring (272) for the maximum liquid pressure control mechanism is sleeved on the side surface of the coil spring type hollow shell (271) for the maximum liquid pressure control mechanism, a coil spring type hollow structure (273) for the maximum liquid pressure control mechanism is arranged at the center inside the coil spring type hollow shell (271) for the maximum liquid pressure control mechanism, a coil spring type liquid discharge hole (274) for the maximum liquid pressure control mechanism is arranged at one side of the coil spring type hollow structure (273) for the maximum liquid pressure control mechanism, one end of the coil spring type liquid discharge hole (274) for the maximum liquid pressure control mechanism is communicated with one end of the coil spring type hollow shell (271) for the maximum liquid pressure control mechanism, and the coil spring type hollow shell (271) for the maximum liquid pressure control mechanism is positioned at the other end of the coil spring type hollow shell (271) for the maximum liquid pressure control mechanism A coil spring type valve plate insertion space (121) for the maximum liquid pressure control mechanism is provided on the other side of the hollow structure (273) for the pressure control mechanism, a coil spring type liquid inlet hole (276) for the maximum liquid pressure control mechanism is provided on one side of the coil spring type valve plate insertion space (121) for the maximum liquid pressure control mechanism, the coil spring type liquid inlet hole (276) for the maximum liquid pressure control mechanism communicates with the other side of the coil spring type hollow housing (271) for the maximum liquid pressure control mechanism, a coil spring type moving plate (277) for the maximum liquid pressure control mechanism is mounted inside the coil spring type hollow structure (273) for the maximum liquid pressure control mechanism, the coil spring type moving plate (277) for the maximum liquid pressure control mechanism is provided with a coil spring type valve plate (278) for the maximum liquid pressure control mechanism, which is of an integrated structure with the coil spring type moving plate (277) located on one side of the coil spring type valve plate insertion space (121), the side surface of the coil spring type moving plate (277) for the maximum liquid pressure control mechanism is provided with a coil spring type liquid through hole (279) for the maximum liquid pressure control mechanism, which communicates with the two end surfaces of the coil spring type moving plate, and the other end surface of the coil spring type moving plate (277) for the maximum liquid pressure control mechanism is provided with a coil spring type coil spring (2710) for the maximum liquid pressure control mechanism.
6. The gas compression driving device for a pneumatic liquid transporting mechanism according to claim 5, wherein: the coil spring type air-liquid sealing ring (272) for the maximum liquid pressure control mechanism is clamped in the exhaust hole (26), and one end of the liquid inlet hole (276) for the maximum liquid pressure control mechanism is communicated with the inside of the air storage space (2).
7. The gas compression driving device for a pneumatic liquid transporting mechanism according to claim 5, wherein: the initial length of the coil spring type coil spring (2710) for the maximum liquid pressure control mechanism is longer than the lateral length of the hollow structure (273) for the maximum liquid pressure control mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010561635.4A CN111706484A (en) | 2020-06-18 | 2020-06-18 | Gas compression driving device for pneumatic liquid conveying mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010561635.4A CN111706484A (en) | 2020-06-18 | 2020-06-18 | Gas compression driving device for pneumatic liquid conveying mechanism |
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| Publication Number | Publication Date |
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| CN111706484A true CN111706484A (en) | 2020-09-25 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202010561635.4A Withdrawn CN111706484A (en) | 2020-06-18 | 2020-06-18 | Gas compression driving device for pneumatic liquid conveying mechanism |
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| CN (1) | CN111706484A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112123566A (en) * | 2020-10-16 | 2020-12-25 | 王恺 | Telescopic control device for clay dispersion device in screw mud production |
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| CN105569974A (en) * | 2015-12-01 | 2016-05-11 | 龙文凯 | Solar pressurized energy storage type micro waterhead fluid energy water pumping system |
| CN107448404A (en) * | 2017-09-18 | 2017-12-08 | 黄田 | A kind of high efficiency air compression plant |
| CN209875410U (en) * | 2019-04-18 | 2019-12-31 | 深圳市思特克气动液压有限公司 | Low-noise gas booster pump |
| CN110886711A (en) * | 2019-12-12 | 2020-03-17 | 王欣欣 | Constant-pressure control type thrust control device |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105569974A (en) * | 2015-12-01 | 2016-05-11 | 龙文凯 | Solar pressurized energy storage type micro waterhead fluid energy water pumping system |
| CN107448404A (en) * | 2017-09-18 | 2017-12-08 | 黄田 | A kind of high efficiency air compression plant |
| CN209875410U (en) * | 2019-04-18 | 2019-12-31 | 深圳市思特克气动液压有限公司 | Low-noise gas booster pump |
| CN110886711A (en) * | 2019-12-12 | 2020-03-17 | 王欣欣 | Constant-pressure control type thrust control device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112123566A (en) * | 2020-10-16 | 2020-12-25 | 王恺 | Telescopic control device for clay dispersion device in screw mud production |
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Application publication date: 20200925 |