CN206615388U - One kind is used for unmanned plane automatic balancing bracket - Google Patents
One kind is used for unmanned plane automatic balancing bracket Download PDFInfo
- Publication number
- CN206615388U CN206615388U CN201720348066.9U CN201720348066U CN206615388U CN 206615388 U CN206615388 U CN 206615388U CN 201720348066 U CN201720348066 U CN 201720348066U CN 206615388 U CN206615388 U CN 206615388U
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- unmanned plane
- bracket
- hole
- platform
- mounting platform
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Abstract
It is used for unmanned plane automatic balancing bracket the utility model discloses one kind, including body rack and balance bracket, body rack is divided into mounting platform and support platform, mounting platform is arranged on above support platform, connected by support, balance bracket one end top is connected bottom with mounting platform and is connected with support platform, connected mode is welding, in gyroscope setting and support platform, pipeline is provided with balance bracket, when unmanned plane during flying is uneven, gyroscope collects after information and to release the balancing weight set in corresponding balance bracket laterally.It is helicitic texture to be provided with described mounting platform inside connecting hole and airflow hole, connecting hole, can install accessory additional according to different situations, airflow hole is through hole.It is provided with above the mounting platform above control module, control module and is provided with radar.
Description
Technical field
The utility model is related to unmanned machine support, and in particular to one kind is used for unmanned plane automatic balancing bracket.
Background technology
Unmanned plane is not on the premise of other equipment is installed, and its center of gravity is located at the axis of fuselage.But it is due to that unmanned plane should
With the difference in field, its equipment carried also has different changes, and its weight carried also has larger difference.For example take
The position of centre of gravity of unmanned plane can all be influenceed by carrying digital camera or video camera, so that balance when influenceing unmanned plane during flying.It is existing
In technology, the general balance for ensureing unmanned plane by the way of counterweight, but because the weight of equipment carried is variant, flight
Posture is continually changing, and center of gravity is also required to continuous adjustment, the size of counterweight be also required to it is corresponding change so as to unmanned plane
Balance adjustment make troubles.
Utility model content
Technical problem to be solved in the utility model is that carrying equipment varies in weight, and flight attitude is continually changing, and is caused
Mass centre changing, it is necessary to the continuous size of adjustment counterweight, it is therefore intended that provide it is a kind of be used for unmanned plane automatic balancing bracket, solve
Above-mentioned the problem of.
The utility model is achieved through the following technical solutions：
One kind is used for unmanned plane automatic balancing bracket, including body rack and balance bracket, and it is flat that body rack is divided into installation
Platform and support platform, mounting platform are arranged on above support platform, are connected by support, and balance bracket one end top is flat with installing
Platform connection bottom is connected with support platform, and connected mode is welding, and gyroscope is set with support platform, being set in balance bracket
There is pipeline, when unmanned plane during flying is uneven, gyroscope collects the counterweight that will be set after information in corresponding balance bracket
Block is released laterally.Be provided with described mounting platform inside connecting hole and airflow hole, connecting hole is helicitic texture, Neng Gougen
Accessory is installed additional according to different situations, and airflow hole is through hole.It is provided with above control module, control module and sets above the mounting platform
It is equipped with radar；It can be connected through a screw thread, be connected from different accessories on connecting hole, because accessory weight is inconsistent, center of gravity
Difference is, it is necessary to which control system adjusts flight attitude and balancing weight position in real time, it is ensured that unmanned plane is in stable during flight
Under state.
Further, the control module is used for, and receives the state of flight of gyroscope collection, balancing weight is operated,
Control unmanned plane during flying state.The control module includes signal receiver, microprocessor, central controller, sender unit；
The signal receiver is used for, and receives the state of flight of gyroscope collection, and collection signal is sent into microprocessor；It is described micro-
Processor is used for, and the analog signal that signal receiver is sent is converted into electric signal, and the signal after processing is sent into
Entreat controller；The central controller is used for, and the balancing weight amount of movement on different balance brackets is adjusted according to different flight state；
The sender unit is used for, and the control signal of central controller is sent to balance bracket.
Further, mounting hole is provided with the balance bracket other end, mounting hole is screwed hole, being capable of connection screw thread
Fixed rotor.Lower surface is connected with support column in the middle part of the balance bracket, and support column selects aluminum alloy material, aluminum alloy material compared with
Gently, but with stronger anti-pressure ability.
The utility model compared with prior art, has the following advantages and advantages：
1st, the utility model one kind is used for unmanned plane automatic balancing bracket, according to flight configuration and can carry accessory at any time
Difference in real time adjustment balancing weights, keep flight stability；
2nd, the utility model one kind is used to be provided with multiple connecting holes, energy on unmanned plane automatic balancing bracket, mounting platform
Enough assemble various accessories；
Brief description of the drawings
Accompanying drawing described herein is used for providing further understanding the utility model embodiment, constitutes the one of the application
Part, does not constitute the restriction to the utility model embodiment.In the accompanying drawings：
Fig. 1 is the utility model top view；
Fig. 2 is the utility model structural representation.
Mark and corresponding parts title in accompanying drawing：
1- body racks, 2- balance brackets, 11- mounting platforms, 12- support platforms, 111- connecting holes, 112- airflow holes,
113- control modules, 114- radars, 21- mounting holes, 22- support columns.
Embodiment
For the purpose of this utility model, technical scheme and advantage is more clearly understood, with reference to embodiment and accompanying drawing,
The utility model is described in further detail, and exemplary embodiment of the present utility model and its explanation are only used for explaining this
Utility model, is not intended as limiting of the present utility model.
Embodiment one
As shown in figure 1, the utility model one kind is used for unmanned plane automatic balancing bracket, including body rack 1 and balance branch
Frame 2,1 point of body rack is mounting platform 11 and support platform 12, and mounting platform 11 is arranged on the top of support platform 12, passes through branch
Frame is connected, and one end top of balance bracket 2 is connected bottom with mounting platform 11 and is connected with support platform 12, and connected mode is welding,
Gyroscope is set with support platform 12, pipeline is provided with balance bracket 2, and when unmanned plane during flying is uneven, gyroscope is adopted
Collect the balancing weight after information by setting in corresponding balance bracket 2 to release laterally.Set on described mounting platform 11
There are connecting hole 111 and airflow hole 112, the inside of connecting hole 111 is helicitic texture, can install accessory, air-flow additional according to different situations
Hole 112 is through hole.The top of mounting platform 11 is provided with control module 113, and the top of control module 113 is provided with radar 114；
It can be connected through a screw thread, be connected from different accessories, because accessory weight is inconsistent, center of gravity is also different on connecting hole 111, be needed
Want control system to adjust flight attitude and balancing weight position in real time, it is ensured that unmanned plane is under stable state during flight.
Embodiment two
Further, the control module 114 is used for, and receives the state of flight of gyroscope collection, balancing weight is grasped
Make, control unmanned plane during flying state.The control module 114 includes signal receiver, microprocessor, central controller, signal
Transmitter；The signal receiver is used for, and receives the state of flight of gyroscope collection, and collection signal is sent into microprocessor
Device；The microprocessor is used for, and the analog signal that signal receiver is sent is converted into electric signal, and by the signal after processing
Send to central controller；The central controller is used for, and the counterweight on different balance brackets is adjusted according to different flight state
Block amount of movement；The sender unit is used for, and the control signal of central controller is sent to balance bracket.The balance bracket
Mounting hole 21 is provided with 2 other ends, mounting hole is screwed hole, being capable of connection screw thread fixation rotor.Rotor is arranged on body branch
The outside of frame 1, can make body obtain enough lift, operationally pass through the adjustment of the balancing weight on balance bracket, Yi Jixuan
The wing rotates to control the state of flight of unmanned plane.
Above-described embodiment, is entered to the purpose of this utility model, technical scheme and beneficial effect
One step is described in detail, be should be understood that and be the foregoing is only embodiment of the present utility model, is not used to limit
Fixed protection domain of the present utility model, all any modifications within spirit of the present utility model and principle, made, is equally replaced
Change, improve, should be included within protection domain of the present utility model.
Claims (6)
1. one kind is used for unmanned plane automatic balancing bracket, it is characterised in that including body rack (1) and balance bracket (2), body
Support (1) is divided into mounting platform (11) and support platform (12), and mounting platform (11) is arranged on above support platform (12), passed through
Support is connected, and balance bracket (2) one end top is connected bottom with mounting platform (11) and is connected with support platform (12), connected mode
For welding, gyroscope is set with support platform (12), pipeline is provided with balance bracket (2), when unmanned plane during flying is uneven
When, the balancing weight that gyroscope collects after information by setting in corresponding balance bracket (2) is released laterally.
2. it is according to claim 1 a kind of for unmanned plane automatic balancing bracket, it is characterised in that described mounting platform
(11) it is provided with connecting hole (111) and airflow hole (112) on, is helicitic texture inside connecting hole (111), can be according to not sympathizing with
Condition installs accessory additional, and airflow hole (112) is through hole.
3. it is according to claim 1 a kind of for unmanned plane automatic balancing bracket, mounting platform (11) middle part top
It is provided with end face above control module (113), control module (113) and is provided with radar (114)；
The control module is used for, and receives the state of flight of gyroscope collection, balancing weight is operated, and controls unmanned plane during flying
State.
4. according to claim 3 a kind of for unmanned plane automatic balancing bracket, the control module includes signal and received
Device, microprocessor, central controller, sender unit；
The signal receiver is used for, and receives the state of flight of gyroscope collection, and collection signal is sent into microprocessor；
The microprocessor is used for, and the analog signal that signal receiver is sent is converted into electric signal, and by the letter after processing
Number send to central controller；
The central controller is used for, and the balancing weight amount of movement on different balance brackets (2) is adjusted according to different flight state；
The sender unit is used for, and the control signal of central controller is sent to balance bracket (2).
5. one kind according to claim 1 is used to set on unmanned plane automatic balancing bracket, balance bracket (2) other end
Mounting hole (21) is equipped with, mounting hole (21) is screwed hole, being capable of connection screw thread fixation rotor.
6. it is according to claim 1 a kind of for unmanned plane automatic balancing bracket, balance bracket (2) middle part lower surface
It is connected with support column (22), support column (22) selects aluminum alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720348066.9U CN206615388U (en) | 2017-04-05 | 2017-04-05 | One kind is used for unmanned plane automatic balancing bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720348066.9U CN206615388U (en) | 2017-04-05 | 2017-04-05 | One kind is used for unmanned plane automatic balancing bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206615388U true CN206615388U (en) | 2017-11-07 |
Family
ID=60235479
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720348066.9U Expired - Fee Related CN206615388U (en) | 2017-04-05 | 2017-04-05 | One kind is used for unmanned plane automatic balancing bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206615388U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107010207A (en) * | 2017-04-19 | 2017-08-04 | 四川智航慧飞无人机科技有限公司 | Automatic balancing bracket for balancing unmanned plane during flying state |
| CN114194382A (en) * | 2022-01-21 | 2022-03-18 | 北京航空航天大学东营研究院 | Automatic balancing device and method for unmanned aerial vehicle |
-
2017
- 2017-04-05 CN CN201720348066.9U patent/CN206615388U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107010207A (en) * | 2017-04-19 | 2017-08-04 | 四川智航慧飞无人机科技有限公司 | Automatic balancing bracket for balancing unmanned plane during flying state |
| CN114194382A (en) * | 2022-01-21 | 2022-03-18 | 北京航空航天大学东营研究院 | Automatic balancing device and method for unmanned aerial vehicle |
| CN114194382B (en) * | 2022-01-21 | 2024-02-27 | 东营航空产业技术研究院 | Automatic balancing device and method for unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171107 Termination date: 20180405 |