CN213323660U - Portable many rotor unmanned aerial vehicle - Google Patents
Portable many rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN213323660U CN213323660U CN202021135243.3U CN202021135243U CN213323660U CN 213323660 U CN213323660 U CN 213323660U CN 202021135243 U CN202021135243 U CN 202021135243U CN 213323660 U CN213323660 U CN 213323660U
- Authority
- CN
- China
- Prior art keywords
- bradyseism
- support
- unmanned aerial
- bracket
- aerial vehicle
- 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.)
- Expired - Fee Related
Links
- 238000003466 welding Methods 0.000 claims abstract description 4
- 239000000463 material Substances 0.000 claims description 10
- 230000035939 shock Effects 0.000 claims description 4
- 239000004033 plastic Substances 0.000 claims description 3
- 229920003023 plastic Polymers 0.000 claims description 3
- 230000000087 stabilizing effect Effects 0.000 claims description 2
- 230000001681 protective effect Effects 0.000 claims 3
- 238000010521 absorption reaction Methods 0.000 claims 2
- 150000001875 compounds Chemical class 0.000 claims 1
- 230000005484 gravity Effects 0.000 abstract description 5
- 239000000956 alloy Substances 0.000 abstract description 3
- 229910045601 alloy Inorganic materials 0.000 abstract description 3
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 abstract description 2
- 230000008602 contraction Effects 0.000 abstract 1
- 238000013016 damping Methods 0.000 abstract 1
- 230000006641 stabilisation Effects 0.000 abstract 1
- 238000011105 stabilization Methods 0.000 abstract 1
- 238000005452 bending Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000638 stimulation Effects 0.000 description 1
Images
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a portable multi-rotor unmanned aerial vehicle, including the unmanned aerial vehicle organism, the flight support, rotor wing protection frame, motor power, the rotor wing, camera device, bradyseism support, a pedestal, a support, stabilize the footboard, the connecting rod, bradyseism device, motor power pivot is installed rotor wing protection frame and rotor wing from bottom to top in proper order, unmanned aerial vehicle location is installed on the base, the support is installed in the connection of base four corners using the pivot, the support end position welding has the stabilization footboard, the connecting rod is installed in the location of front and back support frame body, connect between the left and right sides support and install the bradyseism device, a portable multi-rotor unmanned aerial vehicle, when unmanned aerial vehicle falls, gravity is downward, the left and right sides support moves to the outside, bradyseism connecting rod pulls central mounting bracket, bradyseism spring on the screw rod receives the downforce contraction, brady, the damping design is realized, the stable pedal at the tail end of the support is an alloy plate body, the contact area is large, and the stability in falling is ensured.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, especially a portable many rotor unmanned aerial vehicle.
Background
An unmanned plane, called a drone for short, is an unmanned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently autonomously operated by an on-board computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. When the small-sized portable unmanned aerial vehicle descends, the small-sized portable unmanned aerial vehicle is in hard contact with the ground and does not have a good cushioning structure.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to overcome prior art's shortcoming, provide a portable many rotor unmanned aerial vehicle. In order to realize the purpose, the utility model adopts the following technical scheme:
the utility model provides a portable many rotor unmanned aerial vehicle, including the unmanned aerial vehicle organism, flight support, rotor protection frame, motor power, the rotor, camera device, bradyseism support, a pedestal, and a support, stabilize the footboard, the connecting rod, the bradyseism device, motor power pivot from the bottom up installs rotor protection frame and rotor in proper order, unmanned aerial vehicle location installation is on the base, the support is installed in the pivot connection in base four corners, the welding of support end position has the stable footboard, the connecting rod is installed in front and back support body location, control and connect between the support and install the bradyseism device.
Preferably, the rotor wing protects the material that the frame chooseed for use and is the rubber material, has certain bending property, and impact resistance is strong.
Preferably the bradyseism device is by bradyseism base, the bradyseism connecting rod, central mounting bracket, screw rod and bradyseism spring, the bradyseism base welding is on controlling the support body of rod, central mounting bracket uses screw rod and bradyseism spring location to install on the base, the bradyseism base uses the bradyseism connecting rod to be connected with central mounting bracket location, when unmanned aerial vehicle whereabouts, gravity is downward, control the support motion to the outside, the bradyseism connecting rod pulls central mounting bracket, the bradyseism spring on the screw rod receives the downforce shrink, bradyseism spring elastic reset, will bradyseism connecting rod reverse pulling again, tighten up the left and right sides support, the bradyseism design.
The preferred material that the support chose for use is composite plastic material, and the quality is light, and structural strength is high, is favorable to improving duration.
Compared with the prior art, the utility model has the advantages of it is following: the utility model provides a portable many rotor unmanned aerial vehicle, when unmanned aerial vehicle whereabouts, gravity is downward, controls the support and moves to the outside, and the bradyseism connecting rod pulls central mounting bracket, and the bradyseism spring on the screw rod receives the shrink of holding down force, and bradyseism spring elasticity resets, will bradyseism connecting rod reverse pulling again, tightens up about the support, realizes the bradyseism design, and the terminal stable footboard of support is the alloy plate body, and area of contact is big, has guaranteed the stability when whereabouts.
Drawings
Fig. 1 is the utility model discloses portable many rotor unmanned aerial vehicle's schematic structure diagram.
Fig. 2 is the utility model discloses portable many rotor unmanned aerial vehicle's mounting structure schematic diagram.
Fig. 3 is a schematic structural view of the shock absorbing support of the present invention.
Fig. 4 is a schematic structural view of the shock absorber of the present invention.
In the figure: 1. unmanned aerial vehicle organism, 2, flight support, 3, rotor protection frame, 4, motor power, 5, rotor, 6, camera device, 7, bradyseism support, 8, base, 9, support, 10, stabilize the footboard, 11, connecting rod, 12, bradyseism device, 13, bradyseism base, 14, bradyseism connecting rod, 15, central mounting bracket, 16, screw rod, 17, bradyseism spring.
Detailed Description
The invention is explained in further detail below with reference to the figures and the embodiments.
As shown in fig. 1, fig. 2, fig. 3 and fig. 4, a portable multi-rotor unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a flight support 2, a rotor wing protection frame 3, a power motor 4, a rotor wing 5, a camera device 6, a cushioning support 7, a base 8, a support 9, a stabilizing pedal 10, a connecting rod 11 and a cushioning device 12, wherein the unmanned aerial vehicle body 1 is positioned and installed on the flight support 2 in an outward-inclined 45-degree manner, the tail end of the support body of the flight support 2 is electrically connected with the power motor 4, the rotor wing protection frame 3 and the rotor wing 5 are sequentially installed on a rotating shaft of the power motor 4 from bottom to top, the radius of the rotor wing protection frame 3 is larger than the rotating radius of the rotor wing 5, the camera device 6 is positioned and installed at the center of the front end of the unmanned aerial vehicle body 1, the unmanned aerial vehicle body 1 is positioned and installed on, the front and rear brackets 9 are provided with a connecting rod 11 for positioning, and a cushioning device 12 is connected between the left and right brackets 9.
The rotor wing protection frame 3 is made of rubber, has certain bending performance and is high in impact resistance.
The material that support 9 chose for use is composite plastic material, and the quality is light, and structural strength is high, is favorable to improving duration.
The utility model discloses the theory of operation: the utility model provides a portable many rotor unmanned aerial vehicle, when unmanned aerial vehicle whereabouts, gravity is downward, controls the support and moves to the outside, and the bradyseism connecting rod pulls central mounting bracket, and the bradyseism spring on the screw rod receives the shrink of holding down force, and bradyseism spring elasticity resets, will bradyseism connecting rod reverse pulling again, tightens up about the support, realizes the bradyseism design, and the terminal stable footboard of support is the alloy plate body, and area of contact is big, has guaranteed the stability when whereabouts.
The foregoing is a preferred embodiment of the present invention, and for those skilled in the art to understand the teaching of the present invention, the changes, modifications, replacements and variations to the embodiments will still fall within the protection scope of the present invention without departing from the principle and spirit of the present invention.
Claims (1)
1. A portable multi-rotor unmanned aerial vehicle is characterized by comprising an unmanned aerial vehicle body (1), a flight bracket (2), a rotor wing protective frame (3), a power motor (4), a rotor wing (5), a camera device (6), a shock absorption bracket (7), a base (8), a bracket (9), a stabilizing pedal (10), a connecting rod (11) and a shock absorption device (12), wherein the unmanned aerial vehicle body (1) is positioned and installed on the flight bracket (2) in an outward-inclined 45-degree manner, the tail end of the frame body of the flight bracket (2) is electrically connected with the power motor (4) in a positioning manner, the rotor wing protective frame (3) and the rotor wing (5) are sequentially installed on a rotating shaft of the power motor (4) from bottom to top, the radius of the rotor wing protective frame (3) is larger than the rotating radius of the rotor wing (5), the camera device (6) is positioned and installed at the center of the front end of the unmanned aerial, four corners of the base (8) are connected and installed with a bracket (9) by using a rotating shaft, the tail end of the bracket (9) is welded with a stable pedal (10), the bracket bodies of the front bracket and the rear bracket (9) are positioned and installed with a connecting rod (11), a cushioning device (12) is connected and installed between the left bracket and the right bracket (9), the material that rotor protection frame (3) chooseed for use is the rubber material, bradyseism device (12) are by bradyseism base (13), bradyseism connecting rod (14), central mounting bracket (15), screw rod (16) and bradyseism spring (17), and bradyseism base (13) welding is on controlling support (9) the body of rod, and central mounting bracket (15) use screw rod (16) and bradyseism spring (17) location to install on base (8), and bradyseism base (13) use bradyseism connecting rod (14) and central mounting bracket (15) location to be connected, the material that support (9) chooseed for use is compound plastics material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021135243.3U CN213323660U (en) | 2020-06-18 | 2020-06-18 | Portable many rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021135243.3U CN213323660U (en) | 2020-06-18 | 2020-06-18 | Portable many rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213323660U true CN213323660U (en) | 2021-06-01 |
Family
ID=76080867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021135243.3U Expired - Fee Related CN213323660U (en) | 2020-06-18 | 2020-06-18 | Portable many rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213323660U (en) |
-
2020
- 2020-06-18 CN CN202021135243.3U patent/CN213323660U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209336991U (en) | Unmanned plane undercarriage | |
| CN213323660U (en) | Portable many rotor unmanned aerial vehicle | |
| CN118062296A (en) | A multi-rotor drone carrying an AI pod | |
| CN110683039A (en) | Unmanned aerial vehicle is collected to urban noise | |
| CN211630857U (en) | Unmanned aerial vehicle mows | |
| CN211107986U (en) | Umbelliform unmanned aerial vehicle frame | |
| CN211167458U (en) | Remote control unmanned aerial vehicle high altitude anti-wind anti-shake device | |
| CN218703959U (en) | Adjustable positioning device for surveying and mapping unmanned aerial vehicle camera | |
| CN216546682U (en) | Unmanned aerial vehicle for collecting plant samples | |
| CN210364355U (en) | Lightweight low-energy consumption unmanned aerial vehicle | |
| CN206511113U (en) | A kind of multi-rotor unmanned aerial vehicle damping undercarriage | |
| CN214729649U (en) | Civil air defense patrol unmanned aerial vehicle | |
| CN213036089U (en) | Miniature radar device of unmanned vehicles | |
| CN213443093U (en) | Bird-driving unmanned aerial vehicle | |
| CN110294106A (en) | A kind of lightweight low energy consumption unmanned plane | |
| CN222886412U (en) | Unmanned aerial vehicle undercarriage convenient to fold and accomodate | |
| CN213323677U (en) | Unmanned plane | |
| CN216186024U (en) | Multi-functional photovoltaic power unmanned aerial vehicle | |
| CN210793624U (en) | Survey and drawing unmanned aerial vehicle with buffering safeguard function | |
| CN215475720U (en) | 5G unmanned aerial vehicle with descending shock-absorbing function | |
| CN215043689U (en) | Unmanned aerial vehicle with shock-absorbing function | |
| CN214986034U (en) | Shock absorption support for unmanned aerial vehicle | |
| CN219687609U (en) | Unmanned aerial vehicle miniature camera head cloud platform and unmanned aerial vehicle | |
| CN223355883U (en) | A shock absorption device with real-time dynamic positioning function carried on a drone | |
| CN213535090U (en) | Stable and durable aerial photography unmanned aerial vehicle |
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: 20210601 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |