CN106005384B - Unmanned aerial vehicle that protective properties is high - Google Patents
Unmanned aerial vehicle that protective properties is high Download PDFInfo
- Publication number
- CN106005384B CN106005384B CN201610438237.7A CN201610438237A CN106005384B CN 106005384 B CN106005384 B CN 106005384B CN 201610438237 A CN201610438237 A CN 201610438237A CN 106005384 B CN106005384 B CN 106005384B
- Authority
- CN
- China
- Prior art keywords
- double
- fixedly connected
- unmanned plane
- vane
- supports
- 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
- 230000001681 protective effect Effects 0.000 title claims description 15
- 238000013016 damping Methods 0.000 claims description 14
- 210000002421 cell wall Anatomy 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000035939 shock Effects 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, specially a kind of unmanned plane that protective value is high.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation.Unmanned plane press application field, can be divided into it is military with it is civilian.
Currently, the protective value in the design and fabrication of existing unmanned plane to unmanned plane in flight does not fill specifically
It sets, and unmanned plane needs manual control, unmanned plane can awing collide building if initial contact and operation error
Object or higher object can cause biggish damage to unmanned plane, and less serious case can reduce the service life of unmanned plane, and severe one then can
Directly unmanned plane is caused to continue to use.
Summary of the invention
It is mentioned above in the background art to solve the purpose of the present invention is to provide a kind of unmanned plane that protective value is high
Problem.
To achieve the above object, the invention provides the following technical scheme: a kind of unmanned plane that protective value is high, including casing
Main body, the two sides of the chassis body are fixedly connected to two double-vane brackets, and two double-vane brackets are with the axis of chassis body
Line is symmetrical arranged, and the front and back of the double-vane bracket is symmetrically fixedly connected with driving arm, and the driving arm is separate
One end of double-vane bracket is provided with driving device, on the double-vane bracket and is located at the two sides of driving arm and has been respectively fixedly connected with
One fixed bracket, the fixed bracket are fixedly connected with protection ring far from one end of double-vane bracket, and the protection ring is socketed in drive
The outside of dynamic device, the protection ring offer spring groove far from the side wall of chassis body, are respectively arranged in the spring groove
Limit plate and damping spring, one end of the damping spring are fixedly connected with the cell wall of spring groove, and the damping spring is far from bullet
One end of spring slot is fixedly connected with the side of limit plate, and the limit plate is fixedly connected with buffering far from the side of damping spring
Block, the buffer stopper are fixedly connected through spring groove and with the first cushion being arranged outside protection ring, and the chassis body is left
The protection ring of side is fixedly connected by protection board with the protection ring on the right side of chassis body, and the outer surface of the protection board is provided with
Two cushions.
Preferably, the support bracket fastened quantity of the driving arm side is two, and two fixed brackets are with driving arm
Central axes be symmetrical arranged.
Preferably, the protection board is arcuate structure, and second cushion is located at the arc top of arcuate structure.
Preferably, the protection ring is provided with third cushion far from the side wall of double-vane bracket.
Compared with prior art, the beneficial effects of the present invention are:
(1), the high unmanned plane of protective value of the present invention, structure is simple, easy to use, operates in operator to unmanned plane
Preferable protection can be played when fault to unmanned plane, reduces impact force when collision, propeller will not be caused to hurt
Evil, it is higher to the protective value of unmanned plane, improve the service life of unmanned plane.
(2), the high unmanned plane of protective value of the present invention passes through the first cushion, buffer stopper, limit plate and damping spring
It is used cooperatively, impact force caused by collision can be slowed down, and rammer will not be made directly to cause to contact with unmanned plane, avoided
Hit the situation for causing to unmanned plane larger damage.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention；
Fig. 2 is the partial structurtes sectional view of A-A of the present invention.
In figure: 1 chassis body, 2 double-vane brackets, 3 driving arms, 4 driving devices, 5 fixed brackets, 6 protection rings, 7 springs
Slot, 8 limit plates, 9 damping springs, 10 buffer stoppers, 11 first cushions, 12 protection boards, 13 second cushions, 14 thirds buffering
Pad.
Specific embodiment
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 description, 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.
The present invention provides a kind of technical solution referring to FIG. 1-2: a kind of unmanned plane that protective value is high, including casing master
Body 1, the two sides of chassis body 1 are fixedly connected to two double-vane brackets 2, and two double-vane brackets 2 are with the central axes of chassis body 1
It is symmetrical arranged, the front and back of double-vane bracket 2 is symmetrically fixedly connected with driving arm 3, and driving arm 3 is far from double-vane bracket
2 one end is provided with driving device 4, on double-vane bracket 2 and is located at the two sides of driving arm 3 and has been respectively fixedly connected with a fixed branch
Frame 5, the quantity of the fixation bracket 5 of 3 side of driving arm are two, and two fixed brackets 5 are symmetrical with the central axes of driving arm 3
Setting, fixed bracket 5 are fixedly connected with protection ring 6, side wall of the protection ring 6 far from double-vane bracket 2 far from one end of double-vane bracket 2
It is provided with third cushion 14, protection ring 6 is socketed in the outside of driving device 4, and protection ring 6 is opened far from the side wall of chassis body 1
Equipped with spring groove 7, limit plate 8 and damping spring 9, one end and the spring groove 7 of damping spring 9 are respectively arranged in spring groove 7
Cell wall is fixedly connected, and the one end of damping spring 9 far from spring groove 7 is fixedly connected with the side of limit plate 8, and limit plate 8 is separate to be subtracted
The side of shake spring 9 is fixedly connected with buffer stopper 10, buffer stopper 10 through spring groove 7 and be arranged outside protection ring 6 first
Cushion 11 is fixedly connected, can by being used cooperatively for the first cushion 11, buffer stopper 10, limit plate 8 and damping spring 9
Slow down impact force caused by collision, and rammer will not be made directly to cause to contact with unmanned plane, avoids shock to nobody
Machine causes the situation of larger damage, the protection that the protection ring 6 in 1 left side of chassis body passes through 1 right side of protection board 12 and chassis body
Ring 6 is fixedly connected, by 12 mating protection ring 6 of protection board use, can be comprehensive to unmanned plane protect, protection board 12
Outer surface be provided with the second cushion 13, protection board 12 is arcuate structure, and the second cushion 13 is located at the arc top of arcuate structure
End, structure is simple, easy to use, can play preferable guarantor to unmanned plane when operator is to unmanned plane operation error
Shield, reduces impact force when collision, will not damage to propeller, higher to the protective value of unmanned plane, improves nothing
Man-machine service life.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (4)
1. a kind of unmanned plane that protective value is high, including chassis body (1), it is characterised in that: the two sides of the chassis body (1)
Two double-vane brackets (2) are fixedly connected to, two double-vane brackets (2) are symmetrical arranged with the central axes of chassis body (1), described
The front and back of double-vane bracket (2) is symmetrically fixedly connected with driving arm (3), and the driving arm (3) is far from double-vane branch
One end of frame (2) is provided with driving device (4), is fixed respectively on the double-vane bracket (2) and positioned at the two sides of driving arm (3)
One fixed bracket (5) are connected with, the fixed bracket (5) is fixedly connected with protection ring (6) far from the one end of double-vane bracket (2),
The protection ring (6) is socketed in the outside of driving device (4), and the protection ring (6) offers far from the side wall of chassis body (1)
Spring groove (7), is respectively arranged with limit plate (8) and damping spring (9) in the spring groove (7), and the one of the damping spring (9)
End is fixedly connected with the cell wall of spring groove (7), and the one of the damping spring (9) one end and limit plate (8) far from spring groove (7)
Side is fixedly connected, and the limit plate (8) is fixedly connected with buffer stopper (10), the buffer stopper far from the side of damping spring (9)
(10) it is fixedly connected through spring groove (7) and with the first cushion (11) being arranged outside protection ring (6), the chassis body
(1) protection ring (6) on the left of is fixedly connected by protection board (12) with the protection ring (6) on the right side of chassis body (1), the protection
The outer surface of plate (12) is provided with the second cushion (13).
2. a kind of high unmanned plane of protective value according to claim 1, it is characterised in that: the driving arm (3) one
The quantity of the fixation bracket (5) of side is two, and two fixed brackets (5) are symmetrical arranged with the central axes of driving arm (3).
3. a kind of high unmanned plane of protective value according to claim 1, it is characterised in that: the protection board (12) is arc
Shape structure, second cushion (13) are located at the arc top of arcuate structure.
4. a kind of high unmanned plane of protective value according to claim 1, it is characterised in that: the protection ring (6) is separate
The side wall of double-vane bracket (2) is provided with third cushion (14).
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 CN106005384A (en) | 2016-10-12 |
| CN106005384B true 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) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828951B (en) * | 2017-01-21 | 2019-02-22 | 杭州木书科技有限公司 | Urban public security unmanned plane based on Internet of Things wireless transmission |
| 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 |
| 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 |
| 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 |
| 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 |
| CN110584527B (en) * | 2019-11-03 | 2021-07-06 | 河北工程大学 | A drone for cleaning the exterior walls of high-rise buildings |
| CN111942579A (en) * | 2020-09-24 | 2020-11-17 | 河南鲲之腾教育科技有限公司 | Traversing machine |
| CN111942580A (en) * | 2020-09-24 | 2020-11-17 | 河南鲲之腾教育科技有限公司 | Pass through quick-witted frame and pass through machine |
Family Cites Families (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
Also Published As
| Publication number | Publication date |
|---|---|
| CN106005384A (en) | 2016-10-12 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190104 Termination date: 20210620 |
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| CF01 | Termination of patent right due to non-payment of annual fee |