CN214002034U - Many rotor unmanned aerial vehicle of electric power overhead line - Google Patents
Many rotor unmanned aerial vehicle of electric power overhead line Download PDFInfo
- Publication number
- CN214002034U CN214002034U CN202022311771.6U CN202022311771U CN214002034U CN 214002034 U CN214002034 U CN 214002034U CN 202022311771 U CN202022311771 U CN 202022311771U CN 214002034 U CN214002034 U CN 214002034U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- falling
- prevent falling
- rotor unmanned
- 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
Landscapes
- Catching Or Destruction (AREA)
Abstract
The utility model discloses an electric power overhead line multi-rotor unmanned aerial vehicle, including many rotor unmanned aerial vehicle main parts, the molding of many rotor unmanned aerial vehicle main parts is the octagon, eight angles of many rotor unmanned aerial vehicle main parts respectively can dismantle and connect a set of unmanned aerial vehicle horn, the unmanned aerial vehicle horn is provided with eight groups, the one end upper surface of every group unmanned aerial vehicle horn all can be dismantled and connect a set of unmanned aerial vehicle wing, the unmanned aerial vehicle wing is provided with eight groups, the one end lower surface of every group unmanned aerial vehicle horn all can be dismantled and connect a set of mechanism of preventing falling, it is provided with eight groups to prevent falling the mechanism, the lower extreme surface of many rotor unmanned aerial vehicle main parts can be dismantled and connect the unmanned aerial vehicle bottom plate. A many rotor unmanned aerial vehicle of electric power overhead line, can reduce the vibration through the unmanned aerial vehicle bottom plate that sets up to the unwrapping wire of being convenient for, prevent falling the mechanism through setting up and let unmanned aerial vehicle obtain the protection, bring better use prospect.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field specifically is an electric power stringing multi-rotor unmanned aerial vehicle.
Background
An unmanned aerial vehicle is an unmanned aerial vehicle, which is called as an unmanned aerial vehicle for short, and is an unmanned aerial vehicle utilizing a radio remote control device and a self-contained program control device, and comprises an unmanned helicopter, a fixed wing aircraft, a multi-rotor aircraft, an unmanned airship and an unmanned parachute aircraft, and also comprises a near space aircraft (20-100 kilometers of airspace) such as a stratospheric airship, a high-altitude balloon, a solar unmanned aerial vehicle and the like in a broad sense.
Current electric power stringing unmanned aerial vehicle when installation use, the vibration can influence the photography of camera, need additionally add when electric power stringing and establish the couple, leads to unmanned aerial vehicle out of control to drop with unexpected factor and causes unmanned aerial vehicle impaired, and the use of giving people has brought certain adverse effect, for this reason, we provide an electric power stringing many rotor unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides an electric power stringing multi-rotor unmanned aerial vehicle possesses the damping, is convenient for the unwrapping wire and prevents falling advantages such as, can effectively solve the problem among the background art.
(II) technical scheme
In order to achieve the above purpose, the utility model adopts the following technical scheme: the utility model provides an electric power stringing multi-rotor unmanned aerial vehicle, includes many rotor unmanned aerial vehicle main parts, the molding of many rotor unmanned aerial vehicle main parts is the octagon, eight angles of many rotor unmanned aerial vehicle main parts respectively can be dismantled and connect a set of unmanned aerial vehicle horn, the unmanned aerial vehicle horn is provided with eight groups, the one end upper surface of every unmanned aerial vehicle horn of group all can be dismantled and connect a set of unmanned aerial vehicle wing, the unmanned aerial vehicle wing is provided with eight groups, the one end lower surface of every unmanned aerial vehicle horn of group all can be dismantled and connect a set of mechanism of preventing falling, it is provided with eight groups to prevent falling the mechanism, the lower extreme surface of many rotor unmanned aerial vehicle main parts can be dismantled and connect the unmanned aerial vehicle bottom plate.
Preferably, the lower extreme surface of unmanned aerial vehicle bottom plate is provided with unmanned aerial vehicle foot rest, connecting block, circular rotatory piece and electric power overhead line hanging coil, the unmanned aerial vehicle foot rest is provided with two sets ofly, and corresponds each other, the connecting block is located the middle lower extreme surface of unmanned aerial vehicle bottom plate, circular rotatory piece is located the middle lower extreme surface of connecting block.
Preferably, all be provided with the installation piece between unmanned aerial vehicle bottom plate and the two sets of unmanned aerial vehicle foot rest, the lower extreme surface of unmanned aerial vehicle bottom plate all can dismantle with the upper end surface of two sets of unmanned aerial vehicle foot rests through the installation piece and be connected.
Preferably, the middle of unmanned aerial vehicle bottom plate and connecting block is provided with the set screw, the swivelling chute has been seted up between connecting block and the circular rotatory piece, the lower extreme surface of connecting block passes through swivelling chute and the upper end surface swing joint of circular rotatory piece, circular rotatory piece and electric power overhead line coil integrated into one piece.
Preferably, prevent falling the mechanism including connection piece, fixed slot, prevent falling the support, prevent falling the guardrail and prevent falling the main structure body, the connection piece is located the lower extreme surface of preventing falling the main structure body, the molding of connection piece is the rectangle, the fixed slot is located the one corner of connection piece, the fixed slot is provided with four groups, prevent falling the support and be located the upper end surface of preventing falling the main structure body, prevent falling the support and be provided with five groups, prevent falling the guardrail and be located five groups and prevent falling the upper end surface of support.
Preferably, the fixed slot is seted up on the connection piece, the connection piece with prevent falling the structure main part integrated into one piece, prevent falling the structure main part with prevent falling support integrated into one piece, prevent falling the support with prevent falling guardrail integrated into one piece.
(III) advantageous effects
Compared with the prior art, the utility model provides an electric power stringing multi-rotor unmanned aerial vehicle possesses following beneficial effect:
the electric stringing multi-rotor unmanned aerial vehicle comprises a multi-rotor unmanned aerial vehicle main body, unmanned aerial vehicle arms, unmanned aerial vehicle wings, an unmanned aerial vehicle bottom plate and an anti-falling mechanism, wherein the unmanned aerial vehicle bottom plate is also provided with unmanned aerial vehicle foot rests, connecting blocks, a circular rotating block and an electric stringing coil, the circular rotating block and the electric stringing coil are arranged on the outer surface of the lower end of the unmanned aerial vehicle bottom plate through mounting grooves and fixing screws arranged on the outer surface of the upper end of the unmanned aerial vehicle bottom plate and are arranged on the outer surface of the lower end of the multi-rotor unmanned aerial vehicle main body, the multi-rotor unmanned aerial vehicle can stably land and take off through the two sets of unmanned aerial vehicle foot rests arranged on the unmanned aerial vehicle, the circular rotating block and the electric stringing coil are arranged on the outer surface of the lower end of the unmanned aerial vehicle bottom plate through the connecting blocks arranged on the unmanned aerial vehicle bottom plate, the circular rotating block and the electric stringing coil are integrated into a whole, the circular rotating block arranged on the electric stringing coil can rotate, the unmanned aerial vehicle can not move due to pull, or the power disappears due to unexpected factors, wherein the material of unmanned aerial vehicle bottom plate is the polymer material of absorbing, and this kind of material can absorb the shock wave, and its principle of absorbing is utilized the viscidity damping part in its viscoelasticity, scatters and disappears absorbent energy with hot form, design unmanned aerial vehicle still is provided with prevents falling the mechanism, including connection piece, fixed slot, prevent falling the support, prevent falling the guardrail and prevent falling the main structure body, will prevent falling the mechanism through seting up the fixed slot on the connection piece and install unmanned aerial vehicle on, prevent falling the mechanism through setting up on every unmanned aerial vehicle horn of group, let unmanned aerial vehicle obtain protecting, and because the connection piece, prevent falling the support, prevent falling the guardrail and prevent falling the main structure body as an organic whole to the material is silica gel, in order to reach the best in the molding combination through the design and prevent falling the effect.
Drawings
Fig. 1 is the utility model relates to an electric power stringing multi-rotor unmanned aerial vehicle's overall structure schematic diagram.
Fig. 2 is the utility model relates to a structural schematic of unmanned aerial vehicle bottom plate among many rotor unmanned aerial vehicle of electric power overhead line.
Fig. 3 is the utility model relates to an enlarged view of fig. 2 among many rotor unmanned aerial vehicle of electric power overhead line.
Fig. 4 is the utility model relates to a prevent falling the structural schematic diagram of mechanism among many rotor unmanned aerial vehicle of electric power overhead line.
In the figure: 1. a multi-rotor unmanned aerial vehicle body; 2. an unmanned aerial vehicle arm; 3. wings of the unmanned aerial vehicle; 4. an unmanned aerial vehicle bottom plate; 5. an anti-falling mechanism; 6. an unmanned aerial vehicle foot rest; 7. connecting blocks; 8. a circular rotating block; 9. a power stringing coil; 10. connecting sheets; 11. fixing grooves; 12. an anti-falling bracket; 13. a falling-proof guardrail; 14. prevent falling the main structure body.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
As shown in fig. 1-4, an electric power overhead line many rotor unmanned aerial vehicle, including many rotor unmanned aerial vehicle main part 1, many rotor unmanned aerial vehicle main part 1's molding is the octagon, eight angles of many rotor unmanned aerial vehicle main part 1 respectively can be dismantled and connect a set of unmanned aerial vehicle horn 2, unmanned aerial vehicle horn 2 is provided with eight groups, the one end upper surface of every unmanned aerial vehicle horn 2 of group all can be dismantled and connect a set of unmanned aerial vehicle wing 3, unmanned aerial vehicle wing 3 is provided with eight groups, the one end lower surface of every unmanned aerial vehicle horn 2 of group all can be dismantled and connect a set of mechanism 5 of preventing falling, prevent that falling mechanism 5 is provided with eight groups, the lower extreme surface of many rotor unmanned aerial vehicle main part 1 can be dismantled and connect unmanned aerial vehicle bottom plate 4.
Further, the lower extreme surface of unmanned aerial vehicle bottom plate 4 is provided with unmanned aerial vehicle foot rest 6, connecting block 7, circular rotatory piece 8 and electric power overhead line coil 9, and unmanned aerial vehicle foot rest 6 is provided with two sets ofly, and corresponds each other, and connecting block 7 is located the middle lower extreme surface of unmanned aerial vehicle bottom plate 4, and circular rotatory piece 8 is located the middle lower extreme surface of connecting block 7.
Further, all be provided with the installation piece between unmanned aerial vehicle bottom plate 4 and two sets of unmanned aerial vehicle foot rest 6, the lower extreme surface of unmanned aerial vehicle bottom plate 4 all can dismantle with the upper end surface of two sets of unmanned aerial vehicle foot rest 6 through the installation piece and be connected.
Further, the middle of unmanned aerial vehicle bottom plate 4 and connecting block 7 is provided with the set screw, has seted up the swivelling chute between connecting block 7 and the circular rotatory piece 8, and the lower extreme surface of connecting block 7 passes through the upper end surface swing joint of swivelling chute and circular rotatory piece 8, circular rotatory piece 8 and the 9 integrated into one piece of electric power frame coil.
Further, prevent falling mechanism 5 including connection piece 10, fixed slot 11, prevent falling support 12, prevent falling guardrail 13 and prevent falling main structure body 14, connection piece 10 is located the lower extreme surface of preventing falling main structure body 14, the molding of connection piece 10 is the rectangle, fixed slot 11 is located the one corner of connection piece 10, fixed slot 11 is provided with four groups, prevent falling support 12 and be located the upper end surface of preventing falling main structure body 14, prevent falling support 12 and be provided with five groups, prevent falling guardrail 13 and be located five groups and prevent falling support 12's upper end surface.
Further, fixed slot 11 is seted up on connection piece 10, connection piece 10 with prevent falling structure subject 14 integrated into one piece, prevent falling structure subject 14 and prevent falling support 12 integrated into one piece, prevent falling support 12 and prevent falling guardrail 13 integrated into one piece.
Principle of operation
The electric power stringing multi-rotor unmanned aerial vehicle comprises a multi-rotor unmanned aerial vehicle main body 1, an unmanned aerial vehicle arm 2, unmanned aerial vehicle wings 3, an unmanned aerial vehicle bottom plate 4 and an anti-falling mechanism 5, wherein the unmanned aerial vehicle bottom plate 4 is also provided with an unmanned aerial vehicle foot rest 6, a connecting block 7, a circular rotating block 8 and an electric power stringing hanging ring 9, the circular rotating block 8 and the electric power stringing hanging ring 9 are arranged on the outer surface of the lower end of the unmanned aerial vehicle bottom plate 4 through a mounting groove and a fixing screw arranged on the outer surface of the upper end of the unmanned aerial vehicle bottom plate 4, the multi-rotor unmanned aerial vehicle can stably land and take off through the two sets of the unmanned aerial vehicles 6, the circular rotating block 8 and the electric power stringing hanging ring 9 are arranged on the outer surface of the lower end of the unmanned aerial vehicle bottom plate 4 through the connecting block 7, the circular rotating block 8 and the electric power stringing hanging ring 9 are integrated, the circular foot rest 8 can rotate, the unmanned aerial vehicle can not move due to pulling after being conveniently placed on the electric power stringing hanging ring 9, or because of unexpected factor makes the power disappear, wherein the material of unmanned aerial vehicle bottom plate 4 is the high polymer material of absorbing vibration, and this kind of material can absorb the shock wave, and its principle of absorbing vibration utilizes the viscidity damping part in its viscoelasticity, scatters and disappears absorbent energy with hot form, design unmanned aerial vehicle still is provided with prevents falling mechanism 5, including connection piece 10, fixed slot 11, prevent falling support 12, prevent falling guardrail 13 and prevent falling main structure 14, will prevent falling mechanism 5 and install on unmanned aerial vehicle through seting up fixed slot 11 on connection piece 10, prevent falling mechanism 5 through setting up on every unmanned aerial vehicle horn 2 of group, let unmanned aerial vehicle's obtain protecting, and because connection piece 10, prevent falling support 12, prevent falling guardrail 13 and prevent falling main structure 14 as an organic whole to the material is silica gel, in order to reach the best and prevent falling the effect through the molding combination of design.
It is noted that, herein, relational terms such as first and second (a, b, etc.) 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.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. The utility model provides a many rotor unmanned aerial vehicle of electric power overhead line, includes many rotor unmanned aerial vehicle main part (1), its characterized in that: the molding of many rotor unmanned aerial vehicle main part (1) is the octagon, eight angles of many rotor unmanned aerial vehicle main part (1) respectively can be dismantled and connect a set of unmanned aerial vehicle horn (2), unmanned aerial vehicle horn (2) are provided with eight groups, the one end upper surface of every unmanned aerial vehicle horn of group (2) all can be dismantled and connect a set of unmanned aerial vehicle wing (3), unmanned aerial vehicle wing (3) are provided with eight groups, the one end lower surface of every unmanned aerial vehicle horn of group (2) all can be dismantled and connect a set of mechanism (5) of preventing falling, it is provided with eight groups to prevent falling mechanism (5), the lower extreme surface of many rotor unmanned aerial vehicle main part (1) can be dismantled and connect unmanned aerial vehicle bottom plate (4).
2. An electric stringing multi-rotor unmanned aerial vehicle according to claim 1, wherein: the lower extreme surface of unmanned aerial vehicle bottom plate (4) is provided with unmanned aerial vehicle foot rest (6), connecting block (7), circular rotatory piece (8) and electric power overhead line hanging coil (9), unmanned aerial vehicle foot rest (6) are provided with two sets ofly, and correspond each other, connecting block (7) are located the middle lower extreme surface of unmanned aerial vehicle bottom plate (4), circular rotatory piece (8) are located the middle lower extreme surface of connecting block (7).
3. An electric stringing multi-rotor unmanned aerial vehicle according to claim 2, wherein: all be provided with the installation piece between unmanned aerial vehicle bottom plate (4) and two sets of unmanned aerial vehicle foot rest (6), the lower extreme surface of unmanned aerial vehicle bottom plate (4) all can be dismantled with the upper end surface of two sets of unmanned aerial vehicle foot rest (6) through the installation piece and be connected.
4. An electric stringing multi-rotor unmanned aerial vehicle according to claim 2, wherein: the unmanned aerial vehicle chassis is characterized in that a fixing screw is arranged between the unmanned aerial vehicle chassis (4) and the connecting block (7), a rotating groove is formed between the connecting block (7) and the circular rotating block (8), the outer surface of the lower end of the connecting block (7) is movably connected with the outer surface of the upper end of the circular rotating block (8) through the rotating groove, and the circular rotating block (8) and the electric power frame wire hanging ring (9) are integrally formed.
5. An electric stringing multi-rotor unmanned aerial vehicle according to claim 1, wherein: prevent falling mechanism (5) including connection piece (10), fixed slot (11), prevent falling support (12), prevent falling guardrail (13) and prevent falling subject structure (14), connection piece (10) are located the lower extreme surface of preventing falling subject structure (14), the molding of connection piece (10) is the rectangle, fixed slot (11) are located the one corner of connection piece (10), fixed slot (11) are provided with four groups, prevent falling support (12) and be located the upper end surface of preventing falling subject structure (14), prevent falling support (12) and be provided with five groups, prevent falling guardrail (13) and be located the upper end surface of five groups of preventing falling support (12).
6. An electric stringing multi-rotor unmanned aerial vehicle according to claim 5, wherein: the anti-falling protective device is characterized in that the fixing grooves (11) are formed in the connecting pieces (10), the connecting pieces (10) and the anti-falling structure main bodies (14) are integrally formed, the anti-falling structure main bodies (14) and the anti-falling supports (12) are integrally formed, and the anti-falling supports (12) and the anti-falling guardrails (13) are integrally formed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022311771.6U CN214002034U (en) | 2020-10-16 | 2020-10-16 | Many rotor unmanned aerial vehicle of electric power overhead line |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022311771.6U CN214002034U (en) | 2020-10-16 | 2020-10-16 | Many rotor unmanned aerial vehicle of electric power overhead line |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214002034U true CN214002034U (en) | 2021-08-20 |
Family
ID=77299814
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022311771.6U Active CN214002034U (en) | 2020-10-16 | 2020-10-16 | Many rotor unmanned aerial vehicle of electric power overhead line |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214002034U (en) |
-
2020
- 2020-10-16 CN CN202022311771.6U patent/CN214002034U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN211457048U (en) | Building roof photovoltaic power generation board installation device | |
| CN214002034U (en) | Many rotor unmanned aerial vehicle of electric power overhead line | |
| CN204279940U (en) | A kind of many rotor wing unmanned aerial vehicles device | |
| CN212074463U (en) | Unmanned aerial vehicle multi-angle anti-wind capability test device | |
| CN108860633B (en) | Unmanned aerial vehicle capable of automatically opening air bag when falling after power consumption | |
| CN212556825U (en) | Unmanned aerial vehicle with prevent falling structure | |
| CN109292083B (en) | Anticollision formula rotor unmanned aerial vehicle | |
| CN111011358A (en) | Acousto-optic bird repelling device and using method thereof | |
| CN205293096U (en) | Take unmanned aerial vehicle of structure of acting as go -between | |
| CN207612014U (en) | A kind of 10kV cable terminations platform for making | |
| CN206485554U (en) | Hovering flight device | |
| CN209571066U (en) | A kind of portable multifunctional traffic street lamp | |
| CN204660017U (en) | A kind of kite assisting in flying device | |
| CN205303478U (en) | Prevent high altitude heavy object fall collision solar cell panel | |
| CN214690224U (en) | Unmanned aerial vehicle anticollision framework based on radar | |
| KR20130026066A (en) | Merge power generation street light | |
| CN205396514U (en) | Tumbler spring foam safety aircraft | |
| CN212125498U (en) | Plant protection unmanned aerial vehicle folds horn fast | |
| CN207752637U (en) | A kind of road traffic speed intelligent monitoring device | |
| CN107521719B (en) | Wind power loading device for wing ground resonance test | |
| CN205713222U (en) | Wait platform in a kind of open air | |
| CN204552243U (en) | A kind of electric power pylon | |
| CN215764949U (en) | Helicopter parking apron lightning protection lighting fixture protector | |
| CN110635437A (en) | Complete safety protection equipment for temporarily laying power line on ground | |
| CN220666008U (en) | Sound barrier with wind load adjusting effect |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |