CN108646049A - A kind of multi-functional wind-resources monitoring device - Google Patents
A kind of multi-functional wind-resources monitoring device Download PDFInfo
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- CN108646049A CN108646049A CN201810573474.3A CN201810573474A CN108646049A CN 108646049 A CN108646049 A CN 108646049A CN 201810573474 A CN201810573474 A CN 201810573474A CN 108646049 A CN108646049 A CN 108646049A
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- rotation axis
- fuselage
- cavity
- spur gear
- fixedly connected
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/30—Wind motors specially adapted for installation in particular locations
- F03D9/34—Wind motors specially adapted for installation in particular locations on stationary objects or on stationary man-made structures
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P13/00—Indicating or recording presence, absence, or direction, of movement
- G01P13/02—Indicating direction only, e.g. by weather vane
- G01P13/025—Indicating direction only, e.g. by weather vane indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/728—Onshore wind turbines
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Power Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The invention discloses a kind of multi-functional wind-resources monitoring devices, including fuselage and the cunning chamber being arranged in the fuselage, the first cavity that left and right extends is equipped with above the sliding chamber, the first slide guide chamber that left and right extends is equipped in first cavity, the first slider guide is equipped on rear side of the first slide guide chamber in inner wall, the first slider guide screw-thread fit is connected with the threaded rod that left and right extends, the threaded rod is through the first slide guide chamber left end inner wall and stretches into the fuselage, fixed block is equipped in the first slider guide front inner wall, first motor is equipped in the fixed block, be connected by power has the first spur gear in the first motor；The configuration of the present invention is simple, easy to operate, high degree of automation have environmental protection and energy saving, meanwhile, also there is very high practicability.
Description
Technical field
The present invention relates to wind-resources monitoring technical field, specifically a kind of multi-functional wind-resources monitoring device.
Background technology
With the development of science and technology, wind energy is gradually utilized by human development, the deficient stage will be stepped into traditional energy,
The utilization of wind energy are seemingly that most people brings a dawn, but are difficult to gram there are some in wind energy development technical field
The technical barrier of clothes, such as most of wind energy plants can not detect wind direction position automatically, to enable wind energy plant that cannot maximize
Wind energy is carried out be converted into other energy and store, so the appearance of the device, can be asked with effective solution the above
Topic.
Invention content
Technical problem to be solved by the invention is to provide a kind of multi-functional wind-resources monitoring devices, can solve above-mentioned
The problems in present technology.
The present invention is achieved through the following technical solutions：A kind of multi-functional wind-resources monitoring device of the present invention, packet
The cunning chamber for including fuselage and being arranged in the fuselage, the first cavity that the sliding chamber top extends equipped with left and right, described first
It is equipped with the first slide guide chamber that left and right extends in cavity, is equipped with the first slider guide on rear side of the first slide guide chamber in inner wall, described the
One slider guide screw-thread fit is connected with the threaded rod that left and right extends, the threaded rod through the first slide guide chamber left end inner wall and
The fuselage is stretched into, fixed block is equipped in the first slider guide front inner wall, first motor is equipped in the fixed block, it is described
Be connected by power has the first spur gear in first motor, and first cavity is interior and second is equipped on the right side of first spur gear
Spur gear, first spur gear and the ratcheting connection of the second spur gear, second spur gear is fixedly connected with downward
The first rotation axis stretched, first rotation axis is rotatably assorted with the fuselage to be connect, and the first rotation axis bottom end face is solid
Surely it is connected with the hexagonal rotation axis extended up and down, the hexagonal rotation axis is fully inserted into the sliding intracavitary, and the sliding intracavitary is equipped with
Balladeur train is equipped with the column type axis extended up and down in the balladeur train, is equipped with the hexagon ring communicated in the column type axis, the hexagon ring with
The hexagonal rotation axis is rotatably assorted connection, and the column type axis is equipped with first pulley, far from the first band in the balladeur train
It takes turns one end and is equipped with the second symmetrical belt wheel, frictional connection has conveyer belt between the first pulley and second belt wheel, described
Second belt wheel bottom end face is fixedly connected with the second rotation axis extended up and down, and the second rotation axis bottom end is through described
Fuselage and the external fuselage is stretched into, third spur gear is equipped in first cavity and on the left of first spur gear,
The third spur gear top end surface is fixedly connected with the third rotation axis extended up and down, and the third rotation axis top end is passed through
The fuselage upper surface is worn, the third rotation axis top end surface is fixedly connected with the monitoring case extended up and down, the monitoring case
Equipped with the second symmetrical cavity, it is equipped with the case that tests the speed in second cavity, is equipped with third cavity in the case that tests the speed, described the
Tachymeter is equipped on the right side of three cavitys in inner wall, tachometer disc is equipped on the left of the third cavity, is fixedly connected on the tachometer disc
4th rotation axis of left and right extension, the 4th rotation axis run through babinet on the left of the case that tests the speed and fix company in its left end end
It is connected to fan, second cavity top is equipped with the second motor, and second motor power is connected with threaded rod, the threaded rod
It is stretched into the monitoring box body completely through second cavity and bottom end, the threaded rod and the case screw thread that tests the speed
It is connected, fuselage right end end face is equipped with attachment device.
Preferably technical solution, the monitoring case top end surface are equipped with the fixed link extended up and down, the fixed link
Tip end is equipped with wind energy conversion system, and the wind energy conversion system is fixedly connected with the main shaft that left and right extends, and main shaft left end end is equipped with wind
Power blade.
Preferably technical solution, the fuselage top is equipped with the second fixed link far from the monitoring case side, described
Second fixed link, second fixed link are equipped with lateral disk, the 5th turn extended up and down are equipped at the top of second fixed link
Moving axis, the 5th rotation axis is rotatably assorted with second fixed link to be connect, and the 5th rotation axis top end, which is equipped with, to be surveyed
To device.
Preferably technical solution, the attachment device include the connection machine being arranged on fuselage right end end face
Body, the connection body is interior to be equipped with the slippage slot of opening to the right, and slipping block, the cunning are slidably connected in the slippage slot
It moves block right end end face and is equipped with connector, the sliding is equipped with the adjusting threaded rod that left and right extends, the adjusting threaded rod soon
Left end end be connected by power has a third motor, third motor outer surface be embedded in the slippage slot left end inner wall and
Connection fixed thereto.
The beneficial effects of the invention are as follows：The device be equipped with that left and right extends in the initial state, in first cavity the
One slide guide chamber, the first slide guide chamber rear side inner wall is interior to be equipped with the first slider guide, and the first slider guide screw-thread fit is connected with
The threaded rod that left and right extends, the threaded rod is through the first slide guide chamber left end inner wall and stretches into the fuselage, and described first
It is equipped with fixed block in slider guide front inner wall, first motor is equipped in the fixed block, starts the first motor, described first
Be connected by power has the first spur gear on motor, and first cavity is interior and the second straight-tooth is equipped on the right side of first spur gear
Wheel, first spur gear and the ratcheting connection of the second spur gear, second spur gear is fixedly connected with to be extended up and down
First rotation axis, first rotation axis is rotatably assorted with the fuselage to be connect, and the first rotation axis bottom end face, which is fixed, to be connected
It is connected to the hexagonal rotation axis extended up and down, the hexagonal rotation axis is fully inserted into the sliding intracavitary, and the sliding intracavitary is equipped with balladeur train,
Be equipped with the column type axis extended up and down in the balladeur train, be equipped with the hexagon ring communicated in the column type axis, the hexagon ring with it is described
Hexagonal rotation axis is rotatably assorted connection, and the column type axis is equipped with first pulley, far from the first pulley one in the balladeur train
End is equipped with the second symmetrical belt wheel, and frictional connection has a conveyer belt between the first pulley and second belt wheel, and described second
Belt wheel bottom end face is fixedly connected with the second rotation axis extended up and down, and the second rotation axis bottom end runs through the fuselage
And the external fuselage is stretched into, second rotation axis and the balladeur train slide downward at this time, until second rotation axis is inserted
Enter until earth's surface fixes the device, so the device itself has stronger stability.
When the device is in running order, first slider guide slides to the left, the first slider guide front inner wall
It is interior to be equipped with fixed block, it is equipped with first motor in the fixed block, be connected by power has the first spur gear in the first motor, at this time
First spur gear and the ratcheting connection of third spur gear, the third spur gear top end surface is fixedly connected with downward
The third rotation axis stretched, the third rotation axis top end run through the fuselage upper surface, the third rotation axis top end
Face is fixedly connected with the monitoring case extended up and down, and the monitoring case is equipped with the second symmetrical cavity, is set in second cavity
Test the speed case, and third cavity is equipped in the case that tests the speed, and inner wall is interior equipped with tachymeter on the right side of the third cavity, and the third is empty
It is equipped with tachometer disc on the left of chamber, the 4th rotation axis that left and right extends is fixedly connected on the tachometer disc, the 4th rotation axis is passed through
It wears babinet on the left of the case that tests the speed and is fixedly connected with fan in its left end end, second cavity top is equipped with the second electricity
Machine, second motor power are connected with threaded rod, and the threaded rod is stretched into completely through second cavity and bottom end
In the monitoring box body, the threaded rod is connect with the case screw-thread fit that tests the speed, so the plant automation degree is higher.
The monitoring case top end surface is equipped with the fixed link extended up and down, and the fixed link tip end is equipped with wind energy conversion system,
The wind energy conversion system is fixedly connected with the main shaft that left and right extends, and main shaft left end end is equipped with wind blade, which is this
Device, which provides, can use the energy, so the device energy conservation and environmental protection.
The fuselage top far from the monitoring case side be equipped with the second fixed link, second fixed link, described second
Fixed link is equipped with lateral disk, and the 5th rotation axis extended up and down, the 5th rotation axis are equipped at the top of second fixed link
It is rotatably assorted and connect with second fixed link, the 5th rotation axis top end is equipped with goniometer, therefore the device can be real
When detect wind direction, so that it is had good practicability.
The present invention device structure it is simple, it is easy to operate, on device be equipped with corresponding fixing device, make it have compared with
Power can be carried out controllable type conversion, improve the degree of automation of the device by strong stability, the sliding equipment being equipped in device,
By being equipped with wind energy conversion system on device, to enable it be improved with environmental protection and energy saving further through goniometer is equipped on device
Device working efficiency, meanwhile, also improve device practicability.
Description of the drawings
The present invention is described in detail by following specific embodiment and attached drawing for ease of explanation,.
Fig. 1 is overall structure diagram outside a kind of multi-functional wind-resources monitoring device of the present invention；
Fig. 2 is structural schematic diagram shown in Figure 1A；
Fig. 3 is structural schematic diagram shown in Figure 1B.
Specific implementation mode
As shown in Figure 1, Figure 2 and Figure 3, a kind of multi-functional wind-resources monitoring device of the invention, including fuselage 100 and set
Set the cunning chamber 101 in the fuselage 100,101 top of the sliding chamber is equipped with the first cavity 121 that left and right extends, and described first
It is equipped with the first slide guide chamber 139 that left and right extends in cavity 121, the first slide guide is equipped in the 139 rear side inner wall of the first slide guide chamber
Block 142,142 screw-thread fit of the first slider guide are connected with the threaded rod 140 that left and right extends, and the threaded rod 140 runs through institute
It states 139 left end inner wall of the first slide guide chamber and stretches into the fuselage 100, be equipped with and fix in 142 front inner wall of the first slider guide
Block 138, the fixed block 138 is interior to be equipped with first motor 137, and be connected by power has the first spur gear in the first motor 137
141, first cavity 121 is interior and is equipped with the second spur gear 118 positioned at first spur gear, 141 right side, and described first is straight
Gear 141 and second spur gear, 118 ratcheting connection, second spur gear 118 are fixedly connected with first extended up and down
Rotation axis 110, first rotation axis 110 is rotatably assorted with the fuselage 100 to be connect, 110 bottom end of the first rotation axis
Face is fixedly connected with the hexagonal rotation axis 107 extended up and down, and the hexagonal rotation axis 107 is fully inserted into the sliding chamber 101, institute
It states and is equipped with balladeur train 103 in sliding chamber 101, the column type axis 109 extended up and down is equipped in the balladeur train 103, is set in the column type axis 109
There are the hexagon ring 108 communicated, the hexagon ring 108 to be rotatably assorted and connect with the hexagonal rotation axis 107, the column type axis 109
It is equipped with first pulley 106, separate 106 one end of the first pulley is equipped with the second symmetrical belt wheel in the balladeur train 103
104, frictional connection has conveyer belt 105,104 bottom of the second belt wheel between the first pulley 106 and second belt wheel 104
End face is fixedly connected with the second rotation axis 102 extended up and down, and 102 bottom end of the second rotation axis runs through the fuselage
It 100 and stretches into outside the fuselage 100, third is equipped in first cavity 121 and positioned at first spur gear, 141 left side
Spur gear 120,120 top end surface of third spur gear are fixedly connected with the third rotation axis 122 extended up and down, the third
122 top end of rotation axis runs through 100 upper surface of the fuselage, and 122 top end surface of third rotation axis is fixedly connected with
The monitoring case 133 of lower extension, the monitoring case 133 are equipped with the second symmetrical cavity 136, are equipped in second cavity 136
Test the speed case 134, and third cavity 123 is equipped in the case 134 that tests the speed, tachymeter is equipped in 123 right side inner wall of the third cavity
127,123 left side of the third cavity is equipped with tachometer disc 126, and the left and right extends the 4th is fixedly connected on the tachometer disc 126
Rotation axis 124, the 4th rotation axis 124 134 left side babinet of case and are fixedly connected with through described test the speed in its left end end
Fan 125,136 top of the second cavity are equipped with the second motor 132, and 132 be connected by power of the second motor has threaded rod
135, the threaded rod 135 is stretched into completely through second cavity 136 and bottom end in 133 babinet of the monitoring case, institute
It states threaded rod 135 to connect with 134 screw-thread fit of case that tests the speed, 100 right end end face of the fuselage is equipped with attachment device.
Valuably, 133 top end surface of the monitoring case is equipped with the fixed link 131 extended up and down, 131 top of the fixed link
End is equipped with wind energy conversion system 130, and the wind energy conversion system 130 is fixedly connected with the main shaft 129 that left and right extends, 129 left end of main shaft end
End is equipped with wind blade 128.
Valuably, 100 top of the fuselage far from 133 side of the monitoring case be equipped with the second fixed link 111, described second
Fixed link 111, second fixed link 111 are equipped with lateral disk 112, and second fixed link, 111 top is equipped with to be extended up and down
The 5th rotation axis 113, the 5th rotation axis 113 is rotatably assorted with second fixed link 111 to be connect, it is described 5th rotation
113 top end of axis is equipped with goniometer 115.
Valuably, the attachment device includes the connection body 200 being arranged on 100 right end end face of the fuselage, described
It connects and is equipped with the slippage slot 201 of opening to the right in body 200, slipping block 203 is slidably connected in the slippage slot 201,
203 right end end face of the slipping block is equipped with connector 202, and the sliding fast 203 is equipped with the adjusting threaded rod that left and right extends
204,204 left end end be connected by power of the adjusting threaded rod has third motor 205,205 outer surface of third motor
It is embedded in 201 left end inner wall of the slippage slot and connection fixed thereto.
The first slide guide chamber 139 that left and right extends is equipped with when the device is in original state, in first cavity 121,
The first slider guide 142 is equipped in first slide guide chamber, the 139 rear side inner wall, 142 screw-thread fit of the first slider guide is connected with
The threaded rod 140 that left and right extends, the threaded rod 140 is through the 139 left end inner wall of the first slide guide chamber and stretches into the fuselage
100,142 front inner wall of the first slider guide is interior to be equipped with fixed block 138, and first motor 137 is equipped in the fixed block 138,
Start the first motor 137, be connected by power has the first spur gear 141, first cavity 121 in the first motor 137
Interior and be equipped with the second spur gear 118 positioned at the right side of first spur gear 141, first spur gear 141 is straight with described second
118 ratcheting connection of gear, second spur gear 118 are fixedly connected with the first rotation axis 110 extended up and down, described first turn
Moving axis 110 is rotatably assorted with the fuselage 100 and connect, and 110 bottom end face of the first rotation axis is fixedly connected with extension up and down
Hexagonal rotation axis 107, the hexagonal rotation axis 107 is fully inserted into the sliding chamber 101, and balladeur train is equipped in the sliding chamber 101
103, the balladeur train 103 is interior to be equipped with the column type axis 109 extended up and down, and the hexagon ring 108 communicated is equipped in the column type axis 109,
The hexagon ring 108 is rotatably assorted with the hexagonal rotation axis 107 and connect, and the column type axis 109 is equipped with first pulley 106,
In the balladeur train 103 far from 106 one end of the first pulley be equipped with the second symmetrical belt wheel 104, the first pulley 106 with
Second belt wheel, 104 frictional connections have conveyer belt 105,104 bottom end face of the second belt wheel to be fixedly connected with downward
The second rotation axis 102 stretched, 102 bottom end of the second rotation axis is through the fuselage 100 and stretches into outside the fuselage 100
Portion, second rotation axis 102 and 103 slide downward of the balladeur train, are inserted into earth's surface up to second rotation axis 102 and consolidate at this time
Until the fixed device.
When the device is in running order, first slider guide 142 slides to the left, before first slider guide 142
It is equipped with fixed block 138 in the inner wall of side, first motor 137 is equipped in the fixed block 138, power connects in the first motor 137
It is connected to the first spur gear 141, first spur gear 141 and 120 ratcheting connection of the third spur gear, the third are straight at this time
120 top end surface of gear is fixedly connected with the third rotation axis 122 extended up and down, and 122 top end of third rotation axis is passed through
100 upper surface of the fuselage is worn, 122 top end surface of third rotation axis is fixedly connected with the monitoring case 133 extended up and down, institute
It states monitoring case 133 and is equipped with the second symmetrical cavity 136, the case 134 that tests the speed, the case that tests the speed are equipped in second cavity 136
It is equipped with third cavity 123 in 134, tachymeter 127 is equipped in 123 right side inner wall of the third cavity, the third cavity 123 is left
Side is equipped with tachometer disc 126, and the 4th rotation axis 124 that left and right extends, the 4th rotation are fixedly connected on the tachometer disc 126
Axis 124 134 left side babinet of case and is fixedly connected with fan 125, second cavity 136 through described test the speed in its left end end
Top is equipped with the second motor 132, and 132 be connected by power of the second motor has a threaded rod 135, the threaded rod 135 completely through
Second cavity 136 and bottom end stretch into 133 babinet of the monitoring case, the threaded rod 135 and the case 134 that tests the speed
Screw-thread fit connects.
The beneficial effects of the invention are as follows：The device be equipped with that left and right extends in the initial state, in first cavity the
One slide guide chamber, the first slide guide chamber rear side inner wall is interior to be equipped with the first slider guide, and the first slider guide screw-thread fit is connected with
The threaded rod that left and right extends, the threaded rod is through the first slide guide chamber left end inner wall and stretches into the fuselage, and described first
It is equipped with fixed block in slider guide front inner wall, first motor is equipped in the fixed block, starts the first motor, described first
Be connected by power has the first spur gear, the fixed block that can be moved along the threaded rod on motor, in first cavity and is located at
The second spur gear, first spur gear and the ratcheting connection of the second spur gear are equipped on the right side of first spur gear, it is described
Second spur gear is fixedly connected with the first rotation axis extended up and down, and first rotation axis and the fuselage are rotatably assorted company
It connects, the first rotation axis bottom end face is fixedly connected with the hexagonal rotation axis extended up and down, and the hexagonal rotation axis is stretched completely
Enter the sliding intracavitary, the sliding intracavitary is equipped with balladeur train, the column type axis extended up and down is equipped in the balladeur train, is set in the column type axis
There are the hexagon ring communicated, the hexagon ring to be rotatably assorted and connect with the hexagonal rotation axis, the column type axis is equipped with first band
It takes turns, the second symmetrical belt wheel, the first pulley and described second is equipped with far from described first pulley one end in the balladeur train
Frictional connection has conveyer belt, the second belt wheel bottom end face to be fixedly connected with the second rotation axis extended up and down, institute between belt wheel
The second rotation axis bottom end is stated through the fuselage and stretches into the external fuselage, at this time second rotation axis and the cunning
Frame slide downward, until second rotation axis insertion earth's surface fixes the device, so the device itself is with stronger
Stability.
When the device is in running order, first slider guide slides to the left, the first slider guide front inner wall
It is interior to be equipped with fixed block, it is equipped with first motor in the fixed block, be connected by power has the first spur gear in the first motor, at this time
First spur gear and the ratcheting connection of third spur gear, the third spur gear top end surface is fixedly connected with downward
The third rotation axis stretched, the third rotation axis top end run through the fuselage upper surface, the third rotation axis top end
Face is fixedly connected with the monitoring case extended up and down, and the monitoring case is equipped with the second symmetrical cavity, is set in second cavity
Test the speed case, and third cavity is equipped in the case that tests the speed, and inner wall is interior equipped with tachymeter on the right side of the third cavity, and the third is empty
It is equipped with tachometer disc on the left of chamber, the 4th rotation axis that left and right extends is fixedly connected on the tachometer disc, the 4th rotation axis is passed through
It wears babinet on the left of the case that tests the speed and is fixedly connected with fan in its left end end, second cavity top is equipped with the second electricity
Machine, second motor power are connected with threaded rod, and the threaded rod is stretched into completely through second cavity and bottom end
In the monitoring box body, the threaded rod is connect with the case screw-thread fit that tests the speed, so the plant automation degree is higher.
The monitoring case top end surface is equipped with the fixed link extended up and down, and the fixed link tip end is equipped with wind energy conversion system,
The wind energy conversion system is fixedly connected with the main shaft that left and right extends, and main shaft left end end is equipped with wind blade, which is this
Device, which provides, can use the energy, so the device energy conservation and environmental protection.
The fuselage top far from the monitoring case side be equipped with the second fixed link, second fixed link, described second
Fixed link is equipped with lateral disk, and the 5th rotation axis extended up and down, the 5th rotation axis are equipped at the top of second fixed link
It is rotatably assorted and connect with second fixed link, the 5th rotation axis top end is equipped with goniometer, therefore the device can be real
When detect wind direction, so that it is had good practicability.
The present invention device structure it is simple, it is easy to operate, on device be equipped with corresponding fixing device, make it have compared with
Power can be carried out controllable type conversion, improve the degree of automation of the device by strong stability, the sliding equipment being equipped in device,
By being equipped with wind energy conversion system on device, to enable it be improved with environmental protection and energy saving further through goniometer is equipped on device
Device working efficiency, meanwhile, also improve device practicability.
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 domain should be determined by the scope of protection defined in the claims.
Claims (4)
1. a kind of multi-functional wind-resources monitoring device, including fuselage and the cunning chamber that is arranged in the fuselage, it is characterised in that：
It is equipped with the first cavity that left and right extends above the sliding chamber, the first slide guide chamber that left and right extends, institute are equipped in first cavity
It states and is equipped with the first slider guide on rear side of the first slide guide chamber in inner wall, the first slider guide screw-thread fit is connected with the spiral shell that left and right extends
Rasp bar, the threaded rod is through the first slide guide chamber left end inner wall and stretches into the fuselage, in the first slider guide front side
It is equipped with fixed block in wall, is equipped with first motor in the fixed block, be connected by power has the first spur gear, institute in the first motor
It states in the first cavity and is equipped with the second spur gear on the right side of first spur gear, first spur gear is straight with described second
Gear mesh connects, and second spur gear is fixedly connected with the first rotation axis extended up and down, first rotation axis and institute
It states fuselage to be rotatably assorted connection, the first rotation axis bottom end face is fixedly connected with the hexagonal rotation axis extended up and down, described
Hexagonal rotation axis is fully inserted into the sliding intracavitary, and the sliding intracavitary is equipped with balladeur train, the column type extended up and down is equipped in the balladeur train
Axis, the column type axis is interior to be equipped with the hexagon ring communicated, and the hexagon ring is rotatably assorted with the hexagonal rotation axis and connect, the column
Profile shaft is equipped with first pulley, is equipped with the second symmetrical belt wheel far from described first pulley one end in the balladeur train, and described the
Frictional connection has conveyer belt, the second belt wheel bottom end face to be fixedly connected with extension up and down between one belt wheel and second belt wheel
The second rotation axis, the second rotation axis bottom end is through the fuselage and stretches into the external fuselage, and described first is empty
Intracavitary and third spur gear is equipped on the left of first spur gear, the third spur gear top end surface is fixedly connected with
The third rotation axis of lower extension, the third rotation axis top end run through the fuselage upper surface, third rotation axis top
End surface is fixedly connected with the monitoring case extended up and down, and the monitoring case is equipped with the second symmetrical cavity, second cavity
Interior be equipped with is tested the speed case, is equipped with third cavity in the case that tests the speed, and is equipped with tachymeter on the right side of the third cavity in inner wall, and described the
It is equipped with tachometer disc on the left of three cavitys, the 4th rotation axis that left and right extends, the 4th rotation are fixedly connected on the tachometer disc
Axis runs through babinet on the left of the case that tests the speed and is fixedly connected with fan in its left end end, and second cavity top is equipped with second
Motor, second motor power are connected with threaded rod, and the threaded rod is stretched completely through second cavity and bottom end
Enter in the monitoring box body, the threaded rod is connect with the case screw-thread fit that tests the speed, and fuselage right end end face is equipped with
Attachment device.
2. a kind of multi-functional wind-resources monitoring device according to claim 1, it is characterised in that：The monitoring case top end
Face is equipped with the fixed link extended up and down, and the fixed link tip end is equipped with wind energy conversion system, and the wind energy conversion system is fixedly connected with left and right
The main shaft of extension, main shaft left end end are equipped with wind blade.
3. a kind of multi-functional wind-resources monitoring device according to claim 1, it is characterised in that：The fuselage top is separate
The monitoring case side is equipped with the second fixed link, second fixed link, and second fixed link is equipped with lateral disk, and described the
It is equipped with the 5th rotation axis extended up and down at the top of two fixed links, the 5th rotation axis and second fixed link are rotatably assorted company
It connects, the 5th rotation axis top end is equipped with goniometer.
4. a kind of multi-functional wind-resources monitoring device according to claim 1, it is characterised in that：The attachment device includes
Connection body on fuselage right end end face is set, the slippage slot of opening to the right, the cunning are equipped in the connection body
It moves in slot and is slidably connected with slipping block, slipping block right end end face is equipped with connector, and the sliding is equipped with a left side soon
The adjusting threaded rod of right extension, adjusting threaded rod left end end be connected by power have third motor, the third motor
Outer surface is embedded in the slippage slot left end inner wall and connection fixed thereto.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810573474.3A CN108646049A (en) | 2018-06-06 | 2018-06-06 | A kind of multi-functional wind-resources monitoring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810573474.3A CN108646049A (en) | 2018-06-06 | 2018-06-06 | A kind of multi-functional wind-resources monitoring device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108646049A true CN108646049A (en) | 2018-10-12 |
Family
ID=63751878
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810573474.3A Withdrawn CN108646049A (en) | 2018-06-06 | 2018-06-06 | A kind of multi-functional wind-resources monitoring device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108646049A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109989879A (en) * | 2019-04-22 | 2019-07-09 | 杭州柔晴电子商务有限公司 | A kind of wind electric power generation fan blade |
-
2018
- 2018-06-06 CN CN201810573474.3A patent/CN108646049A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109989879A (en) * | 2019-04-22 | 2019-07-09 | 杭州柔晴电子商务有限公司 | A kind of wind electric power generation fan blade |
| CN109989879B (en) * | 2019-04-22 | 2020-12-29 | 广西电网有限责任公司电力科学研究院 | Wind energy detection device |
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Application publication date: 20181012 |