CN215622662U - Effectual unmanned aerial vehicle foot rest of shock attenuation - Google Patents
Effectual unmanned aerial vehicle foot rest of shock attenuation Download PDFInfo
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- CN215622662U CN215622662U CN202121241035.6U CN202121241035U CN215622662U CN 215622662 U CN215622662 U CN 215622662U CN 202121241035 U CN202121241035 U CN 202121241035U CN 215622662 U CN215622662 U CN 215622662U
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- unmanned aerial
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle foot stool with a good damping effect, which comprises a base, wherein a first limiting rod is fixedly connected inside the base, the outer wall of the first limiting rod is movably connected with a first spring, one end of the first limiting rod is fixedly connected with a buffer table, and the top of the base is fixedly connected with a sleeve. This effectual unmanned aerial vehicle foot rest shock attenuation effect of shock attenuation is better, the buffering effect of the device of being convenient for when descending is better, reduce the vibrations of fuselage, make the fuselage internals can not damage because of vibrations, the shock attenuation effect of device has been increased, make the device portable, and the device is convenient for fold, make area less when not using, and be convenient for carry and carry the device, reduce the degree of difficulty of transport, make the device be convenient for adjust, make the highly convenient to adjust that the device supported, be convenient for change the fuselage high end when descending, be convenient for increase the suitability of device, make the use that is applicable to more class unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle foot rest with a good damping effect.
Background
A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is applied in industries, is really just needed by the unmanned aerial vehicle, is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like at present, greatly expands the application of the unmanned aerial vehicle, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.
Many shock attenuation effects of unmanned aerial vehicle foot rest on the existing market are relatively poor, and the device of not being convenient for buffering when descending can not reduce the vibrations of fuselage for the fuselage internals can damage because of vibrations, has reduced the shock attenuation effect of device.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Aiming at the defects of the prior art, the utility model provides the unmanned aerial vehicle foot rest with good damping effect, which has the advantages of good damping effect and the like, and solves the problem of poor damping effect of the general unmanned aerial vehicle foot rest.
(II) technical scheme
In order to achieve the purpose of good damping effect, the utility model provides the following technical scheme: an unmanned aerial vehicle foot rest with a good damping effect comprises a base, wherein a first limiting rod is fixedly connected inside the base, a first spring is movably connected to the outer wall of the first limiting rod, one end of the first limiting rod is fixedly connected with a buffer table, a sleeve is fixedly connected to the top of the base, a rotating shaft is movably connected to the outer wall of the sleeve, a supporting rod is movably connected to the outer wall of the rotating shaft, one end of the supporting rod is fixedly connected with a supporting seat, and a sponge pad is fixedly connected to the top of the supporting seat;
the bottom fixedly connected with connecting block of base, the bottom fixedly connected with connecting rod of connecting block, the one end fixedly connected with loop bar of connecting rod, the bottom swing joint of loop bar has the heel brace, the positive swing joint of heel brace has the loose axle, the outer wall swing joint of loose axle has the regulation pole, the outer wall fixedly connected with second gag lever post of regulation pole, the outer wall swing joint of second gag lever post has the second spring, the one end fixedly connected with button of second gag lever post, spacing hole has been seted up in the front of loop bar.
Preferably, the first limiting rod is symmetrical to each other along the central line of the base, and the height of the first limiting rod is equal to the inner height of the base, so that the buffer table is convenient to support, the damping effect is better, and the vibration amplitude is convenient to limit.
Preferably, the diameter of the buffering table is equal to the inner diameter of the base, so that a buffering space is provided conveniently, and the damping effect is increased conveniently.
Preferably, the bracing piece is symmetrical each other along the mid point of base, and the quantity of bracing piece is four for it is more firm to support, and is convenient for descend unmanned aerial vehicle.
Preferably, the loose axle runs through the heel brace and adjusts pole swing joint for can not incline and collapse, influence unmanned aerial vehicle's reduction and put.
Preferably, the outer wall of the adjusting rod is movably connected with the inner wall of the loop bar, and the loop bar is symmetrical to each other along the connecting block, so that the support can be adjusted conveniently, and the adjustment is more convenient.
Preferably, the second limiting rod penetrates through the limiting hole and is fixedly connected with one side of the button, so that the length of the adjusting rod is limited conveniently, and the position is fixed.
(III) advantageous effects
Compared with the prior art, the utility model provides an unmanned aerial vehicle foot rest with a good damping effect, which has the following beneficial effects:
1. this effectual unmanned aerial vehicle foot rest of shock attenuation, through the use of mutually supporting of base, first gag lever post, first spring, cushion stage, sleeve, pivot, bracing piece, supporting seat and foam-rubber cushion for the device shock attenuation effect is better, and the device of being convenient for is better at the buffering effect when descending, reduces the vibrations of fuselage, makes the fuselage internals can not damage because of vibrations, has increased the shock attenuation effect of device.
2. This effectual unmanned aerial vehicle foot rest of shock attenuation uses through mutually supporting of sleeve, pivot, bracing piece, supporting seat, foam-rubber cushion, connecting block, connecting rod, loop bar, heel brace and loose axle for device portable, and the device is convenient for fold, makes area less when not using, and is convenient for carry and carry the device, reduces the degree of difficulty of transport, makes the practicality of device higher.
3. This effectual unmanned aerial vehicle foot rest of shock attenuation, through the use of mutually supporting of loop bar, heel brace, loose axle, regulation pole, second gag lever post, second spring, button and spacing hole for the device is convenient for adjust, makes the highly convenient for adjustment of device support, and the high end when being convenient for change fuselage descending is convenient for increase the suitability of device, makes the use that is applicable to more type unmanned aerial vehicle.
Drawings
FIG. 1 is a front cross-sectional view of the present invention;
FIG. 2 is a top view of the present invention;
FIG. 3 is an enlarged view of the utility model at A;
fig. 4 is a schematic front view of the present invention.
In the figure: 1. a base; 2. a first limit rod; 3. a first spring; 4. a buffer table; 5. a sleeve; 6. a rotating shaft; 7. a support bar; 8. a supporting seat; 9. a sponge cushion; 10. connecting blocks; 11. a connecting rod; 12. a loop bar; 13. a foot support; 14. a movable shaft; 15. adjusting a rod; 16. a second limiting rod; 17. a second spring; 18. a button; 19. and a limiting hole.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, an unmanned aerial vehicle foot rest with good damping effect comprises a base 1, a first limiting rod 2 is fixedly connected inside the base 1, a first spring 3 is movably connected to the outer wall of the first limiting rod 2, a buffering table 4 is fixedly connected to one end of the first limiting rod 2, a sleeve 5 is fixedly connected to the top of the base 1, a rotating shaft 6 is movably connected to the outer wall of the rotating shaft 5, a supporting rod 7 is movably connected to the outer wall of the rotating shaft 6, a supporting seat 8 is fixedly connected to one end of the supporting rod 7, a sponge pad 9 is fixedly connected to the top of the supporting seat 8, and the damping effect of the unmanned aerial vehicle foot rest is better due to the mutual matching use of the base 1, the first limiting rod 2, the first spring 3, the buffering table 4, the sleeve 5, the rotating shaft 6, the supporting rod 7, the supporting seat 8 and the sponge pad 9, so that the damping effect of the unmanned aerial vehicle is better when the unmanned aerial vehicle descends, and the vibration of the vehicle body is reduced, the internal parts of the machine body can not be damaged due to vibration, and the damping effect of the device is improved;
the bottom of the base 1 is fixedly connected with a connecting block 10, the bottom of the connecting block 10 is fixedly connected with a connecting rod 11, one end of the connecting rod 11 is fixedly connected with a loop bar 12, the bottom of the loop bar 12 is movably connected with a foot support 13, the front of the foot support 13 is movably connected with a movable shaft 14, the sleeve 5, the rotating shaft 6, a supporting rod 7, a supporting seat 8, a sponge cushion 9, the connecting block 10, the connecting rod 11, the loop bar 12, the foot support 13 and the movable shaft 14 are mutually matched for use, so that the device is convenient to carry, the device is convenient to fold, the occupied area is small when the device is not used, the device is convenient to carry and transport, the difficulty of transport is reduced, the practicability of the device is higher, the outer wall of the movable shaft 14 is movably connected with an adjusting rod 15, the outer wall of the adjusting rod 15 is fixedly connected with a second limiting rod 16, and the outer wall of the second limiting rod 16 is movably connected with a second spring 17, one end of the second limiting rod 16 is fixedly connected with a button 18, the front of the loop bar 12 is provided with a limiting hole 19, the loop bar 12, the foot support 13, the movable shaft 14, the adjusting rod 15, the second limiting rod 16, the second spring 17, the button 18 and the limiting hole 19 are mutually matched for use, so that the device is convenient to adjust, the height of the device support is convenient to adjust, the high bottom of the machine body during landing is convenient to change, the applicability of the device is convenient to increase, the device is suitable for being used in more unmanned aerial vehicles, the first limiting rods 2 are mutually symmetrical along the center line of the base 1, the height of the first limiting rods 2 is equal to the internal height of the base 1, the buffer table 4 is convenient to support, the damping effect is better, the vibration amplitude is convenient to be limited, the diameter of the buffer table 4 is equal to the internal diameter of the base 1, the buffering space is convenient to provide, the damping effect is convenient to increase, the supporting rods 7 are mutually symmetrical along the middle point of the base 1, and the quantity of bracing piece 7 is four, make the support more firm, and be convenient for descend unmanned aerial vehicle, loose axle 14 runs through heel brace 13 and adjusts pole 15 swing joint, make can not incline and collapse, influence unmanned aerial vehicle's reduction and put, adjust the outer wall of pole 15 and the inner wall swing joint of loop bar 12, and loop bar 12 is symmetrical each other along connecting block 10, be convenient for to the regulation of support, make the regulation more convenient, second gag lever post 16 runs through one side fixed connection of spacing hole 19 and button 18, be convenient for to the restriction of adjusting lever 15 length, make the position more fixed.
The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.
When using, unmanned aerial vehicle descends on cushion table 4, and because of the weight influence when descending, make first spring 3 compress and first gag lever post 2 restriction compression degree, make the vibrations when descending reduce, and sleeve 5 is convenient for provide the buffer space of cushion table 4, foam-rubber cushion 9 is convenient for cushion the fuselage, adjustment button 18, make second gag lever post 16 compress, and make the length in loop bar 12 inside of adjusting pole 15 of being convenient for adjust, the influence of second spring 17 elasticity, make second gag lever post 16 extension, and button 18 is convenient for run through spacing hole 19, and adjust pole 15 and be convenient for fix inside loop bar 12, when not using, bracing piece 7 revolute axle 6 is convenient for fold, make bracing piece 7 and base 1 mutually perpendicular, and heel brace 13 is convenient for fold around loose axle 14, and the device is convenient for fold, make the occupation of land space reduce.
To sum up, this effectual unmanned aerial vehicle foot rest shock attenuation effect of shock attenuation is better, the buffering effect of the device of being convenient for when descending is better, reduce the vibrations of fuselage, make the fuselage internals can not damage because of vibrations, the shock attenuation effect of device has been increased, make the device portable, and the device is convenient for fold, make area when not using less, and be convenient for carry and carry the device, reduce the degree of difficulty of transport, make the practicality of device higher, make the device be convenient for adjust, make the highly convenient to adjust that the device supported, the high end when being convenient for change the fuselage descend, be convenient for increase the suitability of device, make the use that is applicable to more type unmanned aerial vehicle.
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 utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an effectual unmanned aerial vehicle foot rest of shock attenuation, includes base (1), its characterized in that: a first limiting rod (2) is fixedly connected to the inside of the base (1), a first spring (3) is movably connected to the outer wall of the first limiting rod (2), a buffer table (4) is fixedly connected to one end of the first limiting rod (2), a sleeve (5) is fixedly connected to the top of the base (1), a rotating shaft (6) is movably connected to the outer wall of the sleeve (5), a supporting rod (7) is movably connected to the outer wall of the rotating shaft (6), a supporting seat (8) is fixedly connected to one end of the supporting rod (7), and a sponge pad (9) is fixedly connected to the top of the supporting seat (8);
the utility model discloses a quick-witted support structure, including base (1), bottom fixedly connected with connecting block (10), the bottom fixedly connected with connecting rod (11) of connecting block (10), the one end fixedly connected with loop bar (12) of connecting rod (11), the bottom swing joint of loop bar (12) has heel brace (13), the positive swing joint of heel brace (13) has loose axle (14), the outer wall swing joint of loose axle (14) has regulation pole (15), the outer wall fixedly connected with second gag lever post (16) of adjusting pole (15), the outer wall swing joint of second gag lever post (16) has second spring (17), the one end fixedly connected with button (18) of second gag lever post (16), spacing hole (19) have been seted up in the front of loop bar (12).
2. The unmanned aerial vehicle foot rest of claim 1, characterized in that: the first limiting rods (2) are symmetrical to each other along the center line of the base (1), and the height of the first limiting rods (2) is equal to the inner height of the base (1).
3. The unmanned aerial vehicle foot rest of claim 1, characterized in that: the diameter of the buffer table (4) is equal to the inner diameter of the base (1).
4. The unmanned aerial vehicle foot rest of claim 1, characterized in that: the supporting rods (7) are symmetrical to each other along the middle point of the base (1), and the number of the supporting rods (7) is four.
5. The unmanned aerial vehicle foot rest of claim 1, characterized in that: the movable shaft (14) penetrates through the foot support (13) and is movably connected with the adjusting rod (15).
6. The unmanned aerial vehicle foot rest of claim 1, characterized in that: the outer wall of the adjusting rod (15) is movably connected with the inner wall of the loop bar (12), and the loop bar (12) is mutually symmetrical along the connecting block (10).
7. The unmanned aerial vehicle foot rest of claim 1, characterized in that: the second limiting rod (16) penetrates through the limiting hole (19) and is fixedly connected with one side of the button (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121241035.6U CN215622662U (en) | 2021-06-04 | 2021-06-04 | Effectual unmanned aerial vehicle foot rest of shock attenuation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121241035.6U CN215622662U (en) | 2021-06-04 | 2021-06-04 | Effectual unmanned aerial vehicle foot rest of shock attenuation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215622662U true CN215622662U (en) | 2022-01-25 |
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ID=79941513
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121241035.6U Expired - Fee Related CN215622662U (en) | 2021-06-04 | 2021-06-04 | Effectual unmanned aerial vehicle foot rest of shock attenuation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215622662U (en) |
-
2021
- 2021-06-04 CN CN202121241035.6U patent/CN215622662U/en not_active Expired - Fee Related
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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 |
Granted publication date: 20220125 |
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| CF01 | Termination of patent right due to non-payment of annual fee |