CN218172630U - Unmanned aerial vehicle flies to control with balanced detection device - Google Patents
Unmanned aerial vehicle flies to control with balanced detection device Download PDFInfo
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- CN218172630U CN218172630U CN202221969904.1U CN202221969904U CN218172630U CN 218172630 U CN218172630 U CN 218172630U CN 202221969904 U CN202221969904 U CN 202221969904U CN 218172630 U CN218172630 U CN 218172630U
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Abstract
The utility model discloses an unmanned aerial vehicle flies to control and uses balanced detection device, including unmanned aerial vehicle mounting substrate and remote terminal, unmanned aerial vehicle mounting substrate's top is provided with the locating plate, the top welding of locating plate has the carriage, the front side at carriage top has the gyroscope sensor through bolt fixed mounting, the front side fixed mounting at carriage top has inclination sensor. The utility model discloses a locating plate, tilt sensor, carriage, air velocity transducer, radio signal transmitter, gyroscope sensor, jack, gag lever post, coupling spring, clamp plate and remote terminal cooperation are used, have solved current balance detection device and can't carry out real-time detection and remote transmission to air current wind speed and fuselage balance, and the installation convenience is relatively poor, increase the staff with device and unmanned aerial vehicle installation operating time, influence experimental detection efficiency, reduced the problem of balance detection device practicality.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle test technical field specifically is an unmanned aerial vehicle flies to control and uses balanced detection device.
Background
The unmanned plane is called as an unmanned plane for short, is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, is applied in the unmanned plane industry in the civil aspect and is really just needed by the unmanned plane; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like, and the use of the unmanned aerial vehicle is greatly expanded.
In order to make unmanned aerial vehicle still keep stable flight in the air current of certain intensity, then in unmanned aerial vehicle production engineering, can use balanced detection device to detect unmanned aerial vehicle flight state, current balanced detection device can't carry out real-time detection and teletransmission to air current wind speed and fuselage balance, and it is relatively poor to install the convenience, increase the staff with device and unmanned aerial vehicle installation operating time, influence experimental detection efficiency, the practicality of balanced detection device has been reduced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle flies to control and uses balanced detection device, possesses the advantage of data remote transmission and convenient installation, has solved current balanced detection device and can't carry out real-time detection and remote transmission to air current wind speed and fuselage balance, and installs the convenience relatively poor, increases the staff and installs operating time with unmanned aerial vehicle installation, influences experimental detection efficiency, has reduced the problem of balanced detection device practicality.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle flies to control and uses balance detection device, includes unmanned aerial vehicle mounting substrate and remote terminal, unmanned aerial vehicle mounting substrate's top is provided with the locating plate, the top welding of locating plate has the carriage, there is the gyroscope sensor front side at carriage top through bolt fixed mounting, the front side fixed mounting at carriage top has inclination sensor, there is wireless transmitter on the right side at carriage top through screw fixed mounting, there is air velocity transducer rear side at carriage top through screw fixed mounting, there is the screw rod at the center department at carriage top through bearing movable mounting, the bottom thread bush on screw rod surface is equipped with the clamp plate, the left and right sides of locating plate all runs through and installs spacing subassembly.
Preferably, the mounting groove that uses with the locating plate cooperation is seted up at unmanned aerial vehicle mounting substrate's top, the welding of the bottom of mounting groove inner chamber has the locating piece, the locating hole that uses with the locating piece cooperation is seted up at the top of locating plate, the jack that uses with spacing subassembly cooperation is all seted up to the left and right sides of mounting groove inner chamber.
Preferably, the output ends of the tilt angle sensor, the wind speed sensor and the gyroscope sensor are in signal connection with the input end of the wireless signal transmitter, and the output end of the wireless signal transmitter is in signal connection with the input end of the remote terminal.
Preferably, the top of the screw rod is welded with an anti-skid torsion block, and the vertical inner diameter of the connecting frame is larger than the vertical length of the pressing plate.
Preferably, the bottom of the inner cavity of the positioning plate is welded with a guide rod, and the top of the pressing plate is provided with a guide hole matched with the guide rod for use.
Preferably, the limiting assembly comprises a limiting rod, the surface of the limiting rod is in sliding contact with the joint of the positioning plate, a connecting spring is sleeved on the surface of the limiting rod, one end of the connecting spring is welded with the joint of the limiting rod, the other end of the connecting spring is fixedly connected with the joint of the positioning plate, and one end of the limiting rod is in surface contact with the pressing plate.
Compared with the prior art, the beneficial effects of the utility model are as follows:
the utility model discloses a locating plate, tilt sensor, carriage, air velocity transducer, radio signal transmitter, gyroscope sensor, jack, gag lever post, coupling spring, clamp plate and remote terminal cooperation are used, have solved current balance detection device and can't carry out real-time detection and remote transmission to air current wind speed and fuselage balance, and the installation convenience is relatively poor, increase the staff with device and unmanned aerial vehicle installation operating time, influence experimental detection efficiency, reduced the problem of balance detection device practicality.
Drawings
FIG. 1 is a perspective view of the present invention;
FIG. 2 is a perspective view of the present invention with the structure separated;
FIG. 3 is a perspective view of the present invention showing a partial structure;
FIG. 4 is a schematic perspective view of the limiting assembly and the pressing plate of the present invention when they are mounted;
fig. 5 is a schematic diagram of the system of the present invention.
In the figure: 1 unmanned aerial vehicle mounting substrate, 2 locating plates, 3 angular transducer, 4 locating pieces, 5 connection frames, 6 air velocity transducer, 7 screw rods, 8 wireless transmitter, 9 gyroscope sensor, 10 locating holes, 11 jacks, 12 mounting grooves, the spacing subassembly of 13, 131 gag lever post, 132 coupling spring, 14 clamp plates, 15 guide bars, 16 guiding holes, 17 remote terminal.
Detailed Description
Referring to fig. 1-5, a balance detection device for unmanned aerial vehicle flight control comprises an unmanned aerial vehicle mounting substrate 1 and a remote terminal 17, wherein a positioning plate 2 is arranged at the top of the unmanned aerial vehicle mounting substrate 1, a connecting frame 5 is welded at the top of the positioning plate 2, the connecting frame 5 is arranged to provide a mounting space for a wind speed sensor 6, a wireless signal transmitter 8, a gyroscope sensor 9 and a tilt angle sensor 3, and the positioning plate 14 plays a role in storage, the gyroscope sensor 9 is fixedly mounted at the front side of the top of the connecting frame 5 through bolts, the tilt angle sensor 3 is fixedly mounted at the front side of the top of the connecting frame 5, the wireless signal transmitter 8 is fixedly mounted at the right side of the top of the connecting frame 5 through screws, the wind speed sensor 6 is fixedly mounted at the rear side of the top of the connecting frame 5 through screws, a screw 7 is movably mounted at the center of the top of the connecting frame 5 through bearings, a pressing plate 14 is sleeved on a bottom thread on the surface of the screw 7, a screw 7 and the pressing plate 14 can play a role in thread transmission, when the screw 7 continuously rotates, and the left and right sides of the positioning plate 2 are respectively provided with a limiting component 13;
the top of the unmanned aerial vehicle mounting substrate 1 is provided with a mounting groove 12 matched with the positioning plate 2 for use, the positioning plate 2 can be accommodated and mounted on the unmanned aerial vehicle mounting substrate 1 by arranging the mounting groove 12, the bottom of the inner cavity of the mounting groove 12 is welded with the positioning block 4, the top of the positioning plate 2 is provided with a positioning hole 10 matched with the positioning block 4 for use, the positioning block 4 and the positioning hole 10 are arranged, the positioning plate 2 can be mounted to play a role in auxiliary positioning, the placing convenience of the positioning plate 2 is improved, the left side and the right side of the inner cavity of the mounting groove 12 are provided with jacks 11 matched with the limiting assemblies 13 for use, and through arrangement of the jacks 11, an insertion space can be provided for the limiting rods 131;
the output ends of the tilt angle sensor 3, the wind speed sensor 6 and the gyroscope sensor 9 are in signal connection with the input end of the wireless signal transmitter 8, and the output end of the wireless signal transmitter 8 is in signal connection with the input end of the remote terminal 17;
the anti-skidding twisting blocks are welded at the tops of the screw rods 7, friction force between the screw rods 7 and a contact object can be increased by arranging the anti-skidding twisting blocks, so that a worker can conveniently drive the screw rods 7 to rotate in actual use, and the vertical inner diameter of the connecting frame 5 is larger than the vertical length of the pressing plate 14;
the bottom of the inner cavity of the positioning plate 2 is welded with a guide rod 15, the top of the pressure plate 14 is provided with a guide hole 16 matched with the guide rod 15, and the guide rod 15 and the guide hole 16 are arranged to guide the vertical displacement of the pressure plate 14;
During the use, each part is in initial condition, clamp plate 14 is located the joint-box 5, and be in screw 7 surface top, connecting spring 132 is in the natural contraction state this moment, and gag lever post 131 is located locating plate 2, at first during the installation under locating piece 4 and locating hole 10 are supplementary, place locating plate 2 accurately in mounting groove 12, gag lever post 131 is in alignment state with jack 11 this moment, corotation screw rod 7, can make clamp plate 14 move down steadily, extrude gag lever post 131 hemisphere end, make gag lever post 131 automatic stretch out and get into jack 11 in, locating plate 2 and unmanned aerial vehicle mounting substrate 1 can't take place relative displacement this moment, realize stable installation, in the unmanned aerial vehicle actual flight test process, air velocity transducer 6 detects the air current wind speed, angular transducer 3 detects unmanned aerial vehicle inclination, gyroscope sensor 9 carries out the mobile positioning to unmanned aerial vehicle, above-mentioned data all transmits to remote terminal 17 through wireless signal transmitter 8, it provides data support to staff's calculation test, staff adjusts unmanned aerial vehicle flight mode in a flexible way, including flying speed and angle, guarantee unmanned aerial vehicle normal stable flight mode.
In conclusion: this unmanned aerial vehicle flies to control and uses balance detection device, through locating plate 2, inclination sensor 3, the connection box 5, air velocity transducer 6, wireless signal transmitter 8, gyroscope sensor 9, jack 11, gag lever post 131, coupling spring 132, clamp plate 14 and remote terminal 17 cooperation are used, current balance detection device has been solved and can't carry out real-time detection and teletransmission to air current wind speed and fuselage balance, and it is relatively poor to install the convenience, it installs operating time with device and unmanned aerial vehicle to increase the staff, influence experimental detection efficiency, the problem of balance detection device practicality has been reduced.
Claims (6)
1. The utility model provides an unmanned aerial vehicle flies to control with balanced detection device, includes unmanned aerial vehicle mounting substrate (1) and remote terminal (17), its characterized in that: the top of unmanned aerial vehicle mounting substrate (1) is provided with locating plate (2), the top welding of locating plate (2) has connecting frame (5), the front side at connecting frame (5) top has gyroscope sensor (9) through bolt fixed mounting, the front side fixed mounting at connecting frame (5) top has inclination sensor (3), there is wireless transmitter (8) on the right side at connecting frame (5) top through screw fixed mounting, the rear side at connecting frame (5) top has wind speed sensor (6) through screw fixed mounting, there is screw rod (7) at the center department at connecting frame (5) top through bearing movable mounting, the bottom thread bush on screw rod (7) surface is equipped with clamp plate (14), the left and right sides of locating plate (2) all runs through and installs spacing subassembly (13).
2. The balance detection device for unmanned aerial vehicle flight control according to claim 1, wherein: mounting groove (12) of using with locating plate (2) cooperation are seted up at the top of unmanned aerial vehicle mounting substrate (1), the bottom welding of mounting groove (12) inner chamber has locating piece (4), locating hole (10) of using with locating piece (4) cooperation are seted up at the top of locating plate (2), jack (11) of using with spacing subassembly (13) cooperation are all seted up to the left and right sides of mounting groove (12) inner chamber.
3. The balance detection device for unmanned aerial vehicle flight control according to claim 1, wherein: the output ends of the inclination angle sensor (3), the wind speed sensor (6) and the gyroscope sensor (9) are all in signal connection with the input end of the wireless signal transmitter (8), and the output end of the wireless signal transmitter (8) is in signal connection with the input end of the remote terminal (17).
4. The balance detection device for unmanned aerial vehicle flight control according to claim 1, characterized in that: the anti-skidding block is welded to the top of the screw rod (7), and the vertical inner diameter of the connecting frame (5) is larger than the vertical length of the pressing plate (14).
5. The balance detection device for unmanned aerial vehicle flight control according to claim 1, characterized in that: the bottom welding of locating plate (2) inner chamber has guide bar (15), guiding hole (16) that use with guide bar (15) cooperation are seted up at the top of clamp plate (14).
6. The balance detection device for unmanned aerial vehicle flight control according to claim 1, characterized in that: spacing subassembly (13) include gag lever post (131), the junction sliding contact of the surface of gag lever post (131) and locating plate (2), coupling spring (132) are established to the surface cover of gag lever post (131), the one end of coupling spring (132) and the junction welding of gag lever post (131), the other end of coupling spring (132) and the junction fixed connection of locating plate (2), the one end of gag lever post (131) and the surface contact of clamp plate (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221969904.1U CN218172630U (en) | 2022-07-28 | 2022-07-28 | Unmanned aerial vehicle flies to control with balanced detection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221969904.1U CN218172630U (en) | 2022-07-28 | 2022-07-28 | Unmanned aerial vehicle flies to control with balanced detection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218172630U true CN218172630U (en) | 2022-12-30 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221969904.1U Active CN218172630U (en) | 2022-07-28 | 2022-07-28 | Unmanned aerial vehicle flies to control with balanced detection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218172630U (en) |
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2022
- 2022-07-28 CN CN202221969904.1U patent/CN218172630U/en active Active
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