CN111114812A - Unmanned aerial vehicle convenient to direction with balance mechanism - Google Patents
Unmanned aerial vehicle convenient to direction with balance mechanism Download PDFInfo
- Publication number
- CN111114812A CN111114812A CN201811277008.7A CN201811277008A CN111114812A CN 111114812 A CN111114812 A CN 111114812A CN 201811277008 A CN201811277008 A CN 201811277008A CN 111114812 A CN111114812 A CN 111114812A
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- Prior art keywords
- main body
- aerial vehicle
- unmanned aerial
- movably arranged
- movably
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- 230000007246 mechanism Effects 0.000 title claims abstract description 17
- 230000000087 stabilizing effect Effects 0.000 claims description 8
- 238000003466 welding Methods 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000008439 repair process Effects 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 241000883990 Flabellum Species 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
- B64C25/64—Spring shock-absorbers; Springs using rubber or like elements
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- 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
- B64F5/40—Maintaining or repairing aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses an unmanned aerial vehicle with a balance mechanism and convenient to guide, which comprises a main body, a bolt and a clamping groove, wherein a guide plate is movably arranged at the top of the main body, an electronic gyroscope is movably arranged on the inner side of the outer wall of the main body, a fixed frame is arranged inside the main body, a camera is movably arranged inside the fixed frame, the bolt is movably arranged on the outer wall of the fixed frame, a nut is movably arranged on the outer wall of the bolt, a support frame is movably arranged at the bottom of the main body and connected with the main body through a screw, an elastic column is connected to the bottom of the support frame, a rubber block is arranged at the bottom of the elastic column, and the clamping groove is movably arranged in the middle of. This unmanned aerial vehicle convenient to direction with balance mechanism is provided with the main part, is swing joint between main part and the guide plate, makes when the guide plate damages if appearing, and user's accessible screw is dismantled the guide plate fast and is restoreed, improves maintenance efficiency.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle devices, in particular to an unmanned aerial vehicle with a balance mechanism and convenient to guide.
Background
The unmanned plane is an unmanned plane for short, is an unmanned plane operated by radio remote control equipment and a self-contained program control device, has no cockpit on the plane, and is provided with an autopilot, a program control device and other equipment. Personnel on the ground, a naval vessel or a mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar and the like, can take off like a common airplane under the radio remote control or launch and lift off by using a boosting rocket, can also be carried to the air by the mother aircraft to launch and fly, and can automatically land in the same way as the landing process of the common airplane during the recovery.
Unmanned aerial vehicle on the market does not possess buffer function in the use for the device falls behind, and the effort conducts to the device body easily, causes the device inner part to damage, to the unable free angle regulation of inner part, reduces the flexibility of device, does not have balancing unit, makes the device produce great rocking easily when using, makes the security reduce when the device moves, and for this reason, we provide an unmanned aerial vehicle who is convenient for to lead who has balance mechanism.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle with a balance mechanism and convenient to guide, and aims to solve the problems that the unmanned aerial vehicle provided in the background art does not have a buffer function in the use process, so that the acting force is easily transmitted to a device body after the device falls down, parts in the device are damaged, the angle of the internal parts cannot be freely adjusted, the flexibility of the device is reduced, the device is easy to generate large shake in use due to the absence of the balance mechanism, and the safety of the device in operation is reduced.
In order to achieve the purpose, the invention provides the following technical scheme: an unmanned aerial vehicle with a balance mechanism and convenient to guide comprises a main body, a bolt and a clamping groove, wherein a guide plate is movably arranged at the top of the main body, an electronic gyroscope is movably arranged on the inner side of the outer wall of the main body, a fixed frame is arranged inside the main body, a camera is movably arranged inside the fixed frame, the bolt is movably arranged on the outer wall of the fixed frame, a nut is movably arranged on the outer wall of the bolt, a supporting frame is movably arranged at the bottom of the main body and is connected with the main body through a screw, an elastic column is connected to the bottom of the supporting frame, a rubber block is arranged at the bottom of the elastic column, the clamping groove is movably arranged in the middle of the bottom end of the main body and is connected with the main body through a screw, connecting plates are movably arranged on two sides of the inner wall of the clamping groove, the inside activity of main part is provided with the steady rest, and the inside arrangement of steady rest has the fan, the inside of fan is provided with the pivot, and the outer wall activity arrangement of pivot has the axle sleeve, the outer wall connection of axle sleeve has the flabellum.
Preferably, the main body is movably connected with the guide plate, and the guide plate is vertically arranged at the top of the main body.
Preferably, the connection mode between the fixed frame and the main body is welding, and the fixed frame and the camera constitute a movable structure through bolts and nuts.
Preferably, the center line of the support frame is parallel to the center line of the main body, and the support frame and the rubber block form an elastic structure through the elastic column.
Preferably, the connecting plate is movably connected with the clamping groove, and the connecting plate and the clamping plate form an elastic telescopic structure through a spring.
Preferably, the fan is fixedly connected with the rotating shaft, and the rotating shaft and the fan blades form a rotating structure through a shaft sleeve.
Compared with the prior art, the invention has the beneficial effects that: the unmanned aerial vehicle with the balance mechanism and convenient to guide is provided with a main body, the main body is movably connected with the guide plate, when the guide plate is damaged, a user can rapidly detach the guide plate through screws for repair, the maintenance efficiency is improved, meanwhile, the guide plate is vertically arranged at the top of the main body, so that the guide plate cannot shake when the unmanned aerial vehicle runs, the stability of the unmanned aerial vehicle is improved, the device is convenient for the user to control for guiding, the connection mode between the fixing frame and the main body is welding, when the unmanned aerial vehicle runs, the fixing frame cannot fall off from the device, the service life of parts is prolonged, meanwhile, the fixing frame forms a movable structure through bolts, nuts and cameras, so that the angle of the cameras can be freely adjusted by the user;
the central line of the support frame is parallel to the central line of the main body, so that the support frame can always keep an absolutely vertical state, the stability of the support frame during bearing is improved, meanwhile, the support frame and the rubber block form an elastic structure through the elastic column, when the device descends, the elastic column and the rubber block can buffer acting force generated during descending, damage to internal parts of the device is avoided, the connecting plate and the clamping groove are movably connected, when a user uses the device, if equipment needs to be carried for use, the clamping groove can be mounted through a screw, the carrying capacity of the device is improved, meanwhile, the connecting plate and the clamping plate form an elastic telescopic structure through a spring, the carried equipment cannot fall off from the device through clamping of the spring, and the carrying stability is improved;
the fan is fixedly connected with the rotating shaft, so that the connection strength between the fan and the rotating shaft is increased, the synchronous harmony between parts is ensured, meanwhile, the rotating shaft passes through the shaft sleeve and the fan blades to form a rotating structure, the wind power generated after the fan blades rotate can lift the device, and the possibility that the device cannot fall off when in use is ensured.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic top view of the present invention;
FIG. 3 is an enlarged schematic view of the structure at A of the present invention.
In the figure: 1. a main body; 2. a baffle; 3. an electronic gyroscope; 4. a fixing frame; 5. a camera; 6. a bolt; 7. a nut; 8. a support frame; 9. an elastic column; 10. a rubber block; 11. a clamping groove; 12. a connecting plate; 13. a spring; 14. a splint; 15. a stabilizer frame; 16. a fan; 17. a rotating shaft; 18. a shaft sleeve; 19. a fan blade.
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. 1-3, the present invention provides a technical solution: an unmanned aerial vehicle convenient to guide and provided with a balance mechanism comprises a main body 1, bolts 6 and clamping grooves 11, wherein a guide plate 2 is movably arranged at the top of the main body 1, an electronic gyroscope 3 is movably arranged on the inner side of the outer wall of the main body 1, the main body 1 is movably connected with the guide plate 2, the guide plate 2 is vertically arranged at the top of the main body 1, when the guide plate 2 is damaged, a user can rapidly detach the guide plate 2 for repair through screws, the maintenance efficiency is improved, a fixing frame 4 is arranged inside the main body 1, a camera 5 is movably arranged inside the fixing frame 4, the fixing frame 4 is welded with the main body 1 in a connecting mode, the fixing frame 4 forms a movable structure through the bolts 6 and the nuts 7 and the camera 5, the fixing frame 4 cannot fall off from a device when the device runs, and the service life of parts is prolonged;
the bolt 6 is movably arranged on the outer wall of the fixed frame 4, the nut 7 is movably arranged on the outer wall of the bolt 6, the support frame 8 is movably arranged at the bottom of the main body 1, the support frame 8 is connected with the main body 1 through a screw, the central line of the support frame 8 is parallel to the central line of the main body 1, the support frame 8 and the rubber block 10 form an elastic structure through an elastic column 9, so that the support frame 8 can always keep an absolute vertical state, the stability of the support frame 8 during bearing is improved, the elastic column 9 is connected with the bottom of the support frame 8, the rubber block 10 is arranged at the bottom of the elastic column 9, the clamping groove 11 is movably arranged in the middle of the bottom end of the main body 1 through a screw, the clamping groove 11 is connected with the main body 1 through a screw, the connecting plates 12 are movably arranged on two sides of the inner wall of the clamping groove 11, the springs 13 are arranged on, when the device is used by a user, if equipment is required to be carried for use, the clamping groove 11 can be mounted through screws, the clamping plate 14 is arranged on the outer wall of the spring 13, the stabilizing frame 15 is movably arranged inside the main body 1, the fan 16 is arranged inside the stabilizing frame 15, the fan 16 is fixedly connected with the rotating shaft 17, the rotating shaft 17 forms a rotating structure through the shaft sleeve 18 and the fan blades 19, the connecting strength between the rotating shaft 17 and the stabilizing frame is increased, the synchronous coordination between parts is ensured, the rotating shaft 17 is arranged inside the fan 16, the shaft sleeve 18 is movably arranged on the outer wall of the rotating shaft 17, and the fan blades 19 are connected to the outer wall of the shaft sleeve 18.
The working principle is as follows: for the unmanned aerial vehicle, firstly, a stabilizing frame 15 is placed into the unmanned aerial vehicle by a user, the unmanned aerial vehicle is fixed with the unmanned aerial vehicle through screws on the stabilizing frame 15, the stabilizing frame 15 is ensured not to shake, a guide plate 2 is arranged at the top of the unmanned aerial vehicle, so that when the unmanned aerial vehicle is guided to fly by a user control device, the guide plate 2 can provide certain stability for the unmanned aerial vehicle, the unmanned aerial vehicle can not generate large deviation, the unmanned aerial vehicle is controlled by the user, a camera 5 (model: MINI 5) is fixed in a fixing frame 4 through a bolt 6 and a nut 7, the user can adjust the angle of the camera 5 through the bolt 6 and the nut 7, the unmanned aerial vehicle is convenient for the device to shoot pictures, when the user needs to use an external device, a clamping groove 11 can be fixed on the unmanned aerial vehicle, a clamping plate 14 is shifted to deform a spring 13, the device needing to be placed into the, the device falls off to cause damage, a user opens the fan 16 to enable the rotating shaft 17 to rotate and then drive the shaft sleeve 18 to rotate, the shaft sleeve 18 drives the fan blades 19 to rotate, the device is pushed by wind to move upwards for use, the electronic gyroscope 3 (type: GY-521) is arranged on the device, the electronic gyroscope 3 can adjust the balance of the device, the device is prevented from shaking greatly, the stability of the device is improved, when the device falls, the elastic column 9 and the rubber block 10 on the support frame 8 can buffer acting force generated by the falling of the device, and the situation that when the device falls, the acting force impacts internal parts of the device to cause damage is avoided.
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 (6)
1. The utility model provides an unmanned aerial vehicle convenient to direction with balance mechanism, includes main part (1), bolt (6) and presss from both sides groove (11), its characterized in that: the top of the main body (1) is movably provided with a guide plate (2), the inner side of the outer wall of the main body (1) is movably provided with an electronic gyroscope (3), the inner part of the main body (1) is provided with a fixed frame (4), the inner part of the fixed frame (4) is movably provided with a camera (5), the bolt (6) is movably arranged on the outer wall of the fixed frame (4), the outer wall of the bolt (6) is movably provided with a nut (7), the bottom of the main body (1) is movably provided with a support frame (8), the support frame (8) is connected with the main body (1) through a screw, the bottom of the support frame (8) is connected with an elastic column (9), the bottom of the elastic column (9) is provided with a rubber block (10), the clamping groove (11) is movably arranged in the middle part of the bottom end of the main body (1), and the, the fan is characterized in that connecting plates (12) are movably arranged on two sides of the inner wall of the clamping groove (11), springs (13) are arranged on the outer walls of the connecting plates (12), clamping plates (14) are arranged on the outer walls of the springs (13), stabilizing frames (15) are movably arranged inside the main body (1), a fan (16) is arranged inside the stabilizing frames (15), a rotating shaft (17) is arranged inside the fan (16), a shaft sleeve (18) is movably arranged on the outer wall of the rotating shaft (17), and fan blades (19) are connected to the outer walls of the shaft sleeve (18).
2. The unmanned aerial vehicle with balance mechanism convenient to guide of claim 1, wherein: the main body (1) and the guide plate (2) are movably connected, and the guide plate (2) is vertically arranged at the top of the main body (1).
3. The unmanned aerial vehicle with balance mechanism convenient to guide of claim 1, wherein: the connecting mode between the fixing frame (4) and the main body (1) is welding, and the fixing frame (4) and the camera (5) form a movable structure through a bolt (6) and a nut (7).
4. The unmanned aerial vehicle with balance mechanism convenient to guide of claim 1, wherein: the center line of the support frame (8) is parallel to the center line of the main body (1), and the support frame (8) and the rubber block (10) form an elastic structure through the elastic column (9).
5. The unmanned aerial vehicle with balance mechanism convenient to guide of claim 1, wherein: the connecting plate (12) is movably connected with the clamping groove (11), and the connecting plate (12) and the clamping plate (14) form an elastic telescopic structure through a spring (13).
6. The unmanned aerial vehicle with balance mechanism convenient to guide of claim 1, wherein: the fan (16) is fixedly connected with the rotating shaft (17), and the rotating shaft (17) and the fan blades (19) form a rotating structure through a shaft sleeve (18).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811277008.7A CN111114812A (en) | 2018-10-30 | 2018-10-30 | Unmanned aerial vehicle convenient to direction with balance mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811277008.7A CN111114812A (en) | 2018-10-30 | 2018-10-30 | Unmanned aerial vehicle convenient to direction with balance mechanism |
Publications (1)
Publication Number | Publication Date |
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CN111114812A true CN111114812A (en) | 2020-05-08 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201811277008.7A Withdrawn CN111114812A (en) | 2018-10-30 | 2018-10-30 | Unmanned aerial vehicle convenient to direction with balance mechanism |
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CN (1) | CN111114812A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112135030A (en) * | 2020-10-09 | 2020-12-25 | 深圳创维-Rgb电子有限公司 | Camera module and display device |
-
2018
- 2018-10-30 CN CN201811277008.7A patent/CN111114812A/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112135030A (en) * | 2020-10-09 | 2020-12-25 | 深圳创维-Rgb电子有限公司 | Camera module and display device |
CN112135030B (en) * | 2020-10-09 | 2022-05-24 | 深圳创维-Rgb电子有限公司 | Camera module and display device |
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Application publication date: 20200508 |
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WW01 | Invention patent application withdrawn after publication |