CN212267857U - Unmanned aerial vehicle carrier and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle carrier and unmanned aerial vehicle Download PDFInfo
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- CN212267857U CN212267857U CN201921650760.1U CN201921650760U CN212267857U CN 212267857 U CN212267857 U CN 212267857U CN 201921650760 U CN201921650760 U CN 201921650760U CN 212267857 U CN212267857 U CN 212267857U
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Abstract
The utility model belongs to the technical field of the aircraft, especially, unmanned aerial vehicle carrier and unmanned aerial vehicle, to the inconvenient different width article problems of centre gripping of current unmanned aerial vehicle carrier, the following scheme is proposed at present, unmanned aerial vehicle carrier wherein includes the arc, the equal fixedly connected with descending support column in bottom both sides of arc, one side that two descending support columns are close to each other is rotated and is connected with same threaded rod, corresponding descending support column and fixedly connected with knob are run through at the both ends of threaded rod, and one side swing joint that one end that two knobs are close to each other kept away from each other with two descending support columns respectively, the outside thread bush of threaded rod is equipped with the cardboard that two symmetries set up. The utility model has the advantages of reasonable design, this unmanned aerial vehicle carrier can be convenient, firm grasp the article of different width, and conveniently connect in the bottom side position in unmanned aerial vehicle cabin, and this carrier plays the guard action to unmanned aerial vehicle cabin and article.
Description
Technical Field
The utility model relates to an aircraft technical field especially relates to an unmanned aerial vehicle carrier and unmanned aerial vehicle.
Background
An unmanned plane is called an unmanned plane for short, and is a flying device operated by utilizing a radio remote control device and a self-contained program control device. Through retrieval, chinese patent with publication No. CN208325659U discloses an unmanned aerial vehicle carrier and an unmanned aerial vehicle, wherein the unmanned aerial vehicle carrier includes: the containing device is used for loading carried articles, and the fixed groove body is connected with the containing device; be provided with the elasticity notch on the fixed cell body, the cooperation of elasticity notch and unmanned aerial vehicle's descending support frame, but the joint is fixed in unmanned aerial vehicle's descending support frame. Through this unmanned aerial vehicle carrier, it is inconvenient to have alleviated the carrying on operation equipment that unmanned aerial vehicle exists, is difficult to the technical problem in the nimble operation of being applied to the difference.
But above-mentioned design still has the weak point, and the unmanned aerial vehicle carrier structural design of above-mentioned design is not reasonable enough, and the article of the different width of inconvenient centre gripping, therefore we have proposed an unmanned aerial vehicle carrier and unmanned aerial vehicle and are used for solving above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming of the inconvenient different width article of centre gripping of current unmanned aerial vehicle carrier, and an unmanned aerial vehicle carrier and unmanned aerial vehicle that propose.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle carrier, includes the arc, the equal fixedly connected with descending support column in bottom both sides of arc, one side that two descending support columns are close to each other is rotated and is connected with same threaded rod, corresponding descending support column and fixedly connected with knob are run through at the both ends of threaded rod, and one side swing joint that one end that two knobs are close to each other was kept away from with two descending support columns respectively each other, the outside thread bush of threaded rod is equipped with the cardboard that two symmetries set up, and the equal fixedly connected with bayonet lock in one side bottom that two cardboards are close to each other, the outside movable sleeve of threaded rod is equipped with the limiting plate, limiting plate fixed connection is on the arc, the.
Preferably, the outside of threaded rod is equipped with two sets of external screw threads, cardboard and corresponding external screw thread mesh mutually, and the screw thread of two external screw threads is turned to oppositely, and the pitch of two external screw threads is the same for the threaded rod can drive splint and remove back to back when rotatory.
Preferably, the fixed cover in the outside of threaded rod is equipped with the baffle, and one side that two baffles kept away from each other respectively with two descending support columns one side swing joint that are close to each other, the baffle is used for supporting the inboard position of descending support column, effectively avoids descending support column to take place bending deformation to the inboard.
Preferably, the bottom both sides of arc all are provided with the mounting hole, and threaded connection has the screw in the mounting hole, conveniently with this carrier fixed mounting in unmanned aerial vehicle cabin bottom.
Preferably, the rotation hole has all been seted up to one side that two descending support columns are close to each other, threaded rod and rotation hole swing joint conveniently alternate the threaded rod between two descending support columns.
The utility model discloses in still provide an unmanned aerial vehicle, include the unmanned aerial vehicle body and as above-mentioned unmanned aerial vehicle carrier, the unmanned aerial vehicle carrier passes through the bottom side of screw fixed connection at the unmanned aerial vehicle body.
In the utility model, the screw hole is arranged at the bottom of the cabin of the unmanned aerial vehicle body, and the screw is screwed into the screw hole, so that the unmanned aerial vehicle carrier can be fixed on the unmanned aerial vehicle body;
the unmanned aerial vehicle carrier in the utility model is provided with a clamping groove with the position matched with the clamping pin in advance at the outer side of an article to be carried, the article to be carried is arranged between two clamping plates, one knob is rotated to drive the knob to drive the threaded rod to rotate, the threaded rod drives the two clamping plates to clamp the article to be carried when rotating, the clamping pin is aligned with the clamping groove, the article to be carried can be stably clamped between the two clamping plates, and when the clamping plates are moved to different positions, the article with different widths can be conveniently clamped;
the utility model has the advantages of reasonable design, this unmanned aerial vehicle carrier can be convenient, firm grasp the article of different width, and conveniently connect in the bottom side position in unmanned aerial vehicle cabin, and this carrier plays the guard action to unmanned aerial vehicle cabin and article.
Drawings
Fig. 1 is a schematic structural view of an unmanned aerial vehicle carrier according to the present invention;
fig. 2 is a schematic structural view of a portion a of an unmanned aerial vehicle carrier according to the present invention;
fig. 3 is the utility model provides an unmanned aerial vehicle's structural schematic.
In the figure: 1. an arc-shaped plate; 2. descending the support column; 3. a threaded rod; 4. a knob; 5. clamping a plate; 6. a limiting plate; 7. a baffle plate; 8. a bayonet lock; 9. mounting holes; 10. a screw; 11. the hole is rotated.
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.
Referring to fig. 1-2, the utility model provides an unmanned aerial vehicle carrier, including arc 1, the equal fixedly connected with descending support column 2 in bottom both sides of arc 1, one side that two descending support columns 2 are close to each other is rotated and is connected with same threaded rod 3, corresponding descending support column 2 and fixedly connected with knob 4 are run through at the both ends of threaded rod 3, and one side swing joint that one end that two knob 4 are close to each other was kept away from with two descending support column 2 respectively each other, the outside thread bush of threaded rod 3 is equipped with cardboard 5 that two symmetries set up, and the equal fixedly connected with bayonet lock 8 in one side bottom that two cardboard 5 are close to each other, the outside movable bush of threaded rod 3 is equipped with limiting plate 6, limiting plate 6 fixed connection is on arc 1, limiting plate 6 is located.
The utility model discloses in, the outside of threaded rod 3 is equipped with two sets of external screw threads, cardboard 5 meshes with corresponding external screw thread mutually, and the screw thread of two external screw threads is revolved to on the contrary, and the pitch of two external screw threads is the same for can drive splint 5 when threaded rod 3 is rotatory and move back on the back mutually.
The utility model discloses in, the fixed cover in the outside of threaded rod 3 is equipped with baffle 7, and one side that two baffles 7 kept away from each other is respectively with two one side swing joint that descending support column 2 is close to each other, and baffle 7 is used for supporting the interior position of descending support column 2, effectively avoids descending support column 2 to take place bending deformation to the inboard.
The utility model discloses in, the bottom both sides of arc 1 all are provided with mounting hole 9, and 9 female connection in mounting hole have screw 10, and the convenience is with this carrier fixed mounting in unmanned aerial vehicle cabin bottom.
The utility model discloses in, the rotation hole 11 has all been seted up to one side that two descending support columns 2 are close to each other, threaded rod 3 with rotate 11 swing joint in hole, the convenience alternates threaded rod 3 between two descending support columns 2.
Referring to fig. 3, the utility model discloses in still provide an unmanned aerial vehicle, including the unmanned aerial vehicle body and as above-mentioned unmanned aerial vehicle carrier, the unmanned aerial vehicle carrier passes through screw 10 fixed connection in the bottom side of unmanned aerial vehicle body.
The utility model discloses in, during the use, set up the screw hole bottom the cabin of unmanned aerial vehicle body, with screw in threaded hole, alright fix the unmanned aerial vehicle carrier on the unmanned aerial vehicle body, position and bayonet lock 8 assorted draw-in groove are seted up in advance in the outside of waiting to carry the thing article, will wait to carry the thing article and arrange in between two cardboard 5, then one of them knob 4 of rotating, it is rotatory to make knob 4 drive threaded rod 3, it carries the thing article to carry to drive two cardboard 5 when threaded rod 3 is rotatory to carry, and aim at the position of bayonet lock 8 draw-in groove, alright will wait to carry the firm centre gripping of thing article between two splint 5, and when splint 5 removes to different positions, can make things convenient for the article of centre gripping different width, adaptability is better.
Claims (6)
1. An unmanned aerial vehicle carrier comprises an arc plate (1), wherein both sides of the bottom of the arc plate (1) are fixedly connected with landing support columns (2), and is characterized in that one side, which is close to each other, of the two landing support columns (2) is rotatably connected with the same threaded rod (3), both ends of the threaded rod (3) penetrate through the corresponding landing support columns (2) and are fixedly connected with knobs (4), one ends, which are close to each other, of the two knobs (4) are respectively movably connected with one sides, which are away from each other, of the two landing support columns (2), the outer side of the threaded rod (3) is sleeved with two symmetrically arranged clamping plates (5), the bottoms, which are close to each other, of the two clamping plates (5) are respectively and fixedly connected with clamping pins (8), the outer side of the threaded rod (3) is movably sleeved with a limiting plate (6), the, the limiting plate (6) is positioned between the two clamping plates (5).
2. The unmanned aerial vehicle carrier of claim 1, wherein the threaded rod (3) is provided at an outer side thereof with two sets of external threads, the catch plate (5) is engaged with the corresponding external threads, the two external threads have opposite thread directions, and the thread pitches of the two external threads are the same.
3. The unmanned aerial vehicle carrier of claim 1, wherein the threaded rod (3) is fixedly sleeved with a baffle (7) at the outer side, and one side of the two baffles (7) away from each other is movably connected with one side of the two landing support columns (2) close to each other.
4. The unmanned aerial vehicle carrier of claim 1, wherein mounting holes (9) are formed in two sides of the bottom of the arc-shaped plate (1), and screws (10) are screwed into the mounting holes (9).
5. The unmanned aerial vehicle carrier of claim 1, wherein the two landing support columns (2) are provided with a rotation hole (11) at a side close to each other, and the threaded rod (3) is movably connected with the rotation hole (11).
6. A drone, comprising a drone body and a drone carrier according to any one of claims 1 to 5, the drone carrier being fixedly attached to the bottom side of the drone body by screws (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921650760.1U CN212267857U (en) | 2019-09-30 | 2019-09-30 | Unmanned aerial vehicle carrier and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921650760.1U CN212267857U (en) | 2019-09-30 | 2019-09-30 | Unmanned aerial vehicle carrier and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212267857U true CN212267857U (en) | 2021-01-01 |
Family
ID=73873112
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921650760.1U Active CN212267857U (en) | 2019-09-30 | 2019-09-30 | Unmanned aerial vehicle carrier and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212267857U (en) |
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2019
- 2019-09-30 CN CN201921650760.1U patent/CN212267857U/en active Active
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