CN210681149U - Detachable wing of unmanned aerial vehicle - Google Patents
Detachable wing of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN210681149U CN210681149U CN201921762982.2U CN201921762982U CN210681149U CN 210681149 U CN210681149 U CN 210681149U CN 201921762982 U CN201921762982 U CN 201921762982U CN 210681149 U CN210681149 U CN 210681149U
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- Prior art keywords
- mounting
- wing
- unmanned aerial
- aerial vehicle
- installation
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- Expired - Fee Related
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Abstract
The utility model discloses a dismantled and assembled wing of unmanned aerial vehicle, including the installation head, be equipped with installation mechanism on the lateral wall of installation head, installation mechanism is including setting up in two symmetrical first draw-in grooves of the lower extreme of installation head, the lower extreme of installation head is equipped with the screw hole, the installation head passes through screw hole threaded connection on the rotatory wing of unmanned aerial vehicle, the installation mechanism interpolation is equipped with rotary mechanism, transition mechanism has been cup jointed on the lateral wall of installation head, be connected with protection mechanism on the lateral wall of transition mechanism, protection mechanism and transition mechanism swing joint. The utility model discloses can help the quick installation wing of staff and dismantle the wing, the staff only need insert and pull out the wing, both can accomplish the installation and the dismantlement of wing, does not need the staff to use the bolt fastening, has reduced staff's work, indirect improvement staff's work efficiency.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equipment technical field especially relates to a dismantled and assembled wing of unmanned aerial vehicle.
Background
The unmanned aerial vehicle is a small-sized airplane using radio equipment and a control device of automatic control equipment, wherein the unmanned aerial vehicle is also divided into military use and civil use, wherein the military unmanned aerial vehicle is more excellent than the civil unmanned aerial vehicle in specification and manufacture, and the civil unmanned aerial vehicle is generally used for entertainment, commercial use and the like.
In actual conditions, in military activities, the user of service generally can use unmanned aerial vehicle to carry out the reconnaissance to various equipment, but current unmanned aerial vehicle is the space that the wing is shared is bigger, therefore the user of service when carrying unmanned aerial vehicle, and unmanned aerial vehicle will occupy a large amount of spaces, and further will influence user of service's removal.
We therefore propose a detachable wing for an unmanned aerial vehicle to address the above problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the dismantled and assembled wing of unmanned aerial vehicle who provides.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the detachable wing of the unmanned aerial vehicle comprises an installing head, wherein an installing mechanism is arranged on the side wall of the installing head, a rotating mechanism is inserted into the installing mechanism, a transition mechanism is sleeved on the side wall of the installing head, a protecting mechanism is connected to the side wall of the transition mechanism, and the protecting mechanism is movably connected with the transition mechanism.
Preferably, the mounting mechanism comprises two symmetrical first clamping grooves arranged at the lower end of the mounting head, the lower end of the mounting head is provided with a threaded hole, the mounting head is connected to the rotating wing of the unmanned aerial vehicle through the threaded hole, the side wall of the mounting head is provided with two symmetrical second clamping grooves, and the rotating mechanism is inserted into the two second clamping grooves.
Preferably, the rotating mechanism comprises connecting rods respectively inserted into the two second clamping grooves, the two connecting rods are fixedly connected with connectors at the ends far away from the second clamping grooves, and wings are fixedly connected to the side walls of the connectors.
Preferably, the transition mechanism includes the lantern ring of cup jointing on installing the head, the inside wall of the lantern ring is connected with the lateral wall of installing the head and rotates, four horizontal poles of fixedly connected with on the lateral wall of the lantern ring, four the equal fixedly connected with installation piece of one end that the lantern ring was kept away from to the horizontal pole, four the upper end of installation piece all is equipped with the mounting hole, protection mechanism is connected with the installation piece respectively.
Preferably, the protection mechanism includes the connecting plate of rotation connection on four installation piece lateral walls respectively, four equal fixedly connected with erection column in upper end of connecting plate, four the upper end of erection column passes four mounting holes respectively and extends to its top, four the erection column respectively with four mounting hole swing joint, four equal fixedly connected with crosses the cab apron on the lateral wall of connecting plate, four cross the equal fixedly connected with baffle of the lower extreme of cab apron, four the equal fixedly connected with permanent magnetism piece of lower extreme of baffle.
Preferably, the height of two baffles is higher than that of the other two baffles, and the permanent magnets are all magnetically connected.
Compared with the prior art, the beneficial effects of the utility model are that:
in the device, an operator can pull the wing from the mounting head through the use of the mounting mechanism and the rotating mechanism, and meanwhile, the wing can also be inserted into the lower end of the mounting head, so that the wing can be stored, the wing is convenient for the operator to carry, the operator can move conveniently, the operator can insert or pull the wing, the installation and the disassembly of the wing can be completed, the operator can work conveniently, and the working efficiency of the operator is indirectly improved.
Meanwhile, the wings of the unmanned aerial vehicle can be protected by the baffle when the unmanned aerial vehicle moves, so that the wings of the unmanned aerial vehicle are prevented from being damaged, and meanwhile, when the wings are stored by workers, the wings can be protected by the baffle and the permanent magnets, so that the wings are prevented from being damaged by the workers when the workers move, and the wings are further protected.
Drawings
Fig. 1 is a schematic structural view of a detachable wing of an unmanned aerial vehicle according to the present invention;
FIG. 2 is a schematic top view;
fig. 3 is a schematic view of a connection structure of the mounting mechanism and the rotating mechanism of the detachable wing of the unmanned aerial vehicle provided by the utility model;
fig. 4 is the utility model provides a connection structure sketch map of the installation mechanism of the dismantled and assembled wing of unmanned aerial vehicle.
In the figure: the mounting structure comprises a mounting head 1, a first clamping groove 2, a threaded hole 3, a second clamping groove 4, a connecting rod 5, wings 6, a 7 lantern ring, a cross rod 8, a mounting block 9, a mounting hole 10, a connecting plate 11, a mounting column 12, a transition plate 13, a baffle plate 14, a permanent magnet block 15 and a connector 16.
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. 1-4, an unmanned aerial vehicle detachable wing includes an installation head 1, a mounting mechanism is provided on a side wall of the installation head 1, the mounting mechanism includes two symmetrical first clamping grooves 2 provided at a lower end of the installation head 1, wherein the first clamping grooves 2 and the second clamping grooves 4 are identical in shape and size, and the first clamping grooves 2 and the second clamping grooves 4 are both triangular, wherein the triangular structure is more stable, and the wing is prevented from falling off.
The lower end of the mounting head 1 is provided with a threaded hole 3, the mounting head 1 is in threaded connection with the rotary wing of the unmanned aerial vehicle through the threaded hole 3, the connection mode of the mounting head 1 is the prior art, no excessive statement is made here, the side wall of the mounting head 1 is provided with two symmetrical second clamping grooves 4, and the rotating mechanism is inserted into the two second clamping grooves 4.
The installation mechanism is internally inserted with a rotating mechanism, the rotating mechanism comprises connecting rods 5 respectively inserted into the two second clamping grooves 4, one ends of the two connecting rods 5 far away from the second clamping grooves 4 are fixedly connected with connectors 16, and wings 6 are fixedly connected to the side walls of the two connectors 16.
The transition mechanism has been cup jointed on the lateral wall of installation head 1, and transition mechanism is including cup jointing lantern ring 7 on installing head 1, and the inside wall of the lantern ring 7 rotates with the lateral wall of installing head 1 to be connected, four horizontal poles 8 of fixedly connected with on the lateral wall of lantern ring 7, and four horizontal poles 8 keep away from the equal fixedly connected with installation piece 9 of the one end of the lantern ring 7, and the upper end of four installation pieces 9 all is equipped with mounting hole 10, and protection mechanism is connected with installation piece 9 respectively.
Be connected with protection mechanism on transition mechanism's the lateral wall, protection mechanism is including rotating respectively and connecting in the connecting plate 11 on the lateral wall of four installation pieces 9, the equal fixedly connected with erection column 12 in upper end of four connecting plates 11, wherein the shape of erection column 12 is the round platform, further make things convenient for connecting plate 11 to fix on mounting panel 9, wherein the upper end of round platform makes things convenient for erection column 12 to insert in mounting hole 10, and the lower extreme of round platform also can further fixed mounting column 12, the droing of erection column 12 has been avoided, the upper end of four erection columns 12 passes four mounting holes 10 respectively and extends to its top.
Four erection columns 12 respectively with four mounting holes 10 swing joint, all fixedly connected with on the lateral wall of four connecting plates 11 crosses cab apron 13, the equal fixedly connected with baffle 14 of lower extreme that four crossed cab apron 13, wherein the height of two baffles 14 is higher than the height of two other baffles 14, baffle 14 about wherein both ends is higher than the height of baffle 13 at both ends around, further can not influence the use of baffle 14 at both ends around, polylith permanent magnetism 15 is all connected magnetically, the equal fixedly connected with permanent magnetism 15 of lower extreme that four baffles 14, wherein two permanent magnetism 15 magnetism in front and back are connected magnetically, and the permanent magnetism 15 magnetism of both ends is connected about and, protection mechanism and transition mechanism swing joint.
The utility model discloses in, when the staff need accomodate wing 6, at first the staff can be earlier rotatory getting off on the unmanned aerial vehicle fuselage to installation head 1, later the staff pulls out wing 6 from second draw-in groove 4 again, and the staff inserts wing 6 again in the first draw-in groove 2 of installation head 1 lower extreme simultaneously, and further just can make wing 6 obtain accomodating.
Meanwhile, a worker can press the mounting column 12, so that the connecting plate 11 can be moved to the lower end of the mounting block 9, when the connecting plate 11 is located at the lower end of the mounting block 9, the two symmetrical permanent magnets 15 can be magnetically connected, and the wing 6 can be further protected.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The utility model provides a dismantled and assembled wing of unmanned aerial vehicle, includes installation head (1), its characterized in that, be equipped with installation mechanism on the lateral wall of installation head (1), installation mechanism interpolation is equipped with rotary mechanism, the transition mechanism has been cup jointed on the lateral wall of installation head (1), be connected with protection mechanism on the lateral wall of transition mechanism, protection mechanism and transition mechanism swing joint.
2. The detachable wing of the unmanned aerial vehicle as claimed in claim 1, wherein the mounting mechanism comprises two symmetrical first clamping grooves (2) arranged at the lower end of the mounting head (1), the lower end of the mounting head (1) is provided with a threaded hole (3), the mounting head (1) is in threaded connection with the rotatable wing of the unmanned aerial vehicle through the threaded hole (3), the side wall of the mounting head (1) is provided with two symmetrical second clamping grooves (4), and the rotating mechanism is inserted into the two second clamping grooves (4).
3. The detachable wing of the unmanned aerial vehicle according to claim 2, wherein the rotating mechanism comprises connecting rods (5) respectively inserted into the two second clamping grooves (4), one ends of the two connecting rods (5) far away from the second clamping grooves (4) are fixedly connected with connectors (16), and the side walls of the two connectors (16) are fixedly connected with wings (6).
4. The detachable wing of the unmanned aerial vehicle as claimed in claim 1, wherein the transition mechanism comprises a sleeve ring (7) sleeved on the mounting head (1), the inner side wall of the sleeve ring (7) is rotatably connected with the outer side wall of the mounting head (1), four cross rods (8) are fixedly connected to the outer side wall of the sleeve ring (7), mounting blocks (9) are fixedly connected to one ends, far away from the sleeve ring (7), of the four cross rods (8), mounting holes (10) are formed in the upper ends of the four mounting blocks (9), and the protection mechanism is connected with the mounting blocks (9) respectively.
5. The detachable wing of an unmanned aerial vehicle according to claim 4, wherein the protection mechanism comprises connecting plates (11) rotatably connected to side walls of four mounting blocks (9), mounting posts (12) are fixedly connected to upper ends of the four connecting plates (11), upper ends of the four mounting posts (12) respectively penetrate through four mounting holes (10) and extend above the four mounting holes, the four mounting posts (12) are movably connected with the four mounting holes (10), transition plates (13) are fixedly connected to side walls of the four connecting plates (11), lower ends of the four transition plates (13) are fixedly connected with baffle plates (14), and lower ends of the four baffle plates (14) are fixedly connected with permanent magnets (15).
6. A detachable wing for unmanned aerial vehicles according to claim 5, wherein the height of two said baffles (14) is higher than the height of the other two baffles (14), and a plurality of said permanent magnets (15) are magnetically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921762982.2U CN210681149U (en) | 2019-10-21 | 2019-10-21 | Detachable wing of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921762982.2U CN210681149U (en) | 2019-10-21 | 2019-10-21 | Detachable wing of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210681149U true CN210681149U (en) | 2020-06-05 |
Family
ID=70895317
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921762982.2U Expired - Fee Related CN210681149U (en) | 2019-10-21 | 2019-10-21 | Detachable wing of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210681149U (en) |
-
2019
- 2019-10-21 CN CN201921762982.2U patent/CN210681149U/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: 20200605 Termination date: 20211021 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |