CN218112985U - Anticollision flight unmanned aerial vehicle - Google Patents
Anticollision flight unmanned aerial vehicle Download PDFInfo
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- CN218112985U CN218112985U CN202221384081.6U CN202221384081U CN218112985U CN 218112985 U CN218112985 U CN 218112985U CN 202221384081 U CN202221384081 U CN 202221384081U CN 218112985 U CN218112985 U CN 218112985U
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Abstract
The utility model discloses an anticollision flight unmanned aerial vehicle, include unmanned aerial vehicle main part, first center pin, second connecting rod, remove wheel and second spring, unmanned aerial vehicle main part lower extreme is connected with the head rod, and is provided with first center pin on the head rod, the lower extreme is connected with the second connecting rod, and second connecting rod lower extreme is provided with removes the wheel, first spring lower extreme is connected with the buffer beam, unmanned aerial vehicle main part upside is provided with first carriage release lever, and is provided with the fender rod outside the first carriage release lever, unmanned aerial vehicle main part upside is provided with the screw, be provided with the gag lever post in the unmanned aerial vehicle main part, and the gag lever post outside is provided with the second carriage release lever, be provided with the second spring in the unmanned aerial vehicle main part. This anticollision unmanned aerial vehicle that flies is provided with the second connecting rod, can protect the second connecting rod through buffer beam and first spring to when it landed, carry out the anticollision to the unmanned aerial vehicle main part, prevent that the second connecting rod from damaging, lead to influencing its use.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an anticollision flight unmanned aerial vehicle.
Background
The unmanned plane is an unmanned plane operated by a radio remote control device and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times.
However, the existing flying unmanned aerial vehicle has the following defects in use;
(1) Easy damage, it is relatively poor that current flight unmanned aerial vehicle in use its anticollision effect to lead to its damage easily when landing.
(2) The structure of protecting does not carry out it, and its screw blade scratch staff's hand easily when using of current flight unmanned aerial vehicle to be inconvenient to use it.
We therefore propose an anti-collision flying drone in order to solve the problems set out above.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an anticollision flight unmanned aerial vehicle to solve its anticollision effect of current flight unmanned aerial vehicle in use that above-mentioned background art provided relatively poor, thereby lead to its damage easily when landing, current flight unmanned aerial vehicle is when using its screw blade scratch staff's hand easily, thereby be not convenient for the problem of using to it.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an anticollision flight unmanned aerial vehicle, includes unmanned aerial vehicle main part, first center pin, second connecting rod, removes wheel and second spring, unmanned aerial vehicle main part lower extreme is connected with the head rod, and is provided with first center pin on the head rod, the lower extreme is connected with the second connecting rod, and the second connecting rod lower extreme is provided with removes the wheel, unmanned aerial vehicle main part lower extreme is provided with the third connecting rod, third connecting rod lower extreme is provided with the bracing piece, and the inside first spring that is provided with of bracing piece, first spring lower extreme is connected with the buffer beam, unmanned aerial vehicle main part upside is provided with first carriage release lever, and is provided with the fender rod outside the first carriage release lever, unmanned aerial vehicle main part upside is provided with the screw, be provided with the gag lever post in the unmanned aerial vehicle main part, and the gag lever post outside is provided with the second carriage release lever, be provided with the second spring in the unmanned aerial vehicle main part.
Preferably, the connection mode of unmanned aerial vehicle main part and first connecting rod is fixed connection, and the connection mode of first connecting rod and first center pin is fixed connection to the connection mode of first center pin and second connecting rod is swing joint.
Preferably, the connected mode of third connecting rod and unmanned aerial vehicle main part is fixed connection, and the number of third connecting rod is the same with the number of first connecting rod to the connected mode of third connecting rod and bracing piece is swing joint.
Preferably, the buffer rods are movably connected with the support rods, the buffer rods form a moving structure in the support rods, and the number of the buffer rods is the same as that of the second connecting rods.
Preferably, the connected mode of first carriage release lever and unmanned aerial vehicle main part is for dismantling being connected, and the connected mode of first carriage release lever and guard bar is fixed connection to the connected mode of first carriage release lever and gag lever post is connected for the contact.
Preferably, the connecting mode of gag lever post and unmanned aerial vehicle main part is swing joint, and the gag lever post constitutes the moving structure in unmanned aerial vehicle main part is inside.
Compared with the prior art, the beneficial effects of the utility model are that: the anti-collision flying unmanned aerial vehicle;
(1) Be provided with the second connecting rod, can protect the second connecting rod through buffer beam and first spring to when it landed, carry out the anticollision to the unmanned aerial vehicle main part, prevent that the second connecting rod from damaging, lead to influencing its use.
(2) Be provided with the gag lever post, can carry on spacingly to first carriage release lever through the gag lever post to can conveniently install and dismantle it, later can protect it through the fender rod, prevent screw blade scratch operating personnel, make its convenient use.
Drawings
FIG. 1 is a schematic view of the structure of the present invention;
FIG. 2 is a schematic top view of the present invention;
FIG. 3 is a schematic view of the structure at A in FIG. 1 according to the present invention;
fig. 4 is a schematic structural diagram of the point B in fig. 1 according to the present invention.
In the figure: 1. an unmanned aerial vehicle main body; 2. a first connecting rod; 3. a first central shaft; 4. a second connecting rod; 5. a moving wheel; 6. a third connecting rod; 7. a support bar; 8. a first spring; 9. a buffer rod; 10. a first moving bar; 11. a guard bar; 12. a propeller; 13. a limiting rod; 14. a second movable bar; 15. a second spring.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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. 1-4, the present invention provides a technical solution: the utility model provides an anticollision flight unmanned aerial vehicle, including unmanned aerial vehicle main part 1, head rod 2, first center pin 3, second connecting rod 4, travelling wheel 5, third connecting rod 6, bracing piece 7, first spring 8, buffer beam 9, first travelling bar 10, fender rod 11, screw 12, gag lever post 13, second travelling bar 14 and second spring 15, 1 lower extreme of unmanned aerial vehicle main part is connected with head rod 2, and be provided with first center pin 3 on the head rod 2, the lower extreme is connected with second connecting rod 4, and 4 lower extremes of second connecting rod are provided with travelling wheel 5, 1 lower extreme of unmanned aerial vehicle main part is provided with third connecting rod 6, 6 lower extremes of third connecting rod is provided with bracing piece 7, and the inside first spring 8 that is provided with of bracing piece 7, 8 lower extreme of first spring is connected with unmanned aerial vehicle 9, 1 upside of unmanned aerial vehicle main part is provided with first travelling bar 10, and the first travelling bar 10 outside is provided with fender rod 11, 1 upside of unmanned aerial vehicle main part is provided with screw 12, be provided with gag lever post 13 in the unmanned aerial vehicle main part 1, and the gag lever post 13 outside is provided with second travelling bar 14, be provided with second spring 15 in the unmanned aerial vehicle main part 1.
Unmanned aerial vehicle main part 1 is fixed connection with the connected mode of head rod 2, and the connected mode of head rod 2 and first center pin 3 is fixed connection, and the connected mode of first center pin 3 and second connecting rod 4 is swing joint, unmanned aerial vehicle main part 1 makes the connection of unmanned aerial vehicle main part 1 and head rod 2 more firm with the connected mode of head rod 2, and the connected mode of head rod 2 and first center pin 3 makes the connection of head rod 2 and first center pin 3 more firm, and the connected mode of first center pin 3 and second connecting rod 4 makes second connecting rod 4 can move about on first center pin 3.
Third connecting rod 6 is fixed connection with the connected mode of unmanned aerial vehicle main part 1, and the number of third connecting rod 6 is the same with the number of head rod 2, and the connected mode of third connecting rod 6 and bracing piece 7 is swing joint, the connected mode of third connecting rod 6 and unmanned aerial vehicle main part 1 makes being connected of third connecting rod 6 and unmanned aerial vehicle main part 1 more firm, thereby conveniently use, and the number of third connecting rod 6 is the same with the number of head rod 2, make its use more stable.
First carriage release lever 10 is connected for dismantling with the connected mode of unmanned aerial vehicle main part 1, and the connected mode of first carriage release lever 10 and fender rod 11 is fixed connection, and the connected mode of first carriage release lever 10 and gag lever post 13 is connected for the contact, the connected mode of first carriage release lever 10 and unmanned aerial vehicle main part 1 is convenient to be dismantled first carriage release lever 10, thereby it is convenient to change it, make it conveniently use, and the connected mode of first carriage release lever 10 and fender rod 11 makes first carriage release lever 10 and fender rod 11 be connected more firmly.
Gag lever post 13 is swing joint with the connected mode of unmanned aerial vehicle main part 1, and gag lever post 13 removes the structure at the inside constitution of unmanned aerial vehicle main part 1, and gag lever post 13 conveniently makes gag lever post 13 remove in unmanned aerial vehicle main part 1 inside with the connected mode of unmanned aerial vehicle main part 1 to conveniently use.
The working principle is as follows: when using this crashproof unmanned aerial vehicle that flies, firstly, will inspect the integrality of device earlier, then transport it to corresponding operating position, use it next, when it lands, through second connecting rod 4 and removal wheel 5 contact ground, then cushion it through buffer beam 9 and first spring 8, thereby can prevent that second connecting rod 4 from breaking, later can protect the staff through guard bar 11, prevent that screw 12 from causing the injury to operating personnel, and when guard bar 11 breaks, can pull second movable rod 14, later drive gag lever post 13 and remove, thereby can change it, and the content that does not describe in detail in this description, for example second spring 15 etc. all belong to the prior art that the professional skilled in the art is known.
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 anticollision unmanned aerial vehicle that flies, includes unmanned aerial vehicle main part (1), first center pin (3), second connecting rod (4), removes wheel (5) and second spring (15), its characterized in that: unmanned aerial vehicle main part (1) lower extreme is connected with head rod (2), and is provided with first center pin (3) on head rod (2), the lower extreme is connected with second connecting rod (4), and second connecting rod (4) lower extreme is provided with travelling wheel (5), unmanned aerial vehicle main part (1) lower extreme is provided with third connecting rod (6), third connecting rod (6) lower extreme is provided with bracing piece (7), and bracing piece (7) inside is provided with first spring (8), first spring (8) lower extreme is connected with buffer beam (9), unmanned aerial vehicle main part (1) upside is provided with first carriage release lever (10), and is provided with fender rod (11) in first carriage release lever (10) outside, unmanned aerial vehicle main part (1) upside is provided with screw (12), be provided with gag lever post (13) on unmanned aerial vehicle main part (1), and be provided with second carriage release lever (14) in the gag lever post (13) outside, be provided with second spring (15) on unmanned aerial vehicle main part (1).
2. The anti-collision flying unmanned aerial vehicle of claim 1, wherein: unmanned aerial vehicle main part (1) is fixed connection with the connected mode of head rod (2), and head rod (2) is fixed connection with the connected mode of first center pin (3) to the connected mode of first center pin (3) and second connecting rod (4) is swing joint.
3. The unmanned aerial vehicle of claim 1, wherein: the connected mode of third connecting rod (6) and unmanned aerial vehicle main part (1) is fixed connection, and the number of third connecting rod (6) is the same with the number of head rod (2) to the connected mode of third connecting rod (6) and bracing piece (7) is swing joint.
4. The anti-collision flying unmanned aerial vehicle of claim 1, wherein: the buffer rods (9) are movably connected with the support rods (7), the buffer rods (9) form a moving structure in the support rods (7), and the number of the buffer rods (9) is the same as that of the second connecting rods (4).
5. The anti-collision flying unmanned aerial vehicle of claim 1, wherein: first carriage release lever (10) are connected for dismantling with the connected mode of unmanned aerial vehicle main part (1), and the connected mode of first carriage release lever (10) and fender rod (11) is fixed connection to the connected mode of first carriage release lever (10) and gag lever post (13) is connected for the contact.
6. The anti-collision flying unmanned aerial vehicle of claim 1, wherein: the connecting mode of gag lever post (13) and unmanned aerial vehicle main part (1) is swing joint, and gag lever post (13) is at the inside removal structure that constitutes of unmanned aerial vehicle main part (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221384081.6U CN218112985U (en) | 2022-06-06 | 2022-06-06 | Anticollision flight unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221384081.6U CN218112985U (en) | 2022-06-06 | 2022-06-06 | Anticollision flight unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218112985U true CN218112985U (en) | 2022-12-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221384081.6U Active CN218112985U (en) | 2022-06-06 | 2022-06-06 | Anticollision flight unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218112985U (en) |
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2022
- 2022-06-06 CN CN202221384081.6U patent/CN218112985U/en active Active
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