CN111361757B - Cantilever driving system horizontal installation device for unmanned aerial vehicle - Google Patents
Cantilever driving system horizontal installation device for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN111361757B CN111361757B CN202010220122.7A CN202010220122A CN111361757B CN 111361757 B CN111361757 B CN 111361757B CN 202010220122 A CN202010220122 A CN 202010220122A CN 111361757 B CN111361757 B CN 111361757B
- Authority
- CN
- China
- Prior art keywords
- adjusting
- vertical
- rod
- unmanned aerial
- aerial vehicle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
Abstract
The invention discloses a horizontal mounting device of a cantilever power system for an unmanned aerial vehicle, which comprises a mounting platform, a first conical gear, a circular level bubble and a second conical gear, wherein an adjusting frame is arranged above the mounting platform, an adjusting rod is arranged on the adjusting frame, the first conical gear is arranged at the left end of the adjusting rod, a push plate is arranged on the outer side of the adjusting rod, a transverse plate is connected above the push plate and positioned above the adjusting frame, a solution is arranged on the inner side of a level ferrule, a limiting bolt is arranged at the lower end of a mounting cover and positioned below the level ferrule. This cantilever driving system horizontal installation device for unmanned aerial vehicle, mounting platform can carry out the level through circular air level and aim at for keep the horizontality of mounting platform self, conveniently after that stabilize the centre gripping with the unmanned aerial vehicle cantilever on the diaphragm through the centre gripping bolt, conveniently adapt to the size model of different unmanned aerial vehicle cantilevers, make things convenient for the unmanned aerial vehicle cantilever to carry out the level simultaneously and place.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a horizontal mounting device for a cantilever power system for an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is a small-size flying machine, is used for mainly taking photo by plane or supplementary agricultural chemicals sprays, and current unmanned aerial vehicle spare part is mostly carried out manual combination by the workman and is assembled, especially cantilever type unmanned aerial vehicle, and its power motor system that flies cantilever and cantilever end all need carry out manual assembly, but current unmanned aerial vehicle can have following problem at the in-process that cantilever motor power system installed usually:
1. the manual installation efficiency is low, meanwhile, the assembly accuracy is not high, and the horizontal state of the power motor in installation cannot be guaranteed, so that the unmanned aerial vehicle is easy to be unstable in the flying process, the unmanned aerial vehicle cannot stably hover or change the flying direction in the flying process, and the normal flying operation is influenced;
2. can not carry out manual level calibration when installing power motor, therefore can't judge the horizontality that power motor installed, install power motor manually simultaneously, even accomplish the level when the installation and look for accurately, nevertheless handheld unstability can appear in manual installation, finally leads to accomplishing the power motor that the level was looked for accurately still can appear the situation of horizontal migration.
Disclosure of Invention
The invention aims to provide a horizontal installation device of a cantilever power system for an unmanned aerial vehicle, which aims to solve the problems that the manual installation efficiency is low, the assembly accuracy is not high, the horizontal state of the power motor in installation cannot be guaranteed, thereby easily causing the unstable situation of the unmanned aerial vehicle in the flying process, leading the unmanned aerial vehicle not to stably hover or change the flying direction in the flying process, influencing the normal flying operation, manual level calibration cannot be performed when the power motor is installed, and thus the level state in which the power motor is installed cannot be determined, while the power motor is manually installed, even if the horizontal alignment is completed during the installation, the manual installation causes unstable hand holding, and finally causes the problem that the power motor completing the horizontal alignment still has a horizontal deviation condition.
In order to achieve the purpose, the invention provides the following technical scheme: a cantilever power system horizontal installation device for an unmanned aerial vehicle comprises an installation platform, a first bevel gear, a circular level bubble and a second bevel gear, wherein an adjusting frame is arranged above the installation platform, an adjusting rod is arranged on the adjusting frame, the first bevel gear is arranged at the left end of the adjusting rod, a push plate is arranged on the outer side of the adjusting rod, a transverse plate is connected above the push plate and is located above the adjusting frame, a vertical plate is arranged on the upper surface of the transverse plate, a clamping bolt is arranged on the vertical plate, a connecting block is arranged on the lower surface of the transverse plate and is located on the inner side of an adjusting groove, the adjusting groove is arranged on the upper surface of the adjusting frame, the transverse plate is connected with the adjusting frame through the connecting block and the adjusting groove, the circular level bubble is arranged on the inner side of the adjusting frame and is embedded on the upper surface of the installation platform, a vertical rod is arranged on the left side of the adjusting frame, and the vertical rod is also arranged on the upper surface of the mounting platform, a vertical groove is arranged on the vertical rod, a vertical shaft is arranged on the inner side of the vertical groove and is connected with the vertical rod, a second bevel gear is arranged at the lower end of the vertical shaft and is positioned inside the lower end of the vertical rod, the vertical shaft is connected with the adjusting rod through the second bevel gear and the first bevel gear, a cross rod is arranged on the outer side of the vertical shaft and is also positioned inside the vertical groove, the right end of the cross rod is connected with a mounting block, a groove is arranged on the lower surface of the mounting block, an adjusting block is arranged on the inner side of the groove and is connected with the mounting block through the groove, a mandril is arranged above the adjusting block and is connected with the mounting block, a mounting cover is arranged below the adjusting block, a leveling ferrule is arranged on the outer side of the mounting cover, and a solution is arranged on the inner side of the leveling ferrule, and the surface of the level ferrule is provided with a level line, the lower end of the mounting cover is provided with a limiting bolt, and the limiting bolt is positioned below the level ferrule.
Preferably, a rotating structure is formed between the adjusting rod and the adjusting frame, a thread is arranged at the middle section of the adjusting rod, and the adjusting rod is in threaded connection with the push plate.
Preferably, the push plate is fixedly connected with the transverse plate, vertical plates are symmetrically distributed on the transverse plate, and clamping bolts penetrate through the vertical plates.
Preferably, the lower surface of the transverse plate is fixedly provided with a connecting block, the regular section of the connecting block is an inverted T-shaped structure, and the transverse plate passes through the connecting block and the adjusting groove to form a sliding structure with the adjusting frame.
Preferably, a rotating structure is formed between the vertical shaft and the vertical rod, and the vertical shaft is meshed and connected with the adjusting rod through a second bevel gear and a first bevel gear.
Preferably, the cross rod forms a sliding structure with the vertical rod through the vertical groove, and the cross rod is in threaded connection with the vertical shaft.
Preferably, the adjusting block is of a spherical structure, the adjusting block is nested inside the groove, and the adjusting block and the mounting block form a rotating structure through the groove.
Preferably, the level collar is made of hollow transparent glass, the level collar is nested outside the mounting cover, and the liquid level of the solution in the level collar is kept flush with the level line.
Compared with the prior art, the invention has the beneficial effects that: the cantilever power system horizontal installation device for the unmanned aerial vehicle,
1. the mounting platform can be horizontally aligned through the round air level so as to keep the self horizontal state of the mounting platform, and then the unmanned aerial vehicle cantilever can be conveniently and stably clamped on the transverse plate through the clamping bolt, so that the mounting platform is convenient to adapt to different sizes and models of the unmanned aerial vehicle cantilever, and meanwhile, the unmanned aerial vehicle cantilever can be conveniently horizontally placed;
2. the push plate can be pushed to move by rotating the adjusting rod, and the push plate drives the transverse plate to slide and displace on the adjusting frame through the connecting block and the adjusting groove, so that the tail end of the cantilever of the unmanned aerial vehicle can conveniently move to the position right below the mounting cover to be aligned with a power motor in the mounting cover, and the subsequent mounting of the power motor is facilitated;
3. the power motor is installed in the inboard of installation cover, unscrews the ejector pin, and under the action of gravity, the installation cover can carry out the self-adaptation rotation in the below of installation piece through the regulating block, and the solution liquid level and the water flat line in the level lasso keep the parallel and level, and the installation cover at this moment is the horizontality, and the power motor in the installation cover is the horizontality equally, makes things convenient for the follow-up horizontal installation that carries on of power motor.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of a connecting structure of an adjusting block and a mounting block according to the present invention;
FIG. 3 is a schematic side sectional view of the adjusting bracket of the present invention;
FIG. 4 is a schematic top view of the mounting bracket of the present invention;
FIG. 5 is a schematic top view of the cross plate of the present invention;
fig. 6 is a schematic sectional structure view of the mounting cover of the present invention.
In the figure: 1. mounting a platform; 2. an adjusting bracket; 3. adjusting a rod; 4. a first bevel gear; 5. pushing the plate; 6. a transverse plate; 7. a vertical plate; 8. clamping the bolt; 9. connecting blocks; 10. an adjustment groove; 11. a circular level bubble; 12. a vertical rod; 13. a vertical slot; 14. a vertical axis; 15. a second bevel gear; 16. a cross bar; 17. mounting blocks; 18. a groove; 19. an adjusting block; 20. a top rod; 21. mounting a cover; 22. a leveling collar; 23. a solution; 24. a leveling line; 25. and a limiting bolt.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-6, the present invention provides a technical solution: a horizontal installation device of a cantilever power system for an unmanned aerial vehicle comprises an installation platform 1, a first bevel gear 4, a circular level bubble 11 and a second bevel gear 15, wherein an adjusting frame 2 is arranged above the installation platform 1, an adjusting rod 3 is arranged on the adjusting frame 2, the first bevel gear 4 is arranged at the left end of the adjusting rod 3, a push plate 5 is arranged outside the adjusting rod 3, a transverse plate 6 is connected above the push plate 5, the transverse plate 6 is positioned above the adjusting frame 2, a vertical plate 7 is arranged on the upper surface of the transverse plate 6, a clamping bolt 8 is arranged on the vertical plate 7, a connecting block 9 is arranged on the lower surface of the transverse plate 6, the connecting block 9 is positioned on the inner side of an adjusting groove 10, the adjusting groove 10 is arranged on the upper surface of the adjusting frame 2, the transverse plate 6 is mutually connected with the adjusting frame 2 through the connecting block 9 and the adjusting groove 10, the circular level bubble 11 is arranged on the inner side of the adjusting frame 2, and the circular level bubble 11 is embedded on the upper surface of the installation platform 1, a vertical rod 12 is arranged at the left side of the adjusting frame 2, the vertical rod 12 is also arranged on the upper surface of the mounting platform 1, a vertical groove 13 is arranged on the vertical rod 12, a vertical shaft 14 is arranged at the inner side of the vertical groove 13, the vertical shaft 14 is connected with the vertical rod 12, a second bevel gear 15 is arranged at the lower end of the vertical shaft 14, the second bevel gear 15 is positioned inside the lower end of the vertical rod 12, the vertical shaft 14 is connected with the adjusting rod 3 through the second bevel gear 15 and the first bevel gear 4, a cross rod 16 is arranged at the outer side of the vertical shaft 14, the cross rod 16 is also positioned inside the vertical groove 13, a mounting block 17 is connected at the right end of the cross rod 16, a groove 18 is arranged at the lower surface of the mounting block 17, an adjusting block 19 is arranged at the inner side of the groove 18, the adjusting block 19 is connected with the mounting block 17 through the groove 18, a mandril 20 is arranged above the adjusting block 19, and the mandril 20 is connected with the mounting block 17, an installation cover 21 is arranged below the adjusting block 19, a level ferrule 22 is arranged on the outer side of the installation cover 21, a solution 23 is arranged on the inner side of the level ferrule 22, a level line 24 is arranged on the surface of the level ferrule 22, a limiting bolt 25 is arranged at the lower end of the installation cover 21, and the limiting bolt 25 is positioned below the level ferrule 22.
In the embodiment, a rotating structure is formed between the adjusting rod 3 and the adjusting frame 2, a thread is arranged at the middle section of the adjusting rod 3, and the adjusting rod 3 is in threaded connection with the push plate 5, so that when the adjusting rod 3 rotates on the adjusting frame 2, the adjusting rod 3 can push the push plate 5 to move synchronously through the thread;
the push plate 5 is fixedly connected with the transverse plate 6, the transverse plate 6 is symmetrically provided with vertical plates 7, the vertical plates 7 are provided with clamping bolts 8 in a penetrating mode, the push plate 5 can drive the transverse plate 6 to move synchronously while the push plate 5 moves, and the vertical plates 7 and the clamping bolts 8 which are symmetrically arranged on the transverse plate 6 can stably clamp the unmanned aerial vehicle cantilever;
the lower surface of the transverse plate 6 is fixedly provided with the connecting block 9, the front section of the connecting block 9 is of an inverted T-shaped structure, and the transverse plate 6 forms a sliding structure with the adjusting frame 2 through the connecting block 9 and the adjusting groove 10, so that the transverse plate 6 can conveniently slide on the adjusting frame 2 through the connecting block 9 and the adjusting groove 10, and meanwhile, the transverse plate 6 is always connected with the adjusting frame 2 through the connecting block 9 and the adjusting groove 10;
a rotating structure is formed between the vertical shaft 14 and the vertical rod 12, and the vertical shaft 14 is meshed with the adjusting rod 3 through the second bevel gear 15 and the first bevel gear 4, so that the adjusting rod 3 can drive the vertical shaft 14 to synchronously rotate through the first bevel gear 4 and the second bevel gear 15 while the adjusting rod 3 rotates;
the cross rod 16 forms a sliding structure with the vertical rod 12 through the vertical groove 13, the cross rod 16 is in threaded connection with the vertical shaft 14, and when the vertical shaft 14 rotates, the vertical shaft 14 can push the cross rod 16 to synchronously slide on the inner side of the vertical groove 13 through threads;
the adjusting block 19 is of a spherical structure, the adjusting block 19 is nested on the inner side of the groove 18, the adjusting block 19 and the mounting block 17 form a rotating structure through the groove 18, the adjusting block 19 can conveniently perform self-adaptive rotation adjustment below the mounting block 17 through the groove 18 under the action of gravity, and the subsequent mounting cover 21 can conveniently perform angle adjustment;
the leveling collar 22 is made of hollow transparent glass, the leveling collar 22 is nested on the outer side of the mounting cover 21, the liquid level of the solution 23 in the leveling collar 22 is kept flush with the leveling line 24, and when the liquid level of the solution 23 in the leveling collar 22 is kept flush with the leveling line 24, the mounting cover 21 is in a horizontal state at the moment, so that the horizontal state of the mounting cover 21 can be judged conveniently according to the position condition between the liquid level of the solution 23 and the leveling line 24, and subsequent adjustment is facilitated.
The working principle is as follows: as shown in fig. 1 and 3, the mounting platform 1 is first horizontally placed by means of the circular vials 11 on the upper surface, after the mounting platform 1 is horizontally placed, the unmanned aerial vehicle cantilever is placed above the transverse plate 6, according to the illustration in fig. 5, the clamping bolts 8 on the vertical plate 7 are then manually screwed, and the clamping bolts 8 stably clamp the unmanned aerial vehicle cantilever above the transverse plate 6, so that the unmanned aerial vehicle cantilever horizontally clamps above the transverse plate 6, according to fig. 1 and 6, the unmanned aerial vehicle power motor is placed inside the mounting cover 21, then the limit bolt 25 on the mounting cover 21 is manually tightened until the limit bolt 25 clamps the power motor stably against the inside of the mounting cover 21, according to fig. 1 and 6, the ejector rod 20 above the mounting block 17 is unscrewed manually, and the mounting cover 21 naturally hangs down below the mounting block 17 under the action of gravity through the spherical adjusting block 19 and the groove 18;
according to the illustration in fig. 6, while the mounting cover 21 naturally hangs down below the mounting block 17 through the spherical adjusting block 19 and the groove 18, the liquid level position of the solution 23 in the leveling collar 22 outside the mounting cover 21 is observed, when the liquid level of the solution 23 is aligned with the level line 24 on the surface of the leveling collar 22, the mounting cover 21 is in a horizontal state, when the liquid level of the solution 23 is not aligned with the level line 24 on the surface of the leveling collar 22, the mounting cover 21 is manually pushed to rotate below the mounting block 17 through the adjusting block 19 and the groove 18 until the liquid level of the solution 23 is aligned with the level line 24 on the surface of the leveling collar 22, and after the liquid level of the solution 23 is aligned with the level line 24, the push rod 20 above the mounting block 17 is manually tightened according to the illustration in fig. 2, so that the push rod 20 at this time tightly pushes and fixes the adjusting block 19 in the groove 18, the position and angle of the mounting cover 21 are fixed and maintained in a horizontal state;
according to fig. 1, 3 and 4, after the position angle of the mounting cover 21 is horizontally fixed, the adjusting rod 3 is manually screwed to perform a rotating motion, the rotating adjusting rod 3 pushes the push plate 5 to perform a synchronous motion through a screw thread, while the push plate 5 moves, the push plate 5 at this time drives the horizontal plate 6 to perform a sliding displacement above the adjusting frame 2 through the connecting block 9 and the adjusting groove 10, the horizontal plate 6 drives the unmanned aerial vehicle cantilever to perform a synchronous sliding displacement leftward through the clamping bolt 8, while the horizontal plate 6 moves, the rotating adjusting rod 3 at this time pushes the vertical shaft 14 to rotate on the vertical rod 12 through the first bevel gear 4 and the second bevel gear 15, so that the rotating vertical shaft 14 pushes the cross rod 16 to perform a sliding motion on the inner side of the vertical groove 13 through a screw thread, and the cross rod 16 drives the mounting block 17 to perform a sliding motion downward in the vertical groove 13, the mounting block 17 drives the power motor to synchronously move downwards through the mounting cover 21 until the mounting cover 21 drives the power motor to be inserted into a reserved mounting position at the tail end of the cantilever of the unmanned aerial vehicle, wherein when the mounting cover 21 and the transverse plate 6 synchronously slide to be contacted with each other, the mounting position of the mounting cover 21 and the reserved mounting position at the tail end of the cantilever of the unmanned aerial vehicle can be matched, and meanwhile, the mounting position of the cantilever of the unmanned aerial vehicle can be adjusted on the transverse plate 6, so that the clamping position of the cantilever of the unmanned aerial vehicle can be adjusted only by loosening and tightening the clamping bolt 8, after the clamping position of the cantilever of the unmanned aerial vehicle on the transverse plate 6 when the power motor is just inserted into the tail end of the cantilever of the unmanned aerial vehicle is adjusted for the first time, the power motor can be ensured to be just inserted into the reserved mounting position at the tail end of the cantilever of the unmanned aerial vehicle only by clamping other cantilevers to the corresponding positions at each subsequent time, therefore power motor this moment then has accomplished the level at unmanned aerial vehicle cantilever end and has placed, and the convenience of installation has been promoted in the convenient follow-up horizontal installation calibration that carries on, and such a cantilever driving system horizontal installation device for unmanned aerial vehicle conveniently uses.
It is to be understood that the terms "central," "longitudinal," "lateral," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the figures to facilitate a simplified description of the present invention, and do not indicate or imply that the devices or elements being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus are not to be considered as limiting the scope of the present invention.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a cantilever driving system horizontal installation device for unmanned aerial vehicle, includes mounting platform (1), first bevel gear (4), circular air level (11) and second bevel gear (15), its characterized in that: the mounting platform is characterized in that an adjusting frame (2) is arranged above the mounting platform (1), an adjusting rod (3) is installed on the adjusting frame (2), a first bevel gear (4) is installed at the left end of the adjusting rod (3), a push plate (5) is arranged on the outer side of the adjusting rod (3), a transverse plate (6) is connected above the push plate (5), the transverse plate (6) is located above the adjusting frame (2), a vertical plate (7) is installed on the upper surface of the transverse plate (6), a clamping bolt (8) is installed on the vertical plate (7), a connecting block (9) is installed on the lower surface of the transverse plate (6), the connecting block (9) is located on the inner side of an adjusting groove (10), the adjusting groove (10) is arranged on the upper surface of the adjusting frame (2), the transverse plate (6) is connected with the adjusting frame (2) through the connecting block (9) and the adjusting groove (10), and a circular level bubble (11) is arranged on the inner side of the adjusting frame (2), the round level bubble (11) is embedded on the upper surface of the mounting platform (1), a vertical rod (12) is arranged on the left side of the adjusting frame (2), the vertical rod (12) is also mounted on the upper surface of the mounting platform (1), a vertical groove (13) is formed in the vertical rod (12), a vertical shaft (14) is arranged on the inner side of the vertical groove (13), the vertical shaft (14) is connected with the vertical rod (12), a second bevel gear (15) is mounted at the lower end of the vertical shaft (14), the second bevel gear (15) is located inside the lower end of the vertical rod (12), the vertical shaft (14) is connected with the adjusting rod (3) through the second bevel gear (15) and the first bevel gear (4), a cross rod (16) is arranged on the outer side of the vertical shaft (14), the cross rod (16) is also located on the inner side of the vertical groove (13), and a mounting block (17) is connected with the right end of the cross rod (16), a groove (18) is arranged on the lower surface of the mounting block (17), an adjusting block (19) is arranged on the inner side of the groove (18), the adjusting block (19) is of a spherical structure, the adjusting block (19) is nested on the inner side of the groove (18), the adjusting block (19) and the mounting block (17) form a rotating structure through a groove (18), a top rod (20) is arranged above the adjusting block (19), and the mandril (20) is connected with the mounting block (17), a mounting cover (21) is arranged below the adjusting block (19), a leveling ferrule (22) is arranged on the outer side of the mounting cover (21), a solution (23) is arranged on the inner side of the leveling ferrule (22), and the surface of the level ferrule (22) is provided with a level line (24), the lower end of the mounting cover (21) is provided with a limiting bolt (25), and the limiting bolt (25) is positioned below the level ferrule (22).
2. The horizontal installation device of the cantilever power system for the unmanned aerial vehicle as claimed in claim 1, wherein: a rotating structure is formed between the adjusting rod (3) and the adjusting frame (2), threads are arranged at the middle section of the adjusting rod (3), and the adjusting rod (3) is in threaded connection with the push plate (5).
3. The horizontal installation device of the cantilever power system for the unmanned aerial vehicle as claimed in claim 1, wherein: the push plate (5) is fixedly connected with the transverse plate (6), the transverse plate (6) is symmetrically provided with vertical plates (7), and the vertical plates (7) are provided with clamping bolts (8) in a penetrating mode.
4. The horizontal installation device of the cantilever power system for the unmanned aerial vehicle as claimed in claim 1, wherein: the lower surface fixed mounting of diaphragm (6) has connecting block (9), and the positive section of connecting block (9) is "T" style of calligraphy structure of inversion to diaphragm (6) pass through between connecting block (9) and adjusting groove (10) and adjusting bracket (2) and constitute sliding construction.
5. The horizontal installation device of the cantilever power system for the unmanned aerial vehicle as claimed in claim 1, wherein: a rotating structure is formed between the vertical shaft (14) and the vertical rod (12), and the vertical shaft (14) is meshed and connected with the adjusting rod (3) through a second bevel gear (15) and a first bevel gear (4).
6. The horizontal installation device of the cantilever power system for the unmanned aerial vehicle as claimed in claim 1, wherein: the cross rod (16) forms a sliding structure with the vertical rod (12) through the vertical groove (13), and the cross rod (16) is in threaded connection with the vertical shaft (14).
7. The horizontal installation device of the cantilever power system for the unmanned aerial vehicle as claimed in claim 1, wherein: the leveling collar (22) is made of hollow transparent glass, the leveling collar (22) is nested outside the mounting cover (21), and the liquid level of the solution (23) in the leveling collar (22) is kept flush with the leveling line (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010220122.7A CN111361757B (en) | 2020-03-25 | 2020-03-25 | Cantilever driving system horizontal installation device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010220122.7A CN111361757B (en) | 2020-03-25 | 2020-03-25 | Cantilever driving system horizontal installation device for unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111361757A CN111361757A (en) | 2020-07-03 |
| CN111361757B true CN111361757B (en) | 2021-10-26 |
Family
ID=71202632
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010220122.7A Active CN111361757B (en) | 2020-03-25 | 2020-03-25 | Cantilever driving system horizontal installation device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111361757B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206869471U (en) * | 2017-04-07 | 2018-01-12 | 东莞市鸿威模具有限公司 | It is a kind of can accurate limiting from Horizontal clamp |
| CA2977143A1 (en) * | 2016-11-09 | 2018-05-09 | The Boeing Company | Apparatus, system, and method for performing automated finishing operations on a workpiece |
| CN109056572A (en) * | 2018-09-10 | 2018-12-21 | 孙江花 | A kind of traffic wide-angle lens device of rotation water removal |
| CN109732515A (en) * | 2019-01-25 | 2019-05-10 | 吴清槐 | A kind of unmanned plane dynamical system is horizontally mounted debugging apparatus |
| CN109926920A (en) * | 2017-12-17 | 2019-06-25 | 福建和暄实业有限公司 | A kind of stroke sander |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3292709B2 (en) * | 1999-07-01 | 2002-06-17 | エスエムシー株式会社 | Air chuck with measuring function |
| CN209618790U (en) * | 2019-01-15 | 2019-11-12 | 中国建筑第二工程局有限公司 | A kind of lifting device for building |
| CN209793546U (en) * | 2019-04-24 | 2019-12-17 | 江西省环球陶瓷有限公司 | Potsherd is waxed and is used adjustable fixture |
| CN209985627U (en) * | 2019-05-16 | 2020-01-24 | 福建省统仕金属制品有限公司 | Automatic paint spraying device for baking paint bucket |
| CN110817736A (en) * | 2019-12-06 | 2020-02-21 | 数恒（苏州）新材料科技有限公司 | Stacker elevating system |
-
2020
- 2020-03-25 CN CN202010220122.7A patent/CN111361757B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2977143A1 (en) * | 2016-11-09 | 2018-05-09 | The Boeing Company | Apparatus, system, and method for performing automated finishing operations on a workpiece |
| CN206869471U (en) * | 2017-04-07 | 2018-01-12 | 东莞市鸿威模具有限公司 | It is a kind of can accurate limiting from Horizontal clamp |
| CN109926920A (en) * | 2017-12-17 | 2019-06-25 | 福建和暄实业有限公司 | A kind of stroke sander |
| CN109056572A (en) * | 2018-09-10 | 2018-12-21 | 孙江花 | A kind of traffic wide-angle lens device of rotation water removal |
| CN109732515A (en) * | 2019-01-25 | 2019-05-10 | 吴清槐 | A kind of unmanned plane dynamical system is horizontally mounted debugging apparatus |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111361757A (en) | 2020-07-03 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205716278U (en) | Adjustable pan and tilt head framework | |
| CN209223261U (en) | A kind of C-shaped beam cutter device for air suspension of automobile | |
| CN210676395U (en) | Multi-steel-pipe machining clamp for steel pipe production line | |
| CN111361757B (en) | Cantilever driving system horizontal installation device for unmanned aerial vehicle | |
| CN212080769U (en) | Convenient and reliable camera installation adjusting device | |
| CN210241046U (en) | Robot vision system is with arbitrary rotatory camera | |
| CN212195900U (en) | Unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning | |
| CN218042063U (en) | Self-adaptive gravity adjusting device | |
| CN211893675U (en) | Special laser range finder mounting bracket of unmanned aerial vehicle | |
| CN204383542U (en) | Steering column adjustment structure | |
| CN109085011B (en) | Portable sampler for sampling micro-damage of in-service equipment | |
| CN109237258B (en) | Traffic monitoring equipment mounting bracket with improved structure | |
| CN107941244B (en) | Cross coupling debugging device and method for triaxial inertial system | |
| CN211420948U (en) | But height-adjusting's limit for height pole for town road fast | |
| CN220843014U (en) | Unmanned aerial vehicle inspection auxiliary device | |
| CN207974433U (en) | A kind of frame adjustment component for being mounted on frame | |
| CN212500192U (en) | Manual calibration device of camera before car | |
| CN109578400A (en) | Multistation liquid switch bonding adjustment device | |
| CN212353498U (en) | Cart traction fixator and AGV trolley connecting device with same | |
| CN216690406U (en) | Concrete distributing device for building construction | |
| CN218520575U (en) | Displacement and level adjustable device for clamp | |
| CN211842035U (en) | Mechanical clamping equipment for machining | |
| CN213750324U (en) | Traffic monitoring radar device | |
| CN213057556U (en) | Unmanned aerial vehicle camera mounting bracket is used in training | |
| CN112038769A (en) | Adjustable support component and adjustable installation part for equipment installation |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211207 Address after: 430000 South Taizi Lake innovation Valley Qidi Xiexin science and Technology Innovation Park, Wuhan Economic and Technological Development Zone, Hubei Province (qdxx-f2306) Patentee after: Wuhan Xinze Technology Co.,Ltd. Patentee after: Wuhan Xingchuang Ditai Technology Co., Ltd Address before: No.1 Xijing Road, Chang'an District, Xi'an City, Shaanxi Province 710100 Patentee before: XIJING University |
|
| TR01 | Transfer of patent right |