CN216233013U - Unmanned aerial vehicle based on wireless energy transmission - Google Patents
Unmanned aerial vehicle based on wireless energy transmission Download PDFInfo
- Publication number
- CN216233013U CN216233013U CN202122496087.4U CN202122496087U CN216233013U CN 216233013 U CN216233013 U CN 216233013U CN 202122496087 U CN202122496087 U CN 202122496087U CN 216233013 U CN216233013 U CN 216233013U
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- unmanned aerial
- aerial vehicle
- organism
- vehicle based
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle based on wireless energy transmission, which comprises a machine body, wherein a connecting device is clamped at the top of the machine body, a buffer device is fixedly connected at the top of the connecting device, four extension rods which are annular and distributed at equal intervals are fixedly connected to the outer side of the buffer device, installation rods with one ends extending to the outer side of the machine body are movably connected to the inner parts of the four extension rods, and a protective cover positioned on the outer side of the machine body is fixedly connected to the outer sides of the four installation rods. This unmanned aerial vehicle based on wireless energy transmission possesses advantages such as protection effect is good, has solved current unmanned aerial vehicle based on wireless energy transmission and has been equipped with external protection casing, but the protection casing can only all carry out local protection to the side of screw, installs the protection network additional in screw top and below and can cause the disturbance to the air current and the lift effect of greatly reduced screw, the not good problem of protection effect.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles based on wireless energy transmission, in particular to an unmanned aerial vehicle based on wireless energy transmission.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Although current unmanned aerial vehicle based on wireless energy transmission is equipped with external protection casing, the protection casing can only all carry out local protection to the side of screw, installs the protection network additional in screw top and below and can cause the disturbance to the air current and the lift effect of greatly reduced screw, and the protection effect is not good, so proposes an unmanned aerial vehicle based on wireless energy transmission and solves the above-mentioned problem of providing.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Aiming at the defects of the prior art, the utility model provides an unmanned aerial vehicle based on wireless energy transmission, which has the advantages of good protection effect and the like, and solves the problems that although the existing unmanned aerial vehicle based on wireless energy transmission is provided with an external protection cover, the protection cover only can locally protect the side surface of a propeller, protective nets are additionally arranged above and below the propeller to cause disturbance to air flow, so that the lift effect of the propeller is greatly reduced, and the protection effect is poor.
(II) technical scheme
The technical scheme for solving the technical problems is as follows: the utility model provides an unmanned aerial vehicle based on wireless energy transmission, includes the organism, the top joint of organism has connecting device, connecting device's top fixedly connected with buffer, buffer's outside fixedly connected with quantity is four and is the extension rod that annular equidistance distributes, four the equal swing joint in inside of extension rod has the installation pole that one end extends to the organism outside, four the equal fixedly connected with in outside of installation pole is located the protection casing in the organism outside.
The utility model has the beneficial effects that: through connecting device with buffer fixed connection at the top of organism, the top of the cooperation protection organism through buffer and extension rod when meetting the impact force that the top transmitted, the swing joint through protection casing and extension rod when meetting the impact force that the side transmitted mutually coordinates the outside of protection organism, prevents to hurt the major structure of organism.
This unmanned aerial vehicle based on wireless energy transmission has possessed the effectual advantage of protection.
On the basis of the technical scheme, the utility model can be further improved as follows.
Further, connecting device includes the connecting box, the draw-in groove with connecting box looks adaptation is seted up at the top of organism, the foam-rubber cushion of connecting box bottom fixedly connected with and organism top contact, the inside swing joint of connecting box has quantity to be two and extends to the kellies of the connecting box left and right sides respectively, two equal fixedly connected with is located the first spring in the homonymy kellies outside between kellies and the connecting box, two the cardboard of the equal fixedly connected with in the back of the body one side of the back of the body and organism joint of kellies.
The sponge cushion has the beneficial effects that the sponge cushion is made of soft materials and can play a role in buffering and absorbing energy.
Further, buffer includes the box body, box body and connecting device's top fixed connection, the inside swing joint of box body has one end to extend to the buffer beam of box body top, the bottom of buffer beam and connecting device's top fixedly connected with is located the inside second spring of box body, the top fixedly connected with installation block of buffer beam.
Adopt above-mentioned further scheme's beneficial effect be, the spring possesses elasticity, can further strengthen the protection to the organism top.
Further, the outside of extension rod is streamlined setting, the extension rod is hardened plastics, the inside fixedly connected with of extension rod and installation pole sliding connection's slide bar.
Adopt above-mentioned further scheme's beneficial effect be, the extension rod of streamlined setting can slow down the extension rod and to the disturbance of organism top air, improves flight stationarity.
Further, fixedly connected with is located the third spring in the slide bar outside between one side that the installation pole is close to the organism and the extension rod, the spout with slide bar looks adaptation is seted up to the inside of installation pole.
Adopt above-mentioned further scheme's beneficial effect is that, the spring possesses elasticity, can slow down the side impact force of organism, improves the protection effect.
Further, the outside fixedly connected with of protection casing and installation pole outside fixed connection's ya keli frame, the protection casing is the arc setting.
The beneficial effect of adopting above-mentioned further scheme is that, acrylic frame material matter is light and the good non-deformable of designability, is convenient for improve the protective effect of protection casing to the organism side.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a front view of the external structure of the present invention;
FIG. 3 is a top view of the connecting structure of the extension rod and the mounting rod according to the present invention;
FIG. 4 is a perspective view of the connection structure of the buffer device and the connecting device according to the present invention.
In the figure: 1. a body; 2. a connecting device; 201. a connection box; 202. a clamping rod; 203. a first spring; 204. clamping a plate; 3. a buffer device; 301. a box body; 302. a buffer rod; 303. a second spring; 304. mounting blocks; 4. an extension rod; 5. mounting a rod; 6. a shield.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the embodiment, as shown in fig. 1-4, the unmanned aerial vehicle based on wireless energy transmission comprises a machine body 1, wherein a connecting device 2 is clamped at the top of the machine body 1, a buffering device 3 is fixedly connected at the top of the connecting device 2, four extending rods 4 which are annularly and equidistantly distributed are fixedly connected to the outer side of the buffering device 3, mounting rods 5 with one ends extending to the outer side of the machine body 1 are movably connected to the inner parts of the four extending rods 4, and protective covers 6 positioned on the outer side of the machine body 1 are fixedly connected to the outer sides of the four mounting rods 5;
the connecting device 2 comprises a connecting box 201, the top of the machine body 1 is provided with a clamping groove matched with the connecting box 201, the bottom of the connecting box 201 is fixedly connected with a sponge cushion contacted with the top of the machine body 1, the inside of the connecting box 201 is movably connected with two clamping rods 202, the two clamping rods 202 are respectively extended to the left side and the right side of the connecting box 201, a first spring 203 positioned on the outer side of the clamping rod 202 on the same side is fixedly connected between the two clamping rods 202 and the connecting box 201, and clamping plates 204 clamped with the machine body 1 are fixedly connected on the opposite sides of the two clamping rods 202;
the spongy cushion is made of softer material and can play a role in buffering and absorbing energy;
the buffer device 3 comprises a box body 301, the box body 301 is fixedly connected with the top of the connecting device 2, a buffer rod 302 with one end extending to the upper part of the box body 301 is movably connected inside the box body 301, a second spring 303 positioned inside the box body 301 is fixedly connected with the bottom of the buffer rod 302 and the top of the connecting device 2, and a mounting block 304 is fixedly connected with the top of the buffer rod 302;
the spring has elasticity, and can further strengthen the protection on the upper part of the machine body 1;
the outer side of the extension rod 4 is arranged in a streamline shape, the extension rod 4 is made of hardened plastics, and a sliding rod which is connected with the mounting rod 5 in a sliding manner is fixedly connected inside the extension rod 4;
the extension rod 4 in streamline arrangement can slow down the disturbance of the extension rod 4 to the air above the machine body 1, and improve the flight stability;
a third spring positioned outside the sliding rod is fixedly connected between one side of the mounting rod 5 close to the machine body 1 and the extension rod 4, and a sliding groove matched with the sliding rod is formed in the mounting rod 5;
the spring has elasticity, so that the side impact force of the machine body 1 can be relieved, and the protection effect is improved;
the outer side of the protective cover 6 is fixedly connected with an acrylic frame fixedly connected with the outer side of the mounting rod 5, and the protective cover is arranged in an arc shape;
the acrylic frame is light in material, good in flexibility and not easy to deform, and the protection effect of the protection cover on the side face of the machine body 1 is improved conveniently.
The working principle is as follows:
the implementation steps of innovation points are as follows:
the first step is as follows: the clamping plate 204 is fixed on the outer side of the machine body 1 through the matching of the connecting box 201 of the connecting device 2, the clamping rod 202 and the first spring 203, and the buffer device 3 is fixedly connected to the top of the machine body through the connecting device 2;
the second step is that: when encountering impact force transmitted from the top of the machine body 1 in the flying or landing process, the buffer rod 302 of the buffer device 3 presses the second spring 303 to match with the spongy cushion at the bottom of the connecting device 2 and contacted with the top of the machine body 1 so as to protect the upper part of the machine body 1, and meanwhile, the extension rod 4 protects the blades of the machine body 1 from being damaged;
the third step: when meeting the impact force that the organism 1 side transmitted at the in-process of flight or descending, oppress the third spring through installation pole 5 and carry out the energy-absorbing to the side impact force of organism 1 and slow down the impact force, protect the major structure who prevents to damage organism 1 simultaneously through protection casing 6 to the paddle of organism 1, the arc setting through protection casing 6 reduces the area of contact of protection casing and external barrier simultaneously, reduces the influence to the flight of organism 1.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle based on wireless energy transmission, includes organism (1), its characterized in that: the top joint of organism (1) has connecting device (2), the top fixedly connected with buffer (3) of connecting device (2), the outside fixedly connected with quantity of buffer (3) is four and is extension rod (4) that annular equidistance distributes, four the equal swing joint in inside of extension rod (4) has installation pole (5), four that one end extends to the organism (1) outside the equal fixedly connected with in outside of installation pole (5) is located protection casing (6) in organism (1) outside.
2. The unmanned aerial vehicle based on wireless energy transmission of claim 1, wherein: connecting device (2) are including connecting box (201), the draw-in groove with connecting box (201) looks adaptation is seted up at the top of organism (1), the foam-rubber cushion of connecting box (201) bottom fixedly connected with and organism (1) top contact, the inside swing joint of connecting box (201) has that quantity is two and extends to the kelly (202) of connecting box (201) left and right sides respectively, two equal fixedly connected with is located first spring (203) in homonymy kelly (202) outside between kelly (202) and connecting box (201), two cardboard (204) of the equal fixedly connected with in the back of the body one side of the back of the body and organism (1) joint of kelly (202).
3. The unmanned aerial vehicle based on wireless energy transmission of claim 1, wherein: buffer (3) include box body (301), the top fixed connection of box body (301) and connecting device (2), the inside swing joint of box body (301) has buffer beam (302) that one end extends to box body (301) top, the bottom of buffer beam (302) and the top fixedly connected with of connecting device (2) are located the inside second spring (303) of box body (301), the top fixedly connected with installation piece (304) of buffer beam (302).
4. The unmanned aerial vehicle based on wireless energy transmission of claim 1, wherein: the outside of extension rod (4) is streamlined setting, extension rod (4) are hardening plastics, the inside fixedly connected with of extension rod (4) and installation pole (5) sliding connection's slide bar.
5. A unmanned aerial vehicle based on wireless energy transmission according to claim 4, wherein: the mounting rod (5) is close to the third spring that is located the slide bar outside fixedly connected with between one side of organism (1) and extension rod (4), the spout with slide bar looks adaptation is seted up to the inside of mounting rod (5).
6. The unmanned aerial vehicle based on wireless energy transmission of claim 1, wherein: the outside fixedly connected with of protection casing (6) and installation pole (5) outside fixed connection's ya keli frame, protection casing (6) are the arc setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122496087.4U CN216233013U (en) | 2021-10-15 | 2021-10-15 | Unmanned aerial vehicle based on wireless energy transmission |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122496087.4U CN216233013U (en) | 2021-10-15 | 2021-10-15 | Unmanned aerial vehicle based on wireless energy transmission |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216233013U true CN216233013U (en) | 2022-04-08 |
Family
ID=80985913
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122496087.4U Active CN216233013U (en) | 2021-10-15 | 2021-10-15 | Unmanned aerial vehicle based on wireless energy transmission |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216233013U (en) |
-
2021
- 2021-10-15 CN CN202122496087.4U patent/CN216233013U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209921623U (en) | Scalable collision avoidance device of unmanned aerial vehicle | |
| CN216233013U (en) | Unmanned aerial vehicle based on wireless energy transmission | |
| CN208102336U (en) | Rotor protection mechanism in a kind of unmanned plane | |
| CN210761306U (en) | Old city reforms transform and uses unmanned aerial vehicle shock-absorbing structure | |
| CN204473119U (en) | Lightweight unmanned plane | |
| CN208683121U (en) | A kind of more rotor logistics unmanned plane airplane parking areas | |
| CN205971889U (en) | Automatic structure of continuing a journey of unmanned aerial vehicle | |
| CN209719910U (en) | A kind of dynamic mount for three rotor wing unmanned aerial vehicles | |
| CN216546682U (en) | Unmanned aerial vehicle for collecting plant samples | |
| CN210852908U (en) | Wing protective structure for unmanned aerial vehicle | |
| CN211033000U (en) | Unmanned aerial vehicle with safeguard function | |
| CN207670682U (en) | A kind of unmanned plane support construction of stability when can improve ejection | |
| CN111017204A (en) | Rapid take-off and landing unmanned aerial vehicle and take-off and landing control method of unmanned aerial vehicle | |
| CN218617227U (en) | Unmanned aerial vehicle flies to control shock-absorbing structure | |
| CN209719904U (en) | A kind of quadrotor drone landing damping device | |
| CN211364922U (en) | Device for taking off and landing aerial photography device on water | |
| CN214356647U (en) | Take shock absorber support's unmanned aerial vehicle | |
| CN218641079U (en) | Unmanned aerial vehicle flies accuse ware | |
| CN217496532U (en) | A anticollision protection structure for unmanned aerial vehicle | |
| CN216684836U (en) | Unmanned aerial vehicle is with frame that rises and falls | |
| CN216253616U (en) | Unmanned aerial vehicle flight controller | |
| CN209535436U (en) | A kind of multi-rotor unmanned aerial vehicle fairing | |
| CN212195861U (en) | Automatic keep away barrier unmanned aerial vehicle | |
| CN204473124U (en) | Without empennage unmanned plane | |
| CN214241222U (en) | Unmanned aerial vehicle falls buffering fender bracket |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |