CN216424788U - Platform for detecting lifting force of unmanned aerial vehicle - Google Patents
Platform for detecting lifting force of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN216424788U CN216424788U CN202123062676.8U CN202123062676U CN216424788U CN 216424788 U CN216424788 U CN 216424788U CN 202123062676 U CN202123062676 U CN 202123062676U CN 216424788 U CN216424788 U CN 216424788U
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- Prior art keywords
- unmanned aerial
- aerial vehicle
- cask
- water
- bottom plate
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 86
- 238000003860 storage Methods 0.000 claims description 10
- 238000001514 detection method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000010923 batch production Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000012384 transportation and delivery Methods 0.000 description 1
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Abstract
The utility model provides a platform for detecting unmanned aerial vehicle lifting force. A platform for detecting drone lift, comprising: the bottom plate, the cask has been placed on the bottom plate, be provided with the connection rope on the cask, the connection rope is used for being connected with unmanned aerial vehicle, be provided with force sensor on the bottom plate, install the stay cord between cask and the force sensor, be provided with the water tank on the bottom plate, the top of bottom plate still is provided with the water pump, installs inlet tube and outlet pipe on the water pump, the inlet tube is connected with the water tank, the outlet pipe is located the top of cask, and the outlet pipe is used for carrying water in the cask. The utility model provides a platform for detecting unmanned aerial vehicle lifting force can confirm the critical value of unmanned aerial vehicle's the biggest lifting force through measuring the water yield in cask and the cask.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle detects technical field, especially relates to a platform for detecting unmanned aerial vehicle lifting force.
Background
Along with the development of science and technology in recent years, unmanned aerial vehicle's application field is also more and more extensive, and simultaneously, also more and more be harsh to the requirement of unmanned aerial vehicle various performance, unmanned aerial vehicle is before batch production, need pass through a series of tests, with whether meet the requirements of various performance of detection, also be the one side in the detection to unmanned aerial vehicle lifting force detection, the detection to unmanned aerial vehicle lifting force is for detecting unmanned aerial vehicle can promote multiple article, because some unmanned aerial vehicles are as the shooting instrument, it need carry shooting equipment, in order to ensure that unmanned aerial vehicle lifting force can meet the requirements, it is necessary to provide a platform that is used for detecting unmanned aerial vehicle lifting force in order to solve the problem of detecting unmanned aerial vehicle lifting force.
SUMMERY OF THE UTILITY MODEL
The utility model provides a technical problem provide a platform for detecting unmanned aerial vehicle lifting force can confirm the critical value of unmanned aerial vehicle's the biggest lifting force through measuring the water yield in cask and the cask.
In order to solve the technical problem, the utility model provides a platform for detecting unmanned aerial vehicle lifting power, include: the bottom plate, the cask has been placed on the bottom plate, be provided with the connection rope on the cask, the connection rope is used for being connected with unmanned aerial vehicle, be provided with force sensor on the bottom plate, install the stay cord between cask and the force sensor, be provided with the water tank on the bottom plate, the top of bottom plate still is provided with the water pump, installs inlet tube and outlet pipe on the water pump, the inlet tube is connected with the water tank, the outlet pipe is located the top of cask, and the outlet pipe is used for carrying water in the cask.
Preferably, a plurality of legs are installed at the bottom of the water tub.
Preferably, a display is further arranged on the bottom plate and used for displaying the stress numerical value of the tension sensor in real time.
Preferably, four supporting rods are arranged on the bottom plate, a return plate is installed at the tops of the four supporting rods, the connecting rope penetrates through the return plate, and the water pump is fixed to the bottom of the return plate.
Preferably, an MCU controller, a storage module and a display module are arranged in the display, and the MCU controller is electrically connected with the storage module, the display module and the water pump.
Preferably, a water flow meter is arranged on the water pump, and the water flow meter and the tension sensor are both electrically connected with the MCU controller.
Compared with the prior art, the utility model provides a platform for detecting unmanned aerial vehicle lifting force has following beneficial effect:
(1) this device is examining time measuring to unmanned aerial vehicle lifting force, the cask receives unmanned aerial vehicle's promotion, make the stay cord be in the state of flare-outing, the force sensor atress, the restart water pump, can make in the water tank water enter into the cask, it takes place to bend to drive the stay cord, the pulling force that force sensor received is zero hour promptly, the weight of cask and water wherein is the critical value of the biggest lifting force of unmanned aerial vehicle, thereby detectable unmanned aerial vehicle's the biggest lifting force.
(2) This device makes the detection to unmanned aerial vehicle lifting force more intelligent through setting up MCU controller, storage module, display module, force transducer and water flowmeter, can improve the degree of accuracy that detects to a certain extent, makes to detect simple, easy operation.
Drawings
Fig. 1 is a schematic structural diagram of a platform for detecting lifting force of an unmanned aerial vehicle provided by the present invention;
fig. 2 is a schematic structural diagram of a platform for detecting lifting force of an unmanned aerial vehicle provided by the present invention;
fig. 3 is the utility model provides a functional block diagram of a platform for detecting unmanned aerial vehicle lifting force.
Reference numbers in the figures: 1. the water tank comprises a bottom plate, 2, a water tank, 3, a connecting rope, 4, a tension sensor, 5, a pull rope, 6, supporting legs, 7, a water tank, 8, a water pump, 9, a water inlet pipe, 10, a water outlet pipe, 11, a display, 12, a supporting rod, 13 and a return plate.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and embodiments.
As shown in fig. 1-3, a platform for detecting the lift of an unmanned aerial vehicle, comprising: a bottom plate 1, a water bucket 2 is placed on the bottom plate 1, the water bucket 2 is used for containing water, the water bucket 2 is used as an object for lifting an unmanned aerial vehicle, a connecting rope 3 is arranged on the water bucket 2, the connecting rope 3 is used for being connected with the unmanned aerial vehicle so that the unmanned aerial vehicle can take off to drive the water bucket 2 to move upwards, a tension sensor 4 is arranged on the bottom plate 1, a pull rope 5 is arranged between the water bucket 2 and the tension sensor 4, the tension sensor 4 is pulled by the pull rope 5 after the water bucket 2 moves upwards for a certain distance, a water tank 7 is arranged on the bottom plate 1, meanwhile, a water pump 8 is also arranged above the water tank 1, a water inlet pipe 9 and a water outlet pipe 10 are arranged on the water pump 8, the water inlet pipe 9 is connected with the water tank 7, the water outlet pipe 10 is positioned above the water bucket 2, water flowing out through the water outlet pipe 10 can flow into the water bucket 2, after the unmanned aerial vehicle takes off, the water bucket 2 can be lifted by the unmanned aerial vehicle, upward movement, simultaneously cask 2 drives stay cord 5 and stretches, be in the state of flare-outing up stay cord 5, make force sensor 4 atress, at this moment, cask 2 still is located the below of outlet pipe 10, through starting water pump 8, can make the water in the water tank 7 enter into cask 2, it takes place the bending to drive stay cord 5, the pulling force that force sensor 4 received promptly is zero hour, the weight of cask 2 and water wherein is the critical value of the biggest lifting force of unmanned aerial vehicle (the weight of connecting rope 3 and stay cord 5 can neglect), thereby can know unmanned aerial vehicle's the biggest lifting force.
As shown in fig. 1, a plurality of legs 6 are installed at the bottom of the water tub 2, and the legs 6 are installed to place the bottom of the water tub 2 in contact with the tension sensor 4.
As shown in fig. 1, a display 11 is further disposed on the bottom plate 1, and the display 11 can display the stress condition of the tension sensor 4 in real time, so that a person can timely view that the stress of the tension sensor 4 is in a zero state.
As shown in fig. 1, set up four bracing pieces 12, four on the bottom plate 1 return board 13 is installed at the top of bracing piece 12, connect rope 3 to pass return board 13, water pump 8 is fixed return board 13's bottom, return board 13 and can regard as unmanned aerial vehicle's platform of taking off, simultaneously, still play certain limiting displacement, unmanned aerial vehicle when taking off, can take place certain rocking to drive and connect rope 3 and take place the slope, return board 13 and can be with the slope control of connecting rope 3 at certain scope, thereby provide the reference for unmanned aerial vehicle's the position of hovering.
The MCU controller is arranged in the display 11, the storage module and the display module are arranged in the display 11, the water flowmeter is arranged on the water pump 8, wherein the water flowmeter and the tension sensor 4 are electrically connected with the MCU controller, the MCU controller is electrically connected with the storage module, the display module and the water pump 8, after the unmanned aerial vehicle takes off, the water bucket 2 moves upwards, so that the pull rope 5 pulls the tension sensor 4, the pulling force received by the tension sensor 4 is transmitted to the MCU controller in the form of an electric signal, the MCU controller processes the signal and transmits the signal to the display module, so that the pulling force received by the tension sensor 4 is displayed in real time, the personnel can conveniently observe in time, meanwhile, the MCU controller also sends an instruction for starting the water pump 8, the water pump 8 is started, water in the water tank 7 is input into the water bucket 2, and meanwhile, the water flowmeter detects the flow of the water in real time, and give MCU controller with signal transmission, at the in-process to 2 water deliveries in the cask, the gravity that unmanned aerial vehicle received is bigger and bigger, the pulling force that can make force sensor 4 receive is more and more littleer, the pulling force that receives up to force sensor 4 is zero, the water pump 8 is closed to the MCU controller, and simultaneously, the numerical value that 4 pulling forces of storage module storage force sensor are zero, and the discharge that corresponds, personnel are through transferring corresponding data, can know the critical value of unmanned aerial vehicle's the biggest lifting force.
The utility model provides a theory of operation for detecting platform of unmanned aerial vehicle lifting force as follows:
at first, confirm the weight of cask 2, then, be connected unmanned aerial vehicle with being connected rope 3 again, start unmanned aerial vehicle, under unmanned aerial vehicle's drive, stay cord 5 is flare-outed, and make force sensor 4 atress, force sensor 4 passes the signal to the MCU controller, MCU controller control water pump 8 is to 2 interior water injections of cask, until force sensor 4 atress is zero, the water pump water injection, it is zero to show the force sensor atress on the display, the personnel are through the data in the retrieval storage module, can know the critical value of unmanned aerial vehicle's maximum lifting force.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.
Claims (6)
1. A platform for detecting unmanned aerial vehicle lifting power, comprising:
the bottom plate, the cask has been placed on the bottom plate, be provided with the connection rope on the cask, the connection rope is used for being connected with unmanned aerial vehicle, be provided with force sensor on the bottom plate, install the stay cord between cask and the force sensor, be provided with the water tank on the bottom plate, the top of bottom plate still is provided with the water pump, installs inlet tube and outlet pipe on the water pump, the inlet tube is connected with the water tank, the outlet pipe is located the top of cask, and the outlet pipe is used for carrying water in the cask.
2. The platform for detecting unmanned aerial vehicle lifting force of claim 1, wherein a plurality of legs are mounted to the bottom of the bucket.
3. The platform for detecting unmanned aerial vehicle lifting force of claim 1, wherein a display is further arranged on the bottom plate, and the display is used for displaying the force value of the tension sensor in real time.
4. The platform for detecting unmanned aerial vehicle lifting force of claim 1, wherein four support rods are arranged on the bottom plate, a return plate is mounted on the tops of the four support rods, the connecting rope passes through the return plate, and the water pump is fixed on the bottom of the return plate.
5. The platform of claim 3, wherein the display is internally provided with an MCU controller, a storage module and a display module, and the MCU controller is electrically connected with the storage module, the display module and the water pump.
6. The platform for detecting unmanned aerial vehicle lifting force of claim 5, wherein a water flow meter is arranged on the water pump, and the water flow meter and the tension sensor are both electrically connected with the MCU controller.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202123062676.8U CN216424788U (en) | 2021-12-07 | 2021-12-07 | Platform for detecting lifting force of unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202123062676.8U CN216424788U (en) | 2021-12-07 | 2021-12-07 | Platform for detecting lifting force of unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
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CN216424788U true CN216424788U (en) | 2022-05-03 |
Family
ID=81342944
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202123062676.8U Expired - Fee Related CN216424788U (en) | 2021-12-07 | 2021-12-07 | Platform for detecting lifting force of unmanned aerial vehicle |
Country Status (1)
Country | Link |
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CN (1) | CN216424788U (en) |
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2021
- 2021-12-07 CN CN202123062676.8U patent/CN216424788U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220503 |