CN220263078U - Unmanned aerial vehicle testboard - Google Patents
Unmanned aerial vehicle testboard Download PDFInfo
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- CN220263078U CN220263078U CN202321968945.3U CN202321968945U CN220263078U CN 220263078 U CN220263078 U CN 220263078U CN 202321968945 U CN202321968945 U CN 202321968945U CN 220263078 U CN220263078 U CN 220263078U
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Abstract
The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle test board, which comprises a fixed table, a sliding table and an unmanned aerial vehicle mounting frame, wherein the top of the sliding table is positioned above the fixed table, the sliding table is vertically and slidably connected with the fixed table, the unmanned aerial vehicle mounting frame is arranged at the top of the sliding table, the unmanned aerial vehicle mounting frame can be freely offset and rotated relative to the sliding table, the unmanned aerial vehicle is fixed on the unmanned aerial vehicle mounting frame during unmanned aerial vehicle test, the sliding table adapts to the ascending and descending test of the unmanned aerial vehicle through vertical sliding with the fixed table, the unmanned aerial vehicle mounting frame adapts to the inclination test of the unmanned aerial vehicle through free offset with the sliding table, and the unmanned aerial vehicle mounting frame adapts to the steering test of the unmanned aerial vehicle through rotation with the sliding table.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle test bench.
Background
Along with development of scientific technology, unmanned aerial vehicles show unusual capability in various fields, unmanned aerial vehicles with various sizes and functions are designed like bamboo shoots after raining, power devices of the unmanned aerial vehicles, namely engines and propellers, have different models and matching modes, and as the power devices directly influence the flight performance of the unmanned aerial vehicles, the power matching is crucial, the power matching modes are various, the pursuing speed and the general power of a special model airplane are large, the unmanned aerial vehicles with navigation measurement have long endurance time, small power consumption, stable performance and the like, and the testing method of the power devices is various, and generally, one or more power matching modes are selected for actual flight comparison after calculation.
Because the unmanned aerial vehicle is subjected to test flight for the first time and test flight after maintenance, various problems such as sideslip and overturning accidents, unnecessary losses are often caused due to structural, installation, compass interference, GPS navigation module interference, flight control parameter configuration deviation and the like, and particularly, the unmanned aerial vehicle is more likely to be lost due to the conditions of the explosion machine when subjected to project tests such as maximum take-off weight test, wind resistance test and rain resistance test, so that the unmanned aerial vehicle is required to be fixed on a test bench to complete related tests, and then the flight test is required to be carried out after unnecessary errors and faults are eliminated.
For guarantee unmanned aerial vehicle test effect, carry out the complete machine capability test to unmanned aerial vehicle generally, mainly carry out lifting test to it, back-and-forth movement test and side-tipping test etc. but current unmanned aerial vehicle testboard is either simple structure, and test function is single, can't test unmanned aerial vehicle complete machine capability effectively, or is the structure complicacy, application scope is little, inconvenient simple and easy to test unmanned aerial vehicle like patent number: CN211844950 discloses an unmanned aerial vehicle comprehensive test platform, by base, outer loop, inner ring constitute, but this testboard structure is complicated, and manufacturing cost is higher, and unmanned aerial vehicle need put test platform inner ring inside, only is applicable to small-size many rotor unmanned aerial vehicle and tests, and many rotor unmanned aerial vehicle of jumbo size need make very big just can satisfy the installation demand with the testboard.
Disclosure of Invention
The utility model aims at: the utility model provides an unmanned aerial vehicle test board for conveniently performing relevant tests on an unmanned aerial vehicle, which aims at performing the performance test on the unmanned aerial vehicle, has the advantages of simple structure, single test function, incapability of effectively testing the performance of the unmanned aerial vehicle, or complex structure, high manufacturing cost and small application range.
In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:
the utility model provides an unmanned aerial vehicle testboard, includes fixed station, sliding table and unmanned aerial vehicle mounting bracket, the sliding table top is located the fixed station top, the sliding table with fixed station sliding connection, the unmanned aerial vehicle mounting bracket sets up the sliding table top, the unmanned aerial vehicle mounting bracket can be relative sliding table free offset and rotation.
The utility model discloses an unmanned aerial vehicle test bench, which comprises a fixed bench, a sliding table and an unmanned aerial vehicle mounting frame, wherein the sliding table top is positioned above the fixed bench and is in vertical sliding connection with the fixed bench, the unmanned aerial vehicle mounting frame is arranged at the sliding table top, the unmanned aerial vehicle mounting frame can be free to deviate relative to the sliding table, when the unmanned aerial vehicle is tested, the unmanned aerial vehicle is fixed on the unmanned aerial vehicle mounting frame, when the unmanned aerial vehicle needs to be subjected to ascending and descending test, the sliding table is in vertical sliding connection with the fixed table to adapt to ascending and descending of the unmanned aerial vehicle, when the unmanned aerial vehicle needs to be subjected to inclination test, the unmanned aerial vehicle mounting frame can be free to adapt to inclination test of the unmanned aerial vehicle through the free deviation with the sliding table, when the unmanned aerial vehicle needs to be subjected to steering test, the unmanned aerial vehicle mounting frame can be rotated relative to adapt to steering test of the unmanned aerial vehicle through rotation with the sliding table, the unmanned aerial vehicle mounting frame can realize cooperative ascending and descending of the unmanned aerial vehicle, the sliding table can be more suitable for the unmanned aerial vehicle, the unmanned aerial vehicle can be adjusted to have the same size as the unmanned aerial vehicle, and the unmanned aerial vehicle is in the unmanned aerial vehicle is easy to realize, and the unmanned aerial vehicle test bench can be more suitable for the unmanned aerial vehicle test bench has a large-sized, and the unmanned aerial vehicle test bench can be suitable for the unmanned aerial vehicle test bench can be well, and has a large size.
As the preferable scheme of the utility model, the unmanned aerial vehicle mounting frame can freely deviate and rotate relative to the sliding table through the ball joint bearing, and the top of the sliding table and the unmanned aerial vehicle mounting frame are respectively connected through the ball joint bearing.
The unmanned aerial vehicle mounting frame comprises a sliding table, a telescopic supporting component and a telescopic supporting component. When unmanned aerial vehicle is installed on the unmanned aerial vehicle installing frame, the unmanned aerial vehicle installing frame is leveled through the telescopic supporting component, so that the unmanned aerial vehicle is in a horizontal state, and the unmanned aerial vehicle related performance test is facilitated.
As a preferable mode of the utility model, the telescopic supporting member comprises a telescopic strut which is circumferentially arranged at the top of the sliding table around the ball joint bearing.
As a preferable mode of the utility model, the telescopic supporting component comprises an annular air bag, the annular air bag is arranged at the top of the sliding table, and the ball joint bearing is positioned at the center of the annular air bag.
As a preferable scheme of the utility model, the fixed table comprises a fixed table top plate, a fixed table bottom plate and a first sliding rod, wherein two ends of the first sliding rod are respectively connected to the fixed table top plate and the fixed table bottom plate, and the fixed table bottom plate is used for fixing the fixed table. The fixed station bottom plate is used for fixing the fixed station to increase the stability of fixed station, avoid the fixed station to be pulled away ground or turn on one's side, so as to test the unmanned aerial vehicle of different take-off quality, further, increase weight to the fixed station according to unmanned aerial vehicle take-off quality, make the fixed station more firm.
As a preferable scheme of the utility model, the sliding table comprises a sliding table top plate, a sliding table bottom plate and a second sliding rod, wherein two ends of the second sliding rod are respectively connected to the sliding table top plate and the sliding table bottom plate, the sliding table bottom plate is used for placing a balancing weight, and the weight of the sliding table is adjusted by placing the balancing weight on the sliding table bottom plate so as to adjust the balancing weight according to different take-off weights of the unmanned aerial vehicle, thereby testing the power requirements of the unmanned aerial vehicle under different attached weights.
According to the utility model, the sliding table top plate is arranged above the fixed table, the sliding table bottom plate is arranged between the fixed table top plate and the fixed table bottom plate, the sliding table bottom plate is vertically and slidably connected with the first sliding rod, the second sliding rod is vertically and slidably connected with the fixed table top plate, the sliding table bottom plate is arranged between the fixed table top plate and the fixed table bottom plate by arranging the sliding table top plate above the fixed table, so that the sliding table is prevented from being separated from the fixed table, the fixed table plays a limiting role on the sliding table, and further, when the unmanned aerial vehicle freely ascends and descends, the fixed table is prevented from being separated from the unmanned aerial vehicle when the unmanned aerial vehicle freely ascends and descends, so that the unmanned aerial vehicle is prevented from being damaged due to collision after the unmanned aerial vehicle falls off the fixed table, the sliding table bottom plate is vertically and slidably connected with the fixed table top plate by the first sliding rod of the sliding table bottom plate, and the sliding table top plate is vertically and slidably connected with the fixed table top plate, and the unmanned aerial vehicle is adapted to free ascent and descent.
As a preferable scheme of the utility model, the second sliding rod is vertically and slidably connected with the fixed table top plate through a second linear bearing, and the sliding table bottom plate is vertically and slidably connected with the first sliding rod through a first linear bearing.
As a preferable mode of the present utility model, a pressure sensor is provided between the fixed table and the slide table. The tension of the unmanned aerial vehicle in the test process is monitored through the pressure sensor.
In summary, due to the adoption of the technical scheme, the beneficial effects of the utility model are as follows:
1. the utility model discloses an unmanned aerial vehicle test bench, which comprises a fixed bench, a sliding table and an unmanned aerial vehicle mounting frame, wherein the sliding table top is positioned above the fixed bench and is in vertical sliding connection with the fixed bench, the unmanned aerial vehicle mounting frame is arranged at the sliding table top, the unmanned aerial vehicle mounting frame can be free to deviate relative to the sliding table, when the unmanned aerial vehicle is tested, the unmanned aerial vehicle is fixed on the unmanned aerial vehicle mounting frame, when the unmanned aerial vehicle needs to be subjected to ascending and descending test, the sliding table is in vertical sliding connection with the fixed table to adapt to ascending and descending of the unmanned aerial vehicle, when the unmanned aerial vehicle needs to be subjected to inclination test, the unmanned aerial vehicle mounting frame can be free to adapt to inclination test of the unmanned aerial vehicle through the free deviation with the sliding table, when the unmanned aerial vehicle needs to be subjected to steering test, the unmanned aerial vehicle mounting frame can be rotated relative to adapt to steering test of the unmanned aerial vehicle through rotation with the sliding table, the unmanned aerial vehicle mounting frame can realize cooperative ascending and descending of the unmanned aerial vehicle, the sliding table can be more suitable for the unmanned aerial vehicle, the unmanned aerial vehicle can be adjusted to have the same size as the unmanned aerial vehicle, and the unmanned aerial vehicle is in the unmanned aerial vehicle is easy to realize, and the unmanned aerial vehicle test bench can be more suitable for the unmanned aerial vehicle test bench has a large-sized, and the unmanned aerial vehicle test bench can be suitable for the unmanned aerial vehicle test bench can be well, and has a large size.
Drawings
Fig. 1 is a schematic structural view of the present utility model.
Fig. 2 is a perspective view of the present utility model.
Fig. 3 is a second perspective view of the present utility model.
Fig. 4 is a schematic diagram of the cooperation of the unmanned aerial vehicle and the present utility model.
Fig. 5 is a schematic diagram of a drone mated with the present utility model (drone offset).
Fig. 6 is a schematic diagram of the cooperation of the drone with the present utility model (drone ascending).
Fig. 7 is a top view of fig. 4.
Fig. 8 is a top view two (unmanned steering) of fig. 4.
Fig. 9 is a schematic view of a preferred construction of the present utility model.
Fig. 10 is a perspective view of a preferred construction of the present utility model.
Fig. 11 is a perspective view of a preferred construction of the present utility model.
The marks in the figure: the device comprises a 1-fixed table, a 11-fixed table top plate, a 12-fixed table bottom plate, a 13-first sliding rod, a 14-supporting rod, a 2-sliding table, a 21-sliding table top plate, a 22-sliding table bottom plate, a 23-second sliding rod, a 4-ball joint bearing, a 5-telescopic strut, a 6-unmanned aerial vehicle mounting frame, a 7-annular air bag, an 8-first linear bearing, a 9-second linear bearing, a 10-unmanned aerial vehicle and a 101-connecting frame.
Detailed Description
The present utility model will be described in detail with reference to the accompanying drawings.
The present utility model will be described in further detail with reference to the drawings and examples, in order to make the objects, technical solutions and advantages of the present utility model more apparent. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the utility model.
Example 1
As shown in fig. 1-8, the unmanned aerial vehicle test board according to the embodiment comprises a fixed table 1, a sliding table 2 and an unmanned aerial vehicle mounting frame 6, wherein the top of the sliding table 2 is located above the fixed table 1, the sliding table 2 is vertically and slidably connected with the fixed table 1, the unmanned aerial vehicle mounting frame 6 is arranged at the top of the sliding table 2, and the unmanned aerial vehicle mounting frame 6 can freely deviate and rotate relative to the sliding table 2.
This embodiment an unmanned aerial vehicle testboard, including fixed station 1, sliding table 2 and unmanned aerial vehicle mounting bracket 6, sliding table 2 top is located fixed station 1 top and sliding table 2 and the vertical sliding connection of fixed station 1, unmanned aerial vehicle mounting bracket 6 sets up at sliding table 2 top, unmanned aerial vehicle mounting bracket 6 can freely deviate from sliding table 2, when carrying out the unmanned aerial vehicle test, fix unmanned aerial vehicle 10 on unmanned aerial vehicle mounting bracket 6, when unmanned aerial vehicle 10 needs to go up and down the test, because sliding table 2 and the vertical sliding connection of fixed station 1, sliding table 2 is through the vertical slip with fixed station 1 adapt to unmanned aerial vehicle 10's the decline that rises, when unmanned aerial vehicle 10 needs to carry out the inclination test, because unmanned aerial vehicle mounting bracket 6 can the free deviation with sliding table 2, when unmanned aerial vehicle 10 needs to turn to the test, because unmanned aerial vehicle mounting bracket 6 can the relative sliding table 2 rotation, unmanned aerial vehicle mounting bracket 6 is through the rotation with sliding table 2 and is adapted to unmanned aerial vehicle 10, this utility model can be through the fixed station 1, can not be adjusted to the size through the fixed station 2, the unmanned aerial vehicle 1 can be adjusted to the size is more easily and the unmanned aerial vehicle 10, the unmanned aerial vehicle is suitable for the size is realized, the unmanned aerial vehicle is not suitable for the unmanned aerial vehicle mounting bracket 1, the unmanned aerial vehicle is suitable for the size is 6 and the unmanned aerial vehicle is suitable for the size is 1, the unmanned aerial vehicle is suitable for the size.
In a preferred manner, as shown in fig. 1, the unmanned aerial vehicle further comprises a ball joint bearing 4, one end of the ball joint bearing 4 is connected to the top of the sliding table 2, the other end of the ball joint bearing 4 is connected with an unmanned aerial vehicle mounting frame 6, the unmanned aerial vehicle mounting frame 6 can be freely offset and rotated relative to the sliding table 2 through the ball joint bearing 4, the top of the sliding table 2 and the unmanned aerial vehicle mounting frame 6 are respectively connected through the ball joint bearing 4, and the unmanned aerial vehicle mounting frame 6 can be freely offset and rotated relative to the sliding table 2 due to the function of angle adjustment of the ball joint bearing 4, as shown in fig. 4-5, the unmanned aerial vehicle mounting frame 6 can be freely offset relative to the sliding table 2 through the ball joint bearing 4, the unmanned aerial vehicle mounting frame 6 can be adapted to the inclination of the unmanned aerial vehicle 10 through the free offset relative to the sliding table 2, as shown in fig. 4 and 7-8, the unmanned aerial vehicle mounting frame 6 can be freely offset relative to the sliding table 2 through the ball joint bearing 4, and the unmanned aerial vehicle mounting frame 6 can be adapted to the steering test of the unmanned aerial vehicle 10 through the rotation of the sliding table 2, wherein the ball joint bearing 4 can be rotatably manufactured by a water-selecting city, and the bearing model of the spherical joint manufactured by a company limited company is TBS 10.
1-3, still include flexible supporting part, flexible supporting part sets up at slide table 2 top, and flexible supporting part is used for supporting unmanned aerial vehicle mounting bracket 6, when installing unmanned aerial vehicle 10 on unmanned aerial vehicle mounting bracket 6, comes to leveling unmanned aerial vehicle mounting bracket 6 through flexible supporting part to make unmanned aerial vehicle 10 be in the horizontality, be convenient for to unmanned aerial vehicle 10 correlation capability test.
In a preferred manner, as shown in fig. 2-3, the telescopic supporting component comprises a telescopic supporting rod 5, the telescopic supporting rod 5 is circumferentially arranged at the top of the sliding table 2 around the ball joint bearing 4, the unmanned aerial vehicle mounting frame 6 is mounted on the ball joint bearing 4, the screw rod of the ball joint bearing 4 and the length of the telescopic supporting rod 5 enable the unmanned aerial vehicle mounting frame 6 to be horizontal, further, the telescopic supporting rod 5 can be controlled electrically or pneumatically, when the unmanned aerial vehicle 10 is unlocked and the rotor rotates stably and thickly, all the telescopic supporting rods 5 can be controlled by the control device to be separated from the unmanned aerial vehicle mounting frame 6 so as to test whether the unmanned aerial vehicle 10 has a tilting trend, as shown in fig. 4-5, the unmanned aerial vehicle mounting frame 6 can be moved within a certain angle range by controlling the distance between the telescopic supporting rod 5 and the unmanned aerial vehicle mounting frame 6, so that the unmanned aerial vehicle 10 can tilt within the certain angle range, and the certain angle range is 0- ±35°, wherein the number of the telescopic supporting rods 5 is not less than 3, so as to better support the unmanned aerial vehicle mounting frame 6.
In a preferred manner, as shown in fig. 1, the fixed table 1 comprises a fixed table top plate 11, a fixed table bottom plate 12 and a first sliding rod 13, wherein two ends of the first sliding rod 13 are respectively connected to the fixed table top plate 11 and the fixed table bottom plate 12, the fixed table bottom plate 12 is used for fixing the fixed table 1, so that stability of the fixed table 1 is improved, the fixed table 1 is prevented from being pulled away from the ground or turned over during testing of the unmanned aerial vehicle 10, the unmanned aerial vehicle 10 with different take-off qualities is tested, and further, weight is increased for the fixed table 1 according to the take-off quality adaptation of the unmanned aerial vehicle 10, so that the fixed table 1 is more stable.
In a preferred manner, as shown in fig. 1, the sliding table 2 comprises a sliding table top plate 21, a sliding table bottom plate 22 and a second sliding rod 23, two ends of the second sliding rod 23 are respectively connected to the sliding table top plate 21 and the sliding table bottom plate 22, the sliding table bottom plate 22 is used for placing a balancing weight, the balancing weight can be bound on the sliding table bottom plate 22 by adopting a binding belt, and the weight of the sliding table 2 is adjusted by placing the balancing weight on the sliding table bottom plate 22, so that the balancing weight is adjusted according to different take-off weights of the unmanned aerial vehicle 10, and thus the power requirements of the unmanned aerial vehicle under different attached weights are tested.
In a preferred manner, as shown in fig. 1 and 6, the sliding table top plate 21 is located above the fixed table 1, the sliding table bottom plate 22 is arranged between the fixed table top plate 11 and the fixed table bottom plate 12, the sliding table bottom plate 22 is vertically and slidably connected with the first sliding rod 13, the second sliding rod 23 is vertically and slidably connected with the fixed table top plate 11, by arranging the sliding table top plate 21 above the fixed table 1, the sliding table bottom plate 22 is arranged between the fixed table top plate 11 and the fixed table bottom plate 12, thereby ensuring that the sliding table 2 is not separated from the fixed table 1, limiting the sliding table 2 by the fixed table 1, further, when the unmanned aerial vehicle 10 freely ascends and descends, the unmanned aerial vehicle 10 is not separated from the fixed table 1 due to the limiting effect of the fixed table 1, so as to avoid damage caused by collision after the unmanned aerial vehicle 10 falls off the fixed table 1, by vertically sliding the slide table bottom plate 22 with the first slide bars 13 of the fixed table 1 and vertically sliding the second slide bars 14 of the slide table 2 with the fixed table top plate 11, the sliding connection of the slide table 2 with the fixed table 1 is realized to accommodate the free rising and falling of the unmanned aerial vehicle 10, as shown in fig. 6, further, the number of the first slide bars 13 provided with the fixed table 1 is not less than two, the number of the second slide bars 23 provided with the slide table 2 is not less than 2, further, the second slide bars 23 are vertically sliding connected with the fixed table top plate 11 through the second linear bearings 9, the slide table bottom plate 22 is vertically sliding connected with the first slide bars 13 through the first linear bearings 8, wherein the vertical direction refers to the direction in which the height between the slide table 2 and the fixed table 1 changes, in this embodiment, the fixed table bottom plate 12 of the fixed table 1 is installed on the ground, the distance between the sliding table 2 and the fixed table 1 changes in the height between the sliding table 2 and the fixed table 1, and further, the first linear bearing 8 and the second linear bearing 9 can be selected from linear bearings with model number of LMH10UU manufactured by Ninte precision transmission parts Co.
In a preferred manner, a pressure sensor is arranged between the stationary table 1 and the sliding table 2, by means of which the tension of the unmanned aerial vehicle 10 during the test is monitored.
A preferred mode still is provided with link 101 between unmanned aerial vehicle 10 and unmanned aerial vehicle mounting bracket 6, and link 101 bottom surface is connected with unmanned aerial vehicle mounting bracket 6, and the connected mode is bolted connection or welding, and link 101 top surface is fixed mutually with unmanned aerial vehicle 10, and the fixed mode includes buckle fixedly, ligature fixedly, bolted connection etc..
Example 2
As shown in fig. 9-11, the difference between the unmanned aerial vehicle test stand according to the present embodiment and embodiment 1 is that the telescopic support member includes an annular air bag 7, the annular air bag 7 is disposed at the top of the sliding stand 2, the ball joint bearing 4 is disposed at the center of the annular air bag 7, as shown in fig. 7-8, the annular air bag 7 is inflated through the length of the screw rod of the ball joint bearing 4 until the annular air bag 7 fully abuts against the sliding stand top plate of the sliding stand 2, so as to enable the unmanned aerial vehicle mounting frame 6 to be horizontal, as shown in fig. 9, the annular air bag 7 can adjust inflation pressure, when the unmanned aerial vehicle 10 is unlocked and the rotor rotates smoothly and thick, the supporting force of the annular air bag 7 on the unmanned aerial vehicle mounting frame 6 can be reduced by controlling all the annular air bag 7 pressures, so as to test whether the unmanned aerial vehicle 10 has tilting tendency, and the unmanned aerial vehicle mounting frame 6 can be moved within a certain angle range by controlling the air pressure in the annular air bag 7, so that the unmanned aerial vehicle 10 can tilt within a certain angle range of 0-35 DEG
The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, and alternatives falling within the spirit and principles of the utility model.
Claims (10)
1. The utility model provides an unmanned aerial vehicle testboard, its characterized in that, including fixed station (1), sliding table (2) and unmanned aerial vehicle mounting bracket (6), sliding table (2) top is located fixed station (1) top, sliding table (2) with vertical sliding connection of fixed station (1), unmanned aerial vehicle mounting bracket (6) set up sliding table (2) top, unmanned aerial vehicle mounting bracket (6) can be relative sliding table (2) free offset and rotation.
2. The unmanned aerial vehicle test stand according to claim 1, wherein the unmanned aerial vehicle mounting frame (6) can freely deviate and rotate relative to the sliding stand (2) through the ball joint bearing (4).
3. The unmanned aerial vehicle test stand according to claim 2, further comprising a telescopic support member provided on top of the slide stand (2), the telescopic support member being for supporting the unmanned aerial vehicle mounting frame (6).
4. A test bench for unmanned aerial vehicle according to claim 3, wherein the telescopic support member comprises a telescopic strut (5), the telescopic strut (5) being circumferentially arranged around the ball joint bearing (4) at the top of the slide table (2).
5. A test bench for unmanned aerial vehicle according to claim 3, wherein the telescopic support member comprises an annular air bag (7), the annular air bag (7) is arranged at the top of the sliding table (2), and the ball joint bearing (4) is arranged at the center of the annular air bag (7).
6. An unmanned aerial vehicle test stand according to any of claims 1 to 5, wherein the fixed stand (1) comprises a fixed stand top plate (11), a fixed stand bottom plate (12) and a first sliding rod (13), two ends of the first sliding rod (13) are respectively connected to the fixed stand top plate (11) and the fixed stand bottom plate (12), and the fixed stand bottom plate (12) is used for fixing the fixed stand (1).
7. The unmanned aerial vehicle test stand according to claim 6, wherein the slide stand (2) comprises a slide stand top plate (21), a slide stand bottom plate (22) and a second slide rod (23), both ends of the second slide rod (23) are respectively connected to the slide stand top plate (21) and the slide stand bottom plate (22), and the slide stand bottom plate (22) is used for placing a balancing weight.
8. An unmanned aerial vehicle test stand according to claim 7, wherein the slide table top plate (21) is located above the fixed table (1), the slide table bottom plate (22) is arranged between the fixed table top plate (11) and the fixed table bottom plate (12), the slide table bottom plate (22) is vertically slidably connected with the first slide rod (13), and the second slide rod (23) is vertically slidably connected with the fixed table top plate (11).
9. The unmanned aerial vehicle test stand according to claim 8, wherein the second slide bar (23) is vertically slidably connected to the fixed stand top plate (11) via a second linear bearing (9), and the slide stand bottom plate (22) is vertically slidably connected to the first slide bar (13) via a first linear bearing (8).
10. The unmanned aerial vehicle test bench according to claim 9, wherein a pressure sensor is arranged between the stationary bench (1) and the sliding bench (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321968945.3U CN220263078U (en) | 2023-07-25 | 2023-07-25 | Unmanned aerial vehicle testboard |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321968945.3U CN220263078U (en) | 2023-07-25 | 2023-07-25 | Unmanned aerial vehicle testboard |
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| Publication Number | Publication Date |
|---|---|
| CN220263078U true CN220263078U (en) | 2023-12-29 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202321968945.3U Active CN220263078U (en) | 2023-07-25 | 2023-07-25 | Unmanned aerial vehicle testboard |
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| CN (1) | CN220263078U (en) |
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2023
- 2023-07-25 CN CN202321968945.3U patent/CN220263078U/en active Active
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