CN217945507U - Antidetonation type unmanned aerial vehicle undercarriage - Google Patents
Antidetonation type unmanned aerial vehicle undercarriage Download PDFInfo
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- CN217945507U CN217945507U CN202221288877.1U CN202221288877U CN217945507U CN 217945507 U CN217945507 U CN 217945507U CN 202221288877 U CN202221288877 U CN 202221288877U CN 217945507 U CN217945507 U CN 217945507U
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- unmanned aerial
- aerial vehicle
- undercarriage
- fixed sleeve
- platform
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Abstract
The utility model discloses an antidetonation type unmanned aerial vehicle undercarriage, including the undercarriage main part, be equipped with the platform that rises and falls in the undercarriage main part, undercarriage main part lower extreme both sides all are equipped with the fixed sleeve, and evenly are equipped with the non-slip nail on the fixed sleeve, the fixed sleeve both ends all are connected with the locating lever, and the locating lever other end is equipped with fastening seat, all overlap on the locating lever and be equipped with the connecting seat, and all be connected with the supporting leg on the connecting seat, the supporting leg other end is connected with the platform that rises and falls, and one side between the supporting leg is connected with the connecting rod, the platform lower extreme that rises and falls is equipped with the fixed plate, and the fixed plate side evenly is connected with the bracing piece to the bracing piece other end is connected with the connecting rod. This antidetonation type unmanned aerial vehicle undercarriage can the efficient carry out antidetonation and handle, effectively prolongs the life of unmanned aerial vehicle undercarriage, avoids influencing unmanned aerial vehicle's use.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle undercarriage technical field specifically is an antidetonation type unmanned aerial vehicle undercarriage.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing radio remote control equipment and a self-contained program control device, has the advantages of small volume, low cost, convenient use, low requirement on the operation environment, strong battlefield viability and the like, and is widely applied to aerial reconnaissance, monitoring, communication, anti-diving, electronic interference and the like.
When current unmanned aerial vehicle used, it is steady that the environment that can not effectual guarantee rises and falls, generally speaking location processing through the unmanned aerial vehicle undercarriage, but unmanned aerial vehicle undercarriage when descending, the unmanned aerial vehicle undercarriage can receive great impact force, and unmanned aerial vehicle undercarriage antidetonation effect is not good, can influence the life of unmanned aerial vehicle undercarriage, and then influences unmanned aerial vehicle's the processing of rising and falling.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an antidetonation type unmanned aerial vehicle undercarriage to solve unmanned aerial vehicle on the existing market that above-mentioned background art provided when descending, the unmanned aerial vehicle undercarriage can receive great impact force, and unmanned aerial vehicle undercarriage antidetonation effect is not good, can influence the life of unmanned aerial vehicle undercarriage, and then influences unmanned aerial vehicle's the problem of handling that rises and falls.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an antidetonation type unmanned aerial vehicle undercarriage, includes the undercarriage main part, be equipped with the platform that rises and falls in the undercarriage main part, undercarriage main part lower extreme both sides all are equipped with the fixed sleeve, and evenly are equipped with the non-slip nail on the fixed sleeve, the fixed sleeve both ends all are connected with the locating lever, and the locating lever other end is equipped with fastening seat, all overlap on the locating lever and be equipped with the connecting seat, and all be connected with the supporting leg on the connecting seat, the supporting leg other end is connected with the platform that rises and falls, and one side between the supporting leg is connected with the connecting rod, the platform lower extreme that rises and falls is equipped with the fixed plate, and the fixed plate side evenly is connected with the bracing piece to the bracing piece other end is connected with the connecting rod.
Preferably, the two ends of the supporting rod are movably connected with the fixed plate and the connecting rod through rotating rods respectively, and a spring is fixed in the middle of the supporting rod through welding.
Preferably, the supporting rods and the supporting legs are arranged in an inclined mode, and a triangular structure is formed among the supporting rods, the supporting legs and the lifting platform.
Preferably, the positioning rod is movably connected with the connecting seat in a penetrating manner, and the positioning rod is fixed with the fixed sleeve through a threaded structure.
Preferably, the distance between the connecting seats is greater than the length of the fixing sleeve.
Preferably, the fixing sleeve is of a cylindrical structure, and the fixing sleeve and the anti-skid nails are of an integral structure.
Compared with the prior art, the beneficial effects of the utility model are that: this antidetonation type unmanned aerial vehicle undercarriage can the efficient carry out antidetonation and handle, effectively prolongs the life of unmanned aerial vehicle undercarriage, avoids influencing unmanned aerial vehicle's use. This antidetonation type unmanned aerial vehicle undercarriage carries out the bottom sprag through the fixed sleeve that has the tyre stud and handles, can effectively carry out the steady support in various topography and handle, improves the stability of unmanned aerial vehicle undercarriage to the unmanned aerial vehicle undercarriage of being convenient for carries out the antidetonation and handles.
Drawings
Fig. 1 is a schematic structural view of an anti-seismic landing gear of an unmanned aerial vehicle of the present invention;
fig. 2 is a side view of the anti-seismic landing gear of the unmanned aerial vehicle;
fig. 3 is the utility model relates to a fixed sleeve and connecting seat of antidetonation type unmanned aerial vehicle undercarriage pass through locating lever connection structure schematic diagram.
In the figure: 1. a landing gear body; 2. a landing platform; 3. a fixing plate; 4. a spring; 5. a support bar; 6. a connecting rod; 7. supporting legs; 8. anti-skid nails; 9. positioning a rod; 10. a connecting seat; 11. fixing the sleeve; 12. and a fastening seat.
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 work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: an anti-seismic landing gear of an unmanned aerial vehicle comprises a landing gear body 1, wherein a landing platform 2 is arranged on the landing gear body 1, two sides of the lower end of the landing gear body 1 are respectively provided with a fixing sleeve 11, anti-skid nails 8 are uniformly arranged on the fixing sleeves 11, two ends of the fixing sleeves 11 are respectively connected with a positioning rod 9, the other end of the positioning rod 9 is provided with a fastening seat 12, the fastening seats 12 play a role in limiting the end part of a connecting seat 10, the connecting seats 10 are respectively sleeved on the positioning rods 9, the positioning rods 9 are movably connected with the connecting seats 10 in a penetrating manner, the positioning rods 9 are fixed with the fixing sleeves 11 through thread structures, the connecting seats 10 can rotate relative to the positioning rods 9, so that the positioning rods 9 and the fixing sleeves 11 can rotate relative to the connecting seats 10, and the landing gear body 1 can be supported and processed by the fixing sleeves 11 when being placed, the fixing sleeve 11 can be used for grabbing processing through the anti-skid nails 8 on the side surface, the stability of the landing gear main body 1 is improved, the distance between the connecting seats 10 is larger than the length of the fixing sleeve 11, the structure can enable the connecting seats 10 to move relative to the fixing sleeve 11, the rotation processing of the fixing sleeve 11 and the positioning rod 9 relative to the connecting seats 10 is facilitated, the fixing sleeve 11 is of a cylindrical structure, the fixing sleeve 11 and the anti-skid nails 8 are of an integrated structure, the anti-skid nails 8 can reduce the contact area with a fixing surface through the tip structures of the end parts, the pressure of the anti-skid nails 8 on the fixing surface is increased, when the pressure is the same, the contact area is smaller, the pressure is larger, the fixing sleeve 11 is more stably supported on the fixing surface, the cylindrical structure of the fixing sleeve 11 can facilitate rolling processing, the connecting seats 10 are connected with the supporting legs 7, and the other ends of the supporting legs 7 are connected with the landing platform 2, and one side between the supporting leg 7 is connected with connecting rod 6, 2 lower extremes of platform that rises and falls are equipped with fixed plate 3, and 3 sides of fixed plate evenly are connected with bracing piece 5, bracing piece 5 both ends pass through bull stick swing joint with fixed plate 3 and connecting rod 6 respectively, and bracing piece 5 middle part has spring 4 through welded fastening, this structure makes bracing piece 5 can carry out the change of length through the extension of spring 4, thereby make platform 2 that rises and falls when receiving the impact force, bracing piece 7 can carry out shock resistance treatment through the effect of spring 4 on the bracing piece 5, improve the stability of platform 2 that rises and falls, bracing piece 5 changes the length back through the extension of spring 4, can rotate the processing to fixed plate 3 and connecting rod 6 relatively, bracing piece 5 and supporting leg 7 all incline the setting, and bracing piece 5, constitute the triangular structure between supporting leg 7 and the platform 2 that rises and falls, this structure can improve the steadiness of supporting leg 7 relative platform 2 that rises and falls, supporting leg 7 inclines to set up, can let platform 2 steadily place, and the bracing piece 5 other end is connected with connecting rod 6, connecting rod 6 can play the effect of connecting the firm to supporting leg 7 with one side.
The working principle is as follows: when using this antidetonation type unmanned aerial vehicle undercarriage, at first undercarriage main part 1 is placing subaerial time, fixing sleeve 11 passes through cleat 8 and stationary plane contact, improve undercarriage main part 1's steadiness, fixing sleeve 11 can rotate relative connecting seat 10 under the effect of locating lever 9 simultaneously, let fixing sleeve 11 can adjust suitable fixed position, fastening seat 12 plays the spacing effect of tip to connecting seat 10, after undercarriage main part 1 steadily places, when unmanned aerial vehicle rises and falls through landing platform 2, undercarriage main part 1 receives the impact force, landing platform 2 pushes down under the action of gravity, make landing platform 2 relative supporting leg 7 rotate, the relative landing platform 2's of supporting leg 7 contained angle increase this moment, and bracing piece 5 can receive tensile processing after the angle increase between supporting leg 7 and landing platform 2, bracing piece 5 carries out the change of length through the extension of spring 4, realize undercarriage main part 1's buffer processing, fixed plate 3 and connecting rod 6 make bracing piece 5 can carry out corresponding adjustment through rotating after changing length, thereby accomplish a series of work.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.
Claims (6)
1. The utility model provides an antidetonation type unmanned aerial vehicle undercarriage, includes undercarriage main part (1), be equipped with landing platform (2), its characterized in that on undercarriage main part (1): landing gear main part (1) lower extreme both sides all are equipped with fixed sleeve (11), and evenly are equipped with on fixed sleeve (11) anti-skidding nail (8), fixed sleeve (11) both ends all are connected with locating lever (9), and the locating lever (9) other end is equipped with fastening seat (12), all overlap on locating lever (9) and be equipped with connecting seat (10), and all be connected with supporting leg (7) on connecting seat (10), the supporting leg (7) other end is connected with the platform (2) of rising and falling, and one side between supporting leg (7) is connected with connecting rod (6), platform (2) lower extreme of rising and falling is equipped with fixed plate (3), and fixed plate (3) side evenly is connected with bracing piece (5) to the bracing piece (5) other end is connected with connecting rod (6).
2. An anti-seismic unmanned aerial vehicle landing gear according to claim 1, wherein: the two ends of the supporting rod (5) are respectively movably connected with the fixed plate (3) and the connecting rod (6) through rotating rods, and the middle of the supporting rod (5) is fixedly provided with a spring (4) through welding.
3. An anti-seismic unmanned aerial vehicle landing gear according to claim 1, wherein: the support rods (5) and the support legs (7) are all obliquely arranged, and a triangular structure is formed among the support rods (5), the support legs (7) and the lifting platform (2).
4. An anti-seismic unmanned aerial vehicle landing gear according to claim 1, wherein: the positioning rod (9) is movably connected with the connecting seat (10) in a penetrating way, and the positioning rod (9) is fixed with the fixed sleeve (11) through a thread structure.
5. An anti-seismic unmanned aerial vehicle landing gear according to claim 1, wherein: the distance between the connecting seats (10) is greater than the length of the fixed sleeve (11).
6. An anti-seismic landing gear for unmanned aerial vehicles according to claim 1, wherein: the fixed sleeve (11) is of a cylindrical structure, and the fixed sleeve (11) and the anti-skid nails (8) are of an integrated structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221288877.1U CN217945507U (en) | 2022-05-26 | 2022-05-26 | Antidetonation type unmanned aerial vehicle undercarriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221288877.1U CN217945507U (en) | 2022-05-26 | 2022-05-26 | Antidetonation type unmanned aerial vehicle undercarriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217945507U true CN217945507U (en) | 2022-12-02 |
Family
ID=84214206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221288877.1U Active CN217945507U (en) | 2022-05-26 | 2022-05-26 | Antidetonation type unmanned aerial vehicle undercarriage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217945507U (en) |
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2022
- 2022-05-26 CN CN202221288877.1U patent/CN217945507U/en active Active
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