CN108622427A - A kind of unmanned plane anti-collision protection device - Google Patents
A kind of unmanned plane anti-collision protection device Download PDFInfo
- Publication number
- CN108622427A CN108622427A CN201810640043.4A CN201810640043A CN108622427A CN 108622427 A CN108622427 A CN 108622427A CN 201810640043 A CN201810640043 A CN 201810640043A CN 108622427 A CN108622427 A CN 108622427A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- loop bar
- moving lever
- protection device
- collision protection
- 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.)
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Links
- 239000000872 buffer Substances 0.000 claims abstract description 13
- 238000009434 installation Methods 0.000 claims description 9
- 230000003139 buffering effect Effects 0.000 claims description 8
- 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 claims description 6
- 238000000034 method Methods 0.000 abstract description 3
- 238000012423 maintenance Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Dampers (AREA)
Abstract
The invention discloses a kind of unmanned plane anti-collision protection devices of air vehicle technique field,Including drone body,The other side of the gantry base is threadedly coupled organic frame,Side of the rack far from gantry base is installed by motor,The output end of the motor installs rotor,The outer side surface centre position of the motor is provided with bumper post,The other end of the bumper post installs guard circle,Loop bar is installed between the adjacent rack,It is plugged with moving lever on the loop bar,The intracavity bottom of the loop bar installs fixed block,The other side of the fixed block is installed by scissor-type holder,And the other end of scissor-type holder is mounted on moving lever,The outside of guard circle is extended at the top of the moving lever and Crashworthy plate is installed,The device can be when unmanned plane generates collision to the object of surrounding by Crashworthy plate and bumper post,Pass through elastic buffer,Reduce impact force impact force caused by the component inside drone body,Damage caused by reduction,Save maintenance cost.
Description
Technical field
The present invention relates to air vehicle technique field, specially a kind of unmanned plane anti-collision protection device.
Background technology
Unmanned plane take photo by plane, rescue, forest fire protection, many fields such as security protection are widely used, mainly by machine
Body and multiple rotors form, and any protective device are not arranged on the rotor of traditional unmanned plane, therefore when outer flight indoors,
When especially in the more complicated forest of environment or city, unmanned plane may be made in environment with misoperation inside
Object collides, while various branches or fallen leaves may interfere rotor in forest, in this way can be to unmanned plane
Mechanical structure causes larger damage, may cause it is out of control or the case where fall, for this purpose, it is proposed that a kind of unmanned plane anticollision
Protective device.
Invention content
It is mentioned above in the background art to solve the purpose of the present invention is to provide a kind of unmanned plane anti-collision protection device
Problem.
To achieve the above object, the present invention provides the following technical solutions：A kind of unmanned plane anti-collision protection device, including nobody
Machine ontology, the upper and lower ends of the drone body and left and right ends are mounted on gantry base, and are offered in gantry base
The other side of threaded hole, the gantry base is threadedly coupled organic frame, and the bottom outer wall of rack is equipped with and matches with threaded hole
Screw thread, side of the rack far from gantry base install motor, and the output end of the motor installs rotor, the motor
Outer side surface centre position is provided with bumper post, and the other end of the bumper post installs guard circle, the adjacent rack it
Between loop bar is installed, be plugged with moving lever on the loop bar, the intracavity bottom of the loop bar installs fixed block, and fixed block and nobody
Machine body outer wall is fixedly mounted, and scissor-type holder, and the other end installation of scissor-type holder are installed in the other side of the fixed block
On moving lever, the outside of guard circle is extended at the top of the moving lever and Crashworthy plate is installed.
Preferably, the Crashworthy plate includes fixed plate, and rubber slab, and spring are installed in the top of the fixed plate by spring
For the identical compressed spring of four groups of structures, anti-skid bulge is uniformly provided at the top of the rubber slab.
Preferably, the fixed plate vertical direction offers the through-hole to match with moving lever, the fixed plate level side
Screw hole is offered upwards, the left and right sides of the screw hole, which is slided, is provided with bolt, and rubber pad is equipped at the top of bolt.
Preferably, the bumper post includes fixed link, and the top and bottom of the fixed link are plugged with buffering loop bar, institute
The outer wall installation buffer spring of fixed link is stated, and the both ends of buffer spring are connect with buffering loop bar, the top buffering loop bar
Upper installation link block, and the connecting hole to match with link block is offered on guard circle.
Preferably, the guard circle is rubber ring, and the cushion hole to match with moving lever is offered on guard circle.
Preferably, the bottom of the drone body is equipped with pedestal, and drone body is fixed by screws in pedestal
On.
Compared with prior art, the beneficial effects of the invention are as follows：The apparatus structure is simple, convenient for disassembly and assembly, passes through Crashworthy plate
, by elastic buffer, impact force can be reduced to nobody when unmanned plane generates collision to the object of surrounding with bumper post
Impact force caused by the component of machine body interior, damage caused by reduction, saves maintenance cost.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is rack construction schematic diagram of the present invention；
Fig. 3 is anticollision plate structure schematic diagram of the present invention；
Fig. 4 is fixed plate structure schematic diagram of the present invention；
Fig. 5 is bumper post structural schematic diagram of the present invention.
In figure：1 drone body, 2 gantry bases, 3 racks, 4 rotors, 5 bumper posts, 51 fixed links, 52 buffer springs, 53
Buffer loop bar, 54 link blocks, 6 guard circles, 7 loop bars, 8 fixed blocks, 9 scissor-type holders, 10 moving levers, 11 Crashworthy plates, 111 fixations
Plate, 1111 through-holes, 1112 screw holes, 1113 bolts, 1114 rubber pads, 112 springs, 113 rubber slabs, 114 anti-skid bulges, 12 electricity
Machine.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
- 5 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of unmanned plane anti-collision protection device, including unmanned plane
Ontology 1, the upper and lower ends of drone body 1 and left and right ends are mounted on gantry base 2, and offer spiral shell in gantry base 2
The other side of pit, gantry base 2 is threadedly coupled organic frame 3, and the bottom outer wall of rack 3 is equipped with the spiral shell to match with threaded hole
Line 31, easy to disassemble, motor 12 is installed in side of the rack 3 far from gantry base 2, ensures that unmanned plane has during flight
The output end of enough power, motor 12 installs rotor 4, and the outer side surface centre position of motor 12 is provided with bumper post 5,
The other end of bumper post 5 installs guard circle 6, and loop bar 7 is installed between adjacent rack 3, moving lever 10, loop bar 7 are plugged on loop bar 7
Intracavity bottom fixed block 8 is installed, and fixed block 8 and 1 outer wall of drone body are fixedly mounted, the other side installation of fixed block 8
Scissor-type holder 9, and the other end of scissor-type holder 9 is mounted on moving lever 10, the top of moving lever 10 extends to guard circle 6
Outside and Crashworthy plate 11 is installed, pass through elastic buffer, reduce impact force impact force caused by the component inside unmanned plane.
Wherein, Crashworthy plate 11 includes fixed plate 111, and the top of fixed plate 111 is installed rubber slab 113 by spring 112, prevented
Only unmanned plane collides with object damages unmanned plane, and spring 112 is the identical compressed spring of four groups of structures, is conducive to improve
The top of cushioning effect, rubber slab 113 is uniformly provided with anti-skid bulge 114, is conducive to increase the friction between object；
111 vertical direction of fixed plate offers the through-hole 1111 to match with moving lever 10, in 111 horizontal direction of fixed plate
Screw hole 1112 is offered, the left and right sides of screw hole 1112, which is slided, is provided with bolt 1113, and the top of bolt 1113 is equipped with
Rubber pad 1114 prevents extruding from being damaged to moving lever 10, is conducive to fix moving lever 10 by bolt 1113, while conveniently
Dismounting；
Bumper post 5 includes fixed link 51, and the top and bottom of fixed link 51 are plugged with buffering loop bar 53, fixed link 51
Outer wall installs buffer spring 52, and the both ends of buffer spring 52 are connect with buffering loop bar 53, are installed on top cushion loop bar 53
Link block 54, and the connecting hole to match with link block 54 is offered on guard circle 6, further play the role of buffering, it is right
Drone body 1 is protected；
Guard circle 6 is rubber ring, is conducive to the weight for mitigating unmanned plane, saves cost of manufacture, and offered on guard circle 6
The cushion hole to match with moving lever 10；
The bottom of drone body 1 is equipped with pedestal, and drone body 1 is fixed by screws on pedestal, is conveniently torn open
Unload installation.
Operation principle：Rack 3 is symmetrically loaded onto in the surrounding of drone body 1, rotor 4 is installed in the end of rack 3, and
Guard circle 6 is fixed by bumper post 5, by installing Crashworthy plate 11, mitigates the overall weight of unmanned plane, ensures that unmanned plane is flying
There is enough power, and Crashworthy plate 11 and bumper post 5 can generate collision in unmanned plane to the object of surrounding in capable process
When, by elastic buffer, reduce impact force impact force caused by the component inside unmanned plane, in forest detects,
Unmanned plane generates shock to trunk, and when progress low latitude is taken photo by plane in city, shock etc. is generated to the wall of building body, simple in structure,
It is convenient for disassembly and assembly.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of unmanned plane anti-collision protection device, including drone body (1), it is characterised in that：The drone body (1)
Upper and lower ends and left and right ends are mounted on gantry base (2), and threaded hole, the frame ground are offered in gantry base (2)
The other side of seat (2) is threadedly coupled organic frame (3), and the bottom outer wall of rack (3) is equipped with the screw thread to match with threaded hole
(31), side installation motor (12) of the rack (3) far from gantry base (2), the output end installation rotation of the motor (12)
The outer side surface centre position of the wing (4), the motor (12) is provided with bumper post (5), the other end of the bumper post (5)
Guard circle (6) is installed, loop bar (7) is installed between the adjacent rack (3), moving lever (10), institute are plugged on the loop bar (7)
The intracavity bottom installation fixed block (8) of loop bar (7) is stated, and fixed block (8) is fixedly mounted with drone body (1) outer wall, it is described
The other side installation scissor-type holder (9) of fixed block (8), and the other end of scissor-type holder (9) is mounted on moving lever (10),
The outside of guard circle (6) is extended at the top of the moving lever (10) and Crashworthy plate (11) is installed.
2. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that：The Crashworthy plate (11) includes
Rubber slab (113) is installed in the top of fixed plate (111), the fixed plate (111) by spring (112), and spring (112) is four
The identical compressed spring of structure is organized, anti-skid bulge (114) is uniformly provided at the top of the rubber slab (113).
3. a kind of unmanned plane anti-collision protection device according to claim 2, it is characterised in that：The fixed plate (111) is perpendicular
Histogram offers spiral shell to the through-hole (1111) to match with moving lever (10) is offered in fixed plate (111) horizontal direction
Hole (1112), the left and right sides of the screw hole (1112), which is slided, is provided with bolt (1113), and the top peace of bolt (1113)
Equipped with rubber pad (1114).
4. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that：The bumper post (5) includes
Fixed link (51), the top and bottom of the fixed link (51), which are plugged with, buffers loop bar (53), outside the fixed link (51)
Wall installs buffer spring (52), and the both ends of buffer spring (52) are connect with buffering loop bar (53), the top buffering loop bar
(53) link block (54) is installed on, and offers the connecting hole to match with link block (54) on guard circle (6).
5. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that：The guard circle (6) is rubber
Cushion rubber, and the cushion hole to match with moving lever (10) is offered on guard circle (6).
6. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that：The drone body (1)
Bottom pedestal is installed, and drone body (1) is fixed by screws on pedestal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810640043.4A CN108622427A (en) | 2018-06-21 | 2018-06-21 | A kind of unmanned plane anti-collision protection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810640043.4A CN108622427A (en) | 2018-06-21 | 2018-06-21 | A kind of unmanned plane anti-collision protection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108622427A true CN108622427A (en) | 2018-10-09 |
Family
ID=63692104
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810640043.4A Withdrawn CN108622427A (en) | 2018-06-21 | 2018-06-21 | A kind of unmanned plane anti-collision protection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108622427A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436350A (en) * | 2018-10-16 | 2019-03-08 | 河北国泰航空科技有限公司 | A kind of novel unmanned plane |
| CN112158344A (en) * | 2020-09-23 | 2021-01-01 | 成都儒气合商贸有限公司 | Anti-collision protection equipment for security protection unmanned aerial vehicle |
-
2018
- 2018-06-21 CN CN201810640043.4A patent/CN108622427A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436350A (en) * | 2018-10-16 | 2019-03-08 | 河北国泰航空科技有限公司 | A kind of novel unmanned plane |
| CN112158344A (en) * | 2020-09-23 | 2021-01-01 | 成都儒气合商贸有限公司 | Anti-collision protection equipment for security protection unmanned aerial vehicle |
| CN112158344B (en) * | 2020-09-23 | 2021-12-21 | 福建联政信息技术有限公司 | Anti-collision protection equipment for security protection unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181009 |
|
| WW01 | Invention patent application withdrawn after publication |