CN107010207A - Automatic balancing bracket for balancing unmanned plane during flying state - Google Patents
Automatic balancing bracket for balancing unmanned plane during flying state Download PDFInfo
- Publication number
- CN107010207A CN107010207A CN201710257877.2A CN201710257877A CN107010207A CN 107010207 A CN107010207 A CN 107010207A CN 201710257877 A CN201710257877 A CN 201710257877A CN 107010207 A CN107010207 A CN 107010207A
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- Prior art keywords
- balance
- bracket
- unmanned plane
- balancing
- plane during
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- 238000003466 welding Methods 0.000 claims abstract description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 230000005484 gravity Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
- B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Motorcycle And Bicycle Frame (AREA)
Abstract
The invention discloses the automatic balancing bracket for balancing unmanned plane during flying state, 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 present invention relates to unmanned machine support, and in particular to the automatic balancing bracket for balancing unmanned plane during flying state.
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.
The content of the invention
The technical problems to be solved by the invention are that carrying equipment varies in weight, and flight attitude is continually changing, caused weight
The heart changes, it is necessary to constantly adjust the size of counterweight, it is therefore intended that provide the autobalance branch for balancing unmanned plane during flying state
Frame, the problem of solving above-mentioned.
The present invention is achieved through the following technical solutions：
Automatic balancing bracket for balancing unmanned plane during flying state, including body rack and balance bracket, body rack
It is divided into mounting platform and support platform, mounting platform is arranged on above support platform, connected by support, on balance bracket one end
Portion is connected bottom with mounting platform and is connected with support platform, and connected mode is welding, and gyroscope is set with support platform, balancing
Pipeline is provided with support, when unmanned plane during flying is uneven, gyroscope is collected in corresponding balance bracket after information
The balancing weight of setting is released laterally.Be provided with described mounting platform inside connecting hole and airflow hole, connecting hole is screw thread
Structure, can install accessory additional according to different situations, and airflow hole is through hole.Control module is installed above the mounting platform, controlled
Radar is provided with above molding block；It can be connected through a screw thread, be connected from different accessories, because accessory weight is not on connecting hole
Unanimously, center of gravity is also different, it is necessary to which control system adjusts flight attitude and balancing weight position in real time, it is ensured that during flight nobody
Machine is under stable 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 present invention compared with prior art, has the following advantages and advantages：
1st, the present invention is used for the automatic balancing bracket for balancing unmanned plane during flying state, according to flight configuration and can take at any time
The difference for carrying accessory adjusts balancing weight in real time, keeps flight stability；
2nd, the present invention is used to be provided with multiple connections on the automatic balancing bracket for balancing unmanned plane during flying state, mounting platform
Hole, can assemble various accessories；
Brief description of the drawings
Accompanying drawing described herein is used for providing further understanding the embodiment of the present invention, constitutes one of the application
Point, do not constitute the restriction to the embodiment of the present invention.In the accompanying drawings：
Fig. 1 is top view of the present invention；
Fig. 2 is schematic structural view of the invention.
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 object, technical solutions and advantages of the present invention are more clearly understood, with reference to embodiment and accompanying drawing, to this
Invention is described in further detail, and exemplary embodiment and its explanation of the invention is only used for explaining the present invention, does not make
For limitation of the invention.
Embodiment one
As shown in figure 1, the present invention is used for the automatic balancing bracket for balancing unmanned plane during flying state, including the He of body rack 1
Balance bracket 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,
Connected by support, 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, when unmanned plane during flying is uneven, gyro
The balancing weight that instrument collects after information by setting in corresponding balance bracket 2 is released laterally.On described mounting platform 11
Connecting hole 111 and airflow hole 112 are provided with, the inside of connecting hole 111 is helicitic texture, can install accessory additional according to different situations,
Airflow 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 accessory on connecting hole 111, because accessory weight is inconsistent, center of gravity is not yet
With, it is necessary to which control system adjusts flight attitude and balancing weight position in real time, it is ensured that unmanned plane, which is in, during flight stablizes shape
Under state.
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, has been carried out further to the purpose of the present invention, technical scheme and beneficial effect
Describe in detail, should be understood that the embodiment that the foregoing is only the present invention, be not intended to limit the present invention
Protection domain, within the spirit and principles of the invention, any modification, equivalent substitution and improvements done etc. all should be included
Within protection scope of the present invention.
Claims (5)
1. the automatic balancing bracket for balancing unmanned plane during flying state, it is characterised in that including body rack (1) and balance branch
Frame (2), body rack (1) is divided into mounting platform (11) and support platform (12), and mounting platform (11) is arranged on support platform
(12) top, is connected, balance bracket (2) one end top is connected bottom and support platform (12) with mounting platform (11) by support
Connection, connected mode is welding, and gyroscope is set with support platform (12), pipeline being provided with balance bracket (2), when nobody
When machine flight is uneven, the balancing weight that gyroscope collects after information by setting in corresponding balance bracket (2) is pushed away laterally
Go out, it is screw thread knot to be provided with described mounting platform (11) inside connecting hole (111) and airflow hole (112), connecting hole (111)
Structure, can install accessory additional according to different situations, and airflow hole (112) is through hole.
2. the automatic balancing bracket according to claim 1 for being used to balance unmanned plane during flying state, the mounting platform
(11) it is provided with the end face of middle part top 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.
3. the automatic balancing bracket according to claim 2 for being used to balance unmanned plane during flying state, the control module bag
Include 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；
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).
4. the automatic balancing bracket according to claim 1 for being used to balance unmanned plane during flying state, the balance bracket (2)
Mounting hole (21) is provided with the other end, mounting hole (21) is screwed hole, being capable of connection screw thread fixation rotor.
5. the automatic balancing bracket according to claim 1 for being used to balance unmanned plane during flying state, the balance bracket (2)
Middle part lower surface is connected with support column (22), and support column (22) selects aluminum alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710257877.2A CN107010207A (en) | 2017-04-19 | 2017-04-19 | Automatic balancing bracket for balancing unmanned plane during flying state |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710257877.2A CN107010207A (en) | 2017-04-19 | 2017-04-19 | Automatic balancing bracket for balancing unmanned plane during flying state |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107010207A true CN107010207A (en) | 2017-08-04 |
Family
ID=59446683
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710257877.2A Withdrawn CN107010207A (en) | 2017-04-19 | 2017-04-19 | Automatic balancing bracket for balancing unmanned plane during flying state |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107010207A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107608375A (en) * | 2017-09-13 | 2018-01-19 | 广西电网有限责任公司北海供电局 | Faulty insulator detecting system and method based on unmanned plane |
| CN107765134A (en) * | 2017-10-24 | 2018-03-06 | 深圳供电局有限公司 | A kind of method and unmanned plane of the lightning arrester live-line test for carrying out transmission line of electricity |
| CN108128457A (en) * | 2017-12-24 | 2018-06-08 | 中山市得高行知识产权中心（有限合伙） | A kind of unmanned plane vertically soaring level(l)ing mechanism |
| CN112224416A (en) * | 2020-10-21 | 2021-01-15 | 郑法林 | Medicine unmanned aerial vehicle is spouted to counter weight balanced type agricultural |
| CN113791567A (en) * | 2021-10-14 | 2021-12-14 | 杭州电子科技大学 | Aircraft self-stabilizing device based on gyroscope technology and control system |
| 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 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103979106A (en) * | 2014-04-29 | 2014-08-13 | 浙江大学 | Rotor-type unmanned aerial vehicle automatically adjusting gravity center and adjustment method |
| CN204998755U (en) * | 2015-08-24 | 2016-01-27 | 深圳市诺亚星辰科技开发有限公司 | Rotor unmanned aerial vehicle balance adjustment device |
| CN206615388U (en) * | 2017-04-05 | 2017-11-07 | 四川智航慧飞无人机科技有限公司 | One kind is used for unmanned plane automatic balancing bracket |
-
2017
- 2017-04-19 CN CN201710257877.2A patent/CN107010207A/en not_active Withdrawn
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103979106A (en) * | 2014-04-29 | 2014-08-13 | 浙江大学 | Rotor-type unmanned aerial vehicle automatically adjusting gravity center and adjustment method |
| CN204998755U (en) * | 2015-08-24 | 2016-01-27 | 深圳市诺亚星辰科技开发有限公司 | Rotor unmanned aerial vehicle balance adjustment device |
| CN206615388U (en) * | 2017-04-05 | 2017-11-07 | 四川智航慧飞无人机科技有限公司 | One kind is used for unmanned plane automatic balancing bracket |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107608375A (en) * | 2017-09-13 | 2018-01-19 | 广西电网有限责任公司北海供电局 | Faulty insulator detecting system and method based on unmanned plane |
| CN107608375B (en) * | 2017-09-13 | 2021-01-15 | 广西电网有限责任公司北海供电局 | Degraded insulator detection system and method based on unmanned aerial vehicle |
| CN107765134A (en) * | 2017-10-24 | 2018-03-06 | 深圳供电局有限公司 | A kind of method and unmanned plane of the lightning arrester live-line test for carrying out transmission line of electricity |
| CN107765134B (en) * | 2017-10-24 | 2023-11-14 | 深圳供电局有限公司 | Method for carrying out live test on lightning arrester of power transmission line and unmanned aerial vehicle |
| CN108128457A (en) * | 2017-12-24 | 2018-06-08 | 中山市得高行知识产权中心（有限合伙） | A kind of unmanned plane vertically soaring level(l)ing mechanism |
| CN112224416A (en) * | 2020-10-21 | 2021-01-15 | 郑法林 | Medicine unmanned aerial vehicle is spouted to counter weight balanced type agricultural |
| CN112224416B (en) * | 2020-10-21 | 2022-05-31 | 北京麦麦趣耕科技有限公司 | Medicine unmanned aerial vehicle is spouted to counter weight balanced type agricultural |
| CN113791567A (en) * | 2021-10-14 | 2021-12-14 | 杭州电子科技大学 | Aircraft self-stabilizing device based on gyroscope technology and control system |
| CN113791567B (en) * | 2021-10-14 | 2024-04-12 | 杭州电子科技大学 | Aircraft self-stabilizing device and control system based on gyroscope technology |
| 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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| Date | Code | Title | Description |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170804 |
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| WW01 | Invention patent application withdrawn after publication |