CN110206738B - Pressure boosting device with output pressure control function - Google Patents
Pressure boosting device with output pressure control function Download PDFInfo
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- CN110206738B CN110206738B CN201910493431.9A CN201910493431A CN110206738B CN 110206738 B CN110206738 B CN 110206738B CN 201910493431 A CN201910493431 A CN 201910493431A CN 110206738 B CN110206738 B CN 110206738B
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- unit control
- maximum rotation
- rotation force
- force unit
- control mechanism
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
- F04D13/06—Units comprising pumps and their driving means the pump being electrically driven
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D15/00—Control, e.g. regulation, of pumps, pumping installations or systems
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/301—Pressure
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses a supercharging device with an output pressure control function, which comprises a bottom mounting substrate, wherein a plurality of main bolts for mounting are arranged in the bottom mounting substrate. The device is used for the pressurization effect of liquid output, so that the pressure value and the flow of output liquid are ensured, the maximum pressure value of the pressurization value can be effectively controlled, the water pressure and the water flow in a main water pumping pipeline are not influenced too much, the adaptability is strong, the device is provided with a maximum rotation force unit control mechanism, the maximum torque force during rotation can be effectively controlled, and the maximum torque force is converted into the maximum output pressure value during pressurization.
Description
Technical Field
The invention relates to the technical field of machinery, in particular to a supercharging device with an output pressure control function.
Background
At present, in some places, in order to realize the altitude difference discharge of liquid, all use pumping device, and because the influence of altitude difference, lead to some pumping device's output height not enough or weak, at this moment, just need supercharging device, and general supercharging device is uncontrollable to output pressure, so lead to the inside pressure value of main pipeline that draws water unstably, can influence the normal flow of the inside water pressure of main pipeline that draws water.
Disclosure of Invention
The present invention is directed to a pressure boosting device with output pressure control function, so as to solve the problems of the background art mentioned above.
In order to achieve the purpose, the invention provides the following technical scheme: a supercharging device with output pressure control function comprises a bottom mounting substrate, wherein a plurality of main bolts for mounting are arranged in the bottom mounting substrate, a motor mounting plate is mounted on one side of the upper surface of the bottom mounting substrate, a turbine mounting substrate is mounted on the other side of the upper surface of the bottom mounting substrate, a motor is mounted on the top of the motor mounting plate, a turbine supercharging mounting mechanism is mounted on the top of the turbine mounting substrate, an auxiliary rotating shaft is mounted at the center of the turbine supercharging mounting mechanism, the shaft body of the auxiliary rotating shaft is mounted in the turbine supercharging mounting mechanism through a main bearing, a main turbine is mounted on the shaft body positioned in the turbine supercharging mounting mechanism through the auxiliary rotating shaft, the end part of a main shaft of the motor is connected with a hollow rotating shell through a connecting plate, and a main hollow structure is arranged at the center of the hollow rotating shell, the center of a hollow rotatory shell terminal surface is provided with the main through-hole structure of the main hollow structure of intercommunication, hollow rotatory shell terminal surface is provided with a plurality ofly about the axial lead of hollow rotatory shell is the screw hole that the annular array set up for the centre of a circle, an internally mounted main rotation axis of main through-hole structure, main rotation axis is lieing in a main plectane of the inside one end installation of main hollow structure, a terminal surface of main plectane is provided with a plurality of main hemisphere groove structure that the axle center about main plectane is the annular array setting for the centre of a circle, every the inside of screw hole all connects a maximum rotation dynamics unit control mechanism through main thread structure, the horizontal length adjustment mechanism of another end installation elasticity of main rotation axis, the one end of the horizontal length adjustment mechanism of elasticity and the tip fixed connection of vice rotation axis.
Further, the maximum rotation force unit control mechanism comprises a hollow shell for the maximum rotation force unit control mechanism, an external thread structure for the maximum rotation force unit control mechanism, a limiting plate for the maximum rotation force unit control mechanism, a through hole structure for the maximum rotation force unit control mechanism, a hollow structure for the maximum rotation force unit control mechanism, a moving plate for the maximum rotation force unit control mechanism, a spiral spring for the maximum rotation force unit control mechanism, a push rod for the maximum rotation force unit control mechanism and a hemispherical head for the maximum rotation force unit control mechanism; the outer side of the hollow shell for the maximum rotation force unit control mechanism is provided with an external thread structure for the maximum rotation force unit control mechanism, one end of the side surface of the hollow shell for the maximum rotation force unit control mechanism is provided with a limiting plate for the maximum rotation force unit control mechanism which is of an integral structure with the hollow shell, the hollow structure for the maximum rotation force unit control mechanism is arranged in the hollow shell for the maximum rotation force unit control mechanism, a through hole structure for the maximum rotation force unit control mechanism is arranged at the center of one end surface of the hollow shell for the maximum rotation force unit control mechanism, a movable plate for the maximum rotation force unit control mechanism is placed in the hollow structure for the maximum rotation force unit control mechanism, and one end surface of the movable plate for the maximum rotation force unit control mechanism is provided with a spiral spring for the maximum rotation force unit control mechanism in a compressed state, the other end center of the movable plate for the maximum rotation force unit control mechanism is provided with a push rod for the maximum rotation force unit control mechanism, the rod body of the push rod for the maximum rotation force unit control mechanism penetrates through the through hole structure for the maximum rotation force unit control mechanism, and the end part of the push rod for the maximum rotation force unit control mechanism is provided with a hemispherical head for the maximum rotation force unit control mechanism in an integrated structure.
Further, the maximum rotation force unit control mechanism is engaged with an internal thread structure in the main thread structure by an external thread structure.
Further, the structural shape and the size of the hemispherical head for the maximum rotation force unit control mechanism are correspondingly the same as those of the hemispherical groove structure.
Further, the telescopic transverse length adjusting mechanism comprises a hollow shell for the telescopic transverse length adjusting mechanism, a hollow structure for the telescopic transverse length adjusting mechanism, a through hole structure for the telescopic transverse length adjusting mechanism, a strip-shaped hemispherical groove structure for the telescopic transverse length adjusting mechanism, a moving plate for the telescopic transverse length adjusting mechanism and a hemispherical protrusion structure for the telescopic transverse length adjusting mechanism; the center in the hollow shell for the telescopic transverse length adjusting mechanism is provided with a hollow structure for the telescopic transverse length adjusting mechanism, the center of one end face of the hollow shell for the telescopic transverse length adjusting mechanism is provided with a through hole structure for the telescopic transverse length adjusting mechanism, two ends of the through hole structure for the telescopic transverse length adjusting mechanism are respectively communicated with the hollow structure for the telescopic transverse length adjusting mechanism and the outside, the hollow shell for the telescopic transverse length adjusting mechanism is provided with a plurality of strip-shaped hemispherical groove structures for the telescopic transverse length adjusting mechanism arranged in an annular array at the inner side of the hollow structure for the telescopic transverse length adjusting mechanism, and the hollow shell for the telescopic transverse length adjusting mechanism is internally provided with a movable plate for the telescopic transverse length adjusting mechanism, the side of the movable plate for the telescopic transverse length adjusting mechanism is provided with a plurality of hemispherical protruding structures for the telescopic transverse length adjusting mechanism which are arranged in an annular array, the center of one end face of the movable plate for the telescopic transverse length adjusting mechanism is fixedly connected with one end of an auxiliary rotating shaft, and a shaft body of the auxiliary rotating shaft penetrates through the through hole structure for the telescopic transverse length adjusting mechanism.
Furthermore, the center of the other end face of the hollow shell for the telescopic transverse length adjusting mechanism is fixedly connected with one end of the main rotating shaft.
Furthermore, the strip-shaped hemispherical groove structures for the telescopic transverse length adjusting mechanisms and the hemispherical convex structures for the telescopic transverse length adjusting mechanisms are arranged in an annular array around the axis of the hollow shell for the telescopic transverse length adjusting mechanisms as the circle center.
Further, the turbocharging mounting mechanism comprises a cylindrical hollow shell for the turbocharging mounting mechanism, a turbine mounting space for the turbocharging mounting mechanism, a bearing mounting hole for the turbocharging mounting mechanism, a liquid inlet pipeline body for the turbocharging mounting mechanism, a liquid outlet pipeline body for the turbocharging mounting mechanism, a liquid inlet pipeline hole for the turbocharging mounting mechanism and a liquid outlet pipeline hole for the turbocharging mounting mechanism; the center of the interior of the cylindrical hollow shell for the turbo-charging installation mechanism is provided with a turbo-charging installation space for the turbo-charging installation mechanism, one side of the top of the cylindrical hollow shell for the turbo-charging installation mechanism is provided with a liquid inlet pipeline body for the turbo-charging installation mechanism which is of an integral structure with the cylindrical hollow shell for the turbo-charging installation mechanism, the interior of the liquid inlet pipeline body for the turbo-charging installation mechanism is provided with a liquid inlet pipeline hole for the turbo-charging installation mechanism which is communicated with the outside and the turbo-charging installation space for the turbo-charging installation mechanism, one side of the bottom of the cylindrical hollow shell for the turbo-charging installation mechanism is provided with a liquid outlet pipeline body for the turbo-charging installation mechanism which is of an integral structure with the cylindrical hollow shell for the turbo-charging installation mechanism, the interior of the liquid outlet pipeline body for the, the center of the cylindrical hollow shell for the turbocharging installation mechanism is provided with a bearing installation hole for the turbocharging installation mechanism.
Furthermore, the main bearing is installed in the bearing installation hole for the turbocharger installation mechanism, and the bottom of the cylindrical hollow shell for the turbocharger installation mechanism is fixed to the top of the turbine installation base plate.
Further, the liquid inlet pipeline body for the turbocharging installation mechanism and the side line of the liquid discharge pipeline body for the turbocharging installation mechanism are connected with the circumference of the cylindrical hollow shell for the turbocharging installation mechanism in a tangent mode.
Compared with the prior art, the invention has the beneficial effects that: the device is used for the pressurization effect of liquid output, so that the pressure value and the flow of output liquid are ensured, the maximum pressure value of the pressurization value can be effectively controlled, the water pressure and the water flow in a main water pumping pipeline are not influenced too much, the adaptability is strong, the device is provided with a maximum rotation force unit control mechanism, the maximum torque force during rotation can be effectively controlled, and the maximum torque force is converted into the maximum output pressure value during pressurization.
Drawings
FIG. 1 is a schematic diagram of a full-sectional structure of a pressure boosting device with output pressure control function according to the present invention;
fig. 2 is a schematic structural diagram of a control mechanism of a maximum rotation force unit in a pressure boosting device with an output pressure control function according to the present invention;
FIG. 3 is a schematic structural view of a transverse length adjustment mechanism for flexibility in a pressure boosting apparatus with output pressure control according to the present invention;
FIG. 4 is a schematic structural diagram of a turbocharger mounting mechanism in a pressure increasing device with output pressure control according to the present invention;
in the figure: 1, bottom mounting base plate, 2, main bolt, 3, motor mounting plate, 4, motor, 5, turbine mounting base plate, 6, motor spindle, 7, hollow rotating housing, 8, main hollow structure, 9, main through hole structure, 10, screw hole, 11, main thread structure, 12, maximum rotation force unit control mechanism, 121, hollow housing for maximum rotation force unit control mechanism, 122, external thread structure for maximum rotation force unit control mechanism, 123, limiting plate for maximum rotation force unit control mechanism, 124, through hole structure for maximum rotation force unit control mechanism, 125, hollow structure for maximum rotation force unit control mechanism, 126, external thread structure for maximum rotation force unit control mechanism, 123, movable plate for maximum rotation force unit control mechanism, 128, push rod for maximum rotation force unit control mechanism, movable plate, and the like, 129, hemispherical head for maximum rotation force unit control mechanism, 13, main rotating shaft, 14, main circular plate, 15, main hemispherical groove structure, 16, telescopic lateral length adjusting mechanism, 161, hollow housing for telescopic lateral length adjusting mechanism, 162, hollow structure for telescopic lateral length adjusting mechanism, 163, through hole structure for telescopic lateral length adjusting mechanism, 164, strip-shaped hemispherical groove structure for telescopic lateral length adjusting mechanism, 165, moving plate for telescopic lateral length adjusting mechanism, 166, hemispherical protrusion structure for telescopic lateral length adjusting mechanism, 17, auxiliary rotating shaft, 18, turbo-charging installation mechanism, 181, cylindrical hollow housing for turbo-charging installation mechanism, 182, turbo-charging installation mechanism turbine installation space, 183, bearing installation hole for turbo-charging installation mechanism, 184, liquid inlet pipe body for turbo-charging installation mechanism, liquid inlet pipe body for liquid inlet pipe body, and liquid outlet pipe body, 185, liquid discharge pipe bodies 186 for a turbocharging installation mechanism, liquid inlet pipe holes 187 for the turbocharging installation mechanism, liquid discharge pipe holes 19 for the turbocharging installation mechanism, main turbines 20 and main bearings.
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 device comprises a bottom mounting base plate 1, a plurality of main bolts 2 for mounting are arranged in the bottom mounting base plate 1, a motor mounting plate 3 is mounted on one side of the upper surface of the bottom mounting base plate 1, a turbine mounting base plate 5 is mounted on the other side of the upper surface of the bottom mounting base plate 1, a motor 4 is mounted on the top of the motor mounting plate 3, a turbocharger mounting mechanism 18 is mounted on the top of the turbine mounting base plate 5, an auxiliary rotating shaft 17 is mounted at the center of the turbocharger mounting mechanism 18, the shaft body of the auxiliary rotating shaft 17 is mounted in the turbocharger mounting mechanism 18 through a main bearing 20, a main turbine 19 is mounted on the shaft body positioned in the turbocharger mounting mechanism 18 on the auxiliary rotating shaft 17, and the end part of a motor main shaft 6 in the motor 4 is connected with a hollow rotating shell 7 through a connecting plate, a main hollow structure 8 is arranged at the center of the hollow rotary shell 7, a main through hole structure 9 communicated with the main hollow structure 8 is arranged at the center of one end face of the hollow rotary shell 7, a plurality of threaded holes 10 arranged in an annular array around the axis of the hollow rotary shell 7 as the circle center are arranged at the end face of the hollow rotary shell 7, a main rotating shaft 13 is arranged inside the main through hole structure 9, a main circular plate 14 is arranged at one end inside the main hollow structure 8 of the main rotating shaft 13, a plurality of main hemispherical groove structures 15 arranged in an annular array around the axis of the main circular plate 14 as the circle center are arranged at one end face of the main circular plate 14, a maximum rotary force unit control mechanism 12 is connected inside each threaded hole 10 through a main threaded structure 11, and a transverse telescopic length adjusting mechanism 16 is arranged at the other end of the main rotating shaft 13, one end of the telescopic transverse length adjusting mechanism 16 is fixedly connected with the end of the auxiliary rotating shaft 17.
Referring to fig. 2, the maximum rotation force unit control mechanism 12 includes a hollow housing 121 for the maximum rotation force unit control mechanism, an external thread structure 122 for the maximum rotation force unit control mechanism, a limiting plate 123 for the maximum rotation force unit control mechanism, a through hole structure 124 for the maximum rotation force unit control mechanism, a hollow structure 125 for the maximum rotation force unit control mechanism, a moving plate 126 for the maximum rotation force unit control mechanism, a coil spring 127 for the maximum rotation force unit control mechanism, a push rod 128 for the maximum rotation force unit control mechanism, and a hemispherical head 129 for the maximum rotation force unit control mechanism; the outer side of the hollow shell 121 for the maximum rotation force unit control mechanism is provided with an external thread structure 122 for the maximum rotation force unit control mechanism, one end of the side of the hollow shell 121 for the maximum rotation force unit control mechanism is provided with a limit plate 123 for the maximum rotation force unit control mechanism of an integral structure with the hollow shell, the inside of the hollow shell 121 for the maximum rotation force unit control mechanism is provided with a hollow structure 125 for the maximum rotation force unit control mechanism, the center of one end face of the hollow shell 121 for the maximum rotation force unit control mechanism is provided with a through hole structure 124 for the maximum rotation force unit control mechanism, the inside of the hollow structure 125 for the maximum rotation force unit control mechanism is provided with a movable plate 126 for the maximum rotation force unit control mechanism, one end face of the movable plate 126 for the maximum rotation force unit control mechanism is provided with a spiral spring 127 for the maximum rotation force unit control mechanism in a compressed state, a push rod 128 for the maximum rotation force unit control mechanism is installed at the center of the other end of the moving plate 126 for the maximum rotation force unit control mechanism, the rod body of the push rod 128 for the maximum rotation force unit control mechanism penetrates through the through hole structure 124 for the maximum rotation force unit control mechanism, and the end of the push rod 128 for the maximum rotation force unit control mechanism is provided with a hemispherical head 129 for the maximum rotation force unit control mechanism which is integrated with the push rod; the external thread structure 122 for the maximum rotation force unit control mechanism is meshed with the internal thread structure in the main thread structure 11; the structural shape and size of the hemispherical head 129 for the maximum rotation force unit control mechanism are the same as those of the hemispherical groove structure 15, and the maximum rotation force unit control mechanism mainly has the following functions: since the maximum rotation force unit control mechanism is engaged with the internal thread structure in the main thread structure 11 by the external thread structure 122; the structure appearance and the size of the hemispherical head 129 for the maximum rotation force unit control mechanism correspond to the structure appearance and the size of the hemispherical groove structure 15, so the device can be screwed into the inner part of each threaded hole 10 under the action of a threaded structure, and because the helical spring 127 for the maximum rotation force unit control mechanism is in a compression state, the hemispherical head 129 for the maximum rotation force unit control mechanism can be abutted to the inner part of the hemispherical groove structure 15, when the force required by rotation is greater than the elastic force of the helical spring 127 for the maximum rotation force unit control mechanism, the helical spring 127 for the maximum rotation force unit control mechanism can be compressed, and the hemispherical head 129 for the maximum rotation force unit control mechanism can exit the hemispherical groove structure 15, so that relative rotation is realized.
Referring to fig. 3, the stretchable lateral length adjustment mechanism 16 includes a stretchable lateral length adjustment mechanism hollow housing 161, a stretchable lateral length adjustment mechanism hollow structure 162, a stretchable lateral length adjustment mechanism through hole structure 163, a stretchable lateral length adjustment mechanism strip-shaped hemispherical groove structure 164, a stretchable lateral length adjustment mechanism moving plate 165, and a stretchable lateral length adjustment mechanism hemispherical protrusion structure 166; a hollow structure 162 for a telescopic transverse length adjusting mechanism is arranged at the center inside the hollow shell 161 for the telescopic transverse length adjusting mechanism, a through hole structure 163 for the telescopic transverse length adjusting mechanism is arranged at the center of one end face of the hollow shell 161 for the telescopic transverse length adjusting mechanism, two ends of the through hole structure 163 for the telescopic transverse length adjusting mechanism are respectively communicated with the hollow structure 162 for the telescopic transverse length adjusting mechanism and the outside, the hollow shell 161 for the telescopic transverse length adjusting mechanism is provided with a plurality of strip-shaped hemispherical groove structures 164 for the telescopic transverse length adjusting mechanism arranged in an annular array at the inner side of the hollow structure 162 for the telescopic transverse length adjusting mechanism, and a movable plate 165 for the telescopic transverse length adjusting mechanism is arranged inside the hollow structure 162 for the telescopic transverse length adjusting mechanism, a plurality of hemispherical convex structures 166 for the telescopic transverse length adjusting mechanism are arranged on the side surface of the movable plate 165 for the telescopic transverse length adjusting mechanism in an annular array, the center of one end surface of the movable plate 165 for the telescopic transverse length adjusting mechanism is fixedly connected with one end of the auxiliary rotating shaft 17, and the shaft body of the auxiliary rotating shaft 17 penetrates through the through hole structure 163 for the telescopic transverse length adjusting mechanism; the center of the other end face of the hollow housing 161 for the telescopic transverse length adjustment mechanism is fixedly connected with one end of the main rotating shaft 13; the plurality of bar-shaped hemispherical groove structures 164 for the telescopic transverse length adjusting mechanism and the hemispherical protrusion structures 166 for the telescopic transverse length adjusting mechanism are all arranged in an annular array around the axis line of the hollow shell 161 for the telescopic transverse length adjusting mechanism as the circle center, and mainly function as: the center of the other end face of the hollow housing 161 for the telescopic transverse length adjustment mechanism is fixedly connected with one end of the main rotating shaft 13; since the plurality of bar-shaped hemispherical groove structures 164 for the stretchable lateral length adjustment mechanism and the plurality of hemispherical protrusion structures 166 for the stretchable lateral length adjustment mechanism are arranged in an annular array around the axis line of the hollow housing 161 for the stretchable lateral length adjustment mechanism as the center of circle, the hollow housing 161 for the stretchable lateral length adjustment mechanism and the movable plate 165 for the stretchable lateral length adjustment mechanism can transmit the rotation state therebetween without affecting the lateral movement of the movable plate 165 for the stretchable lateral length adjustment mechanism.
Referring to fig. 4, the turbocharger mounting mechanism 18 includes a cylindrical hollow housing 181 for the turbocharger mounting mechanism, a turbine mounting space 182 for the turbocharger mounting mechanism, a bearing mounting hole 183 for the turbocharger mounting mechanism, a liquid inlet pipe body 184 for the turbocharger mounting mechanism, a liquid discharge pipe body 185 for the turbocharger mounting mechanism, a liquid inlet pipe hole 186 for the turbocharger mounting mechanism, and a liquid discharge pipe hole 187 for the turbocharger mounting mechanism; the inside center of cylindrical hollow shell 181 for turbocharged installation mechanism is provided with turbo installation space 182 for installation mechanism, one side at cylindrical hollow shell 181 top for turbocharged installation mechanism is provided with the inlet channel body 184 for turbocharged installation mechanism of cylindrical hollow shell 181 formula structure as an organic whole for installation mechanism of turbocharged installation, the inside of inlet channel body 184 for installation mechanism of turbocharged installation is provided with the outside inlet channel hole 186 for installation mechanism of turbocharged installation that communicates with turbo installation space 182 for installation mechanism of turbocharged installation mechanism with the outside, one side of cylindrical hollow shell 181 bottom for installation mechanism of turbocharged installation is provided with the drain channel body 185 for installation mechanism of turbocharged installation mechanism with cylindrical hollow shell 181 formula structure as an organic whole, the inside of drain channel body 185 for installation mechanism of turbocharged installation is provided with the outside and turbo installation space 182 for installation of turbocharged installation mechanism's turbo installation space A liquid discharge pipe hole 187 for a pressure mounting mechanism, wherein a bearing mounting hole 183 for a turbo charging mounting mechanism is provided in the center of the cylindrical hollow housing 181 for a turbo charging mounting mechanism; the main bearing 17 is installed in the bearing installation hole 183 for the turbo-charging installation mechanism, and the bottom of the cylindrical hollow shell 181 for the turbo-charging installation mechanism is fixed on the top of the turbine installation base plate 5; the liquid inlet pipeline body 184 for the turbocharging installation mechanism and the liquid discharge pipeline body 185 for the turbocharging installation mechanism are connected with the circumference tangent type of the cylindrical hollow shell 181 for the turbocharging installation mechanism, and the main functions are as follows: when the liquid inlet pipeline body 184 for the turbocharging installation mechanism is used, the end part of the liquid inlet pipeline body 184 for the turbocharging installation mechanism is connected with a pipeline placed in a reservoir, and then the end part of the liquid outlet pipeline body 185 for the turbocharging installation mechanism is connected with a pipeline connected with a main drainage pipeline.
The specific use mode is as follows: in the work of the invention, the bottom mounting base plate 1 is fixed on a work position through a bolt, then a water pumping pipeline is connected with the turbocharging mounting mechanism 18, when the water pumping pipeline works, the motor 4 is turned on, at the moment, the motor 4 drives each part to rotate, under the transmission of force, the main turbine 19 rapidly rotates, so that liquid in the reservoir enters the main discharge pipeline, when the water pressure is too high due to the too high rotating speed of the main turbine 19, the maximum rotating force unit control mechanism 12 works, so that the motor 4 continues to rotate, and the main turbine 19 stops working, thereby preventing the too high water pressure.
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. A supercharging device with output pressure control function, comprising a bottom mounting substrate (1), characterized in that: the bottom mounting base plate (1) is internally provided with a plurality of main bolts (2) for mounting, one side of the upper surface of the bottom mounting base plate (1) is provided with a motor mounting plate (3), the other side of the upper surface of the bottom mounting base plate (1) is provided with a turbine mounting base plate (5), the top of the motor mounting plate (3) is provided with a motor (4), the top of the turbine mounting base plate (5) is provided with a turbine supercharging mounting mechanism (18), the center of the turbine supercharging mounting mechanism (18) is provided with an auxiliary rotating shaft (17), the shaft body of the auxiliary rotating shaft (17) is mounted in the turbine supercharging mounting mechanism (18) through a main bearing (20), the auxiliary rotating shaft (17) is provided with a main turbine (19) on the shaft body positioned in the turbine supercharging mounting mechanism (18), and the end part of a motor main shaft (6) in the motor (4) is connected with a hollow rotating shell (7) through a connecting, the center of the hollow rotating shell (7) is provided with a main hollow structure (8), the center of one end face of the hollow rotating shell (7) is provided with a main through hole structure (9) communicated with the main hollow structure (8), the end face of the hollow rotating shell (7) is provided with a plurality of threaded holes (10) which are arranged in an annular array mode by taking the axial lead of the hollow rotating shell (7) as the circle center, a main rotating shaft (13) is installed inside the main through hole structure (9), one end of the main rotating shaft (13) positioned inside the main hollow structure (8) is provided with a main circular plate (14), one end face of the main circular plate (14) is provided with a plurality of main hemispherical groove structures (15) which are arranged in an annular array mode by taking the axial lead of the main circular plate (14) as the circle center, and the inside of each threaded hole (10) is connected with a maximum rotating force unit control mechanism (12) through a main threaded structure (, the other end of the main rotating shaft (13) is provided with a telescopic transverse length adjusting mechanism (16), and one end of the telescopic transverse length adjusting mechanism (16) is fixedly connected with the end part of the auxiliary rotating shaft (17);
the telescopic transverse length adjusting mechanism (16) comprises a hollow shell (161) for the telescopic transverse length adjusting mechanism, a hollow structure (162) for the telescopic transverse length adjusting mechanism, a through hole structure (163) for the telescopic transverse length adjusting mechanism, a strip-shaped hemispherical groove structure (164) for the telescopic transverse length adjusting mechanism, a moving plate (165) for the telescopic transverse length adjusting mechanism and a hemispherical convex structure (166) for the telescopic transverse length adjusting mechanism; the horizontal length adjustment mechanism of elasticity is with hollow structure (162) for the horizontal length adjustment mechanism of elasticity is provided with at the inside center of hollow shell (161) for the horizontal length adjustment mechanism of elasticity, horizontal length adjustment mechanism of elasticity is with hollow shell (161) terminal surface center of being provided with horizontal length adjustment mechanism of elasticity through-hole structure (163) for the horizontal length adjustment mechanism of elasticity, the horizontal length adjustment mechanism of elasticity communicates horizontal length adjustment mechanism respectively with hollow structure (162) for the horizontal length adjustment mechanism of elasticity and external world, horizontal length adjustment mechanism of elasticity is in being located hollow shell (161) for the horizontal length adjustment mechanism of elasticity is provided with a plurality of horizontal length adjustment mechanism of elasticity for the horizontal length adjustment mechanism of elasticity bar half spherical groove structure (164) that are the ring array setting, horizontal length adjustment mechanism of elasticity is in being located hollow shell (161) for the horizontal length adjustment mechanism of elasticity is with an internally mounted scalability of hollow structure (162) A movable plate (165) for a transverse length adjusting mechanism, wherein a plurality of hemispherical convex structures (166) which are arranged in an annular array and used for the telescopic transverse length adjusting mechanism are arranged on the side surface of the movable plate (165) for the telescopic transverse length adjusting mechanism, the center of one end surface of the movable plate (165) for the telescopic transverse length adjusting mechanism is fixedly connected with one end of an auxiliary rotating shaft (17), and a shaft body of the auxiliary rotating shaft (17) penetrates through a through hole structure (163) used for the telescopic transverse length adjusting mechanism;
the center of the other end face of the hollow shell (161) for the telescopic transverse length adjusting mechanism is fixedly connected with one end of the main rotating shaft (13);
the plurality of bar-shaped hemispherical groove structures (164) for the telescopic transverse length adjusting mechanism and the hemispherical protrusion structures (166) for the telescopic transverse length adjusting mechanism are arranged in an annular array around the axis line of the hollow shell (161) for the telescopic transverse length adjusting mechanism as the circle center.
2. A booster device with an output pressure control function according to claim 1, wherein: the maximum rotation force unit control mechanism (12) comprises a hollow shell (121) for the maximum rotation force unit control mechanism, an external thread structure (122) for the maximum rotation force unit control mechanism, a limiting plate (123) for the maximum rotation force unit control mechanism, a through hole structure (124) for the maximum rotation force unit control mechanism, a hollow structure (125) for the maximum rotation force unit control mechanism, a moving plate (126) for the maximum rotation force unit control mechanism, a spiral spring (127) for the maximum rotation force unit control mechanism, a push rod (128) for the maximum rotation force unit control mechanism and a hemispherical head (129) for the maximum rotation force unit control mechanism; the outer side of the hollow shell (121) for the maximum rotation force unit control mechanism is provided with an external thread structure (122) for the maximum rotation force unit control mechanism, one end of the side surface of the hollow shell (121) for the maximum rotation force unit control mechanism is provided with a limiting plate (123) for the maximum rotation force unit control mechanism which is of an integral structure with the hollow shell, the inside of the hollow shell (121) for the maximum rotation force unit control mechanism is provided with a hollow structure (125) for the maximum rotation force unit control mechanism, the center of one end surface of the hollow shell (121) for the maximum rotation force unit control mechanism is provided with a through hole structure (124) for the maximum rotation force unit control mechanism, and a movable plate (126) for the maximum rotation force unit control mechanism is placed in the hollow structure (125) for the maximum rotation force unit control mechanism, the end face of the movable plate (126) for the maximum rotation force unit control mechanism is provided with a spiral spring (127) for the maximum rotation force unit control mechanism in a compressed state, the other end center of the movable plate (126) for the maximum rotation force unit control mechanism is provided with a push rod (128) for the maximum rotation force unit control mechanism, the rod body of the push rod (128) for the maximum rotation force unit control mechanism penetrates through the through hole structure (124) for the maximum rotation force unit control mechanism, and the end part of the push rod (128) for the maximum rotation force unit control mechanism is provided with a hemispherical head (129) for the maximum rotation force unit control mechanism in an integrated structure.
3. A booster device with an output pressure control function according to claim 2, wherein: the maximum rotation force unit control mechanism is meshed with an internal thread structure in the main thread structure (11) through an external thread structure (122).
4. A booster device with an output pressure control function according to claim 2, wherein: the structural shape and the size of the hemispherical head (129) for the maximum rotation force unit control mechanism are correspondingly the same as those of the hemispherical groove structure (15).
5. A booster device with an output pressure control function according to claim 1, wherein: the turbocharging installation mechanism (18) comprises a cylindrical hollow shell (181) for the turbocharging installation mechanism, a turbocharging installation space (182) for the turbocharging installation mechanism, a bearing installation hole (183) for the turbocharging installation mechanism, a liquid inlet pipeline body (184) for the turbocharging installation mechanism, a liquid outlet pipeline body (185) for the turbocharging installation mechanism, a liquid inlet pipeline hole (186) for the turbocharging installation mechanism and a liquid outlet pipeline hole (187) for the turbocharging installation mechanism; the turbine installation mechanism is provided with turbine installation space (182) for the turbine pressurization installation mechanism at the center inside cylindrical hollow shell (181), one side at the top of the cylindrical hollow shell (181) for the turbine pressurization installation mechanism is provided with a liquid inlet pipeline body (184) for the turbine pressurization installation mechanism of the integrated structure with the cylindrical hollow shell (181) for the turbine pressurization installation mechanism, the inside of the liquid inlet pipeline body (184) for the turbine pressurization installation mechanism is provided with a liquid inlet pipeline hole (186) for the turbine pressurization installation mechanism which is communicated with the turbine installation space (182) for the turbine pressurization installation mechanism, one side at the bottom of the cylindrical hollow shell (181) for the turbine pressurization installation mechanism is provided with a liquid outlet pipeline body (185) for the turbine pressurization installation mechanism of the integrated structure with the cylindrical hollow shell (181) for the turbine pressurization installation mechanism, the inside of the liquid discharge pipeline body (185) for the turbocharging installation mechanism is provided with a liquid discharge pipeline hole (187) for the turbocharging installation mechanism, which is communicated with the outside and a turbocharging installation space (182) for the turbocharging installation mechanism, and the center of the cylindrical hollow shell (181) for the turbocharging installation mechanism is provided with a bearing installation hole (183) for the turbocharging installation mechanism.
6. A booster device with an output pressure control function according to claim 5, wherein: the main bearing (17) is arranged in the bearing mounting hole (183) for the turbocharging mounting mechanism, and the bottom of the cylindrical hollow shell (181) for the turbocharging mounting mechanism is fixed on the top of the turbocharging mounting base plate (5).
7. A booster device with an output pressure control function according to claim 5, wherein: the liquid inlet pipeline body (184) for the turbocharging installation mechanism and the liquid discharge pipeline body (185) for the turbocharging installation mechanism are connected with the circumference of the cylindrical hollow shell (181) for the turbocharging installation mechanism in a tangent mode.
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| CN110653231A (en) * | 2019-10-16 | 2020-01-07 | 徐福余 | Roller fixing and rotating device for cleaning interior of roller-shaped object |
| CN111108857A (en) * | 2020-02-18 | 2020-05-08 | 泉州佰特产品设计服务有限公司 | Gardens are with supporting shell type of agricultural machinery and dig concave device |
| CN111365382A (en) * | 2020-03-17 | 2020-07-03 | 泉州市鑫鼎合德技术服务有限公司 | Integrative multi-functional formula rotary part middle part connecting device |
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| CN203674953U (en) * | 2013-03-22 | 2014-06-25 | 林英楠 | Permanent magnet speed regulation, brake or load apparatus capable of stepless adjustment of magnetic field intensity |
| CN204755329U (en) * | 2015-06-28 | 2015-11-11 | 响水县智诚知识产权信息服务有限公司 | Velocity of flow adjustable water pump |
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