CN221543908U - Fast-assembling formula lifting load thing aerial posture regulator - Google Patents
Fast-assembling formula lifting load thing aerial posture regulator Download PDFInfo
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- CN221543908U CN221543908U CN202323505607.9U CN202323505607U CN221543908U CN 221543908 U CN221543908 U CN 221543908U CN 202323505607 U CN202323505607 U CN 202323505607U CN 221543908 U CN221543908 U CN 221543908U
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- 239000013598 vector Substances 0.000 claims abstract description 19
- 230000003014 reinforcing effect Effects 0.000 claims description 6
- 229910000617 Mangalloy Inorganic materials 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 4
- 230000033228 biological regulation Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 5
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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Abstract
The utility model discloses a fast-assembled lifting object air posture regulator, which is characterized by comprising the following components: a telescopic sleeve rod, the interior of which is hollow; the symmetrical telescopic rods are respectively arranged at one end of the telescopic sleeve rod; the symmetrical vector propulsion equipment is respectively arranged on one side of the corresponding telescopic rods and is respectively and fixedly connected with the corresponding telescopic rods. The utility model relates to the field of lifting gesture adjustment, in particular to a fast-assembled lifting object air gesture adjuster. The utility model aims to solve the technical problem of providing a quick-assembly lifting object air posture regulator which is beneficial to realizing the air posture regulation of the lifting object.
Description
Technical Field
The utility model relates to the field of lifting gesture adjustment, in particular to a fast-assembled lifting object air gesture adjuster.
Background
When lifting equipment such as a traditional crane and a crane tower is used for lifting cargoes and placing cargoes, the problem that a person cannot interfere with a carrying platform is faced, and the lifting rope cannot rotate automatically. This presents a series of challenges for the lifting operation, including the need for rotation of the load platform and micro displacement of the cargo. Meanwhile, the adjustment of the posture of the suspended vehicle-mounted object after the suspended is also an important link, the swing and collision of the suspended object can be effectively avoided by keeping the horizontal or preset angle, the suspended time and energy consumption are reduced, and the integral suspended efficiency and the safety coefficient are improved.
At present, the adjustment of the posture of the suspended object is usually carried out by a ground manual rope pulling mode, but the mode has the problems of low control precision, potential danger to ground personnel and the like.
Disclosure of utility model
The utility model aims to solve the technical problem of providing a quick-assembly lifting object air posture regulator which is beneficial to realizing the air posture regulation of the lifting object.
The utility model adopts the following technical scheme to realize the aim of the utility model:
A quick-assembly lifting load air attitude adjuster, comprising: a telescopic sleeve rod, the interior of which is hollow; the symmetrical telescopic rods are respectively arranged at one end of the telescopic sleeve rod; the symmetrical vector propulsion equipment is respectively arranged on one side of the corresponding telescopic rods and is respectively and fixedly connected with the corresponding telescopic rods.
As a further limitation of the technical scheme, two ends of the telescopic loop bar are respectively and fixedly connected with lifting lugs.
As a further limitation of the technical scheme, the symmetrical lifting lugs are respectively tied with one end of a lifting rope.
As a further limitation of the technical scheme, the symmetrical telescopic rods are respectively and fixedly connected with the lifting hooks.
As a further limitation of the technical scheme, the symmetrical hooks are respectively and fixedly connected with symmetrical elastic clamping pieces.
As a further limitation of the technical scheme, the elastic clamping piece is made of a manganese steel sheet.
As a further limitation of the technical scheme, the symmetrical lifting hooks are respectively and fixedly connected with the reinforcing inclined rods, and the symmetrical reinforcing inclined rods are respectively and fixedly connected with the corresponding telescopic rods.
As a further limitation of the technical scheme, two ends of the telescopic loop rod are respectively provided with a group of uniformly distributed adjusting holes.
Compared with the related art, the quick-assembly lifting object air posture regulator provided by the utility model has the following beneficial effects:
(1) The device realizes multidimensional motion control of the cargo platform, including rotation and micro-translation by introducing vector propulsion equipment. The hoisting operation is more flexible and has stronger adaptability on the non-manual contact carrying platform.
(2) The safety of hoisting operation is greatly improved by introducing a remote control system. Ground personnel can accurately control the propulsion equipment through the remote equipment at a safe position, and potential risk factors are reduced.
(3) Through the use of the multi-sensor system, the invention is excellent in realizing the adjustment and stabilization of the suspended object posture. The stability of the suspended object in the air is greatly improved, and the vibration and shaking in the hoisting process are reduced, so that the operation efficiency and the safety are improved.
Drawings
Fig. 1 is a schematic structural view of the present utility model.
In the figure: 1. the lifting rope, 2, vector propulsion equipment, 3, lifting lug, 4, flexible loop bar, 5, telescopic link, 6, regulation hole, 7, lifting hook, 8, elasticity clamping piece.
Detailed Description
The utility model will be further described with reference to the drawings and embodiments.
A quick-mount lift load air attitude adjuster comprising: a telescopic loop bar 4, the interior of which is hollow; the symmetrical telescopic rods 5 are respectively arranged at one end of the telescopic sleeve rod 4; the symmetrical vector propulsion devices 2 are respectively arranged on one sides of the corresponding telescopic rods 5 and are respectively and fixedly connected with the corresponding telescopic rods 5.
The two ends of the telescopic loop bar 4 are respectively and fixedly connected with the lifting lug 3.
The symmetrical lifting lugs 3 are respectively tied with one end of the lifting rope 1.
The symmetrical telescopic rods 5 are respectively and fixedly connected with a lifting hook 7.
The symmetrical hooks 7 are respectively and fixedly connected with symmetrical elastic clamping pieces 8.
The elastic clamping piece 8 is made of manganese steel sheets.
The lifting hooks 7 are respectively and fixedly connected with reinforcing inclined rods, and the reinforcing inclined rods are respectively and fixedly connected with the corresponding telescopic rods 5.
Two ends of the telescopic loop bar 4 are respectively provided with a group of uniformly distributed adjusting holes 6.
The telescopic rod 5 is in threaded connection with a group of mounting bolts, and the mounting bolts are matched with the adjusting holes 6.
The middle position of the telescopic loop bar 4 is fixedly connected with a group of angle sensors and magnetic force sensors so as to monitor the inclination and rotation states of the suspended objects in real time.
The angle sensor employs an MPU6050.
The magnetic force sensor adopts HMC5883L.
The middle position of the telescopic loop rod 4 is fixedly connected with a controller, and the angle sensor, the magnetic force sensor and the vector propulsion equipment 2 are respectively and electrically connected with the controller.
The controller is connected with an upper computer, such as a mobile phone, a computer, a PC, a display and the like in a wireless way. 5. The operator is allowed to monitor the state of the suspended object in real time through a remote interface, the direction of the vector propulsion equipment is adjusted by manual interference, the micro displacement of the suspended object is realized, and the accuracy of the hoisting process is ensured.
The vector propulsion device 2 is composed of a plurality of independently controlled propulsion units, each propulsion unit comprises a high-performance motor (model: 2812 brushless motor), a paddle and a vector control unit, and the vector control unit is a core of a vector propulsion technology and is essentially a device for controlling the paddle to rotate at multiple angles, so that accurate dynamic adjustment in horizontal, vertical and rotating directions is realized. The propulsion units are skillfully arranged at the two ends of the boom, ensuring the omnibearing control. Are well known to those skilled in the art.
The controller is equipped with an efficient intelligent control algorithm which analyzes the state of the suspended object in real time based on sensor data and enables the suspended object to maintain a preset posture by adjusting the direction of the vector propulsion device 2. For example, as the crane rotates, the control algorithm responds momentarily, adjusting the blade direction in the vector propulsion device 2 to smoothly adjust the crane attitude.
The utility model provides a fast-assembled lifting object air posture regulator, which has the following working principle:
According to the size of the hoisted object, the extension of the telescopic rod 5 relative to the telescopic sleeve rod 4 is adjusted. The bolts are screwed into the appropriate adjustment holes 6. The two ends of the hanging object are respectively hung in the hanging hook 7, so that the hanging object is positioned at the lower side of the elastic clamping piece 8.
In the hoisting process, the angle sensor and the magnetic force sensor monitor the inclination and rotation state data of the hoisted object and upload the data to the controller, the controller enables the vector control unit in the vector pushing equipment 2 to adjust the direction of the blade by vectors through an intelligent control algorithm, and the controller controls the posture of the hoisted object, for example, when the hoisted object rotates clockwise, the control program can adjust the direction of the blade, and the anticlockwise acting force of the hoisted object is given, so that the posture is stable. In addition, when in hoisting, personnel can also adjust the direction of the vector control device through the remote control system, so that the hoisted object can slightly displace and accurately reach the hoisting position.
Compared with the related art, the quick-assembly lifting object air posture regulator provided by the utility model has the following beneficial effects:
The device realizes multidimensional motion control of the cargo platform, including rotation and micro-translation, by introducing vector propulsion equipment 2. The hoisting operation is more flexible and has stronger adaptability on the non-manual contact carrying platform.
The safety of hoisting operation is greatly improved by introducing a remote control system. Ground personnel can accurately control the propulsion equipment through the remote equipment at a safe position, and potential risk factors are reduced.
Through the use of the multi-sensor system, the invention is excellent in realizing the adjustment and stabilization of the suspended object posture. The stability of the suspended object in the air is greatly improved, and the vibration and shaking in the hoisting process are reduced, so that the operation efficiency and the safety are improved.
The foregoing description is only illustrative of the present utility model and is not intended to limit the scope of the utility model, and all equivalent structures or equivalent processes or direct or indirect application in other related technical fields are included in the scope of the present utility model.
Claims (8)
1. A quick-assembly lifting load air attitude adjuster, comprising:
a telescopic sleeve rod (4) which is hollow;
The symmetrical telescopic rods (5) are respectively arranged at one end of the telescopic sleeve rod (4);
The symmetrical vector propulsion equipment (2) is respectively arranged at one side of the corresponding telescopic rods (5) and is respectively and fixedly connected with the corresponding telescopic rods (5).
2. The quick-fit lifting load air attitude adjuster of claim 1, characterized by: the two ends of the telescopic loop bar (4) are respectively and fixedly connected with the lifting lugs (3).
3. The quick-fit lifting load air attitude adjuster of claim 2, characterized by: the symmetrical lifting lugs (3) are respectively tied with one end of the lifting rope (1).
4. The quick-fit lifting load air attitude adjuster of claim 1, characterized by: the symmetrical telescopic rods (5) are respectively and fixedly connected with a lifting hook (7).
5. The quick-fit lifting load air attitude adjuster of claim 4, wherein: the symmetrical lifting hooks (7) are respectively and fixedly connected with symmetrical elastic clamping pieces (8).
6. The quick-fit lifting load air attitude adjuster of claim 5, wherein: the elastic clamping piece (8) is made of manganese steel sheets.
7. The quick-fit lifting load air attitude adjuster of claim 4, wherein: the lifting hooks (7) are respectively and fixedly connected with the reinforcing inclined rods, and the reinforcing inclined rods are respectively and fixedly connected with the corresponding telescopic rods (5).
8. The quick-fit lifting load air attitude adjuster of claim 1, characterized by: two ends of the telescopic loop rod (4) are respectively provided with a group of uniformly distributed adjusting holes (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323505607.9U CN221543908U (en) | 2023-12-21 | 2023-12-21 | Fast-assembling formula lifting load thing aerial posture regulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323505607.9U CN221543908U (en) | 2023-12-21 | 2023-12-21 | Fast-assembling formula lifting load thing aerial posture regulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221543908U true CN221543908U (en) | 2024-08-16 |
Family
ID=92249110
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323505607.9U Active CN221543908U (en) | 2023-12-21 | 2023-12-21 | Fast-assembling formula lifting load thing aerial posture regulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221543908U (en) |
-
2023
- 2023-12-21 CN CN202323505607.9U patent/CN221543908U/en active Active
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