CN107472535A - A kind of unmanned plane hood of shatter-resistant - Google Patents
A kind of unmanned plane hood of shatter-resistant Download PDFInfo
- Publication number
- CN107472535A CN107472535A CN201710849535.XA CN201710849535A CN107472535A CN 107472535 A CN107472535 A CN 107472535A CN 201710849535 A CN201710849535 A CN 201710849535A CN 107472535 A CN107472535 A CN 107472535A
- Authority
- CN
- China
- Prior art keywords
- hood
- main body
- unmanned plane
- flabellum
- guard 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.)
- Pending
Links
- 241000883990 Flabellum Species 0.000 claims abstract description 51
- 238000013016 damping Methods 0.000 claims abstract description 21
- 241000237983 Trochidae Species 0.000 claims abstract description 15
- 230000003139 buffering effect Effects 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Filtering Of Dispersed Particles In Gases (AREA)
Abstract
The invention discloses a kind of unmanned plane hood of shatter-resistant, including hood main body and support feet, hood accessory body is installed above the hood main body, and flabellum guard ring is fixed with the outside of hood main body, flabellum is provided with the inside of the flabellum guard ring, and flabellum guard ring and the junction of hood main body are fixed with fixing bolt, damping spring is installed on the downside of the hood accessory body, and the lower end of damping spring is fixedly connected with main body top shell, the upper end of the support feet is fixedly connected with unmanned plane body, and the upside of unmanned plane body is connected by fixing bolt and fixing threaded hole with hood main body.The unmanned plane hood of the shatter-resistant is provided with hood accessory body and damping spring, row buffering can be entered to hood main body by damping spring, to prevent hood main body to be damaged, and then it ensure that the safe handling of whole unmanned plane, flabellum guard ring is additionally provided with hood main body, it can avoid flabellum that accidental damage occurs, also indirectly ensure that the service life of the unmanned plane.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, the unmanned plane hood of specially a kind of shatter-resistant.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, Huo Zheyou
Car-mounted computer fully or intermittently independently operates.
Increasingly mature with unmanned air vehicle technique, its use range is increasing, but during the use of unmanned plane,
Often make unmanned plane during transport or use, collide or drop with other things, this will make unmanned plane
It is damaged, and then lessens the service life of unmanned plane, also reduces the use value of unmanned plane, so we have proposed
The unmanned plane hood of a kind of shatter-resistant, in order to solve the problems, such as above-mentioned middle proposition.
The content of the invention
It is an object of the invention to provide a kind of unmanned plane hood of shatter-resistant, to solve the current of above-mentioned background technology proposition
The problem of in the market unmanned plane collides or is easily damaged when dropping.
To achieve the above object, the present invention provides following technical scheme：A kind of unmanned plane hood of shatter-resistant, including hood master
Body and support feet, hood accessory body is installed above the hood main body, and flabellum guard ring is fixed with the outside of hood main body,
Flabellum is provided with the inside of the flabellum guard ring, and flabellum guard ring and the junction of hood main body are fixed with fixing bolt,
Damping spring is installed, and the lower end of damping spring is fixedly connected with main body top shell, the support on the downside of the hood accessory body
The upper end of pin is fixedly connected with unmanned plane body, and the upside of unmanned plane body passes through fixing bolt and fixing threaded hole and hood master
Body phase connects.
Preferably, it is structure as a whole between the hood main body, flabellum guard ring and main body top shell.
Preferably, the profile of the hood accessory body is convex disk, and hood accessory body is located at the centre bit of hood main body
Put, and the peak of hood accessory body upper side is higher than the peak of flabellum guard ring.
Preferably, the internal diameter of the flabellum guard ring is more than the maximum outside diameter of the rotation of flabellum, and flabellum guard ring
Width is more than the vertical width of flabellum.
Preferably, the fixing bolt runs through hood main body, and fixing bolt and hood main body and nothing by fixing threaded hole
Man-machine body is threaded connection, and fixing bolt is embedded in hood body interior.
Preferably, the damping spring is provided with three, and it is evenly distributed between hood accessory body and main body top shell, and
And between the upper and lower ends of damping spring and hood accessory body and main body top shell it is to be fixedly connected.
Compared with prior art, the beneficial effects of the invention are as follows：The unmanned plane hood of the shatter-resistant be provided with hood accessory body and
Damping spring, when can be collided or drop in hood accessory body, row buffering is entered to hood main body by damping spring,
To prevent hood main body to be damaged, and then the safe handling of whole unmanned plane is ensure that, fan is additionally provided with hood main body
Leaf guard ring, effectively flabellum can be protected, and then avoid flabellum that accidental damage occurs, influence the normal of the unmanned plane
Use, also indirectly ensure that the service life of the unmanned plane, improve the use value of the unmanned plane, also set up on device
There are fixing bolt and fixing threaded hole, the stable connection between hood main body and unmanned plane body can be effectively ensured, and then ensure
The service behaviour of the unmanned plane.
Brief description of the drawings
Fig. 1 is overlooking the structure diagram of the present invention；
Fig. 2 is main view part section structural representation of the present invention；
Fig. 3 is hood main body present invention looks up structural representation of the present invention；
Fig. 4 is that hood main body side of the present invention cuts open structural representation.
In figure：1st, hood main body, 2, hood accessory body, 3, flabellum guard ring, 4, flabellum, 5, fixing bolt, 6, damping spring,
7th, main body top shell, 8, support feet, 9, unmanned plane body, 10, fixing threaded hole.
Embodiment
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 clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
Fig. 1-4 are referred to, the present invention provides a kind of technical scheme：A kind of unmanned plane hood of shatter-resistant, including hood main body
1st, hood accessory body 2, flabellum guard ring 3, flabellum 4, fixing bolt 5, damping spring 6, main body top shell 7, support feet 8, unmanned plane machine
Body 9 and fixing threaded hole 10, the top of hood main body 1 is provided with hood accessory body 2, and the outside of hood main body 1 is fixed with flabellum and prevented
Guard ring 3, it is structure as a whole between hood main body 1, flabellum guard ring 3 and main body top shell 7, it is ensured that the unmanned plane hood
Performance, the profile of hood accessory body 2 is convex disk, and hood accessory body 2 is located at the center of hood main body 1, and
The peak of the upper side of hood accessory body 2 is higher than the peak of flabellum guard ring 3, ensure that the performance of hood accessory body 2, and then
The security performance of the unmanned plane is improved, the inner side of flabellum guard ring 3 is provided with flabellum 4, and flabellum guard ring 3 and hood main body
1 junction is fixed with fixing bolt 5, and the internal diameter of flabellum guard ring 3 is more than the maximum outside diameter of the rotation of flabellum 4, and flabellum
The width of guard ring 3 is more than the vertical width of flabellum 4, can both ensure that flabellum guard ring 3 worked the normal guard of flabellum 4,
Harmful effect of the flabellum guard ring 3 to flabellum 4 can be avoided again, fixing bolt 5 runs through hood main body 1 by fixing threaded hole 10,
And fixing bolt 5 is to be threadedly coupled with hood main body 1 and unmanned plane body 9, and fixing bolt 5 is embedded in hood main body 1
Portion, the stable connection between hood main body 1 and unmanned plane body 9 can be effectively ensured, and then ensure that the work of the unmanned plane
Performance, the downside of hood accessory body 2 is provided with damping spring 6, and the lower end of damping spring 6 is fixedly connected with main body top shell 7, damping
Spring 6 is provided with three, and it is evenly distributed between hood accessory body 2 and main body top shell 7, and up and down the two of damping spring 6
End can be effectively ensured the stress performance of hood accessory body 2, also carry with being to be fixedly connected between hood accessory body 2 and main body top shell 7
The high operating efficiency of hood accessory body 2, the upper end of support feet 8 is fixedly connected with unmanned plane body 9, and unmanned plane body 9 is upper
Side is connected by fixing bolt 5 and fixing threaded hole 10 with hood main body 1.
Operation principle：When using the unmanned plane hood of the shatter-resistant, first, hood main body 1 is arranged to unmanned plane body 9
On, meanwhile, the flabellum guard ring 3 in the outside of hood main body 1 can get up the protection of flabellum 4 on unmanned plane body 9, then fix spiral shell
Bolt 5, can be so that hood main body 1 and unmanned plane body 9 to be fixed together by the fixing threaded hole 10 in hood main body 1, the above
Just the installation wage of the unmanned plane hood is completed, when unmanned plane is being collided, or in-flight dropped, hood pair
Body 2 and flabellum guard ring 3 can be in contact with the external world first, and flabellum guard ring 3 can avoid flabellum 4 from being damaged, and hood accessory body 2
The damping spring 6 of downside can buffer the impulsive force suffered by the unmanned plane, and then ensure that the safe to use of the unmanned plane, with
On just complete protected working of the unmanned plane hood to unmanned plane, and the content not being described in detail in this specification belongs to
Prior art known to professional and technical personnel in the field.
Although the present invention is described in detail with reference to the foregoing embodiments, for those skilled in the art,
It can still modify to the technical scheme described in foregoing embodiments, or which part technical characteristic is carried out etc.
With replacing, within the spirit and principles of the invention, any modification, equivalent substitution and improvements made etc., this should be included in
Within the protection domain of invention.
Claims (6)
1. a kind of unmanned plane hood of shatter-resistant, including hood main body（1）And support feet（8）, it is characterised in that：The hood main body
（1）Top hood accessory body is installed（2）, and hood main body（1）Outside be fixed with flabellum guard ring（3）, the flabellum prevents
Guard ring（3）Inner side be provided with flabellum（4）, and flabellum guard ring（3）With hood main body（1）Junction be fixed with fixing bolt
（5）, the hood accessory body（2）Downside damping spring is installed（6）, and damping spring（6）Lower end be fixedly connected with main body
Top shell（7）, the support feet（8）Upper end be fixedly connected with unmanned plane body（9）, and unmanned plane body（9）Upside pass through
Fixing bolt（5）And fixing threaded hole（10）With hood main body（1）It is connected.
A kind of 2. unmanned plane hood of shatter-resistant according to claim 1, it is characterised in that：The hood main body（1）, flabellum
Guard ring（3）With main body top shell（7）Between be structure as a whole.
A kind of 3. unmanned plane hood of shatter-resistant according to claim 1, it is characterised in that：The hood accessory body（2）It is outer
Shape is convex disk, and hood accessory body（2）Positioned at hood main body（1）Center, and hood accessory body（2）Upper side
Peak is higher than flabellum guard ring（3）Peak.
A kind of 4. unmanned plane hood of shatter-resistant according to claim 1, it is characterised in that：The flabellum guard ring（3）'s
Internal diameter is more than flabellum（4）Rotation maximum outside diameter, and flabellum guard ring（3）Width be more than flabellum（4）Vertical width.
A kind of 5. unmanned plane hood of shatter-resistant according to claim 1, it is characterised in that：The fixing bolt（5）Pass through
Fixing threaded hole（10）Through hood main body（1）, and fixing bolt（5）With hood main body（1）With unmanned plane body（9）It is screw thread
Connection, and fixing bolt（5）Embedded hood main body（1）It is internal.
A kind of 6. unmanned plane hood of shatter-resistant according to claim 1, it is characterised in that：The damping spring（6）Set
There are three, and it is evenly distributed on hood accessory body（2）With main body top shell（7）Between, and damping spring（6）Upper and lower ends with
Hood accessory body（2）With main body top shell（7）Between be to be fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710849535.XA CN107472535A (en) | 2017-09-20 | 2017-09-20 | A kind of unmanned plane hood of shatter-resistant |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710849535.XA CN107472535A (en) | 2017-09-20 | 2017-09-20 | A kind of unmanned plane hood of shatter-resistant |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107472535A true CN107472535A (en) | 2017-12-15 |
Family
ID=60585660
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710849535.XA Pending CN107472535A (en) | 2017-09-20 | 2017-09-20 | A kind of unmanned plane hood of shatter-resistant |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107472535A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108100238A (en) * | 2018-02-05 | 2018-06-01 | 成都市煜沣科技有限公司 | A kind of safe floor stand of Small Civil unmanned plane |
| 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 |
| CN108163186A (en) * | 2018-01-16 | 2018-06-15 | 安徽翼讯飞行安全技术有限公司 | A kind of unmanned plane landing damping device |
| CN111055992A (en) * | 2020-01-07 | 2020-04-24 | 北京致媒科技有限公司 | Unmanned aerial vehicle aircraft bonnet and unmanned aerial vehicle of combined material |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN205198967U (en) * | 2015-11-28 | 2016-05-04 | 刘晓峰 | Many rotors flight simulator |
| CN106005384A (en) * | 2016-06-20 | 2016-10-12 | 深圳市勤新科技有限公司 | Unmanned aerial vehicle that protective properties is high |
| KR20170058526A (en) * | 2015-11-19 | 2017-05-29 | 하태훈 | Disk shaped drone |
| CN206502043U (en) * | 2017-03-04 | 2017-09-19 | 华北电力大学（保定） | A kind of infrared, visible ray dual camera special unmanned plane of taking photo by plane of power-line patrolling |
| CN207274981U (en) * | 2017-09-20 | 2018-04-27 | 王月娟 | A kind of unmanned plane hood of shatter-resistant |
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2017
- 2017-09-20 CN CN201710849535.XA patent/CN107472535A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20170058526A (en) * | 2015-11-19 | 2017-05-29 | 하태훈 | Disk shaped drone |
| CN205198967U (en) * | 2015-11-28 | 2016-05-04 | 刘晓峰 | Many rotors flight simulator |
| CN106005384A (en) * | 2016-06-20 | 2016-10-12 | 深圳市勤新科技有限公司 | Unmanned aerial vehicle that protective properties is high |
| CN206502043U (en) * | 2017-03-04 | 2017-09-19 | 华北电力大学（保定） | A kind of infrared, visible ray dual camera special unmanned plane of taking photo by plane of power-line patrolling |
| CN207274981U (en) * | 2017-09-20 | 2018-04-27 | 王月娟 | A kind of unmanned plane hood of shatter-resistant |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN108163186A (en) * | 2018-01-16 | 2018-06-15 | 安徽翼讯飞行安全技术有限公司 | A kind of unmanned plane landing damping device |
| CN108100238A (en) * | 2018-02-05 | 2018-06-01 | 成都市煜沣科技有限公司 | A kind of safe floor stand of Small Civil unmanned plane |
| CN111055992A (en) * | 2020-01-07 | 2020-04-24 | 北京致媒科技有限公司 | Unmanned aerial vehicle aircraft bonnet and unmanned aerial vehicle of combined material |
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| 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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171215 |
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| WD01 | Invention patent application deemed withdrawn after publication |