CN209506106U - A kind of unmanned plane during flying anticollision device, collision-prevention device - Google Patents
A kind of unmanned plane during flying anticollision device, collision-prevention device Download PDFInfo
- Publication number
- CN209506106U CN209506106U CN201821965438.3U CN201821965438U CN209506106U CN 209506106 U CN209506106 U CN 209506106U CN 201821965438 U CN201821965438 U CN 201821965438U CN 209506106 U CN209506106 U CN 209506106U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- collision
- drone body
- fixedly installed
- during flying
- 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
Landscapes
- Toys (AREA)
Abstract
The utility model relates to unmanned flight's technical fields, and disclose a kind of unmanned plane during flying anticollision device, collision-prevention device, including drone body, the two sides of the drone body bottom are fixedly installed with supporting leg, the top of four wings of drone body is fixedly installed with driving flabellum, the bottom of four wings of drone body is fixedly installed with spiral shell block, the other end screw thread of spiral shell block is socketed with connecting rod, the other end screw thread of connecting rod is socketed with supporting plate, and the other end of supporting plate extends to the outside of drone body.The unmanned plane during flying anticollision device, collision-prevention device; pass through the compound action of spiral shell block, connecting rod, supporting plate, support rod and protecting crust; it is protected convenient for the periphery to driving flabellum; be conducive to improve the device to the protective capability of unmanned plane rotor; it effectively prevent the rotor of unmanned plane and the collision of other objects; it avoids causing the rotor of unmanned plane biggish damage and causing body out of control or fall, to improve the anticollision ability of unmanned plane.
Description
Technical field
The utility model relates to unmanned flight's technical field, specially a kind of unmanned plane during flying anticollision device, collision-prevention device.
Background technique
Unmanned plane take photo by plane, rescue, many fields such as forest fire protection and security protection are widely used, mainly by
Body and multiple rotors form, not set any protective device on the rotor of traditional unmanned plane, therefore when outer flight indoors,
When especially in the more complicated city of environment, misoperation and cause unmanned plane to collide with the object in environment, it is right
The rotor of unmanned plane causes biggish damage, and it is out of control or the case where fall to may cause body, for this purpose, it is proposed that a kind of nothing
Man-machine flight anticollision device, collision-prevention device.
Utility model content
In view of the deficiencies of the prior art, the utility model provides a kind of unmanned plane during flying anticollision device, collision-prevention device, has to nothing
The advantages of man-machine outer is protected solves not set any protective device on the rotor of traditional unmanned plane, and manual operation is not
When and cause unmanned plane to collide with the object in environment, biggish damage is caused to the rotor of unmanned plane, body is caused to lose
The problem of controlling or falling.
The utility model provides the following technical solutions: a kind of unmanned plane during flying anticollision device, collision-prevention device, including drone body, institute
The two sides for stating drone body bottom are fixedly installed with supporting leg, the fixed peace in the top of four wings of drone body
Equipped with driving flabellum, the bottom of four wings of drone body is fixedly installed with spiral shell block, the other end spiral shell of the spiral shell block
Line is socketed with connecting rod, and the other end screw thread of the connecting rod is socketed with supporting plate, and the other end of the supporting plate extends to unmanned plane
The outside of ontology, the support rod being fixedly installed at the top of the supporting plate on the outside of drone body, the support rod it is another
One end is fixedly installed with protecting crust, and the protecting crust shrouds the outside in driving flabellum, and the inner wall of the protecting crust and driving are fanned
There are gaps between leaf.
Preferably, the bottom end movable sleeve of the supporting leg is connected to motion bar, and the other end of the motion bar is fixedly installed with
The upper surface of rubber pad, the rubber pad is connected by the bottom driving of buffer spring and supporting leg.
Preferably, the buffer spring movable set is in the outer surface of motion bar, the upper and lower ends point of the buffer spring
It is not fixedly connected at the top of the bottom of motion bar and rubber pad.
Preferably, the bottom of the supporting leg offers cavity compatible with motion bar, and the top of the motion bar is prolonged
Extend in cavity and be fixedly installed with limit plate, the outer surface of the motion bar and limit plate connects with the inner wall activity of cavity
It connects.
Preferably, the bottom of the rubber pad is hemispherical.
Preferably, the shape of the protecting crust is fan-shaped guard ring, and the lateral surface of the protecting crust is hollow design and deposits
In three gaps.
Preferably, the driving flabellum is made of attachment base and blade, and the interior welds of the attachment base have motor, described
Blade is fixedly set on the output shaft of motor.
Preferably, the interior welds of the drone body have lithium battery and by the input terminal of conducting wire and four motors electricity
Property connection.
Be compared with the prior art, the utility model have it is following the utility model has the advantages that
1, the unmanned plane during flying anticollision device, collision-prevention device passes through the group cooperation of spiral shell block, connecting rod, supporting plate, support rod and protecting crust
With, it is protected convenient for the periphery to driving flabellum, is conducive to improve the device to the protective capability of unmanned plane rotor, it is effectively anti-
The only collision of the rotor of unmanned plane and other objects avoids causing the rotor of unmanned plane biggish damage and causing body out of control
Or fall, to improve the anticollision ability of unmanned plane.
2, the unmanned plane during flying anticollision device, collision-prevention device can effectively dredge air-flow by three gaps on protecting crust, reduce
The abnormal influence to unmanned plane rotor of air-flow, is conducive to the practicability for improving the device, then by rubber pad drive motion bar to
Cavity inside supporting leg is mobile, so that buffer spring stress deformation, occurs elastic deformation using buffer spring and generate anti-
To active force, realize the buffering to supporting leg, be conducive to improve buffer capacity when unmanned plane falls, avoid falling it is unstable and by
Damage, to improve the practicability of the device.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model;
Fig. 2 is the overlooking structure diagram of the utility model drone body;
Fig. 3 is the partial profile structure of the utility model supporting leg;
Fig. 4 is the enlarged structure schematic diagram that the utility model drives flabellum.
In figure: 1, drone body;2, supporting leg;3, flabellum is driven;31, attachment base;32, blade;4, spiral shell block;5, even
Extension bar;6, supporting plate;7, support rod;8, protecting crust;9, motion bar;10, rubber pad;11, buffer spring;12, limit plate.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1-4, a kind of unmanned plane during flying anticollision device, collision-prevention device, including drone body 1,1 bottom of drone body
Two sides be fixedly installed with supporting leg 2, the bottom end movable sleeve of supporting leg 2 is connected to motion bar 9, and the bottom of supporting leg 2 offers
Cavity compatible with motion bar 9, the top of motion bar 9 extend in cavity and are fixedly installed with limit plate 12,9 He of motion bar
The outer surface of limit plate 12 is flexibly connected with the inner wall of cavity, and the other end of motion bar 9 is fixedly installed with rubber pad 10, rubber
The bottom of pad 10 is hemispherical, and the upper surface of rubber pad 10 is connect with the bottom driving of supporting leg 2 by buffer spring 11, buffered
11 movable set of spring in the outer surface of motion bar 9, the upper and lower ends of buffer spring 11 respectively with the bottom of motion bar 9 and rubber
The top of pad 10 is fixedly connected, and drives motion bar 9 mobile to the cavity inside supporting leg 2 by rubber pad 10, so that buffering elastic
11 stress deformation of spring, the opposition generated using the generation elastic deformation of buffer spring 11, is realized to the slow of supporting leg 2
Punching is conducive to improve buffer capacity when unmanned plane falls, and avoids falling unstable and being damaged, to improve the practical of the device
Property, the top of 1 four wings of drone body is fixedly installed with driving flabellum 3, drives flabellum 3 by attachment base 31 and blade 32
Composition, the interior welds of attachment base 31 have motor, and blade 32 is fixedly set on the output shaft of motor, and drone body 1 four
The bottom of wing is fixedly installed with spiral shell block 4, and the interior welds of drone body 1 have lithium battery and by conducting wire and four motors
Input terminal be electrically connected, the other end screw thread of spiral shell block 4 is socketed with connecting rod 5, and the other end screw thread of connecting rod 5 is socketed with branch
Plate 6, the other end of supporting plate 6 extend to the outside of drone body 1, and the top of supporting plate 6 is fixedly installed with positioned at drone body
The support rod 7 in 1 outside, the other end of support rod 7 are fixedly installed with protecting crust 8, pass through spiral shell block 4, connecting rod 5, supporting plate 6, support
The compound action of bar 7 and protecting crust 8 protects convenient for the periphery to driving flabellum 3, is conducive to improve the device to unmanned plane
The protective capability of rotor effectively prevent the rotor of unmanned plane and the collision of other objects, avoid causing the rotor of unmanned plane compared with
Big damage and cause body out of control or fall, to improve the anticollision ability of unmanned plane, the shape of protecting crust 8 is sector
Guard ring, for the lateral surface of protecting crust 8 for hollow design and there are three gaps, protecting crust 8 shrouds the outside in driving flabellum 3,
There are gaps between the inner wall and driving flabellum 3 of protecting crust 8 can effectively dredge gas by three gaps on protecting crust 8
Stream reduces the abnormal influence to unmanned plane rotor of air-flow, is conducive to the practicability for improving the device.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (8)
1. a kind of unmanned plane during flying anticollision device, collision-prevention device, including drone body (1), it is characterised in that: the drone body (1)
The two sides of bottom are fixedly installed with supporting leg (2), and the top of (1) four wing of drone body is fixedly installed with drive
Dynamic flabellum (3), the bottom of (1) four wing of drone body are fixedly installed with spiral shell block (4), the spiral shell block (4) it is another
Threaded one end is socketed with connecting rod (5), and the other end screw thread of the connecting rod (5) is socketed with supporting plate (6), the supporting plate (6)
The other end extends to the outside of drone body (1), is fixedly installed at the top of the supporting plate (6) positioned at drone body (1)
The other end of the support rod (7) in outside, the support rod (7) is fixedly installed with protecting crust (8), and the protecting crust (8) is shrouded
The outside of flabellum (3) is driven, there are gaps between the inner wall and driving flabellum (3) of the protecting crust (8).
2. a kind of unmanned plane during flying anticollision device, collision-prevention device according to claim 1, it is characterised in that: the supporting leg (2)
Bottom end movable sleeve is connected to motion bar (9), and the other end of the motion bar (9) is fixedly installed with rubber pad (10), the rubber pad
(10) upper surface is connect by buffer spring (11) with the bottom driving of supporting leg (2).
3. a kind of unmanned plane during flying anticollision device, collision-prevention device according to claim 2, it is characterised in that: the buffer spring (11)
Movable set in the outer surface of motion bar (9), the upper and lower ends of the buffer spring (11) respectively with the bottom of motion bar (9) and
Rubber pad is fixedly connected at the top of (10).
4. a kind of unmanned plane during flying anticollision device, collision-prevention device according to claim 1, it is characterised in that: the supporting leg (2)
Bottom, which is offered, to be extended in cavity and is fixedly installed with motion bar (9) compatible cavity, the top of the motion bar (9)
The outer surface of limit plate (12), the motion bar (9) and limit plate (12) is flexibly connected with the inner wall of cavity.
5. a kind of unmanned plane during flying anticollision device, collision-prevention device according to claim 2, it is characterised in that: the rubber pad (10)
Bottom is hemispherical.
6. a kind of unmanned plane during flying anticollision device, collision-prevention device according to claim 1, it is characterised in that: the protecting crust (8)
Shape is fan-shaped guard ring, and the lateral surface of the protecting crust (8) is hollow design and there are three gaps.
7. a kind of unmanned plane during flying anticollision device, collision-prevention device according to claim 1, it is characterised in that: the driving flabellum (3)
It is made of attachment base (31) and blade (32), the interior welds of the attachment base (31) have motor, blade (32) fixing sleeve
On the output shaft of motor.
8. a kind of unmanned plane during flying anticollision device, collision-prevention device according to claim 1, it is characterised in that: the drone body
(1) interior welds have lithium battery and are electrically connected by the input terminal of conducting wire and four motors.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821965438.3U CN209506106U (en) | 2018-11-27 | 2018-11-27 | A kind of unmanned plane during flying anticollision device, collision-prevention device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821965438.3U CN209506106U (en) | 2018-11-27 | 2018-11-27 | A kind of unmanned plane during flying anticollision device, collision-prevention device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN209506106U true CN209506106U (en) | 2019-10-18 |
Family
ID=68191071
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201821965438.3U Active CN209506106U (en) | 2018-11-27 | 2018-11-27 | A kind of unmanned plane during flying anticollision device, collision-prevention device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN209506106U (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112208762A (en) * | 2020-09-25 | 2021-01-12 | 赵荣菊 | Aerial monitoring formula unmanned aerial vehicle |
CN112550705A (en) * | 2020-12-04 | 2021-03-26 | 安徽天德无人机科技有限公司 | Highway patrol unmanned aerial vehicle that breaks rules and regulations |
CN112678163A (en) * | 2021-02-25 | 2021-04-20 | 黄根水 | Unmanned aerial vehicle anticollision protection architecture |
CN113479323A (en) * | 2021-07-28 | 2021-10-08 | 宁波阿瑞斯自动化技术有限公司 | Unmanned aerial vehicle protection device |
-
2018
- 2018-11-27 CN CN201821965438.3U patent/CN209506106U/en active Active
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112208762A (en) * | 2020-09-25 | 2021-01-12 | 赵荣菊 | Aerial monitoring formula unmanned aerial vehicle |
CN112550705A (en) * | 2020-12-04 | 2021-03-26 | 安徽天德无人机科技有限公司 | Highway patrol unmanned aerial vehicle that breaks rules and regulations |
CN112678163A (en) * | 2021-02-25 | 2021-04-20 | 黄根水 | Unmanned aerial vehicle anticollision protection architecture |
CN113479323A (en) * | 2021-07-28 | 2021-10-08 | 宁波阿瑞斯自动化技术有限公司 | Unmanned aerial vehicle protection device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN209506106U (en) | A kind of unmanned plane during flying anticollision device, collision-prevention device | |
CN204822090U (en) | Unmanned aerial vehicle | |
CN105000180B (en) | Aerodynamic configuration of aircraft device | |
CN209617463U (en) | A kind of anti-crash protective device of unmanned plane | |
CN104044155A (en) | Gravity offset device | |
CN107264767A (en) | A kind of rotor wing unmanned aerial vehicle of Novel lightweight six | |
CN104772751B (en) | The parallel institution of Three Degree Of Freedom | |
CN209037840U (en) | A kind of unmanned plane wing safeguard structure | |
CN209617446U (en) | A kind of clamp-close type unmanned plane propeller replacement structure | |
CN204279926U (en) | A kind of Brattice type multi-rotor aerocraft alighting gear with guide functions | |
CN208775012U (en) | A kind of VTOL flying platform high efficiency lift unit | |
CN111123981A (en) | Machine room inspection robot | |
CN209322264U (en) | A kind of lifting device of the building hoist with stabilization function | |
CN211442764U (en) | Long-endurance large-load hybrid four-rotor unmanned aerial vehicle | |
CN211174456U (en) | Environment-friendly externally-hung type unmanned aerial vehicle wind power generation endurance equipment | |
CN210349517U (en) | Low-voltage reactive compensation reactor | |
CN207454171U (en) | A kind of wind paddle variable-distance structure for changing pitch and front face area | |
CN208248501U (en) | A kind of forest fire detection robot | |
CN208498793U (en) | A kind of minitype bionic flapping wing robot | |
CN113911373B (en) | Industrial unmanned aerial vehicle | |
CN212605859U (en) | Unmanned aerial vehicle aircraft that stability is good | |
CN205076042U (en) | Many rotor unmanned aerial vehicle box structure horn | |
CN205034333U (en) | Pressure type driven multiaxis gyroplane | |
CN110588967A (en) | Aircraft and aircraft system | |
CN103963967B (en) | Multiple bladed rotors tandem aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |