CN207985193U - A kind of intelligent flight instruments with barrier avoiding function for bridge machinery - Google Patents
A kind of intelligent flight instruments with barrier avoiding function for bridge machinery Download PDFInfo
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- CN207985193U CN207985193U CN201820208297.4U CN201820208297U CN207985193U CN 207985193 U CN207985193 U CN 207985193U CN 201820208297 U CN201820208297 U CN 201820208297U CN 207985193 U CN207985193 U CN 207985193U
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- main body
- bridge
- cylinder
- flight instruments
- barrier avoiding
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Abstract
The utility model is related to a kind of intelligent flight instruments with barrier avoiding function for bridge machinery,Including main body,Protection ring,Testing agency,Bindiny mechanism,Buffer gear and four aviation mechanisms,Testing agency includes camera,Link block,Telescopic component and adjusting part,Telescopic component includes air pump,Cylinder,Piston and two hinge units,Buffer gear includes several Buffer Units,Buffer Unit includes casing,First spring,Mandril and steel ball,Bindiny mechanism includes several connection components,Connection component includes second spring,Pressure plare and connecting rod,The intelligent flight instruments with barrier avoiding function for being used for bridge machinery are moved and are rotated to camera by testing agency,The angle orientation for keeping camera different is shot,Avoid the occurrence of shooting blind spot,Moreover,It prevents from colliding with bridge and bridge pier when main body flight by buffer gear and protection ring,It ensure that the safe flight of device,To improve the practicability of device.
Description
Technical field
It is the utility model is related to bridge machinery repair apparatus field, more particularly to a kind of that there is avoidance for bridge machinery
The intelligent flight instruments of function.
Background technology
Bridge needs periodically to carry out appearance detection to bridge after building up and coming into operation, to exclude the incipient fault of bridge,
Therefore, it is assessment bridge health situation to bridge periodic detection, understands and control bridge defect and state of development, it is reasonable to formulate
Maintenance program extends bridge service life and ensures the condition of bridge service phase safety.Currently, people's generally use bridge is examined
Measuring car carries out periodic detection to bridge.
But detection vehicle is parked on bridge when carrying out detection operation, not only be easy to cause highway blocking, but also due to detection
Vehicle self reason cannot carry out bridge comprehensive detection, many blind spots be easy tod produce in detection process, also, due to inspection
Measuring car build is huge, is only applicable to be detected some large bridges, and can not pacify to some small bridges in small towns
Full assessment, causes existing Bridge Testing Equipment practicability to reduce.
Utility model content
The technical problems to be solved in the utility model is：For overcome the deficiencies in the prior art, it provides a kind of for bridge
The intelligent flight instruments with barrier avoiding function of detection.
Technical solution adopted by the utility model to solve its technical problems is：It is a kind of that there is avoidance for bridge machinery
The intelligent flight instruments of function, including main body, protection ring, sunpender, testing agency, bindiny mechanism, buffer gear, four flights
Mechanism and four stabilizer blades, the protection ring are set in main body, and the bindiny mechanism is arranged between protection ring and main body, described
The top of sunpender is fixed on the lower section of main body, and the aviation mechanism is circumferentially evenly distributed on the periphery of the bottom end of sunpender, each stabilizer blade
It is arranged in the lower section of two neighboring aviation mechanism, the buffer gear and testing agency are arranged at the top of main body；
The testing agency includes camera, link block, telescopic component and adjusting part, and the telescopic component setting is being taken the photograph
As the lower section of head, the telescopic component includes air pump, cylinder, piston and two hinge units, and two hinge units are respectively set
In the both sides of cylinder, the bottom end of the cylinder is connect by hinge unit with main body, and the air pump is fixed on cylinder, the gas
Pump is connected to cylinder, and the bottom end of the piston is arranged in cylinder, and the top of the piston is fixedly connected with link block, described to take the photograph
As head is fixed on the top of link block, the adjusting part is connect with cylinder-driven；
The buffer gear includes several Buffer Units, and the Buffer Unit is circumferentially evenly distributed on the top of main body, institute
It includes that casing, the first spring, mandril and steel ball, described sleeve pipe are fixed in main body to state Buffer Unit, and the bottom end of the mandril is set
It sets in casing, the bottom end of first spring and the bottom of casing connect, the bottom end on the top and mandril of first spring
The top of connection, the mandril is equipped with recess, and the steel ball matches with recess, and the steel ball is arranged in recess, the steel
The centre of sphere of pearl is located in recess；
The bindiny mechanism includes several connection components, and the connection component is circumferentially evenly distributed on the periphery of main body, institute
It includes second spring, pressure plare and connecting rod to state connection component, and one end of the second spring is connect with main body, second bullet
The other end of spring and the side of pressure plare connect, and the other side of the pressure plare is fixedly connected by connecting rod with protection ring.
Preferably, in order to realize that the flight function of equipment, the aviation mechanism include side lever, first motor, the first drive
Moving axis and two rotors, the first motor are fixedly connected by side lever with the bottom end of sunpender, and the first motor is driven with first
Driving-axle gearing connects, and two rotors are separately positioned on the both sides of first motor.
Preferably, for the ease of adjusting the shooting angle of camera, the adjusting part includes the second motor, buffering
Block, the second drive shaft, movable block, hinged block and strut, second motor and buffer stopper are each attached in main body, and described second
Drive shaft is arranged between the second motor and buffer stopper, and second motor and the second drive shaft are sequentially connected, and described second drives
The periphery of moving axis is equipped with external screw thread, and the movable block is set in the second drive shaft, and internal thread is equipped in the movable block, described
Internal thread in movable block matches with the external screw thread in the second drive shaft, and the movable block is hinged by strut and hinged block,
The hinged block is fixed on cylinder.
Preferably, for the ease of the rotation of cylinder, the hinge unit includes pillar, intubation and inserted link, the intubation
The top of main body is fixed on by pillar, one end of the inserted link is fixedly connected with cylinder, and the other end setting of the inserted link exists
In intubation.
Preferably, in order to ensure that mandril smoothly moves, the buffer cell further includes spacing ring, and the spacing ring is solid
It is scheduled on the inner wall of casing, the spacing ring is set on mandril.
Preferably, violent effect of jitter equipment flight occurs for protection ring in order to prevent, the both sides of the second spring are set
It includes fixed link and slip ring to have limit assembly, the limit assembly, and the fixed link is fixed in main body, and the slip ring is set in
In fixed link, the slip ring is fixedly connected with pressure plare.
Preferably, in order to ensure that slip ring can smoothly slide in fixed link, the slip ring is matched with fixed link for gap
It closes.
Preferably, for the ease of detecting the deformation quantity of second spring, pressure sensor is equipped in the pressure plare.
Preferably, for the ease of detection camera at a distance from bridge bottom surface, while brightness is shot by increase and is ensured
Camera acquires clear image, and the link block is equipped with light compensating lamp and range sensor.
Preferably, in order to improve the intelligence degree of equipment, it is equipped with PLC and antenna in the main body, the antenna, the
One motor, the second motor, air pump, pressure sensor, light compensating lamp and range sensor are electrically connected with PLC.
The utility model has the beneficial effects that the intelligent flight instruments with barrier avoiding function for being used for bridge machinery are logical
It crosses testing agency camera is moved and rotated, the angle orientation for keeping camera different is shot, and is avoided the occurrence of
Blind spot is shot, compared with traditional testing agency, which can be comprehensive by the flexible rotating of camera and mobile realization
Shooting moreover prevent from colliding with bridge and bridge pier when main body flight by buffer gear and protection ring, ensure that
The safe flight of device, compared with traditional buffer gear, which is rolled after being contacted with bridge bottom surface by steel ball
It is dynamic, it prevents mandril from rubbing with bridge bottom surface and causes the damage of bridge bottom surface, while being also convenient for the flight of equipment, to improve dress
The practicability set.
Description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is the structural representation of the intelligent flight instruments with barrier avoiding function for bridge machinery of the utility model
Figure；
Fig. 2 is the vertical view of the intelligent flight instruments with barrier avoiding function for bridge machinery of the utility model；
Fig. 3 is the testing agency of the intelligent flight instruments with barrier avoiding function for bridge machinery of the utility model
Structural schematic diagram；
Fig. 4 is the Buffer Unit of the intelligent flight instruments with barrier avoiding function for bridge machinery of the utility model
Structural schematic diagram；
Fig. 5 is the connection component of the intelligent flight instruments with barrier avoiding function for bridge machinery of the utility model
Structural schematic diagram；
In figure：1. main body, 2. protection rings, 3. sunpenders, 4. stabilizer blades, 5. cameras, 6. link blocks, 7. air pumps, 8. cylinders, 9.
Piston, 10. casings, 11. first springs, 12. mandrils, 13. steel balls, 14. second springs, 15. pressure plares, 16. connecting rods, 17.
Side lever, 18. first motors, 19. first drive shafts, 20. rotors, 21. second motors, 22. buffer stoppers, 23. second drive shafts,
24. movable block, 25. hinged blocks, 26. struts, 27. pillars, 28. intubations, 29. inserted links, 30. spacing rings, 31. fixed links, 32. slide
Ring, 33. pressure sensors, 34. light compensating lamps, 35. range sensors.
Specific implementation mode
The utility model is described in further detail presently in connection with attached drawing.These attached drawings are simplified schematic diagram,
Only illustrate the basic structure of the utility model in a schematic way, therefore it only shows composition related with the utility model.
As shown in Figs. 1-2, a kind of intelligent flight instruments with barrier avoiding function for bridge machinery, including main body 1,
Protection ring 2, sunpender 3, testing agency, bindiny mechanism, buffer gear, four aviation mechanisms and four stabilizer blades 4, the protection ring 2
It is arranged on the body 1, the bindiny mechanism is arranged between protection ring 2 and main body 1, and the top of the sunpender 3 is fixed on main body 1
Lower section, the aviation mechanism is circumferentially evenly distributed on the periphery of the bottom end of sunpender 3, and each stabilizer blade 4 is arranged in two neighboring flight
The lower section of mechanism, the buffer gear and testing agency are arranged at the top of main body 1；
This is used to detect the intelligent flight instruments of bridge in use, controlling aviation mechanism operation by main body 1, makes flying machine
Structure drives main body 1 to fly, and under bridge, is detected to bridge by the testing agency of 1 top of main body, compared to bridge machinery
Vehicle, the detection device build is small, is equally applicable to the bridge small-sized to some and is detected, while being not take up vehicle in detection process
Road, convenient for the passage of vehicle on bridge pavement, while main body 1 is connect by bindiny mechanism with protection ring 2, is protected by protection ring 2
Card main body 1 avoids collision the bridge pier in horizontal direction in flight course, while protecting main body 1 by buffer gear, prevents from leading
The excessive lower section for colliding bridge of 1 flying height of body, to realize the safe flight of equipment.
As shown in figure 3, the testing agency includes camera 5, link block 6, telescopic component and adjusting part, it is described flexible
Component is arranged in the lower section of camera 5, and the telescopic component includes air pump 7, cylinder 8, piston 9 and two hinge units, two
Hinge unit is separately positioned on the both sides of cylinder 8, and the bottom end of the cylinder 8 is connect by hinge unit with main body 1, the air pump
7 are fixed on cylinder 8, and the air pump 7 is connected to cylinder 8, and the bottom end of the piston 9 is arranged in cylinder 8, the piston 9
Top is fixedly connected with link block 6, and the camera 5 is fixed on the top of link block 6, and the adjusting part is driven with cylinder 8
Connection；
In testing agency, by adjusting part change telescopic component in cylinder 8 angle, cylinder 8 by hinge unit with
Main body 1 connects, consequently facilitating the rotation of cylinder 8, and the air pressure in cylinder 8 can be changed in air pump 7, it is big according to the air pressure in cylinder 8
It is small, make piston 9 that corresponding movement occur, clearly image is acquired convenient for the camera 5 on link block 6.
As shown in figure 4, the buffer gear includes several Buffer Units, the Buffer Unit is circumferentially evenly distributed on main body
1 top, the Buffer Unit include that casing 10, the first spring 11, mandril 12 and steel ball 13, described sleeve pipe 10 are fixed on main body
On 1, the bottom end of the mandril 12 is arranged in casing 10, and the bottom end of first spring 11 is connect with the bottom of casing 10, institute
The top for stating the first spring 11 is connect with the bottom end of mandril 12, and the top of the mandril 12 is equipped with recess, the steel ball 13 with it is recessed
Mouth matches, and the steel ball 13 is arranged in recess, and the centre of sphere of the steel ball 13 is located in recess；
When main body 1 is below bridge in flight course, if flying height is excessive, first by the buffering group in buffer gear
Part touches bridge ground, prevents main body 1 from colliding bridge and causes equipment damage.At this point, inside Buffer Unit, flight instruments
Flight makes the steel ball 13 on 12 top of mandril be resisted against on bridge bottom surface upwards, while compressing the first spring 11, passes through the first spring
11 to make Buffer Unit contact bridge ground when with certain pooling feature, while on the top of mandril 12, by steel ball 13
Bridge face is contacted, is convenient for that sliding friction is changed into rolling friction in equipment flight course in this way, consequently facilitating reducing buffering group
Frictional force between part and bridge face ensures the smooth flight of flight instruments.
As shown in figure 5, the bindiny mechanism includes several connection components, the connection component is circumferentially evenly distributed on main body
1 periphery, the connection component include second spring 14, pressure plare 15 and connecting rod 16, one end of the second spring 14 with
Main body 1 connects, and the other end of the second spring 14 is connect with the side of pressure plare 15, and the other side of the pressure plare 15 passes through
Connecting rod 16 is fixedly connected with protection ring 2.
In flight instruments flight course, when protection ring 2 collides the bridge pier below bridge, protection ring 2 is resisted against bridge
On pier, keep the deformation quantity of second spring 14 in each connection component different, cushioning effect power is improved by second spring 14, it is main simultaneously
Body 1 is arranged inside protection ring 2, to avoid main body 1 from colliding with bridge pier when protection ring 2 being enable to collide bridge pier, just
In the smooth flight and detection of device.
As shown in Fig. 2, the aviation mechanism includes side lever 17, first motor 18, the first drive shaft 19 and two rotors 20,
The first motor 18 is fixedly connected by side lever 17 with the bottom end of sunpender 3, and the first motor 18 and the first drive shaft 19 pass
Dynamic connection, two rotors 20 are separately positioned on the both sides of first motor 18.First motor 18 is fixed on main body 1 by side lever 17
Lower section, first motor 18 are run, and drive two rotors 20 to rotate by the first drive shaft 19, generate downward air-flow, and four fly
The total active force for the air-flow that row mechanism generates is more than the gravity of device, to make device float the flight function of realization device.
As shown in figure 3, the adjusting part include the second motor 21, buffer stopper 22, the second drive shaft 23, movable block 24,
Hinged block 25 and strut 26, second motor 21 and buffer stopper 22 are each attached in main body 1, and second drive shaft 23 is arranged
Between the second motor 21 and buffer stopper 22, second motor, 21 and second drive shaft 23 is sequentially connected, second driving
The periphery of axis 23 is equipped with external screw thread, and the movable block 24 is set in the second drive shaft 23, and interior spiral shell is equipped in the movable block 24
Line, the internal thread in the movable block 24 match with the external screw thread in the second drive shaft 23, and the movable block 24 passes through strut
26 is hinged with hinged block 25, and the hinged block 25 is fixed on cylinder 8.
In adjusting part, the operation of the second motor 21 drives the rotation of the second drive shaft 23, makes the outer spiral shell in the second drive shaft 23
Line acts on the internal thread in movable block 24, so that movable block 24 is moved along the axis direction of the second drive shaft 23, passes through strut
26 drive hinged block 25 to rotate, to realize the rotation of cylinder 8, by the rotation of cylinder 8, and turn with piston 9 and link block 6
It is dynamic, consequently facilitating adjusting the angle of camera 5.
Preferably, for the ease of the rotation of cylinder 8, the hinge unit includes pillar 27, intubation 28 and inserted link 29, institute
The top that intubation 28 is fixed on main body 1 by pillar 27 is stated, one end of the inserted link 29 is fixedly connected with cylinder 8, the inserted link
29 other end setting is in intubation 28.One end of inserted link 29 is fixed on cylinder 8, and the other end of inserted link 29 can be along intubation
28 axis rotation fixes rotation to facilitate gas bar.
Preferably, in order to ensure that mandril 12 smoothly moves, the buffer cell further includes spacing ring 30, the limit
Ring 30 is fixed on the inner wall of casing 10, and the spacing ring 30 is set on mandril 12.Mandril 12 is secured using spacing ring 30
Lifting track, to make mandril 12 smoothly be moved.
As shown in figure 5, the both sides of the second spring 14 are equipped with limit assembly, the limit assembly includes 31 He of fixed link
Slip ring 32, the fixed link 31 are fixed on the body 1, and the slip ring 32 is set in fixed link 31, the slip ring 32 and pressure
Plate 15 is fixedly connected.It is slided in fixed fixed link 31 using slip ring 32, to limit the scope of activities of pressure plare 15, is led to
The scope of activities that connecting rod 16 limits protection ring 2 is crossed, violent shake occurs when preventing protection ring 2 from colliding bridge pier, is influenced
The flight of equipment.
Preferably, in order to ensure that slip ring 32 can smoothly slide in fixed link 31, the slip ring 32 and fixed link 31
For clearance fit.
Preferably, for the ease of detecting the deformation quantity of second spring 14, pressure sensor is equipped in the pressure plare 15
33.Before 2 collisionless of protection ring, the deformation quantity of second spring 14 is identical in each connection component, what pressure sensor 33 detected
Pressure data is identical, and therefore, with the generation of collision, the deformation quantity of second spring 14 is different, what pressure sensor 33 detected
Pressure data is different.
Preferably, for the ease of detection camera 5 at a distance from bridge bottom surface, while brightness is shot by increase and is ensured
Camera 5 acquires clear image, and the link block 6 is equipped with light compensating lamp 34 and range sensor 35.
Preferably, in order to improve the intelligence degree of equipment, it is equipped with PLC and antenna in the main body 1, the antenna,
First motor 18, the second motor 21, air pump 7, pressure sensor 33, light compensating lamp 34 and range sensor 35 are electrically connected with PLC.
Herein, antenna is mainly used for emitting and receiving wireless signal, by the transmission of wireless signal, realizes that equipment is set with some remote controls
Standby wireless telecommunications addition, is convenient for remote control, and PLC can receive the pressure data and range sensor of pressure sensor 33
35 range data judges whether protection ring 2 collides to bridge pier and detection camera 5 and bridge by two kinds of data respectively
The distance of bottom surface, while PLC air pump 7 can also be controlled according to distance signal and the second motor 21 is run, and changes the angle of camera 5
And position, so that camera 5 is shot from different orientation, and the picture of shooting is given by antenna wireless transmission in remote control
End, PLC can also control the operation of first motor 18, adjust the velocity of rotation of rotor 20, control the gas that each aviation mechanism generates
Size is flowed, to which state of flight can be adjusted when protection ring 2 collides bridge pier, makes protection ring 2 far from bridge pier, realizes equipment
Intelligent regulatory function.
The flight instruments are detected work by the flight in bridge bottom surface, avoid occupancy track from influencing road vehicles logical
Row prevents main body 1 from being collided with bridge by Buffer Unit contact bridge pier bottom face, protects main body 1 by protection ring 2, prevents main body
1 collides bridge pier, drives camera 5 to move by telescopic component, adjusts the position of camera 5, until camera 5 can be clear
Bridge ground is shot, drives cylinder 8 to rotate by translation component, to change the shooting angle of camera 5, makes camera 5 never
Same angle is shot, and blind spot is avoided the occurrence of.
Compared with prior art, which passes through detection machine
Structure is moved and is rotated to camera 5, and the angle orientation for keeping camera 5 different is shot, and it is blind to avoid the occurrence of shooting
Point, compared with traditional testing agency, which can comprehensively be clapped by the flexible rotating and mobile realize of camera 5
It takes the photograph, moreover, prevents from colliding with bridge and bridge pier when 1 flight of main body by buffer gear and protection ring 2, ensure that dress
The safe flight set, compared with traditional buffer gear, which is rolled after being contacted with bridge bottom surface by steel ball 13
It is dynamic, it prevents mandril 12 from rubbing with bridge bottom surface and causes the damage of bridge bottom surface, while being also convenient for the flight of equipment, to improve
The practicability of device.
It is enlightenment, through the above description, related work people with the above-mentioned desirable embodiment according to the utility model
Member can carry out various changes and amendments in the range of without departing from this item utility model technological thought completely.This item is real
It is not limited to the contents of the specification with novel technical scope, it is necessary to which its technology is determined according to right
Property range.
Claims (10)
1. a kind of intelligent flight instruments with barrier avoiding function for bridge machinery, which is characterized in that including main body (1),
Protection ring (2), sunpender (3), testing agency, bindiny mechanism, buffer gear, four aviation mechanisms and four stabilizer blades (4), the guarantor
Retaining ring (2) is set in main body (1), and the bindiny mechanism is arranged between protection ring (2) and main body (1), the sunpender (3)
Top is fixed on the lower section of main body (1), and the aviation mechanism is circumferentially evenly distributed on the periphery of the bottom end of sunpender (3), each stabilizer blade
(4) it is arranged in the lower section of two neighboring aviation mechanism, the buffer gear and testing agency are arranged at the top of main body (1)；
The testing agency includes camera (5), link block (6), telescopic component and adjusting part, and the telescopic component setting exists
The lower section of camera (5), the telescopic component include air pump (7), cylinder (8), piston (9) and two hinge units, two hinges
Order member is separately positioned on the both sides of cylinder (8), and the bottom end of the cylinder (8) is connect by hinge unit with main body (1), described
Air pump (7) is fixed on cylinder (8), and the air pump (7) is connected to cylinder (8), and the bottom end of the piston (9) is arranged in cylinder
(8) in, the top of the piston (9) is fixedly connected with link block (6), and the camera (5) is fixed on the upper of link block (6)
Side, the adjusting part are sequentially connected with cylinder (8)；
The buffer gear includes several Buffer Units, and the Buffer Unit is circumferentially evenly distributed on the top of main body (1), described
Buffer Unit includes casing (10), the first spring (11), mandril (12) and steel ball (13), and described sleeve pipe (10) is fixed on main body
(1) on, the bottom end setting of the mandril (12) is in casing (10), the bottom of the bottom end and casing (10) of first spring (11)
Portion connects, and the top of first spring (11) is connect with the bottom end of mandril (12), and the top of the mandril (12) is equipped with recess,
The steel ball (13) matches with recess, and the steel ball (13) is arranged in recess, and the centre of sphere of the steel ball (13) is located at recess
It is interior；
The bindiny mechanism includes several connection components, and the connection component is circumferentially evenly distributed on the periphery of main body (1), described
Connection component includes second spring (14), pressure plare (15) and connecting rod (16), one end of the second spring (14) and main body
(1) it connects, the other end of the second spring (14) is connect with the side of pressure plare (15), the other side of the pressure plare (15)
It is fixedly connected with protection ring (2) by connecting rod (16).
2. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, which is characterized in that
The aviation mechanism includes side lever (17), first motor (18), the first drive shaft (19) and two rotors (20), first electricity
Machine (18) is fixedly connected by side lever (17) with the bottom end of sunpender (3), and the first motor (18) passes with the first drive shaft (19)
Dynamic connection, two rotors (20) are separately positioned on the both sides of first motor (18).
3. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, which is characterized in that
The adjusting part includes the second motor (21), buffer stopper (22), the second drive shaft (23), movable block (24), hinged block (25)
With strut (26), second motor (21) and buffer stopper (22) are each attached in main body (1), and second drive shaft (23) sets
It sets between the second motor (21) and buffer stopper (22), second motor (21) is sequentially connected with the second drive shaft (23), institute
The periphery for stating the second drive shaft (23) is equipped with external screw thread, and the movable block (24) is set in the second drive shaft (23), the shifting
Internal thread, the internal thread in the movable block (24) and the external screw thread phase in the second drive shaft (23) are equipped in motion block (24)
Match, the movable block (24) is hinged by strut (26) and hinged block (25), and the hinged block (25) is fixed on cylinder (8).
4. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, which is characterized in that
The hinge unit includes that pillar (27), intubation (28) and inserted link (29), the intubation (28) are fixed on master by pillar (27)
One end of the top of body (1), the inserted link (29) is fixedly connected with cylinder (8), and the other end setting of the inserted link (29) is being inserted
It manages in (28).
5. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, which is characterized in that
The Buffer Unit further includes spacing ring (30), and the spacing ring (30) is fixed on the inner wall of casing (10), the spacing ring
(30) it is set on mandril (12).
6. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, which is characterized in that
The both sides of the second spring (14) are equipped with limit assembly, and the limit assembly includes fixed link (31) and slip ring (32), described
Fixed link (31) is fixed in main body (1), and the slip ring (32) is set in fixed link (31), the slip ring (32) and pressure plare
(15) it is fixedly connected.
7. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as claimed in claim 6, which is characterized in that
The slip ring (32) is clearance fit with fixed link (31).
8. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, which is characterized in that
Pressure sensor (33) is equipped in the pressure plare (15).
9. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, which is characterized in that
The link block (6) is equipped with light compensating lamp (34) and range sensor (35).
10. being used for the intelligent flight instruments with barrier avoiding function of bridge machinery as described in claim 1, feature exists
In equipped with PLC and antenna, the antenna, first motor (18), the second motor (21), air pump (7), pressure in the main body (1)
Sensor (33), light compensating lamp (34) and range sensor (35) are electrically connected with PLC.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820208297.4U CN207985193U (en) | 2018-02-06 | 2018-02-06 | A kind of intelligent flight instruments with barrier avoiding function for bridge machinery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820208297.4U CN207985193U (en) | 2018-02-06 | 2018-02-06 | A kind of intelligent flight instruments with barrier avoiding function for bridge machinery |
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| Publication Number | Publication Date |
|---|---|
| CN207985193U true CN207985193U (en) | 2018-10-19 |
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ID=63824040
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820208297.4U Expired - Fee Related CN207985193U (en) | 2018-02-06 | 2018-02-06 | A kind of intelligent flight instruments with barrier avoiding function for bridge machinery |
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| Country | Link |
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| CN (1) | CN207985193U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113998109A (en) * | 2021-11-17 | 2022-02-01 | 北京京能能源技术研究有限责任公司 | Unmanned aerial vehicle with autonomous navigation of space in furnace |
| WO2022070375A1 (en) * | 2020-09-30 | 2022-04-07 | 日本電信電話株式会社 | Propeller guard, flight vehicle, and repulsion mechanism |
| CN114674931A (en) * | 2022-03-18 | 2022-06-28 | 宁波市政工程建设集团股份有限公司 | Multi-functional road bridge concrete structure real-time detection device |
-
2018
- 2018-02-06 CN CN201820208297.4U patent/CN207985193U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022070375A1 (en) * | 2020-09-30 | 2022-04-07 | 日本電信電話株式会社 | Propeller guard, flight vehicle, and repulsion mechanism |
| CN113998109A (en) * | 2021-11-17 | 2022-02-01 | 北京京能能源技术研究有限责任公司 | Unmanned aerial vehicle with autonomous navigation of space in furnace |
| CN113998109B (en) * | 2021-11-17 | 2022-05-13 | 北京京能能源技术研究有限责任公司 | Unmanned aerial vehicle with autonomous navigation function for space in furnace |
| CN114674931A (en) * | 2022-03-18 | 2022-06-28 | 宁波市政工程建设集团股份有限公司 | Multi-functional road bridge concrete structure real-time detection device |
| CN114674931B (en) * | 2022-03-18 | 2023-06-30 | 宁波市政工程建设集团股份有限公司 | Multi-functional road and bridge concrete structure real-time detection device |
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