CN216424733U - Device for enhancing surveying operation stability of propeller type unmanned aerial vehicle - Google Patents
Device for enhancing surveying operation stability of propeller type unmanned aerial vehicle Download PDFInfo
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- CN216424733U CN216424733U CN202122766640.1U CN202122766640U CN216424733U CN 216424733 U CN216424733 U CN 216424733U CN 202122766640 U CN202122766640 U CN 202122766640U CN 216424733 U CN216424733 U CN 216424733U
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- aerial vehicle
- unmanned aerial
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Abstract
The utility model discloses a reinforcing propeller type unmanned aerial vehicle surveys device of job stabilization nature relates to what field. The utility model provides a reinforcing propeller type unmanned aerial vehicle surveys device of operation stability, includes the unmanned aerial vehicle main part, the equal fixedly connected with support in both sides of unmanned aerial vehicle main part, the outside fixedly connected with motor at support top, the output fixedly connected with rotor of motor, the equal fixedly connected with casing in both sides of unmanned aerial vehicle main part bottom. The utility model provides a reinforcing propeller type unmanned aerial vehicle surveys device of operation stability, when the unmanned aerial vehicle main part is descending the in-process, at first the supporting shoe passes through shock pad and ground contact, the supporting shoe cushions on the connecting plate through the support column simultaneously, the connecting plate drives the slider and slides in the spout, wherein through spout and slider, the stability that multiplicable connecting plate removed prevents that the connecting plate from appearing rocking, the connecting plate cushions in the recess through damping spring.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to a device of reinforcing propeller type unmanned aerial vehicle surveys operation stability.
Background
Unmanned aerial vehicle is the unmanned vehicles who utilizes radio remote control equipment and self-contained program control device operation, and unmanned aerial vehicle extensively is used for the hydraulic survey, and hydraulic and hydroelectric engineering is to the topography, cost, precision's requirement is higher and higher, and traditional engineering survey technique deals with high accuracy, real-time data information acquisition work has certain thorn nature, and unmanned aerial vehicle is with its characteristics such as flexible, high resolution, low cost, high ageing.
In propeller type unmanned aerial vehicle surveys the operation in-process, owing to need often rise and fall, need carry on the buffering and increase its stability, current propeller type unmanned aerial vehicle does not have buffer structure, and when propeller type unmanned aerial vehicle in descending, because the impact force is too big easily, lead to its landing leg to appear damaging, and then cause propeller type unmanned aerial vehicle to appear breaking the phenomenon, inconvenient people use.
Therefore, it is necessary to provide a device for enhancing the survey operation stability of the propeller type unmanned aerial vehicle to solve the above technical problems.
SUMMERY OF THE UTILITY MODEL
The utility model provides a reinforcing propeller type unmanned aerial vehicle surveys device of job stabilization nature has solved current propeller type unmanned aerial vehicle, does not have buffer structure, and when propeller type unmanned aerial vehicle in the descending, because the impact force is too big easily, lead to its landing leg to appear damaging, and then cause propeller type unmanned aerial vehicle to appear breaking the phenomenon, the technical problem that inconvenient people used.
In order to solve the technical problems, the utility model provides a device for enhancing the surveying operation stability of propeller type unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, wherein both sides of the unmanned aerial vehicle main body are fixedly connected with a bracket, the outer side of the top of the bracket is fixedly connected with a motor, the output end of the motor is fixedly connected with a rotor wing, both sides of the bottom of the unmanned aerial vehicle main body are fixedly connected with a shell, the top of the inner cavity of the shell is fixedly connected with a buffer spring, the bottom of the buffer spring is fixedly connected with a buffer plate, the front side and the rear side of the bottom of the buffer plate are fixedly connected with buffer columns, the bottom of the buffer columns runs through to the bottom of the shell, the bottom of the buffer columns is provided with grooves, the top of the inner cavity of the grooves is fixedly connected with a damping spring, the bottom of the damping spring is fixedly connected with a connecting plate, and the bottom of the connecting plate is fixedly connected with a supporting column, the bottom of the support column penetrates through the bottom of the groove and is fixedly connected with a support block.
Preferably, the front and the back of the inner cavity of the groove are both provided with sliding grooves, the inner cavity of each sliding groove is connected with a sliding block in a sliding manner, and the inner sides of the sliding blocks are fixedly connected with the front and the back of the connecting plate.
Preferably, the bottom of the supporting block is fixedly connected with a damping pad, and the damping pad is made of rubber materials.
Preferably, the front side and the rear side of the two sides of the buffer plate are both fixedly connected with pulleys, and the outer sides of the pulleys are in contact with the two sides of the inner cavity of the shell.
Preferably, the number of the buffer springs is three, and the three buffer springs are equidistantly arranged on the top of the buffer plate.
Preferably, the front and the back of the buffer plate are fixedly connected with sliding sleeves, inner cavities of the sliding sleeves are connected with sliding rods in a sliding mode, and the tops and the bottoms of the sliding rods are fixedly connected with the tops and the bottoms of the inner cavities of the shells.
Compared with the prior art, the utility model provides a pair of reinforcing propeller type unmanned aerial vehicle surveys device of operation stability has following beneficial effect:
the utility model provides a reinforcing propeller type unmanned aerial vehicle surveys device of operation stability, when the unmanned aerial vehicle main part is descending the in-process, at first the supporting shoe passes through shock pad and ground contact, the supporting shoe cushions on the connecting plate through the support column simultaneously, the connecting plate drives the slider and slides in the spout, wherein through spout and slider, the stability that multiplicable connecting plate removed prevents that the connecting plate from appearing rocking, the connecting plate cushions in the recess through damping spring.
The utility model provides a reinforcing propeller type unmanned aerial vehicle surveys device of operation stability, at this moment, the buffer column cushions on the buffer board, the buffer board drives the pulley and slides in the casing, the buffer board drives the sliding sleeve and slides on the slide bar, wherein pass through the pulley, sliding sleeve and slide bar, to the buffer board the steady effect of removal has been played at the removal in-process, prevent that the buffer board from appearing the card in the use and pausing, synchronous buffer board cushions on buffer spring, make buffer spring offset below pressure, increase the stability of support column and support column.
Drawings
Fig. 1 is a schematic structural diagram of a preferred embodiment of an apparatus for enhancing the survey operation stability of a propeller-type unmanned aerial vehicle according to the present invention;
FIG. 2 is a sectional view of the housing structure of the present invention;
FIG. 3 is a side sectional view of the housing and the bumper structure of the present invention;
fig. 4 is an enlarged view of the structure a-a of the present invention.
The reference numbers in the figures: 1. an unmanned aerial vehicle main body; 2. a support; 3. a motor; 4. a rotor; 5. a housing; 6. a buffer spring; 7. a buffer plate; 8. a buffer column; 9. a groove; 10. a damping spring; 11. a connecting plate; 12. a support pillar; 13. a support block; 14. a chute; 15. a slider; 16. a pulley; 17. a sliding sleeve; 18. a slide bar.
Detailed Description
In order to make the technical solution of the present invention better understood, the present invention is described in detail below with reference to the accompanying drawings, and the description of the present invention is only exemplary and explanatory, and should not be construed as limiting the scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
It should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like refer to the orientation or positional relationship shown in the drawings, or the orientation or positional relationship that the utility model is usually placed when in use, and are used for convenience of description and simplification of description, but do not refer to or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The first embodiment is as follows:
referring to fig. 1-4, the present invention provides a technical solution: a device for enhancing the surveying operation stability of a propeller type unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, wherein two sides of the unmanned aerial vehicle main body 1 are fixedly connected with a support 2, the outer side of the top of the support 2 is fixedly connected with a motor 3, the output end of the motor 3 is fixedly connected with a rotor wing 4, two sides of the bottom of the unmanned aerial vehicle main body 1 are fixedly connected with a shell 5, the top of the inner cavity of the shell 5 is fixedly connected with a buffer spring 6, the bottom of the buffer spring 6 is fixedly connected with a buffer plate 7, the front side and the rear side of the bottom of the buffer plate 7 are fixedly connected with buffer columns 8, the bottom of each buffer column 8 penetrates to the bottom of the shell 5, the bottom of each buffer column 8 is provided with a groove 9, the top of the inner cavity of the groove 9 is fixedly connected with a damping spring 10, the bottom of each damping spring 10 is fixedly connected with a connecting plate 11, the bottom of each connecting plate 11 is fixedly connected with a supporting column 12, the bottom of each supporting block 13 penetrates to the bottom of the groove 9, the bottom fixedly connected with shock pad of supporting shoe 13, and the material of shock pad is rubber materials, and buffer spring 6's quantity is three, and three buffer spring 6 is the equidistance and arranges the top at buffer board 7.
In this embodiment, when unmanned aerial vehicle main part 1 is descending the in-process, at first supporting shoe 13 passes through shock pad and ground contact, supporting shoe 13 cushions on connecting plate 11 through support column 12 simultaneously, connecting plate 11 drives slider 15 and slides in spout 14, wherein through spout 14 and slider 15, the stability of 11 removals of multiplicable connecting plate prevents that connecting plate 11 from appearing rocking, and connecting plate 11 cushions in recess 9 through damping spring 10.
Example two:
referring to fig. 1-4, based on the first embodiment, the present invention provides a technical solution: the front and the back in recess 9 inner chamber have all seted up spout 14, the inner chamber sliding connection of spout 14 has slider 15, the inboard of slider 15 and the front and the back fixed connection of connecting plate 11, the equal fixedly connected with pulley 16 of front side and the rear side of buffer board 7 both sides, the outside of pulley 16 and the both sides contact of casing 5 inner chamber, the front and the equal fixedly connected with sliding sleeve 17 in the back of buffer board 7, sliding sleeve 17's inner chamber sliding connection has slide bar 18, slide bar 18's top and bottom and casing 5 inner chamber's top and bottom fixed connection.
In this embodiment: at this moment, cushion column 8 cushions on buffer board 7, buffer board 7 drives pulley 16 and slides in casing 5, buffer board 7 drives sliding sleeve 17 and slides on slide bar 18, wherein through pulley 16, sliding sleeve 17 and slide bar 18, buffer board 7 has played the steady effect of removal at the removal in-process, prevent that buffer board 7 from appearing the card pause in the use, synchronous buffer board 7 cushions on buffer spring 6, make buffer spring 6 offset below pressure, increase the stability of support column 12 and support column 12.
The utility model provides a pair of reinforcing propeller type unmanned aerial vehicle surveys device of operation stability's theory of operation as follows:
the first innovation point implementation step:
the first step is as follows: when the unmanned aerial vehicle main body 1 is in a landing process, firstly, the supporting block 13 is in contact with the ground through the shock pad, meanwhile, the supporting block 13 is buffered on the connecting plate 11 through the supporting column 12, and the connecting plate 11 drives the sliding block 15 to slide in the sliding groove 14;
the second step is that: wherein through spout 14 and slider 15, the stability that multiplicable connecting plate 11 removed prevents that connecting plate 11 from appearing rocking, and connecting plate 11 cushions in recess 9 through damping spring 10.
The implementation step of the second innovation point:
the first step is as follows: at the moment, the buffer column 8 buffers on the buffer plate 7, the buffer plate 7 drives the pulley 16 to slide in the shell 5, the buffer plate 7 drives the sliding sleeve 17 to slide on the sliding rod 18, and the buffer plate 7 plays a role in stably moving in the moving process through the pulley 16, the sliding sleeve 17 and the sliding rod 18, so that the buffer plate 7 is prevented from being blocked in the using process;
the second step is that: synchronous buffer plate 7 cushions on buffer spring 6, makes buffer spring 6 offset to the below pressure, increases the stability of support column 12 and support column 12.
The standard parts used in this application document all can be purchased from the market, and can be customized according to the record of description and drawings, the concrete connection mode of each part all adopts conventional means such as mature bolt, rivet, welding among the prior art, machinery, part and equipment all adopt conventional model among the prior art, the control mode is automatic control through the controller, the control circuit of controller can realize through technical staff's simple programming in this field, belong to the common general knowledge in this field, and the utility model discloses mainly be used for protecting mechanical device, so the utility model discloses no longer explain control mode and circuit connection in detail, and the peripheral controller that mentions in the description can play the control role for the electrical components that this article mention, and this peripheral controller is conventional known equipment.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
The principles and embodiments of the present invention have been explained herein using specific examples, which are presented only to assist in understanding the methods and their core concepts. It should be noted that there are infinite specific structures due to the limited character expressions, and it will be apparent to those skilled in the art that various improvements, decorations or changes can be made without departing from the principles of the present invention, and the technical features can be combined in a suitable manner; the application of these modifications, variations or combinations, or the application of the concepts and solutions of the present invention in other contexts without modification, is not intended to be considered as a limitation of the present invention.
Claims (7)
1. The utility model provides an reinforcing propeller type unmanned aerial vehicle surveys device of operation stability, includes unmanned aerial vehicle main part (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein supports (2) are fixedly connected to the two sides of the unmanned aerial vehicle body (1), motors (3) are fixedly connected to the outer sides of the tops of the supports (2), rotors (4) are fixedly connected to the output ends of the motors (3), shells (5) are fixedly connected to the two sides of the bottom of the unmanned aerial vehicle body (1), buffer springs (6) are fixedly connected to the tops of the inner cavities of the shells (5), buffer plates (7) are fixedly connected to the bottoms of the buffer springs (6), buffer columns (8) are fixedly connected to the front sides and the rear sides of the bottoms of the buffer plates (7), the bottoms of the buffer columns (8) penetrate through the bottoms of the shells (5), grooves (9) are formed in the bottoms of the buffer columns (8), damping springs (10) are fixedly connected to the tops of the inner cavities of the grooves (9), and connecting plates (11) are fixedly connected to the bottoms of the damping springs (10), the bottom fixedly connected with support column (12) of connecting plate (11), the bottom of support column (12) runs through to the bottom of recess (9) and fixedly connected with supporting shoe (13).
2. The device for enhancing the surveying operation stability of the propeller type unmanned aerial vehicle according to claim 1, wherein sliding grooves (14) are formed in the front and back surfaces of the inner cavity of the groove (9), sliding blocks (15) are slidably connected to the inner cavity of the sliding grooves (14), and the inner sides of the sliding blocks (15) are fixedly connected with the front and back surfaces of the connecting plate (11).
3. The device for enhancing the survey operation stability of the propeller type unmanned aerial vehicle according to claim 1, wherein a shock pad is fixedly connected to the bottom of the supporting block (13), and the shock pad is made of rubber.
4. The device for enhancing the survey operation stability of the propeller type unmanned aerial vehicle according to claim 1, wherein the front side and the rear side of the two sides of the buffer plate (7) are fixedly connected with pulleys (16), and the outer sides of the pulleys (16) are in contact with the two sides of the inner cavity of the shell (5).
5. The device for enhancing the survey operation stability of the propeller type unmanned aerial vehicle according to claim 1, wherein the number of the buffer springs (6) is three, and the three buffer springs (6) are arranged on the top of the buffer plate (7) at equal intervals.
6. The device for enhancing the survey operation stability of the propeller type unmanned aerial vehicle according to claim 1, wherein a sliding sleeve (17) is fixedly connected to the front surface and the back surface of the buffer plate (7).
7. The device for enhancing the survey operation stability of the propeller type unmanned aerial vehicle according to claim 6, wherein the inner cavity of the sliding sleeve (17) is slidably connected with a sliding rod (18), and the top and the bottom of the sliding rod (18) are fixedly connected with the top and the bottom of the inner cavity of the shell (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122766640.1U CN216424733U (en) | 2021-11-12 | 2021-11-12 | Device for enhancing surveying operation stability of propeller type unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122766640.1U CN216424733U (en) | 2021-11-12 | 2021-11-12 | Device for enhancing surveying operation stability of propeller type unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216424733U true CN216424733U (en) | 2022-05-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122766640.1U Active CN216424733U (en) | 2021-11-12 | 2021-11-12 | Device for enhancing surveying operation stability of propeller type unmanned aerial vehicle |
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| CN (1) | CN216424733U (en) |
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- 2021-11-12 CN CN202122766640.1U patent/CN216424733U/en active Active
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