CN217805246U - Buffering support for landing of unmanned aerial vehicle - Google Patents
Buffering support for landing of unmanned aerial vehicle Download PDFInfo
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- CN217805246U CN217805246U CN202221677223.8U CN202221677223U CN217805246U CN 217805246 U CN217805246 U CN 217805246U CN 202221677223 U CN202221677223 U CN 202221677223U CN 217805246 U CN217805246 U CN 217805246U
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Abstract
The utility model discloses an unmanned aerial vehicle is on land with buffering support belongs to unmanned aerial vehicle support field. The utility model discloses an unmanned aerial vehicle lands and uses buffering support, including installation mechanism and supporting mechanism, installation mechanism's below is provided with supporting mechanism, and supporting mechanism is provided with four. The utility model provides a current buffering support only reaches the reduction impact force through setting up bracing piece and telescopic link, realize the buffering, the buffering effect is general, and the direct buffering support mounting with the bottom of unmanned aerial vehicle, make the relatively poor problem of barrier propterty of unmanned aerial vehicle body, unmanned aerial vehicle contacts ground at first supporting mechanism and elastic rod after landing, cushion once, then the mounting panel is close to the movable groove under inertial effect, make the fixing base produce the linkage to the slide under the effect of connecting rod, make the slide extrude to two directions of elastic component, with an elastic component cooperation, reach the effect of second grade buffering, the unmanned aerial vehicle body has effectively been protected.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle support field specifically is an unmanned aerial vehicle is on land with buffering support.
Background
Unmanned aerial vehicle is because factors such as self weight, landing speed regulation error can bump or take place the spring etc. after touchdown with ground when descending, and the violent vibration of foot rest can lead to the precision electronic equipment that the machine carried to break down to take place to damage, need be used to cushion the support and cushion unmanned aerial vehicle when descending.
Chinese patent with publication number CN21633272U discloses a buffering support that unmanned aerial vehicle was convenient for to change, this patent passes through the fixed block, the mounting groove, cooperation between fixture block and the stop gear, make buffering support can separate with unmanned aerial vehicle, and dismantle simple laborsaving of process, reduce unmanned aerial vehicle's volume, make its portable, it is more convenient to use, cooperation through between draw-in groove and the diaphragm, can make the structure of buffering support more stable, make unmanned aerial vehicle's take off and land more will be steady, be convenient for accomodate buffering support simultaneously. However, the above patents have the following drawbacks:
the existing buffering support only achieves the purposes of reducing impact force and achieving buffering through arranging the supporting rod and the telescopic rod, the buffering effect is general, and the unmanned aerial vehicle is directly installed with the buffering support at the bottom, so that the protection performance of the unmanned aerial vehicle body is poor, and the landing safety of the unmanned aerial vehicle is to be improved; therefore, the existing requirements are not met, and a buffer support for landing of the unmanned aerial vehicle is provided for the existing requirements.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is on land with buffering support, unmanned aerial vehicle contacts ground at first supporting mechanism and elastic rod after landing, once cushion, then the mounting panel is close to the movable groove under inertial effect, make the fixing base produce the linkage to the slide under the effect of connecting rod, make the slide extrude to two directions of elastic component, cooperate with elastic component one, reach the effect of second grade buffering, the unmanned aerial vehicle body has effectively been protected, the problem of proposing in the above-mentioned background art has been solved.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle lands with buffering support, includes installation mechanism and supporting mechanism, installation mechanism's below is provided with the supporting mechanism that is used for unmanned aerial vehicle to descend the buffering, and supporting mechanism is provided with four, the supporting mechanism includes interior pole, elastic component three, lower interior pole, spout, slider and urceolus, the inside of urceolus is provided with interior pole, the below of going up interior pole is provided with down interior pole, the fixed base that is provided with in below of pole, connecting block and installation mechanism fixed connection are passed through to the top of going up interior pole, installation mechanism includes fixing base, movable groove, mounting panel, radiating groove, mounting hole, guide bar, elastic component one, elastic component two, slide, connecting rod and protective housing, protective housing's inside is provided with the mounting panel that is used for fixed fuselage bottom position, the lower fixed surface of mounting panel is provided with the fixing base, and the fixing base is provided with two, protective housing's end inner wall is provided with movable groove, and movable groove is provided with two.
Preferably, the four supporting mechanisms are provided with elastic rods at the outer sides, and the elastic rods are fixedly connected with the mounting mechanism.
Preferably, an elastic assembly III is arranged between the lower inner rod and the upper inner rod, sliding blocks are arranged on two sides of the upper inner rod and two sides of the lower inner rod, and the sliding blocks are connected with the outer barrel in a sliding mode through sliding grooves.
Preferably, the inside of mounting panel is provided with the mounting hole, and the mounting hole is provided with four, the central point department of putting of mounting panel is provided with the radiating groove.
Preferably, be provided with elastic component one between mounting panel and the protective housing, and elastic component one is provided with four, four the outside of elastic component one all is provided with the guide bar, and the one end of guide bar extends to the outside of mounting panel.
Preferably, the inside activity chamber that is used for fuselage displacement from top to bottom of offering of protective housing, be provided with the elastic component one that is used for adjusting the fuselage position between mounting panel and the protective housing, and elastic component one is provided with four, four the outside of elastic component one all is provided with the guide bar that is used for injecing the fuselage bottom position, and the one end of guide bar extends to the outside of mounting panel.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses in order to avoid the unmanned aerial vehicle organism to cause the organism inside impaired because produce vibrations with ground contact when landing, through fixing the installation mechanism that is used for the organism buffering in bottom of the body and fixing the supporting mechanism in installation mechanism bottom, play the effect of buffering and protection to unmanned aerial vehicle, earlier by supporting mechanism and ground contact when unmanned aerial vehicle descends, the elastic rod makes unmanned aerial vehicle more stable when landing under the elastic action of its own, be difficult for empting, one deck protective screen has more been added on supporting mechanism and installation mechanism's basis, make unmanned aerial vehicle's landing safer, the radiating groove can effectively dispel the heat to the unmanned aerial vehicle bottom, the protection unmanned aerial vehicle bottom that protective housing can be fine is not struck by hard foreign object and impaired, unmanned aerial vehicle's life has been improved.
2. The utility model discloses when supporting mechanism and ground contact cushioned the downward dynamics of assaulting of organism, lower interior pole and last interior pole played effectual cushioning effect to unmanned aerial vehicle's landing under the effect of elastic component three, the cooperation of slider and spout makes lower interior pole and last interior pole more steady smooth and easy at urceolus internalization, and connecting block and base are the rubber material, have certain cushioning effect, have played the effect of protection to the urceolus.
3. The utility model discloses can press the mounting panel to carry out the displacement when organism downstream, elastic component receives the extrusion and has played effectual buffering to the unmanned aerial vehicle body, unmanned aerial vehicle's safe descending has been guaranteed, the guide bar has played the effect of direction to the mounting panel, unmanned aerial vehicle contacts ground at first supporting mechanism and elastic rod after landing, buffering once, then the mounting panel is close to the movable slot under inertial effect, make the fixing base produce the linkage to the slide under the effect of connecting rod, make the slide extrude to two directions of elastic component, with the cooperation of elastic component, reach the effect of second grade buffering, the protection to the unmanned aerial vehicle body when having realized landing.
Drawings
FIG. 1 is an axial view of the overall structure of the present invention;
fig. 2 is a schematic view of the internal structure of the supporting mechanism of the present invention;
FIG. 3 is a schematic view of the internal structure of the mounting mechanism of the present invention;
fig. 4 is a schematic view of the top view structure of the connecting rod of the present invention.
In the figure: 1. an installation mechanism; 10. a fixed seat; 11. a movable groove; 12. mounting a plate; 13. a heat sink; 14. mounting holes; 15. a guide bar; 16. a first elastic component; 17. a second elastic component; 18. A slide base; 19. a connecting rod; 20. a protective housing; 2. a support mechanism; 21. an upper inner rod; 22. a third elastic component; 23. a lower inner rod; 24. a chute; 25. a slider; 26. an outer cylinder; 3. a base; 4. an elastic rod; 5. and (4) connecting the blocks.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.
In order to solve the technical problem that the unmanned aerial vehicle is easy to be damaged due to the fact that the support has no good buffering and protection effects when the unmanned aerial vehicle lands, please refer to fig. 1-4, the embodiment provides the following technical scheme:
the utility model provides an unmanned aerial vehicle buffering support for landing, including installation mechanism 1 and supporting mechanism 2, the below of installation mechanism 1 is provided with the supporting mechanism 2 that is used for unmanned aerial vehicle to descend the buffering, and supporting mechanism 2 is provided with four, supporting mechanism 2 includes interior pole 21 in the last, elastic component three 22, interior pole 23 in the lower, spout 24, slider 25 and urceolus 26, the inside of urceolus 26 is provided with interior pole 21 in the last, the below of interior pole 21 in the last is provided with interior pole 23 in the lower, the below of interior pole 23 in the lower is fixed and is provided with base 3, the top of interior pole 21 in the last is through connecting block 5 and installation mechanism 1 fixed connection, installation mechanism 1 includes fixing base 10, movable groove 11, mounting panel 12, radiating groove 13, mounting hole 14, guide bar 15, elastic component one 16, elastic component two 17, slide 18, connecting rod 19 and protective housing 20, protective housing 20's inside is provided with mounting panel 12 that is used for fixed fuselage bottom position, the lower fixed surface of mounting panel 12 is provided with fixing base 10, and fixing base 10 is provided with two, protective housing 20's bottom inner wall is provided with movable groove 11, and is provided with movable groove 11.
Specifically, installation mechanism 1 is used for installing with unmanned aerial vehicle, and play the effect of buffering and protection to unmanned aerial vehicle, supporting mechanism 2 has played effectual buffering to unmanned aerial vehicle's landing, connecting block 5 and base 3 are the rubber material, certain cushioning effect has, the effect of protection has been played outer tube 26, protective housing 20's shape has the open-ended rectangular channel for the bottom that is close to the organism, protective housing 20 can be fine the unmanned aerial vehicle bottom do not receive hard foreign object striking and impaired.
In order to solve the technical problem that the safety landing coefficient is low due to insufficient stability after the unmanned aerial vehicle lands, please refer to fig. 1, the embodiment provides the following technical solutions:
the outer sides of the four supporting mechanisms 2 are all provided with elastic rods 4, and the elastic rods 4 are fixedly connected with the mounting mechanism 1.
Specifically, elastic rod 4 adopts the carbon fiber pole, and elastic rod 4 is more stable when making unmanned aerial vehicle land under its elasticity effect itself, is difficult for empting, has added the one deck protective screen on supporting mechanism 2 and installation mechanism 1's basis more for unmanned aerial vehicle's landing is safer.
In order to solve the technical problem that the existing unmanned aerial vehicle cannot land stably due to poor buffering effect of the support when landing, please refer to fig. 2, the embodiment provides the following technical solutions:
an elastic component III 22 is arranged between the lower inner rod 23 and the upper inner rod 21, sliding blocks 25 are arranged on two sides of the upper inner rod 21 and the lower inner rod 23, and the sliding blocks 25 are connected with the outer cylinder 26 in a sliding mode through sliding grooves 24.
Specifically, the third elastic component 22 is a metal spring, the lower inner rod 23 and the upper inner rod 21 play an effective buffering role in landing of the unmanned aerial vehicle under the action of the third elastic component 22, and the lower inner rod 23 and the upper inner rod 21 move more stably and smoothly in the outer barrel 26 due to the cooperation of the sliding block 25 and the sliding groove 24.
In order to solve the technical problems that the unmanned aerial vehicle and the bracket are inconvenient to mount and the heat dissipation effect is poor, please refer to fig. 3, the embodiment provides the following technical scheme:
the mounting plate 12 is provided with four mounting holes 14 inside, and the central position of the mounting plate 12 is provided with a heat sink 13.
Specifically, set up on the organism with 14 matched with circular through-holes of mounting hole, mounting hole 14 is convenient for utilize the fastener to carry out fixed mounting to unmanned aerial vehicle, and the fastener can be that the bolt cooperates with the nut and carries out fastening connection, and is simple quick, when unmanned aerial vehicle descends, can avoid installation mechanism 1 to break away from the condition of unmanned aerial vehicle organism to take place, and radiating groove 13 can effectively dispel the heat to the unmanned aerial vehicle bottom.
In order to solve the technical problem that the unmanned aerial vehicle only depends on the supporting rod to buffer the effect when landing, please refer to fig. 3, the embodiment provides the following technical scheme:
the inside movable chamber that is used for fuselage displacement from top to bottom of offering of protective housing 20, be provided with the elastic component 16 that is used for adjusting the fuselage position between mounting panel 12 and the protective housing 20, and elastic component 16 is provided with four, the outside of four elastic component 16 all is provided with the guide bar 15 that is used for injecing the fuselage bottom position, and the outside of guide bar 15 extends to mounting panel 12, the inside of two movable grooves 11 all slides and is provided with slide 18, one side of slide 18 is fixed and is provided with elastic component two 17, the transmission is provided with connecting rod 19 between slide 18 and the fixing base 10.
It is specific, elastic component 16 is the rubber elastic material and makes, effectual buffering has been played to the unmanned aerial vehicle body, unmanned aerial vehicle's safe descending has been guaranteed, guide bar 15 has played the effect of direction to mounting panel 12, unmanned aerial vehicle contacts ground at first supporting mechanism 2 and elastic rod 4 after landing, cushion once, then mounting panel 12 is close to activity groove 11 under inertial effect, make fixing base 10 produce the linkage to slide 18 under connecting rod 19's effect, make slide 18 extrude to two 17 directions of elastic component, elastic component two 17 is compression spring, receive two 17 of extruded elastic component can cushion the decurrent impact force of organism under the effect of self elastic force, with the cooperation of elastic component 16, reach the effect of second grade buffering, the unmanned aerial vehicle body has effectively been protected.
In summary, the following steps: the utility model discloses in order to avoid the unmanned aerial vehicle organism to produce vibrations because of the contact with the ground when landing and cause the organism inside impaired, through fixing at the organism bottom and being used for organism buffering installation mechanism 1 and fixing at the supporting mechanism 2 of installation mechanism 1 bottom, play the effect of buffering and protection to unmanned aerial vehicle, when unmanned aerial vehicle descends, contact with the ground by supporting mechanism 2 first, elastic rod 4 makes unmanned aerial vehicle more stable when landing under its own elasticity, be difficult for toppling over, add one more layer of barrier on the basis of supporting mechanism 2 and installation mechanism 1, make unmanned aerial vehicle's landing safer, radiating groove 13 can carry out effective heat dissipation to unmanned aerial vehicle bottom, protective housing 20 can be fine protection unmanned aerial vehicle bottom not receive hard foreign object striking and impaired, unmanned aerial vehicle's life has been improved, when supporting mechanism 2 cushions the dynamics of organism downward impact with the ground contact, the lower inner rod 23 and the upper inner rod 21 play an effective buffering role on the landing of the unmanned aerial vehicle under the action of the third elastic component 22, the lower inner rod 23 and the upper inner rod 21 can move more stably and smoothly in the outer barrel 26 due to the cooperation of the sliding block 25 and the sliding groove 24, the connecting block 5 and the base 3 are made of rubber materials and have a certain buffering role, the outer barrel 26 is protected, the mounting plate 12 can be pressed to move when the unmanned aerial vehicle moves downwards, the first elastic component 16 is extruded to effectively buffer the unmanned aerial vehicle body, the safe landing of the unmanned aerial vehicle is ensured, the guide rod 15 plays a guiding role on the mounting plate 12, the unmanned aerial vehicle firstly contacts the ground by the support mechanism 2 and the elastic rod 4 after landing to perform primary buffering, and then the mounting plate 12 approaches to the movable groove 11 under the action of inertia, make fixing base 10 produce the linkage to slide 18 under connecting rod 19's effect for slide 18 extrudees to the second 17 directions of elastic component, with the cooperation of elastic component 16, reaches the effect of second grade buffering, has realized the protection to the unmanned aerial vehicle body when landing.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, 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.
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 lands with buffering support, includes installation mechanism (1) and supporting mechanism (2), its characterized in that: the lower part of the installation mechanism (1) is provided with a supporting mechanism (2) for landing buffering of the unmanned aerial vehicle, the supporting mechanism (2) is provided with four, the supporting mechanism (2) comprises an upper inner rod (21), an elastic component III (22), a lower inner rod (23), a sliding groove (24), a sliding block (25) and an outer barrel (26), the inner part of the outer barrel (26) is provided with the upper inner rod (21), the lower part of the upper inner rod (21) is provided with the lower inner rod (23), the lower part of the lower inner rod (23) is fixedly provided with a base (3), the upper part of the upper inner rod (21) is fixedly connected with the installation mechanism (1) through a connecting block (5), the installation mechanism (1) comprises a fixed seat (10), a movable groove (11), an installation plate (12), a heat dissipation groove (13), an installation hole (14), a guide rod (15), an elastic component I (16), an elastic component II (17), a sliding seat (18), a connecting rod (19) and a protective shell (20), the inner wall (10) is arranged in the protective shell (20), and two movable grooves (11) are arranged.
2. The buffer support for landing of the unmanned aerial vehicle of claim 1, wherein: the outer sides of the four supporting mechanisms (2) are provided with elastic rods (4), and the elastic rods (4) are fixedly connected with the mounting mechanism (1).
3. The buffer support for landing of the unmanned aerial vehicle of claim 1, wherein: an elastic component III (22) is arranged between the lower inner rod (23) and the upper inner rod (21), sliding blocks (25) are arranged on two sides of the upper inner rod (21) and the lower inner rod (23), and the sliding blocks (25) are connected with the outer barrel (26) in a sliding mode through sliding grooves (24).
4. The buffer support for landing of the unmanned aerial vehicle of claim 1, wherein: the inside of mounting panel (12) is provided with mounting hole (14), and mounting hole (14) are provided with four, the central point department of putting of mounting panel (12) is provided with radiating groove (13).
5. The buffer support for landing of the unmanned aerial vehicle of claim 1, wherein: the utility model discloses a fuselage, including protective housing (20), be provided with the movable chamber that is used for fuselage displacement from top to bottom in protective housing (20), be provided with between mounting panel (12) and protective housing (20) elastic component (16) that are used for adjusting the fuselage position, and elastic component (16) are provided with four, four the outside of elastic component (16) all is provided with guide bar (15) that are used for injecing the fuselage bottom position, and the one end of guide bar (15) extends to the outside of mounting panel (12).
6. The buffer support for landing of the unmanned aerial vehicle of claim 1, wherein: a sliding seat (18) is arranged in each of the two movable grooves (11) in a sliding mode, an elastic component II (17) is fixedly arranged on one side of the sliding seat (18), and a connecting rod (19) is arranged between the sliding seat (18) and the fixed seat (10) in a transmission mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221677223.8U CN217805246U (en) | 2022-07-01 | 2022-07-01 | Buffering support for landing of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221677223.8U CN217805246U (en) | 2022-07-01 | 2022-07-01 | Buffering support for landing of unmanned aerial vehicle |
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| CN217805246U true CN217805246U (en) | 2022-11-15 |
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| CN202221677223.8U Active CN217805246U (en) | 2022-07-01 | 2022-07-01 | Buffering support for landing of unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116692070A (en) * | 2023-07-28 | 2023-09-05 | 中冶建筑研究总院（深圳）有限公司 | Automatic intelligent hangar of coming back of unmanned aerial vehicle |
-
2022
- 2022-07-01 CN CN202221677223.8U patent/CN217805246U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116692070A (en) * | 2023-07-28 | 2023-09-05 | 中冶建筑研究总院（深圳）有限公司 | Automatic intelligent hangar of coming back of unmanned aerial vehicle |
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