CN208412099U - A kind of balance bracket for unmanned plane - Google Patents
A kind of balance bracket for unmanned plane Download PDFInfo
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- CN208412099U CN208412099U CN201820906448.3U CN201820906448U CN208412099U CN 208412099 U CN208412099 U CN 208412099U CN 201820906448 U CN201820906448 U CN 201820906448U CN 208412099 U CN208412099 U CN 208412099U
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- unmanned plane
- balancing pole
- platform
- counter weight
- weight device
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Abstract
The utility model relates to a kind of balance brackets for unmanned plane, including the platform being connected with drone body, the platform central symmetry is equipped with more balancing poles, is arranged with counter weight device on the balancing pole, the counter weight device can be slided and be positioned along the balancing pole.When the equipment of UAV flight's different weight, utilize lever principle, by changing position of the counter weight device on balancing pole, to change the center of gravity of fuselage, from regardless of platform carries the device of which kind of quality proportioning of which kind of shape, by the cooperation of the balancing pole and counter weight device, unmanned plane holding torque can be made to balance, to realize the quick adjusting of unmanned plane balance, and it does not need frequently to change counterweight size.
Description
Technical field
The utility model relates to air vehicle technique fields, and in particular to a kind of balance bracket for unmanned plane.
Background technique
With the rapid development of science and technology, the use of unmanned plane is increasingly wider.Unmanned plane has and can hover, in a constant speed
Can be with arbitrary speed flight in degree range the features such as, therefore be basically the platform of an airflight, it can be in platform
Sensor, the camera etc. of upper load oneself.But unmanned plane, before carrying equipment, often its ontology has good symmetrical
Property, but the equipment carried often does not have symmetry, the center of gravity of the center of gravity and institute's charging appliance that will lead to unmanned plane at this time is inclined
Difference is larger, not only affects the shooting angle of equipment, more affects the flight path and stability of unmanned plane.
Utility model content
The utility model provides a kind of balance bracket for unmanned plane, solves the problems, such as techniques discussed above.
The technical solution that the utility model solves above-mentioned technical problem is as follows: a kind of balance bracket for unmanned plane, packet
The platform being connected with drone body is included, the platform central symmetry is equipped with more balancing poles, is arranged on the balancing pole
There is counter weight device, the counter weight device can be slided and be positioned along the balancing pole.Specifically, the counter weight device passes through locking screw
Bolt is positioned in the balancing pole.
The beneficial effects of the utility model are:, using lever principle, passing through when the equipment of UAV flight's different weight
Change position of the counter weight device on balancing pole, to change the center of gravity of fuselage, from regardless of platform carries which kind of matter of which kind of shape
The device for measuring proportion can be such that unmanned plane holding torque balances by the cooperation of the balancing pole and counter weight device, thus real
The quick adjusting of existing unmanned plane balance, and it does not need frequently to change counterweight size.
Based on the above technical solution, the utility model can also do following improvement.
Further, the counter weight device includes sliding block and clump weight, and the sliding block is set on the balancing pole, described to match
Pouring weight is detachably connected below the sliding block.
Beneficial effect using above-mentioned further scheme is: when being not necessarily to carry out counterweight, the clump weight can be dismantled,
To mitigate the load-carrying of entire unmanned plane, and then extend the cruise duration of unmanned plane.It adjusts, can also select for different counterweights
The clump weight of different weight is selected, so as to adjust the balance of unmanned plane rapidly.
Further, the balancing pole is equipped with scale in its length direction.
Beneficial effect using above-mentioned further scheme is: the case where for UAV flight's identical equipment, can pass through
Scale records the counterweight situation of clump weight, to avoid repeatedly adjusting the cumbersome of clump weight under the same conditions.
Further, the balancing pole is equipped with limited block far from platform one end.
Beneficial effect using above-mentioned further scheme is: in adjusting counter weight device moving process, balancing pole is far from flat
The limited block of platform one end can prevent the case where adjusting excessively, counter weight device is caused to skid off from balancing pole.
Further, it is equipped with buffer table below the platform, spring is equipped between the buffer table and platform.
Beneficial effect using above-mentioned further scheme is: the buffer table can buffer during unmanned plane lands
Ground faces the impact of platform, causes to damage or damage to prevent the equipment placed on platform from generating impact.
The above description is merely an outline of the technical solution of the present invention, in order to better understand the skill of the utility model
Art means, and can be implemented in accordance with the contents of the specification, below on the preferred embodiment of the present invention and the accompanying drawings in detail
It describes in detail bright as after.Specific embodiment of the present utility model is shown in detail by following embodiment and its attached drawing.
Detailed description of the invention
Attached drawing described herein is used to provide a further understanding of the present invention, and is constituted part of this application,
The exemplary embodiment of the utility model and the description thereof are used to explain the utility model, does not constitute to the improper of the utility model
It limits.In the accompanying drawings:
Fig. 1 is a kind of balance bracket main view for unmanned plane that an embodiment of the present invention provides.
In attached drawing, parts list represented by the reference numerals are as follows:
1, platform；2, balancing pole；3, clamping screw；4, sliding block；5, clump weight；6, limited block；7, buffer table；8, spring.
Specific embodiment
The principles of the present invention and feature are described below in conjunction with attached drawing 1, example is served only for explaining this reality
With novel, it is not intended to limit the scope of the utility model.
As shown in Figure 1, the utility model provides a kind of balance bracket for unmanned plane, including with drone body phase
Platform 1 even, the 1 outer rim central symmetry of platform are equipped with more balancing poles 2, are arranged with counter weight device on the balancing pole 2, institute
Stating counter weight device can slide and position along the balancing pole 2.Specifically, the counter weight device is by clamping screw 3 described flat
The bar 2 that weighs positions.
Under normal conditions, the platform of unmanned plane can carry a variety of equipment, the often simultaneously non-centrosymmetry of these equipment, this
It will cause the different degrees of inclination of unmanned plane.When the equipment of UAV flight's different weight, using lever principle, pass through change
Position of the counter weight device on balancing pole 2, to change the center of gravity of fuselage, from regardless of platform carries which kind of shape which kind of quality is matched
The device of ratio can be such that unmanned plane holding torque balances, to realize nothing by the cooperation of the balancing pole and counter weight device
The quick adjusting of man-machine balance, and it does not need frequently to change counterweight size.
Preferably, the counter weight device includes sliding block 4 and clump weight 5, and the sliding block 4 is set on the balancing pole 2, institute
It states clump weight 5 and is detachably connected on 4 lower section of sliding block.When being not necessarily to carry out counterweight, the clump weight 5 can be dismantled, from
And mitigate the load-carrying of entire unmanned plane, and then extend the cruise duration of unmanned plane.It adjusts for different counterweights, also can choose
The clump weight 5 of different weight, so as to adjust the balance of unmanned plane rapidly.
Preferably, the balancing pole 2 is equipped with scale in its length direction.The case where equipment identical for UAV flight,
The counterweight situation of clump weight 5 can be recorded by scale, to avoid repeatedly adjusting clump weight 5 under the same conditions
It is cumbersome.
Preferably, the balancing pole 2 is equipped with limited block 6 far from platform one end.In adjusting counter weight device moving process, put down
The case where weighing apparatus bar 2 can prevent from adjusting excessively far from the limited block 6 of platform one end, and counter weight device is caused to skid off from balancing pole hair
It is raw.
Preferably, it is equipped with buffer table 7 below the platform 1, spring is equipped between the buffer table 7 and platform 1.It is described slow
The impact of platform 1 can be faced to buffering during unmanned plane lands by rushing platform 7, to prevent from setting to what is placed on platform 1
Standby generation impact is caused to damage or be damaged.
The above, the only preferred embodiment of the utility model not make in any form the utility model
Limitation；The those of ordinary skill of all industry can be shown in by specification attached drawing and described above and swimmingly to implement this practical
It is novel；But all those skilled in the art are not departing within the scope of technical solutions of the utility model, using being taken off above
The technology contents shown and the equivalent variations of a little variation, modification and evolution made, are the equivalent embodiment of the utility model；
Meanwhile it the change of all substantial technological any equivalent variationss to the above embodiments according to the utility model, modifying and drilling
Become etc., within the protection scope for still falling within the technical solution of the utility model.
Claims (6)
1. a kind of balance bracket for unmanned plane, it is characterised in that: described including the platform (1) being connected with drone body
Platform (1) outer rim central symmetry is equipped with more balancing poles (2), and counter weight device is arranged on the balancing pole (2), described with refitting
Setting can slide and position along the balancing pole (2).
2. a kind of balance bracket for unmanned plane according to claim 1, which is characterized in that the counter weight device passes through lock
Tight bolt (3) positions on the balancing pole (2).
3. a kind of balance bracket for unmanned plane according to claim 1, which is characterized in that the counter weight device includes sliding
Block (4) and clump weight (5), the sliding block (4) are set on the balancing pole (2), and the clump weight (5) is detachably connected on institute
It states below sliding block (4).
4. a kind of balance bracket for unmanned plane according to claim 1, which is characterized in that the balancing pole (2) is at it
Length direction is equipped with scale.
5. a kind of balance bracket for unmanned plane according to claim 1, which is characterized in that the balancing pole (2) is separate
Platform one end is equipped with limited block (6).
6. any one of -5 a kind of balance bracket for unmanned plane according to claim 1, which is characterized in that the platform
(1) lower section is equipped with buffer table (7), and spring is equipped between the buffer table (7) and platform (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820906448.3U CN208412099U (en) | 2018-06-12 | 2018-06-12 | A kind of balance bracket for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820906448.3U CN208412099U (en) | 2018-06-12 | 2018-06-12 | A kind of balance bracket for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208412099U true CN208412099U (en) | 2019-01-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820906448.3U Active CN208412099U (en) | 2018-06-12 | 2018-06-12 | A kind of balance bracket for unmanned plane |
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| CN (1) | CN208412099U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112550742A (en) * | 2020-12-10 | 2021-03-26 | 国网浙江省电力有限公司江山市供电公司 | Rotary unmanned aerial vehicle electroscope |
| 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 |
| CN115126968A (en) * | 2022-05-31 | 2022-09-30 | 国网河北省电力有限公司沧州供电分公司 | Electric power marketing data acquisition device |
-
2018
- 2018-06-12 CN CN201820906448.3U patent/CN208412099U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112550742A (en) * | 2020-12-10 | 2021-03-26 | 国网浙江省电力有限公司江山市供电公司 | Rotary unmanned aerial vehicle electroscope |
| 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 |
| CN115126968A (en) * | 2022-05-31 | 2022-09-30 | 国网河北省电力有限公司沧州供电分公司 | Electric power marketing data acquisition device |
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