CN106005384A - Unmanned aerial vehicle that protective properties is high - Google Patents
Unmanned aerial vehicle that protective properties is high Download PDFInfo
- Publication number
- CN106005384A CN106005384A CN201610438237.7A CN201610438237A CN106005384A CN 106005384 A CN106005384 A CN 106005384A CN 201610438237 A CN201610438237 A CN 201610438237A CN 106005384 A CN106005384 A CN 106005384A
- Authority
- CN
- China
- Prior art keywords
- double
- supports
- fixedly connected
- unmanned plane
- protection ring
- 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.)
- Granted
Links
- 230000001681 protective effect Effects 0.000 title claims description 15
- 238000013016 damping Methods 0.000 claims description 15
- 210000002421 cell wall Anatomy 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Vibration Dampers (AREA)
Abstract
The invention discloses an unmanned aerial vehicle with high protection performance, which comprises a housing main body, wherein two double-wing supports are fixedly connected to two sides of the housing main body, the two double-wing supports are symmetrically arranged along the central axis of the housing main body, driving supports are symmetrically and fixedly connected to the front side and the back side of each double-wing support, one ends, far away from the double-wing supports, of the driving supports are provided with driving devices, fixed supports are respectively and fixedly connected to two sides, far away from the double-wing supports, of the double-wing supports, one ends, far away from the double-wing supports, of the fixed supports are fixedly connected with protection rings, and the protection rings are sleeved outside the driving devices. The unmanned aerial vehicle with high protection performance is simple in structure and convenient to use, can be well protected when an operator mistakenly operates the unmanned aerial vehicle, reduces impact force during collision, cannot damage a propeller, is higher in protection performance of the unmanned aerial vehicle, and prolongs the service life of the unmanned aerial vehicle.
Description
Technical field
The present invention relates to vehicle technology field, the unmanned plane that a kind of protective value is high.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is to utilize wireless remotecontrol to set
The most manned aircraft that presetting apparatus that is standby and that provide for oneself is handled.Unmanned plane presses application, can be divided into army
With with civilian.
At present, in the design and fabrication of existing unmanned plane, unmanned plane is not had in the protective value of flight
Specifically device, and unmanned plane needs Artificial Control, if initial contact and operational error are unmanned
Machine awing can collide the object of building or higher, unmanned plane can cause bigger damage, gently
Person can reduce the service life of unmanned plane, and severe one then can directly cause unmanned plane to be continuing with.
Summary of the invention
It is an object of the invention to provide the unmanned plane that a kind of protective value is high, to solve above-mentioned background technology
The problem of middle proposition.
For achieving the above object, the present invention provides following technical scheme: the unmanned plane that a kind of protective value is high,
Including chassis body, the both sides of described chassis body have been fixedly connected with two double-vane supports, two double-vanes
Support is symmetrical arranged with the axis of chassis body, and the front and back of described double-vane support is all symmetrical fixing
Connecting and have driving arm, described driving arm is provided with driving means away from one end of double-vane support, described
On double-vane support and be positioned at the both sides of driving arm and be respectively fixedly connected with a fixed support, described fixing
Frame is fixedly connected with protection ring away from one end of double-vane support, and described protection ring is socketed in outside driving means
Portion, described protection ring offers spring groove away from the sidewall of chassis body, is respectively provided with in described spring groove
Limited location plate and damping spring, one end of described damping spring is fixing with the cell wall of spring groove to be connected, described
Damping spring is fixed be connected away from one end of spring groove and the side of limiting plate, and described limiting plate is away from damping
The side of spring is fixedly connected with buffer stopper, and described buffer stopper runs through spring groove setting outside with protection ring
The first cushion pad fixing connect, the protection ring on the left of described chassis body passes through protection board and chassis body
The protection ring on right side is fixing to be connected, and the outer surface of described protection board is provided with the second cushion pad.
Preferably, described support bracket fastened quantity is two, and two fixed supports are with the axis of driving arm
Line is symmetrical arranged.
Preferably, described protection board is arcuate structure, and described second cushion pad is positioned at the arc top of arcuate structure
End.
Preferably, described protection ring is provided with the 3rd cushion pad away from the sidewall of double-vane support.
Compared with prior art, the invention has the beneficial effects as follows:
(1), unmanned plane that protective value of the present invention is high, simple in construction, easy to use, operator
To unmanned plane being played preferably protection, hitting when reducing collision when of unmanned plane operational error
Hit power, propeller will not be damaged, higher to the protective value of unmanned plane, improve unmanned plane
Service life.
(2), unmanned plane that protective value of the present invention is high, by the first cushion pad, buffer stopper, limiting plate
With damping spring with the use of, it is possible to slow down the produced impact force of collision, and rammer will not be made
Directly cause with unmanned plane and contact, it is to avoid unmanned plane is caused the situation of bigger damage by shock.
Accompanying drawing explanation
Fig. 1 is present configuration schematic diagram；
Fig. 2 is the partial structurtes profile of A-A of the present invention.
In figure: 1 chassis body, 2 double-vane supports, 3 driving arms, 4 driving means, 5 fixed supports,
6 protection rings, 7 spring grooves, 8 limiting plates, 9 damping springs, 10 buffer stoppers, 11 first cushion pads, 12
Protection board, 13 second cushion pads, 14 the 3rd cushion pads.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the present invention, and
It is not all, of embodiment.Based on the embodiment in the present invention, those of ordinary skill in the art are not doing
Go out the every other embodiment obtained under creative work premise, broadly fall into the scope of protection of the invention.
Referring to Fig. 1-2, the present invention provides a kind of technical scheme: the unmanned plane that a kind of protective value is high, bag
Including chassis body 1, the both sides of chassis body 1 have been fixedly connected with two double-vane supports 2, and two double-vanes prop up
Frame 2 is symmetrical arranged with the axis of chassis body 1, and the front and back of double-vane support 2 is all symmetrical fixing
Connecting and have driving arm 3, driving arm 3 is provided with driving means 4 away from one end of double-vane support 2, double
On wing support 2 and be positioned at the both sides of driving arm 3 and be respectively fixedly connected with a fixed support 5, fix for two
Support 5 is symmetrical arranged with the axis of driving arm 3, and fixed support 5 is away from one end of double-vane support 2
Being fixedly connected with protection ring 6, protection ring 6 is provided with the 3rd cushion pad 14 away from the sidewall of double-vane support 2,
Protection ring 6 is socketed in the outside of driving means 4, and protection ring 6 offers away from the sidewall of chassis body 1
Spring groove 7, is respectively arranged with limiting plate 8 and damping spring 9, one end of damping spring 9 in spring groove 7
Fixing with the cell wall of spring groove 7 being connected, damping spring 9 is away from one end of spring groove 7 and limiting plate 8
Side is fixing to be connected, and limiting plate 8 is fixedly connected with buffer stopper 10 away from the side of damping spring 9, buffering
Block 10 runs through spring groove 7 and first cushion pad 11 that arrange outside with protection ring 6 is fixed and be connected, and passes through
First cushion pad 11, buffer stopper 10, limiting plate 8 and damping spring 9 with the use of, it is possible to slow down and touch
Hit produced impact force, and rammer will not be made directly to cause with unmanned plane contact, it is to avoid shock
Unmanned plane is caused the situation of bigger damage, protection ring on the left of chassis body 16 by protection board 12 with
The fixing connection of protection ring 6 on the right side of chassis body 1, is used by protection board 12 mating protection ring 6, energy
Enough protecting unmanned plane is omnibearing, the outer surface of protection board 12 is provided with the second cushion pad 13, protects
Backplate 12 is arcuate structure, and the second cushion pad 13 is positioned at the arc top of arcuate structure, simple in construction, makes
With convenient, operator are to unmanned plane operational error when, unmanned plane can be played preferably protection,
Reduce impact force during collision, propeller will not be damaged, higher to the protective value of unmanned plane,
Improve the service life of unmanned plane.
Although an embodiment of the present invention has been shown and described, for those of ordinary skill in the art
Speech, it is possible to understand that these embodiments can be carried out without departing from the principles and spirit of the present invention
Multiple change, revising, replace and modification, the scope of the present invention is limited by claims and equivalent thereof
Fixed.
Claims (4)
1. the unmanned plane that protective value is high, including chassis body (1), it is characterised in that: described machine
The both sides of shell main body (1) have been fixedly connected with two double-vane supports (2), two double-vane supports (2) with
The axis of chassis body (1) is symmetrical arranged, and the front and back of described double-vane support (2) is the most symmetrical
Being fixedly connected with driving arm (3), described driving arm (3) sets away from one end of double-vane support (2)
Being equipped with driving means (4), described double-vane support (2) is upper and is positioned at the both sides of driving arm (3) respectively
Being fixedly connected with a fixed support (5), described fixed support (5) is away from one end of double-vane support (2)
Being fixedly connected with protection ring (6), described protection ring (6) is socketed in the outside of driving means (4), institute
State protection ring (6) and offer spring groove (7), described spring groove (7) away from the sidewall of chassis body (1)
Inside it is respectively arranged with limiting plate (8) and damping spring (9), one end of described damping spring (9) and bullet
The cell wall of spring groove (7) is fixing to be connected, and described damping spring (9) is away from one end of spring groove (7) and limit
The side of position plate (8) is fixing to be connected, and described limiting plate (8) is fixed away from the side of damping spring (9)
Connect and have buffer stopper (10), described buffer stopper (10) to run through spring groove (7) with protection ring (6) outward
The first cushion pad (11) that portion is arranged is fixing to be connected, the protection ring (6) in described chassis body (1) left side
It is connected by protection board (12) is fixing with the protection ring (6) on chassis body (1) right side, described protection
The outer surface of plate (12) is provided with the second cushion pad (13).
The unmanned plane that a kind of protective value the most according to claim 1 is high, it is characterised in that: described
The quantity of fixed support (5) is two, and two fixed supports (5) are with the axis of driving arm (3)
It is symmetrical arranged.
The unmanned plane that a kind of protective value the most according to claim 1 is high, it is characterised in that: described
Protection board (12) is arcuate structure, and described second cushion pad (13) is positioned at the arc top of arcuate structure.
The unmanned plane that a kind of protective value the most according to claim 1 is high, it is characterised in that: described
Protection ring (6) is provided with the 3rd cushion pad (14) away from the sidewall of double-vane support (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610438237.7A CN106005384B (en) | 2016-06-20 | 2016-06-20 | Unmanned aerial vehicle that protective properties is high |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610438237.7A CN106005384B (en) | 2016-06-20 | 2016-06-20 | Unmanned aerial vehicle that protective properties is high |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106005384A true CN106005384A (en) | 2016-10-12 |
| CN106005384B CN106005384B (en) | 2019-01-04 |
Family
ID=57088705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610438237.7A Expired - Fee Related CN106005384B (en) | 2016-06-20 | 2016-06-20 | Unmanned aerial vehicle that protective properties is high |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106005384B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741829A (en) * | 2017-02-18 | 2017-05-31 | 河北翔拓航空科技有限公司 | A kind of anti-unmanned plane central frame of integral type three |
| CN106828951A (en) * | 2017-01-21 | 2017-06-13 | 徐志勇 | Based on the urban public security unmanned plane that Internet of Things is wirelessly transferred |
| CN107472535A (en) * | 2017-09-20 | 2017-12-15 | 王月娟 | A kind of unmanned plane hood of shatter-resistant |
| CN108116651A (en) * | 2017-12-31 | 2018-06-05 | 贵州大学 | It is a kind of that there is the unmanned plane of Anti-bumping protection |
| CN108545176A (en) * | 2018-04-20 | 2018-09-18 | 姜英辰 | A kind of novel civilian unmanned plane |
| CN108622426A (en) * | 2018-04-26 | 2018-10-09 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN108928467A (en) * | 2018-06-01 | 2018-12-04 | 芜湖超源力工业设计有限公司 | A kind of drop-proof unmanned plane |
| CN109178332A (en) * | 2018-09-30 | 2019-01-11 | 重庆水利电力职业技术学院 | A kind of energy-saving type forestry pests & diseases intellectual monitoring prevention and treatment unmanned plane |
| CN110584527A (en) * | 2019-11-03 | 2019-12-20 | 河北工程大学 | Be used for clear unmanned aerial vehicle of high building outer wall body |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202170017U (en) * | 2011-07-12 | 2012-03-21 | 北京诚志北分机电技术有限公司 | Unmanned aerial vehicle |
| CN104443411A (en) * | 2014-10-27 | 2015-03-25 | 成都好飞机器人科技有限公司 | Quad-rotor unmanned aerial vehicle with anti-collision protective device |
| CN204750580U (en) * | 2015-07-15 | 2015-11-11 | 长空智能科技（深圳）有限公司 | Agricultural plant protection unmanned aerial vehicle's resistant collision structure |
| CN205311898U (en) * | 2016-01-21 | 2016-06-15 | 苏州盛世十月软件技术有限公司 | Anticollision unmanned aerial vehicle |
-
2016
- 2016-06-20 CN CN201610438237.7A patent/CN106005384B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202170017U (en) * | 2011-07-12 | 2012-03-21 | 北京诚志北分机电技术有限公司 | Unmanned aerial vehicle |
| CN104443411A (en) * | 2014-10-27 | 2015-03-25 | 成都好飞机器人科技有限公司 | Quad-rotor unmanned aerial vehicle with anti-collision protective device |
| CN204750580U (en) * | 2015-07-15 | 2015-11-11 | 长空智能科技（深圳）有限公司 | Agricultural plant protection unmanned aerial vehicle's resistant collision structure |
| CN205311898U (en) * | 2016-01-21 | 2016-06-15 | 苏州盛世十月软件技术有限公司 | Anticollision unmanned aerial vehicle |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828951A (en) * | 2017-01-21 | 2017-06-13 | 徐志勇 | Based on the urban public security unmanned plane that Internet of Things is wirelessly transferred |
| CN106741829B (en) * | 2017-02-18 | 2019-05-14 | 河北翔拓航空科技有限公司 | A kind of integral type three proofings unmanned plane central frame |
| CN106741829A (en) * | 2017-02-18 | 2017-05-31 | 河北翔拓航空科技有限公司 | A kind of anti-unmanned plane central frame of integral type three |
| CN107472535A (en) * | 2017-09-20 | 2017-12-15 | 王月娟 | A kind of unmanned plane hood of shatter-resistant |
| CN108116651A (en) * | 2017-12-31 | 2018-06-05 | 贵州大学 | It is a kind of that there is the unmanned plane of Anti-bumping protection |
| CN108545176A (en) * | 2018-04-20 | 2018-09-18 | 姜英辰 | A kind of novel civilian unmanned plane |
| CN108622426B (en) * | 2018-04-26 | 2019-11-08 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN108622426A (en) * | 2018-04-26 | 2018-10-09 | 合肥职业技术学院 | A kind of unmanned plane impact protector equipment |
| CN108928467A (en) * | 2018-06-01 | 2018-12-04 | 芜湖超源力工业设计有限公司 | A kind of drop-proof unmanned plane |
| CN108928467B (en) * | 2018-06-01 | 2021-09-17 | 芜湖超源力工业设计有限公司 | Anti-falling type unmanned aerial vehicle |
| CN109178332A (en) * | 2018-09-30 | 2019-01-11 | 重庆水利电力职业技术学院 | A kind of energy-saving type forestry pests & diseases intellectual monitoring prevention and treatment unmanned plane |
| CN109178332B (en) * | 2018-09-30 | 2020-12-04 | 重庆水利电力职业技术学院 | Energy-conserving formula forestry plant diseases and insect pests intelligent monitoring prevention and cure unmanned aerial vehicle |
| CN110584527A (en) * | 2019-11-03 | 2019-12-20 | 河北工程大学 | Be used for clear unmanned aerial vehicle of high building outer wall body |
| CN110584527B (en) * | 2019-11-03 | 2021-07-06 | 河北工程大学 | Be used for clear unmanned aerial vehicle of high building outer wall body |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106005384B (en) | 2019-01-04 |
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| CF01 | Termination of patent right due to non-payment of annual fee |
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| CF01 | Termination of patent right due to non-payment of annual fee |