CN109143118A - A kind of energy-saving monitoring equipment - Google Patents
A kind of energy-saving monitoring equipment Download PDFInfo
- Publication number
- CN109143118A CN109143118A CN201811204637.7A CN201811204637A CN109143118A CN 109143118 A CN109143118 A CN 109143118A CN 201811204637 A CN201811204637 A CN 201811204637A CN 109143118 A CN109143118 A CN 109143118A
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- face
- electricity federation
- cavity
- wall
- left end
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R19/00—Arrangements for measuring currents or voltages or for indicating presence or sign thereof
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/44—Testing lamps
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)
Abstract
The invention discloses a kind of energy-saving monitoring equipment, including fuselage and the holding tank being arranged in fuselage right end end face, the holding tank left end is equipped with the first cavity, supports loadboard is slidably connected in the holding tank, the supports loadboard right end is fixedly connected with barrel shell on end face, the barrel shell right end is fixedly connected with annulus pressure head on end face, rubber suction nozzle is equipped in the annulus pressure head, the rubber suction nozzle is heaved end and is put in inside the barrel shell, the supports loadboard right end is embedded with the first pusher in end face, the first pusher right end end is connected by power the pressing plate to squeeze the rubber suction nozzle, the supports loadboard screw-internal thread fit is connected with the threaded rod that symmetrical above and below and left and right extends.
Description
Technical field
The present invention relates to energy-conserving and emission-cutting technology field, specifically a kind of energy-saving monitoring equipment.
Background technique
With the reach of science, social progress, today's society continues to develop energy-saving and emission-reduction objective, and energy conservation is as main
Sustainable development policy, the technology of various aspects requires timely to update and innovate, and in energy-conserving and emission-cutting technology field,
Always exist monitoring aspect technical problem, general energy-saving illuminator there are it is unqualified the problems such as, cause its energy conservation
Effect is poor, does not deposit itself mechanism for monitoring again, and when use is not easy to find specific energy-saving effect, and even if equipped with monitoring
Device, it is also difficult to monitor the data of very standard, observation information is difficult, and the mechanism for providing power-off energy saving also lacks, and installs
Difficulty, the device of the invention solve this problem in that.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of energy-saving monitoring equipment, are able to solve above-mentioned present technology
The problems in.
The present invention is achieved through the following technical solutions: a kind of energy-saving monitoring equipment of the invention, including fuselage with
And the holding tank in fuselage right end end face is set, the holding tank left end is equipped with the first cavity, slides in the holding tank
It is dynamic to be connected with supports loadboard, barrel shell is fixedly connected on supports loadboard right end end face, on barrel shell right end end face
It is fixedly connected with annulus pressure head, is equipped with rubber suction nozzle in the annulus pressure head, the rubber suction nozzle heaves end and puts in the barrel shell
Inside is embedded with the first pusher in supports loadboard right end end face, and the first pusher right end end has been connected by power
To squeeze the pressing plate of the rubber suction nozzle, the supports loadboard screw-internal thread fit is connected with the spiral shell that symmetrical above and below and left and right extends
Rasp bar, the threaded rod left end put in first cavity and are equipped with first pulley, and first cavity left end inner wall is embedded
Equipped with the first motor, the first motor right end end has been connected by power the second belt wheel, second belt wheel and described the
It has been connected by power belt between one belt wheel, the annular groove of opening to the left, the annulus groove top are equipped in the end face of the fuselage left end
It is communicated in portion's inner wall equipped with the second cavity, is fixedly connected with the fixation positioned at the annulus groove center on the end face of the fuselage left end
Block is equipped with hinged ball groove in the end face of the fixed block left end, is hingedly connected with sphere, the sphere left end in the hinged ball groove
End is fixedly connected with light source scanning support plate, and the scanning support plate left end end face is equipped with light source scanner, in the annular groove
It is rotatably assorted and is connected with external tooth cannulated sleeve, external tooth cannulated sleeve left end is equipped with to slide with the light source scanning support plate
The rake of mating connection is embedded with the second motor, the second motor right end end in the inner wall of second cavity left end
End is connected by power to the tooth runner with the ratcheting connection of external tooth cannulated sleeve, and the fuselage left end is embedded with position in end face
In the light source information processor of the fixed block right end, the light source information processor and the light source scanner Electricity Federation are described
The first guide runner being equipped between the annular groove and first cavity in fuselage, first guide runner is interior to be equipped with certainly
Dynamic circuit breaker electricity current monitoring mechanism is equipped in the fuselage bottom end face positioned at the first slide guide trench bottom and Open Side Down the
Two guide runners, second guide runner is interior to be equipped with induction automatic spring elecscreen indication mechanism.
It may be preferred that the current monitoring mechanism that automatically powers off includes communicating to be equipped in the inner wall of first guide runner rear end
Groove, fixed hook is equipped in the groove, is slidably connected with the first slider guide in first guide runner, described the
One slider guide is interior to be equipped with opening backward and the third cavity to communicate with the groove, in the third cavity on the inner wall of left and right
It is fixedly connected with the fixed link that left and right extends, is rotatably assorted in the fixed link and is connected with to be engaged with the fixed hook
Rotational hook, press, which is equipped with, between the rotational hook rear end face and third cavity rear end inner wall is located at the fixed link
The top pressure spring of bottom, the rotational hook front end surface are equipped with the permanent magnets positioned at the top pressure spring front end, and described the
Three cavity bottom inner walls are equipped with the electromagnetic block positioned at the permanent magnets front end, are embedded with described in being located in first slider guide
The current detector of third cavity left end, the interior interlocking electricity equipped with bilateral symmetry opening upwards of the first slider guide top end surface
Join slot, live wire of connecting between interlocking Electricity Federation slot, the current detector and the electromagnetic block described in left end, first slide guide
The terminal screw positioned at the interlocking Electricity Federation groove top portion is embedded in slot top inner wall, the terminal screw bottom end puts in institute
State in the first guide runner and to interlocking Electricity Federation slot interlocking Electricity Federation, the is embedded in the first guide runner bottom interior wall
Two pushers, the second Electricity Federation slot top end is connected by power the telescopic rod extended up and down, consequently facilitating in monitoring current
Timely power-off energy saving while flow.
It may be preferred that the automatic spring elecscreen indication mechanism includes that sliding connection is arranged in second guide runner
The second interior slider guide, is fixedly connected with display elecscreen on the second slider guide bottom end face, at the top of second slider guide
Third pusher, the third pusher are connected by power on end face, third pusher outer surface is embedded at described second
In guide runner top inner wall and connection fixed thereto, it is embedded in second slider guide and the Electricity Federation of the display elecscreen Electricity Federation
Line, the Electricity Federation line run through the second slider guide front/rear end, before and after second guide runner inner wall be equipped with to institute
The export head of Electricity Federation line docking is stated, is equipped with processor in the front fuselage end face, there is heat in processor left end end Electricity Federation
Source scanner, the processor and third pusher Electricity Federation, consequently facilitating the arrival of the automatic sensing people of device, and in time
Be pushed out information display screen for observe data information.
The beneficial effects of the present invention are: the supports loadboard is located at the holding tank left end due in the initial state,
The rubber sucker is fully located in the holding tank, and the rubber sucker is in fully expanded state, first slider guide
Positioned at the first guide runner top, the terminal screw and the interlocking Electricity Federation slot interlocking, the fixed hook with it is described
Rotational hook snapping, second slider guide are located at the second guide runner top, and the display elecscreen is fully located at described
In second guide runner, consequently facilitating the maintenance of device.
When the work is required, device is picked up first and is attached on metope, then started first motor and drive institute
The rotation of the second belt wheel is stated, the supports loadboard, the barrel shell are driven by the belt, the first pulley and the threaded rod
It is integrally moved to right with the annulus pressure head and skids off the holding tank, until the rubber sucker is tightly attached on metope, then opened
It moves pressing plate described in first pushers to move to right, the rubber sucker discharge air is compressed, at this point, device is tightly adsorbed on
On wall, then the household light fixtures of energy-saving monitoring will be needed to access on the terminal screw, the current detector accesses electric current
And its flow is monitored, and if current flow is flowed through according to energy-efficient standard, the electromagnetic block stable operation, the fixed hook and institute
It states rotational hook and stablizes snapping, if electric current index is more than energy conservation standard, the electromagnetic block magnetic force is unstable, the swinging hanger
Rotation is detached from the fixed hook, and due to the effect of the gravity, first slider guide glides, the terminal screw with it is described
Rabbet Electricity Federation slot to be detached from, to power off to lamps and lanterns, if desired restore electric power, need to only start first pusher makes described stretch
Bar elongation, which pushes, to be moved to initial position on first slider guide and accesses electric power, meanwhile, in second motor running simultaneously
Constantly by the rotation of external tooth cannulated sleeve described in the tooth driven by rotating wheel, the external tooth cannulated sleeve is continuous by the inclined plane part
The light source scanning support plate is driven to shake handoff angle, thus lifting device monitoring effect and diversity.
When needing artificial observation energy-saving index, need to only walk about to by device, the heat source scanner automatic sensing heat
Source information, and the processor is communicated information to, due to the processor and third pusher Electricity Federation, push described second
Slider guide moves down, and drives the display elecscreen to move down and skids off second guide runner, until the Electricity Federation line and the export head
Docking, shows information when opening, when people leaves, elecscreen can be shown described in automatic accomodation, thus lifting device practical performance.
The configuration of the present invention is simple, it is easy to operate, by using collect convenient installing mechanism, automatically power off current monitoring mechanism,
Automatic spring elecscreen indication mechanism and multidimensional light source sensing mechanisms are in one, and ingenious in design, structure is simplified, installation convenience, function
Can be comprehensively easy-to-use, it is applicable in monitoring type and enriches, practical performance is preferable.
Detailed description of the invention
The present invention is described in detail by following specific embodiments and drawings for ease of explanation,.
Fig. 1 is overall structure diagram inside a kind of energy-saving monitoring equipment of the invention；
Fig. 2 is the partial enlargement structural representation of A in Fig. 1；
Fig. 3 is the schematic cross-section of B in Fig. 2.
Specific embodiment
As shown in Figure 1, Figure 2 and Figure 3, a kind of energy-saving monitoring equipment of the invention, including fuselage 100 and setting are described
Holding tank 130 in 100 right end end face of fuselage, 130 left end of holding tank is equipped with the first cavity 126, in the holding tank 130
It is slidably connected with supports loadboard 127, is fixedly connected with barrel shell 120, the barrel shell on the 127 right end end face of supports loadboard
It is fixedly connected with annulus pressure head 129 on 120 right end end faces, is equipped with rubber suction nozzle 128, the rubber in the annulus pressure head 129
Suction nozzle 128 is heaved end and is put in inside the barrel shell 120, is embedded with the first pusher in the 127 right end end face of supports loadboard
125, the 125 right end end of the first pusher is connected by power the pressing plate 124 to squeeze the rubber suction nozzle 128, described
127 screw-internal thread fit of supports loadboard is connected with the threaded rod 119 that symmetrical above and below and left and right extends, and 119 left end of threaded rod is stretched
In into first cavity 126 and it is equipped with first pulley 118, it is electronic to be embedded with first in the 126 left end inner wall of the first cavity
Machine 122, the 122 right end end of the first motor have been connected by power the second belt wheel 123, second belt wheel 123 and described the
It has been connected by power belt 121 between one belt wheel 118, the annular groove 102 of opening to the left is equipped in the 100 left end end face of fuselage,
It is communicated in 102 top inner wall of annular groove equipped with the second cavity 103, is fixedly connected with position on the 100 left end end face of fuselage
Fixed block 109 in 102 center of annular groove is equipped with hinged ball groove 149, the hinge in the 109 left end end face of fixed block
Sphere 110 is hingedly connected in ball receiving groove 149, the 110 left end end of sphere is fixedly connected with light source scanning support plate 106, institute
It states scanning 106 left end end face of support plate and is equipped with light source scanner 107, be rotatably assorted in the annular groove 102 and be connected with external tooth sky
Heart sleeve 105,105 left end of external tooth cannulated sleeve are equipped with to be slidably connected with the light source scanning support plate 106
Rake is embedded with the second motor 101, the 101 right end end of the second motor in the 103 left end inner wall of the second cavity
It is connected by power to the tooth runner 104 with the ratcheting connection of the external tooth cannulated sleeve 105, in the 100 left end end face of fuselage
It is embedded with the light source information processor 108 positioned at 109 right end of fixed block, the light source information processor 108 and the light
107 Electricity Federation of source scanner, interior first be equipped between the annular groove 102 and first cavity 126 of the fuselage 100
Guide runner 139, interior be equipped with of the first guide runner 139 automatically power off current monitoring mechanism, set in 100 bottom end face of fuselage
Have and is equipped in 139 bottom of the first guide runner and the second guide runner 115 that Open Side Down, second guide runner 115
Incude automatic spring elecscreen indication mechanism.
Valuably, the current monitoring mechanism that automatically powers off includes communicating to set in the 139 rear end inner wall of the first guide runner
Some grooves 145 are equipped with fixed hook 144 in the groove 145, and the is slidably connected in first guide runner 139
One slider guide 136, first slider guide 136 is interior to be equipped with opening backward and the third cavity to communicate with the groove 145
143, the fixed link 142 that left and right extends is fixedly connected in the third cavity 143 on the inner wall of left and right, in the fixed link 142
Be rotatably assorted the rotational hook 140 being connected with to be engaged with the fixed hook 144,140 rear end face of rotational hook
Press is equipped with the top pressure spring 147 positioned at 142 bottom of fixed link between the 143 rear end inner wall of third cavity, described
140 front end surface of rotational hook is equipped with the permanent magnets 148 positioned at 147 front end of top pressure spring, 143 bottom of third cavity
Portion's inner wall is equipped with the electromagnetic block 141 positioned at 148 front end of permanent magnets, is embedded in first slider guide 136 positioned at institute
The current detector 137 of 143 left end of third cavity is stated, bilateral symmetry is equipped in 136 top end surface of the first slider guide and is open
Upward interlocking Electricity Federation slot 134, interlocking Electricity Federation slot 134, the current detector 137 and the electromagnetic block 141 described in left end it
Between connect live wire 135, be embedded in 139 top inner wall of the first guide runner positioned at 134 top of interlocking Electricity Federation slot
Terminal screw 133,133 bottom end of terminal screw are put in first guide runner 139 and to electric with the interlocking
Join slot 134 and rabbet Electricity Federation, is embedded with the second pusher 131, second Electricity Federation slot in 139 bottom interior wall of the first guide runner
131 top ends are connected by power the telescopic rod 132 extended up and down, consequently facilitating powering off in time while monitoring current flow
Energy conservation.
Valuably, the automatic spring elecscreen indication mechanism includes that sliding connection is arranged in second guide runner
The second slider guide 114 in 115, is fixedly connected with display elecscreen 116 on 114 bottom end face of the second slider guide, and described the
Third pusher 111, the third pusher 111, the third pusher have been connected by power in two slider guides, 114 top end surface
111 outer surfaces are embedded in 115 top inner wall of the second guide runner and connection fixed thereto, in second slider guide 114
It is embedded with the Electricity Federation line 117 with display 116 Electricity Federation of elecscreen, the Electricity Federation line 117 is through 114 front and back of the second slider guide
End face, the 115 front and back inner wall of the second guide runner are equipped with the export head to dock with the Electricity Federation line 117, the fuselage
Processor 113 is equipped in 100 front end surfaces, there are heat source scanner 112, the processing in the 113 left end end Electricity Federation of processor
Device 113 and 111 Electricity Federation of third pusher, consequently facilitating the arrival of the automatic sensing people of device, and timely it is pushed out letter
Display screen is ceased for observing data information.
When original state, the supports loadboard 127 is located at 130 left end of holding tank, and the rubber sucker 128 is completely
In the holding tank 130, the rubber sucker 128 is in fully expanded state, and first slider guide 136 is located at described
First guide runner, 139 top, the terminal screw 133 are rabbeted with interlocking Electricity Federation slot 134, the fixed hook 144 and
140 snapping of rotational hook, second slider guide 114 are located at 115 top of the second guide runner, the display elecscreen
116 are fully located in second guide runner 115.
When the work is required, device is picked up first and is attached on metope, then started first motor 122 and drive
Second belt wheel 123 rotates, and drives the branch by the belt 121, the first pulley 118 and the threaded rod 119
Support support plate 127, the barrel shell 120 and whole move to right of the annulus pressure head 129 skid off the holding tank 130, until the rubber
Sucker 128 is tightly attached on metope, then starts first pusher 125 and the pressing plate 127 is pushed to move to right, described in compression
Then air is discharged in rubber sucker 128 will need the household light fixtures of energy-saving monitoring to connect at this point, device is tightly adsorbed on wall
Enter on the terminal screw 133, the current detector 137 accesses electric current and monitors its flow, if current flow is according to energy conservation
Standard flow through, 141 stable operation of electromagnetic block, the fixed hook 144 stablizes snapping with the rotational hook 140, if
When electric current index is more than energy conservation standard, 141 magnetic force of electromagnetic block is unstable, and the rotation of swinging hanger 140 is detached from described solid
Surely 144 are linked up with, due to the effect of the gravity, first slider guide 136 glides, the terminal screw 133 and the interlocking
Electricity Federation slot 134 is detached from, to power off to lamps and lanterns, if desired restores electric power, and need to only start first pusher 131 makes described stretch
The elongation of contracting bar 132, which pushes, to be moved to initial position on first slider guide 136 and accesses electric power, meanwhile, second motor
The not open close excessively described tooth runner 104 drives the external tooth cannulated sleeve 105 to rotate in 101 operations, the external tooth cannulated sleeve
105 constantly drive the light source scanning support plate 106 to shake handoff angle by the inclined plane part.
When needing artificial observation energy-saving index, need to only walk about to by device, 112 automatic sensing of heat source scanner
Heat source information, and communicate information to the processor 113, due to the processor 113 and 111 Electricity Federation of third pusher,
It pushes second slider guide 114 to move down, drives the display elecscreen 116 to move down and skid off second guide runner 115, until institute
It states Electricity Federation line 117 to dock with the export head, information is shown when opening, when people leaves, can show elecscreen described in automatic accomodation
116。
The beneficial effects of the present invention are: the supports loadboard is located at the holding tank left end due in the initial state,
The rubber sucker is fully located in the holding tank, and the rubber sucker is in fully expanded state, first slider guide
Positioned at the first guide runner top, the terminal screw and the interlocking Electricity Federation slot interlocking, the fixed hook with it is described
Rotational hook snapping, second slider guide are located at the second guide runner top, and the display elecscreen is fully located at described
In second guide runner, consequently facilitating the maintenance of device.
When the work is required, device is picked up first and is attached on metope, then started first motor and drive institute
The rotation of the second belt wheel is stated, the supports loadboard, the barrel shell are driven by the belt, the first pulley and the threaded rod
It is integrally moved to right with the annulus pressure head and skids off the holding tank, until the rubber sucker is tightly attached on metope, then opened
It moves pressing plate described in first pushers to move to right, the rubber sucker discharge air is compressed, at this point, device is tightly adsorbed on
On wall, then the household light fixtures of energy-saving monitoring will be needed to access on the terminal screw, the current detector accesses electric current
And its flow is monitored, and if current flow is flowed through according to energy-efficient standard, the electromagnetic block stable operation, the fixed hook and institute
It states rotational hook and stablizes snapping, if electric current index is more than energy conservation standard, the electromagnetic block magnetic force is unstable, the swinging hanger
Rotation is detached from the fixed hook, and due to the effect of the gravity, first slider guide glides, the terminal screw with it is described
Rabbet Electricity Federation slot to be detached from, to power off to lamps and lanterns, if desired restore electric power, need to only start first pusher makes described stretch
Bar elongation, which pushes, to be moved to initial position on first slider guide and accesses electric power, meanwhile, in second motor running simultaneously
Constantly by the rotation of external tooth cannulated sleeve described in the tooth driven by rotating wheel, the external tooth cannulated sleeve is continuous by the inclined plane part
The light source scanning support plate is driven to shake handoff angle, thus lifting device monitoring effect and diversity.
When needing artificial observation energy-saving index, need to only walk about to by device, the heat source scanner automatic sensing heat
Source information, and the processor is communicated information to, due to the processor and third pusher Electricity Federation, push described second
Slider guide moves down, and drives the display elecscreen to move down and skids off second guide runner, until the Electricity Federation line and the export head
Docking, shows information when opening, when people leaves, elecscreen can be shown described in automatic accomodation, thus lifting device practical performance.
The configuration of the present invention is simple, it is easy to operate, by using collect convenient installing mechanism, automatically power off current monitoring mechanism,
Automatic spring elecscreen indication mechanism and multidimensional light source sensing mechanisms are in one, and ingenious in design, structure is simplified, installation convenience, function
Can be comprehensively easy-to-use, it is applicable in monitoring type and enriches, practical performance is preferable.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention
Protection scope should be determined by the scope of protection defined in the claims.
Claims (3)
1. a kind of energy-saving monitoring equipment exists including fuselage and the holding tank being arranged in fuselage right end end face, feature
In: the holding tank left end is equipped with the first cavity, is slidably connected with supports loadboard, the supports loadboard in the holding tank
It is fixedly connected with barrel shell on right end end face, is fixedly connected with annulus pressure head on barrel shell right end end face, in the annulus pressure head
Equipped with rubber suction nozzle, the rubber suction nozzle is heaved end and is put in inside the barrel shell, and the supports loadboard right end is embedded in end face
First pusher, the first pusher right end end are connected by power the pressing plate to squeeze the rubber suction nozzle, the branch
Support support plate screw-internal thread fit is connected with the threaded rod that symmetrical above and below and left and right extends, and it is empty that the threaded rod left end puts in described first
It is intracavitary and be equipped with first pulley, the first motor, the first motor right end are embedded in the inner wall of first cavity left end
End has been connected by power the second belt wheel, and belt, the fuselage have been connected by power between second belt wheel and the first pulley
It is equipped with the annular groove of opening to the left in the end face of left end, communicates in the annular groove top inner wall equipped with the second cavity, the fuselage
It is fixedly connected with the fixed block positioned at the annulus groove center on the end face of left end, is equipped with hinged ball in the end face of the fixed block left end
Slot is hingedly connected with sphere in the hinged ball groove, and sphere left end end is fixedly connected with light source scanning support plate, described to sweep
It retouches support plate left end end face and is equipped with light source scanner, be rotatably assorted in the annular groove and be connected with external tooth cannulated sleeve, it is described outer
Tooth cannulated sleeve left end is equipped with the rake to be slidably connected with the light source scanning support plate, second cavity left end
Be embedded with the second motor in inner wall, the second motor right end end be connected by power to the external tooth cannulated sleeve
The tooth runner of ratcheting connection is embedded with the light source information processor positioned at the fixed block right end in the end face of the fuselage left end,
The light source information processor and the light source scanner Electricity Federation, interior be equipped with of the fuselage are located at the annular groove and described first
The first guide runner between cavity, interior be equipped with of first guide runner automatically power off current monitoring mechanism, the fuselage bottom end
Equipped with the second guide runner for being located at the first slide guide trench bottom and Open Side Down in face, second guide runner is interior to be equipped with induction
Automatic spring elecscreen indication mechanism.
2. a kind of energy-saving monitoring equipment according to claim 1, it is characterised in that: described to automatically power off current monitoring mechanism
Including communicating the groove being equipped in the inner wall of first guide runner rear end, it is equipped with fixed hook in the groove, described first leads
Be slidably connected with the first slider guide in sliding slot, opening is equipped in first slider guide backward and to the groove phase
Logical third cavity, is fixedly connected with the fixed link that left and right extends in the third cavity on the inner wall of left and right, in the fixed link
Be rotatably assorted the rotational hook being connected with to be engaged with the fixed hook, the rotational hook rear end face and the third
Press is equipped with the top pressure spring positioned at the bottom of fixed between the inner wall of cavity rear end, sets in the rotational hook front end surface
There are the permanent magnets positioned at the top pressure spring front end, the third cavity bottom inner wall is equipped with positioned at the permanent magnets front end
Electromagnetic block is embedded with the current detector positioned at third cavity left end, first slider guide in first slider guide
The interlocking Electricity Federation slot of bilateral symmetry opening upwards is equipped in top end surface, interlocking Electricity Federation slot, the current detector described in left end
It connects live wire, is embedded in the first guide runner top inner wall positioned at interlocking Electricity Federation groove top between the electromagnetic block
The terminal screw in portion, the terminal screw bottom end are put in first guide runner and to embedding with interlocking Electricity Federation slot
Electricity Federation is connect, the second pusher is embedded in the first guide runner bottom interior wall, the second Electricity Federation slot top end power connects
It is connected to the telescopic rod extended up and down.
3. a kind of energy-saving monitoring equipment according to claim 1, it is characterised in that: the automatic spring elecscreen indication mechanism
It is solid on the second slider guide bottom end face including the second slider guide that sliding connection is arranged in second guide runner
Surely it is connected with display elecscreen, has been connected by power third pusher in the second slider guide top end surface, the third pusher,
Third pusher outer surface is embedded in the second guide runner top inner wall and connection fixed thereto, second slide guide
The Electricity Federation line with the display elecscreen Electricity Federation is embedded in block, the Electricity Federation line runs through the second slider guide front/rear end, institute
It states inner wall before and after the second guide runner and is equipped with the export head to dock with the Electricity Federation line, be equipped in the front fuselage end face
There are heat source scanner, the processor and third pusher Electricity Federation in processor, processor left end end Electricity Federation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811204637.7A CN109143118A (en) | 2018-10-16 | 2018-10-16 | A kind of energy-saving monitoring equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811204637.7A CN109143118A (en) | 2018-10-16 | 2018-10-16 | A kind of energy-saving monitoring equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109143118A true CN109143118A (en) | 2019-01-04 |
Family
ID=64812124
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811204637.7A Withdrawn CN109143118A (en) | 2018-10-16 | 2018-10-16 | A kind of energy-saving monitoring equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109143118A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114733399A (en) * | 2022-05-13 | 2022-07-12 | 福建正味生物科技有限公司 | Mixing machine for food processing |
-
2018
- 2018-10-16 CN CN201811204637.7A patent/CN109143118A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114733399A (en) * | 2022-05-13 | 2022-07-12 | 福建正味生物科技有限公司 | Mixing machine for food processing |
| CN114733399B (en) * | 2022-05-13 | 2024-02-09 | 福建正味生物科技有限公司 | Mixing machine for food processing |
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Application publication date: 20190104 |