CN213473498U - Collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle - Google Patents
Collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle Download PDFInfo
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- CN213473498U CN213473498U CN202021413919.0U CN202021413919U CN213473498U CN 213473498 U CN213473498 U CN 213473498U CN 202021413919 U CN202021413919 U CN 202021413919U CN 213473498 U CN213473498 U CN 213473498U
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- Prior art keywords
- aerial vehicle
- unmanned aerial
- telescopic link
- fixedly connected
- swing joint
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- 230000001681 protective effect Effects 0.000 claims abstract description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 2
- 238000010276 construction Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model discloses a collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle, including guardrail, bottom plate, fixed block, runner and protective housing, the bottom fixedly connected with revolution mechanic of bottom plate, and revolution mechanic's bottom swing joint has the second telescopic link, the bottom swing joint of second telescopic link has first telescopic link, and the bottom fixedly connected with fixed block of first telescopic link, and the bottom fixedly connected with protective housing of fixed block, the bottom swing joint of protective housing has the runner. The utility model discloses a swing joint has the pivot in one side of connecting block, and the pivot will be in the same place with two telescopic links of one side link together, and the pivot can be rotatory, and the pivot is rotatory just can drive the telescopic link rotatory, and the telescopic link of different one sides is not enough with same water flat line, and the telescopic link is rotatory just can folding device, and the fixed screw of pivot one side can the fixed rotating shaft to this reaches unmanned aerial vehicle support piece and can carries out folding purpose.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle accessory technical field specifically is a collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle.
Background
Unmanned aerial vehicle is unmanned aircraft's abbreviation, mainly utilizes radio remote control equipment, the program control of self-contained or by the unmanned aircraft of vehicle-mounted computer autonomy ground operation, and unmanned aerial vehicle can be used to take photo by plane, agricultural, plant protection, miniature auto heterodyne, express delivery transportation and disaster rescue etc. aspect, and unmanned aerial vehicle needs an unmanned aerial vehicle support piece to support unmanned aerial vehicle when not using.
In the process of implementing the present invention, the inventor finds that at least the following problems exist in the prior art and are not solved:
(1) the traditional unmanned aerial vehicle supporting piece is difficult to fold, and the device occupies space and is inconvenient to carry when not in use;
(2) the height of the traditional unmanned aerial vehicle support piece is difficult to adjust, and the device cannot adapt to different conditions;
(3) traditional unmanned aerial vehicle support piece is difficult to carry on spacingly to unmanned aerial vehicle, and when unmanned aerial vehicle did not use, unmanned aerial vehicle appeared the skew easily, probably dropped from the device, shined into the damage to unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle to it is difficult to fold, is difficult to adjusting device's height and is difficult to carry out spacing problem to unmanned aerial vehicle to provide unmanned aerial vehicle support piece in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle, includes guardrail, bottom plate, fixed block, runner and protective housing, the bottom fixedly connected with revolution mechanic of bottom plate, and revolution mechanic's bottom swing joint has the second telescopic link, the bottom swing joint of second telescopic link has first telescopic link, and the bottom fixedly connected with fixed block of first telescopic link, and the bottom fixedly connected with protective housing of fixed block, the bottom swing joint of protective housing has the runner, the equal fixedly connected with guardrail in both sides on bottom plate top, the top fixedly connected with limit structure of bottom plate, limit structure's bottom is provided with the recess.
Preferably, the top of fixed block is provided with the draw-in groove, the bottom of first telescopic link is provided with the fixture block, fixed block and first telescopic link constitute the block structure.
Preferably, pulleys are arranged on two sides of the first telescopic rod, sliding grooves are arranged on two sides of the interior of the second telescopic rod, and the first telescopic rod and the second telescopic rod form a sliding structure.
Preferably, fixed screw, connecting block and pivot have set gradually in revolution mechanic's inside, one side swing joint of connecting block has fixed screw, one side swing joint of connecting block has the pivot.
Preferably, threaded rod, connecting rod, limiting plate and mounting panel have set gradually in limit structure's inside, the one end fixedly connected with connecting rod of mounting panel, and the one end fixedly connected with limiting plate of connecting rod, the one end swing joint of limiting plate has the threaded rod.
Preferably, the outer side wall of the threaded rod is evenly provided with external threads, the inner side wall of the mounting plate is evenly provided with internal threads matched with the external threads, and the threaded rod is in threaded connection with the mounting plate.
Compared with the prior art, the beneficial effects of the utility model are that: the foldable unmanned aerial vehicle support piece for the unmanned aerial vehicle not only achieves the purpose that the unmanned aerial vehicle support piece can be folded, achieves the purpose that the height of the unmanned aerial vehicle support piece is convenient to adjust, but also achieves the purpose that the unmanned aerial vehicle support piece can limit the position of the unmanned aerial vehicle;
(1) the rotating shaft is movably connected to one side of the connecting block and connects the two telescopic rods on the same side together, the rotating shaft can rotate, the rotating shaft can drive the telescopic rods to rotate, the telescopic rods on different sides are not in the same horizontal line, the telescopic rods can be folded by rotating, and the rotating shaft can be fixed by the fixing screws on one side of the rotating shaft, so that the purpose that the unmanned aerial vehicle supporting piece can be folded is achieved;
(2) the bottom end of the second telescopic rod is movably connected with the first telescopic rod, the first telescopic rod and the second telescopic rod form a sliding structure, the first telescopic rod can slide in the second telescopic rod, the overall height of the device can be adjusted by sliding the first telescopic rod, and when the device is adjusted to a proper height, the first telescopic rod can be fixed by screwing a screw, so that the purpose that the height of the unmanned aerial vehicle support piece is convenient to adjust is achieved;
(3) be provided with the limiting plate through the one end at the mounting panel, connect through threaded rod and connecting rod between limiting plate and the mounting panel, threaded rod and mounting panel constitute threaded connection, twist the limiting plate that the threaded rod just can drive threaded rod one end and remove, the limiting plate removes and just can fix unmanned aerial vehicle in the centre through two subtend limiting plates, limiting plate and recess constitute sliding construction, the connecting rod can stretch out and draw back, connecting rod and recess can fix a position the limiting plate, prevent that the skew from appearing in the limiting plate, reach here that unmanned aerial vehicle support piece can carry out spacing purpose to unmanned aerial vehicle.
Drawings
Fig. 1 is a schematic front view of a cross-sectional structure of the present invention;
fig. 2 is a schematic side view of the cross-sectional structure of the present invention;
fig. 3 is an enlarged partial sectional view of the utility model at a in fig. 1;
fig. 4 is a schematic top view of the cross-sectional structure of the present invention;
fig. 5 is a schematic view of the front view cross section of the runner of the present invention.
In the figure: 1. a guardrail; 2. a base plate; 3. a fixed block; 4. a rotating wheel; 5. a protective shell; 6. a first telescopic rod; 7. a second telescopic rod; 8. a rotating structure; 801. fixing screws; 802. connecting blocks; 803. a rotating shaft; 9. a limiting structure; 901. a threaded rod; 902. a connecting rod; 903. a limiting plate; 904. mounting a plate; 10. and (4) a groove.
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. 1-5, the present invention provides an embodiment: a foldable unmanned aerial vehicle support for an unmanned aerial vehicle comprises a guardrail 1, a bottom plate 2, a fixing block 3, a rotating wheel 4 and a protective shell 5, wherein the bottom end of the bottom plate 2 is fixedly connected with a rotating structure 8, a fixing screw 801, a connecting block 802 and a rotating shaft 803 are sequentially arranged in the rotating structure 8, one side of the connecting block 802 is movably connected with the fixing screw 801, and one side of the connecting block 802 is movably connected with the rotating shaft 803;
specifically, as shown in fig. 1 and fig. 2, when the structure is used, firstly, the rotating shaft 803 connects two telescopic rods on the same side together, the rotating shaft 803 can rotate, the rotating shaft 803 rotates to drive the telescopic rods to rotate, the telescopic rods on different sides are not on the same horizontal line, the telescopic rods rotate to fold the device, and the fixing screw 801 on one side of the rotating shaft 803 can fix the rotating shaft 803;
the bottom end of the rotating structure 8 is movably connected with a second telescopic rod 7, the bottom end of the second telescopic rod 7 is movably connected with a first telescopic rod 6, pulleys are arranged on two sides of the first telescopic rod 6, sliding grooves are arranged on two sides of the inner part of the second telescopic rod 7, and the first telescopic rod 6 and the second telescopic rod 7 form a sliding structure;
the bottom end of the first telescopic rod 6 is fixedly connected with the fixed block 3, the top end of the fixed block 3 is provided with a clamping groove, the bottom end of the first telescopic rod 6 is provided with a clamping block, and the fixed block 3 and the first telescopic rod 6 form a clamping structure;
the bottom end of the fixed block 3 is fixedly connected with a protective shell 5, the bottom end of the protective shell 5 is movably connected with a rotating wheel 4, two sides of the top end of the bottom plate 2 are fixedly connected with guardrails 1, the top end of the bottom plate 2 is fixedly connected with a limiting structure 9, a threaded rod 901, a connecting rod 902, a limiting plate 903 and a mounting plate 904 are sequentially arranged in the limiting structure 9, one end of the mounting plate 904 is fixedly connected with the connecting rod 902, one end of the connecting rod 902 is fixedly connected with the limiting plate 903, one end of the limiting plate 903 is movably connected with the threaded rod 901, external threads are uniformly arranged on the outer side wall of the threaded rod 901, internal threads matched with the external threads are uniformly arranged on the inner side wall of;
specifically, as shown in fig. 1, fig. 2 and fig. 4, when using this structure, at first connect through threaded rod 901 and connecting rod 902 between limiting plate 903 and the mounting panel 904, threaded rod 901 and mounting panel 904 constitute threaded connection, it just can drive the limiting plate 903 of threaded rod 901 one end to twist threaded rod 901 and remove, limiting plate 903 removes just can fix unmanned aerial vehicle in the middle of through two subtend limiting plate 903, limiting plate 903 and recess 10 constitute sliding structure, connecting rod 902 can stretch out and draw back, connecting rod 902 and recess 10 can fix a position limiting plate 903, prevent that limiting plate 903 from appearing the skew.
The working principle is as follows: the utility model discloses when using, at first, have pivot 803 through one side swing joint at connecting block 802, pivot 803 links together two telescopic links with one side, and pivot 803 can rotate, and pivot 803 is rotatory just can drive the telescopic link rotatory, and the telescopic link of different one sides is not enough same water flat line, and the telescopic link is rotatory just can folding device, and the fixed screw 801 of pivot 803 one side can fixed rotating shaft 803 to this reaches unmanned aerial vehicle support piece and can carries out folding purpose.
Afterwards, there is first telescopic link 6 through the bottom swing joint at second telescopic link 7, first telescopic link 6 and second telescopic link 7 constitute sliding structure, first telescopic link 6 can slide in second telescopic link 7 is inside, first telescopic link 6 slides just can adjusting device's whole height, when the device adjusts to suitable height, it just can fix first telescopic link 6 to screw up the screw, reach the mesh that unmanned aerial vehicle support piece is convenient for adjusting device's height with this.
Finally, one end through at mounting panel 904 is provided with limiting plate 903, connect through threaded rod 901 and connecting rod 902 between limiting plate 903 and the mounting panel 904, threaded rod 901 and mounting panel 904 constitute threaded connection, it just can drive the limiting plate 903 of threaded rod 901 one end to twist threaded rod 901 and remove, limiting plate 903 removes just can fix unmanned aerial vehicle in the middle through two subtend limiting plate 903, limiting plate 903 and recess 10 constitute sliding construction, connecting rod 902 can stretch out and draw back, connecting rod 902 and recess 10 can fix a position limiting plate 903, prevent that the skew from appearing in limiting plate 903, thereby it can carry out spacing purpose to unmanned aerial vehicle to reach unmanned aerial vehicle support piece.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides a collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle, includes guardrail (1), bottom plate (2), fixed block (3), runner (4) and protective housing (5), its characterized in that: the bottom fixedly connected with revolution mechanic (8) of bottom plate (2), and the bottom swing joint of revolution mechanic (8) has second telescopic link (7), the bottom swing joint of second telescopic link (7) has first telescopic link (6), and the bottom fixedly connected with fixed block (3) of first telescopic link (6), and the bottom fixedly connected with protective housing (5) of fixed block (3), the bottom swing joint of protective housing (5) has runner (4), the equal fixedly connected with guardrail (1) in both sides on bottom plate (2) top, the top fixedly connected with limit structure (9) of bottom plate (2), the bottom of limit structure (9) is provided with recess (10).
2. The foldable unmanned aerial vehicle support of claim 1, wherein: the top of fixed block (3) is provided with the draw-in groove, the bottom of first telescopic link (6) is provided with the fixture block, fixed block (3) and first telescopic link (6) constitute the block structure.
3. The foldable unmanned aerial vehicle support of claim 1, wherein: the two sides of the first telescopic rod (6) are provided with pulleys, the two sides of the interior of the second telescopic rod (7) are provided with sliding grooves, and the first telescopic rod (6) and the second telescopic rod (7) form a sliding structure.
4. The foldable unmanned aerial vehicle support of claim 1, wherein: the inside of revolution mechanic (8) has set gradually fixed screw (801), connecting block (802) and pivot (803), one side swing joint of connecting block (802) has fixed screw (801), one side swing joint of connecting block (802) has pivot (803).
5. The foldable unmanned aerial vehicle support of claim 1, wherein: threaded rod (901), connecting rod (902), limiting plate (903) and mounting panel (904) have set gradually in the inside of limit structure (9), the one end fixedly connected with connecting rod (902) of mounting panel (904), and the one end fixedly connected with limiting plate (903) of connecting rod (902), the one end swing joint of limiting plate (903) has threaded rod (901).
6. The foldable unmanned aerial vehicle support of claim 5, wherein: the outer side wall of the threaded rod (901) is uniformly provided with external threads, the inner side wall of the mounting plate (904) is uniformly provided with internal threads matched with the external threads, and the threaded rod (901) is in threaded connection with the mounting plate (904).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021413919.0U CN213473498U (en) | 2020-07-17 | 2020-07-17 | Collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202021413919.0U CN213473498U (en) | 2020-07-17 | 2020-07-17 | Collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
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CN213473498U true CN213473498U (en) | 2021-06-18 |
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ID=76358777
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202021413919.0U Expired - Fee Related CN213473498U (en) | 2020-07-17 | 2020-07-17 | Collapsible unmanned aerial vehicle support piece for unmanned aerial vehicle |
Country Status (1)
Country | Link |
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CN (1) | CN213473498U (en) |
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2020
- 2020-07-17 CN CN202021413919.0U patent/CN213473498U/en not_active Expired - Fee Related
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GR01 | Patent grant | ||
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CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210618 |
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CF01 | Termination of patent right due to non-payment of annual fee |