CN211042213U - Unmanned aerial vehicle track detection device - Google Patents
Unmanned aerial vehicle track detection device Download PDFInfo
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- CN211042213U CN211042213U CN202020091313.3U CN202020091313U CN211042213U CN 211042213 U CN211042213 U CN 211042213U CN 202020091313 U CN202020091313 U CN 202020091313U CN 211042213 U CN211042213 U CN 211042213U
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- unmanned aerial
- aerial vehicle
- detection device
- detector
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Abstract
The utility model discloses an unmanned aerial vehicle flight path detection device. This unmanned aerial vehicle flight path detection device includes the base, installs at support column, circulator, angle adjuster, the detector that detects the flight path at base top, two connecting plates, two fixed plates, two movable rods, two fly leaves, two expanding spring and two dead levers. The utility model discloses an unmanned aerial vehicle track detection device, in the dead lever disect insertion first mounting hole during the installation, because dead lever and the terminal coincidence effect of movable rod, outwards push the movable rod when inserting, simultaneously expanding spring saves elasticity, thereby make can insert completely in the first mounting hole by the dead lever, because expanding spring's elastic action, make inside the very smooth jack that inserts of movable rod, install detector and angle regulator like this, it is both convenient and swift, thereby the installation effectiveness is improved, and then the maintenance efficiency is improved.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to an unmanned aerial vehicle flight path detection device.
Background
An unmanned aerial vehicle, abbreviated as "unmanned aerial vehicle" ("UAV"), is an unmanned aerial vehicle that is operated using a radio remote control device and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.
When the unmanned aerial vehicle carries out some dangerous tasks, for example, a picture is taken at a fixed point of a specific part on a power line tower, due to the fact that lines on the tower are complex and interference of electromagnetic fields exists, has great requirements on the operation of the unmanned aerial vehicle, therefore, the flight path of the unmanned aerial vehicle needs to be evaluated, so that the working personnel can better select the proper unmanned aerial vehicle to carry out the task, the authorization notice number CN207379500U discloses an unmanned aerial vehicle flight path detection device, compared with the prior art that the radar arranged on the unmanned aerial vehicle is positioned by the GPS, the unmanned aerial vehicle track detection device obtains images by shooting through the camera, the shooting of the camera does not influence the flight of the unmanned aerial vehicle, and simultaneously, the camera is fixed on the support frame arranged on the ground, so that the influence of external factors (such as wind power and the flight speed of the unmanned aerial vehicle) is small, and the accuracy of the space position measurement of the unmanned aerial vehicle is further improved; on the other hand, the camera is calibrated through the calibration rod, so that the unmanned aerial vehicle can be quantitatively measured, the aerial three-dimensional coordinate position of the unmanned aerial vehicle is restored, the unmanned aerial vehicle flight path precision is determined by analyzing the camera, the unmanned aerial vehicle flight path precision is improved, and the unmanned aerial vehicle flight capability or the operation level of a flying hand can be accurately evaluated. But this unmanned aerial vehicle flight path detection device is with camera snap-on the support frame, when needs overhaul, and is inconvenient to the dismantlement of whole camera, and the installation is also inconvenient moreover.
SUMMERY OF THE UTILITY MODEL
For the dismantlement degree of difficulty and the installation degree of difficulty of reducing means, the utility model provides an unmanned aerial vehicle flight path detection device.
The utility model discloses a following technical scheme realizes: an unmanned aerial vehicle track detection device, comprising:
the device comprises a base and a detector for detecting a flight path;
the supporting column is arranged at the top of the base;
the rotator is arranged at the top of the supporting column and used for controlling the rotation of the detector in the horizontal direction;
the supporting plate is arranged at the top of the rotator; and
the angle adjuster is arranged at the top of the supporting plate and is used for adjusting the pitch angle of the detector;
the two connecting plates are connected to the corresponding two ends of the angle adjuster in a transmission manner, the tops of the two connecting plates are connected with the detector, and the angle adjuster adjusts the pitch angle of the detector through the two connecting plates; the top parts of the two connecting plates are respectively provided with a first mounting hole, the side surfaces of the two connecting plates are respectively provided with a second mounting hole, and each first mounting hole is communicated with the corresponding second mounting hole so as to form a T-shaped channel;
the two fixing plates are respectively arranged at the openings of the two second mounting holes;
the two movable rods are movably sleeved on the side surfaces of the two fixed plates respectively, and each movable rod extends into the corresponding second mounting hole and is intersected with the corresponding first mounting hole;
each movable plate is movably sleeved in the corresponding second mounting hole and fixedly sleeved on the outer side of the corresponding movable rod;
each telescopic spring is movably sleeved outside the corresponding movable rod, one end of each telescopic spring is fixedly connected with the corresponding movable plate, and the other end of each telescopic spring is fixedly connected with the corresponding fixed plate;
two dead levers, it all sets up in the bottom of detector, and when fixed, two dead levers insert respectively in the corresponding first mounting hole, the one end that every dead lever inserted first mounting hole inserts the wedge for agreeing with each other with the one end that its movable rod that corresponds inserted the second mounting hole, and every dead lever is provided with the jack with the relative one side of movable rod that corresponds, the diameter of movable rod equals with the aperture of jack, when the dead lever inserts completely in the corresponding first mounting hole, the movable rod inserts in the jack that corresponds.
As a further improvement of the above scheme, two guide grooves with limiting blocks at two ends are symmetrically arranged in the second mounting hole, and two guide blocks matched with the two guide grooves are arranged on the side surface of the movable plate.
As a further improvement of the above scheme, the angle adjuster is a double-shaft motor, and the two connecting plates are correspondingly arranged on two transmission shafts of the double-shaft motor.
Furthermore, two rotary rods are fixedly connected to two output shafts of the double-shaft motor respectively, one ends, far away from the double-shaft motor, of the two rotary rods are provided with cross grooves, cross pins matched with the corresponding cross grooves are arranged on the side face of each connecting plate, each cross pin is inserted into the corresponding cross groove, and a nut is screwed at one end, exposed outside the corresponding cross groove, of each rotary rod.
As a further improvement of the scheme, a solar cell panel is arranged on the outer side of the detector, and a storage battery is arranged on the solar cell panel.
Further, the solar cell panel is obliquely arranged on the outer side of the detector upwards.
As a further improvement of the scheme, the supporting column is an electric telescopic column or a pneumatic telescopic column.
As a further improvement of the scheme, the supporting column is fixedly arranged on the base through a hexagon bolt.
Advantageous effects
The utility model discloses an unmanned aerial vehicle track detection device, in the dead lever disect insertion first mounting hole during the installation, because dead lever and the terminal coincidence effect of movable rod, outwards push the movable rod when inserting, simultaneously expanding spring saves elasticity, thereby make can insert completely in the first mounting hole by the dead lever, because expanding spring's elastic action, make inside the very smooth jack that inserts of movable rod, install detector and angle regulator like this, it is both convenient and swift, thereby installation effectiveness has been improved. When needing to dismantle, only need outwards pull the movable rod for the movable rod breaks away from the jack, thereby take the dead lever out can, the operation is simpler, has also further improved dismantlement efficiency and maintenance efficiency.
Drawings
Fig. 1 is a schematic perspective view of the flight path detection device of the unmanned aerial vehicle according to the present invention;
FIG. 2 is a schematic diagram of the internal structure of the detector shown in FIG. 1;
FIG. 3 is a schematic view of the angle adjuster mounting structure of FIG. 1;
FIG. 4 is a schematic diagram of the structure of the connection plate shown in FIG. 3;
FIG. 5 is a schematic structural view of the movable rod of FIG. 1 engaged with the fixed rod;
fig. 6 is a schematic structural view of the movable rod of fig. 5 inserted into the jack.
In the figure: the device comprises a base 1, a detector 2, a support column 3, a rotator 4, a support plate 5, an angle adjuster 6, a connecting plate 7, a first mounting hole 8, a second mounting hole 9, a fixing plate 10, a movable rod 11, a movable plate 12, a telescopic spring 13, a fixed rod 14, a jack 15, a guide groove 16, a guide block 17, a rotary rod 18, a cross groove 19, a cross pin 20, a nut 21, a solar cell panel 22 and a storage battery 23.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.
Referring to fig. 1, the utility model discloses an unmanned aerial vehicle flight path detection device, it includes base 1, installs support column 3, circulator 4, angle regulator 6 at base 1 top, detects detector 2, two connecting plates 7, two fixed plates 10, two movable rods 11, two fly leaves 12, two expanding spring 13 and two dead levers 14 of flight path.
Support column 3 passes through hex bolts fixed mounting on base 1, and base 1 sets up subaerially, and it specifically can be the cement mound, and circulator 4 sets up the rotation that fixed mounting is used for controlling detector 2 in the top of support column 3, and the top of circulator 4 is equipped with backup pad 5, rotates and indirectly drives detector 2 and rotates through driving backup pad 5, and angle regulator 6 that is used for adjusting the detector angle of elevation is installed at the top of backup pad 5. The preferred angle regulator 6 is a double-shaft motor, the two connecting plates 7 are respectively connected with two transmission shafts of the double-shaft motor in a transmission mode, the tops of the two connecting plates 7 are connected with the bottom of the detector 2, and the double-shaft motor drives the two connecting plates 7 to rotate so as to regulate the pitch angle of the detector 2.
The specific installation mode of detector 2 and two connecting plates 7 is as shown in fig. 5, fig. 6, first mounting hole 8 has all been seted up at the top of two connecting plates 7, the side of two connecting plates 7 all is provided with second mounting hole 9, thereby every first mounting hole 8 and corresponding second mounting hole 9 intercommunication form a T type passageway, the opening part of two second mounting holes 9 all is provided with fixed plate 10, the equal movable sleeve in side of two fixed plates 10 is equipped with movable rod 11, every movable rod 11 extends to in the corresponding second mounting hole 9, and intersect with corresponding first mounting hole 8, make movable rod 11 can be in second mounting hole 9 round trip movement like this. Each movable plate 12 is movably sleeved in the corresponding second mounting hole 9 and fixedly sleeved outside the corresponding movable rod 11, so that when the movable rod 11 moves, the movable plates 12 move along with the movable rod 11. Each expansion spring 13 is movably sleeved outside the corresponding movable rod 11, one end of each expansion spring is fixedly connected with the corresponding movable plate 12, and the other end of each expansion spring is fixedly connected with the corresponding fixed plate 10. Two dead levers 14 all set up in the bottom of detector 2, and when fixed, two dead levers 14 insert respectively corresponding first mounting hole 8 in, every dead lever 14 inserts the one end of first mounting hole 8 and inserts the one end of second mounting hole 9 rather than the movable rod 11 that corresponds for agreeing with the wedge each other, when dead lever 14 inserts like this, make movable rod 11 outwards remove through the principle that the wedge agrees with. At the same time, the extension spring 13 accumulates elastic force. Each fixed rod 14 is provided with an insertion hole 15 at a side opposite to the corresponding movable rod 11, the diameter of the movable rod 11 is equal to the aperture of the insertion hole 15, and when the fixed rod 14 is completely inserted into the corresponding first mounting hole 8, the movable rod 11 is rebounded and inserted into the corresponding insertion hole 15 due to the elastic force of the expansion spring 13. In order to avoid the deflection of the movable rod 11 during the movement, two guide grooves 16 with limited blocks at two ends are symmetrically arranged in the second mounting hole 9, and two guide blocks 17 matched with the two guide grooves 16 are arranged on the side surface of the movable plate 12, so that the movable rod 11 can only do straight linear motion through the guide action of the guide grooves 16 and the guide blocks 17, the deflection cannot occur, the torsion of the telescopic spring 14 is further avoided, and the service life of the telescopic spring 14 is prolonged.
For the position of better regulation detector 3, set up support column 3 into flexible post, it can stretch out and draw back through electronic, also can stretch out and draw back through pneumatics, specifically can be electronic flexible post or pneumatic flexible post. Please refer to fig. 2, in order to prevent the power failure during the detection process, the embodiment is further configured with a solar cell panel 9, the solar cell panel 9 selects a jjjrhw cell panel, which is disposed outside the detector 2, and is disposed outside the detector 2 in an upward inclined manner, so as to better receive the irradiation of sunlight, absorb more solar energy, obtain more electric energy, a storage battery 10 is disposed inside the detector 2, the storage battery 10 can store the electric energy converted by the solar cell panel 9 for standby, the storage battery 10 can supply power to the detector 3, the rotator 4 and the angle adjuster 6, and if the support column 3 is an electric telescopic rod, the support column 3 can also be supplied with power. Referring to fig. 3 and 4, two rotating rods 18 are fixedly connected to two output shafts of the dual-axis motor respectively, one ends, far away from the dual-axis motor, of the rotating rods 18 are provided with cross grooves 19, threads are arranged on the outer sides of the rotating rods 18, cross pins 20 matched with the cross grooves 19 are arranged on the side faces of the connecting plate 7, the connecting plate 7 can be inserted into the cross grooves 19 through the cross pins 20 during fixing, and then the fixing is achieved through nuts 21, so that the connecting plate is convenient and fast to overhaul, and the connecting plate 7 can be better fixed.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.
Claims (8)
1. An unmanned aerial vehicle track detection device, comprising:
a base (1) and a detector (2) for detecting a flight path;
the supporting column (3) is arranged at the top of the base (1);
the rotator (4) is arranged at the top of the supporting column (3) and used for controlling the rotation of the detector (2) in the horizontal direction;
a support plate (5) arranged on the top of the rotator (4); and
the angle adjuster (6) is arranged at the top of the supporting plate (5) and is used for adjusting the pitch angle of the detector (2);
its characterized in that, unmanned aerial vehicle track detection device still includes:
the two connecting plates (7) are connected to the two corresponding ends of the angle adjuster (6) in a transmission mode, the tops of the two connecting plates (7) are connected with the detector (2), and the angle adjuster (6) adjusts the pitch angle of the detector (2) through the two connecting plates (7); the top parts of the two connecting plates (7) are respectively provided with a first mounting hole (8), the side surfaces of the two connecting plates (7) are respectively provided with a second mounting hole (9), and each first mounting hole (8) is communicated with the corresponding second mounting hole (9) to form a T-shaped channel;
two fixing plates (10) which are respectively arranged at the openings of the two second mounting holes (9);
the two movable rods (11) are movably sleeved on the side surfaces of the two fixed plates (10) respectively, and each movable rod (11) extends into the corresponding second mounting hole (9) and is intersected with the corresponding first mounting hole (8);
each movable plate (12) is movably sleeved in the corresponding second mounting hole (9) and fixedly sleeved on the outer side of the corresponding movable rod (11);
each telescopic spring (13) is movably sleeved on the outer side of the corresponding movable rod (11), one end of each telescopic spring (13) is fixedly connected with the corresponding movable plate (12), and the other end of each telescopic spring is fixedly connected with the corresponding fixed plate (10);
two dead levers (14), it all sets up in the bottom of detector (2), and during fixed, insert corresponding first mounting hole (8) respectively in two dead levers (14), the one end that every dead lever (14) inserted first mounting hole (8) inserts the one end of second mounting hole (9) rather than corresponding movable rod (11) for agreeing with the wedge each other, and every dead lever (14) is provided with jack (15) with the one side that corresponds movable rod (11) is relative, the diameter of movable rod (11) equals with the aperture of jack (15), when dead lever (14) insert corresponding first mounting hole (8) completely in, movable rod (11) insert in corresponding jack (15).
2. The unmanned aerial vehicle track detection device of claim 1, characterized in that: two guide grooves (16) with limiting blocks at two ends are symmetrically arranged in the second mounting hole (9), and two guide blocks (17) matched with the two guide grooves (16) are arranged on the side surface of the movable plate (12).
3. The unmanned aerial vehicle track detection device of claim 1, characterized in that: the angle regulator (6) is a double-shaft motor, and the two connecting plates (7) are correspondingly arranged on two transmission shafts of the double-shaft motor.
4. An unmanned aerial vehicle track detection device as defined in claim 3, wherein: two output shafts of the double-shaft motor are respectively and fixedly connected with two rotating rods (18), the two rotating rods (18) are far away from one end of the double-shaft motor is provided with a cross groove (19), the side face of each connecting plate (7) is provided with a cross pin (20) matched with the corresponding cross groove (19), each cross pin (20) is inserted into the corresponding cross groove (19), and one end of each rotating rod (18) exposed outside the corresponding cross groove (19) is connected with a nut (21) in a threaded mode.
5. The unmanned aerial vehicle track detection device of claim 1, characterized in that: the detector is characterized in that a solar cell panel (22) is arranged on the outer side of the detector (2), and a storage battery (23) is arranged on the solar cell panel (22).
6. An unmanned aerial vehicle track detection device as defined in claim 5, wherein: the solar cell panel (22) is arranged on the outer side of the detector (2) in an upward inclined mode.
7. The unmanned aerial vehicle track detection device of claim 1, characterized in that: the support column (3) is an electric telescopic column or a pneumatic telescopic column.
8. The unmanned aerial vehicle track detection device of claim 1, characterized in that: the support column (3) is fixedly arranged on the base (1) through a hexagon bolt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020091313.3U CN211042213U (en) | 2020-01-16 | 2020-01-16 | Unmanned aerial vehicle track detection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020091313.3U CN211042213U (en) | 2020-01-16 | 2020-01-16 | Unmanned aerial vehicle track detection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211042213U true CN211042213U (en) | 2020-07-17 |
Family
ID=71567522
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020091313.3U Expired - Fee Related CN211042213U (en) | 2020-01-16 | 2020-01-16 | Unmanned aerial vehicle track detection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211042213U (en) |
-
2020
- 2020-01-16 CN CN202020091313.3U patent/CN211042213U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200717 Termination date: 20210116 |