CN107600416A - A kind of split type unmanned plane of good damping effect - Google Patents
A kind of split type unmanned plane of good damping effect Download PDFInfo
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- CN107600416A CN107600416A CN201710877279.5A CN201710877279A CN107600416A CN 107600416 A CN107600416 A CN 107600416A CN 201710877279 A CN201710877279 A CN 201710877279A CN 107600416 A CN107600416 A CN 107600416A
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- unmanned plane
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- rotor motor
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Abstract
A kind of split type unmanned plane of good damping effect, unmanned plane main body is box-like, the front and rear sides of the unmanned plane main body are respectively provided with a rotor support, rotor motor is installed in the outboard end of the rotor support, each corresponding 24 rotor blades of rotor motor, the rotor blade is arranged on the rotating shaft outer wall of rotor motor, the rotor blade angularly around corresponding rotor motor rotating shaft center line one week, a pair of upper magnetic sheets for including beam are respectively installed before and after the unmanned plane bottom part body, the inverted U-shaped landing gear has a pair, the top of the inverted U-shaped landing gear respectively has a pair of lower magnetic sheets for including beam corresponding with the upper magnetic sheet for including beam.The application unmanned plane uses split-type design, and beam of the original design in bottom is designed between up-down structure, so as to which the integral shock-absorbing effect of unmanned plane greatly improved, and can carry out assembling as needed using split design and improve properties of product.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of split type unmanned plane of good damping effect.
Background technology
Science and technology is constantly improving, and with the continuous development of artificial intelligence technology, unmanned air vehicle technique development is extremely rapid, tradition
Unmanned plane is generally an entirety, and this unmanned plane is primarily present following problem；The bad dismounting of 1 structure, function are more single；2
Descent is easily damaged its internals by greater impact reduces the unmanned plane life-span；3 are not easy to produce in batches, a foregone conclusion be present
Limit.
The content of the invention
In order to solve above-mentioned problem, the present invention provides a kind of split type unmanned plane of good damping effect, this nobody
Machine uses split-type design, beam of the original design in bottom is designed between up-down structure, so as to which nothing greatly improved
Man-machine integral shock-absorbing effect, and can carry out assembling as needed using split design and improve properties of product, for up to this
Purpose, the present invention provide a kind of split type unmanned plane of good damping effect, including unmanned plane main body, rotor support, rotor motor,
Rotor blade, inverted U-shaped landing gear, the upper magnetic sheet for including beam and the lower magnetic sheet for including beam, the unmanned plane main body are
Box-like, the front and rear sides of the unmanned plane main body are respectively provided with a rotor support, pacify in the outboard end of the rotor support
Equipped with rotor motor, each rotor motor corresponds to 2-4 rotor blade, and the rotor blade is arranged on outside the rotating shaft of rotor motor
Wall, the rotor blade angularly around corresponding rotor motor rotating shaft center line one week, before and after the unmanned plane bottom part body
A pair of upper magnetic sheets for including beam are respectively installed, the inverted U-shaped landing gear has a pair, and the top of the inverted U-shaped landing gear is each
There are a pair of lower magnetic sheets for including beam corresponding with the upper magnetic sheet for including beam.
Further improvement of the present invention, the front and rear side of the unmanned plane main body are installed with infrared inductor, set sense
Device is answered to be monitored with surrounding environment.
A damping sucker is respectively fixedly mounted in further improvement of the present invention, the both ends of the inverted U-shaped landing gear, and setting subtracts
Shake sucker can reduce to be impacted caused by landing.
The present invention provides a kind of split type unmanned plane of good damping effect, and it is changed to traditional industry with unmanned plane structure
Make, using split-type design, the connection of its up-down structure is using the upper magnetic sheet for including beam, this particular design, above design
The damping performance of unmanned plane can be greatly improved, then coordinates the damping sucker using effect of landing gear more preferable, the application is from entirety
On significantly reduce in descent bad effect caused by vibrations.
Brief description of the drawings
Fig. 1 is schematic diagram of the present invention；
Component in figure is：
1st, unmanned plane main body；2nd, rotor support；3rd, rotor motor；4th, rotor blade；5th, infrared inductor；6th, inverted U-shaped landing
Frame；7th, the upper magnetic sheet of beam is included；8th, the lower magnetic sheet of beam is included；9th, damping sucker.
Embodiment
The present invention is described in further detail with embodiment below in conjunction with the accompanying drawings：
The present invention provides a kind of split type unmanned plane of good damping effect, and the unmanned plane uses split-type design, will designed originally
Beam in bottom is designed between up-down structure, so as to which the integral shock-absorbing effect of unmanned plane greatly improved, and is used
Split design can carry out assembling as needed and improve properties of product.
The application provides a kind of embodiment.A kind of split type unmanned plane of good damping effect as shown in Figure 1, including nobody
Owner's body 1, rotor support 2, rotor motor 3, rotor blade 4, inverted U-shaped landing gear 6, the upper magnetic sheet 7 for including beam and include
The lower magnetic sheet 8 of beam, the unmanned plane main body 1 are box-like, and the front and rear sides of the unmanned plane main body 1 are respectively provided with a rotation
Wing support 2, rotor motor 3, each rotor motor 3 corresponding 2-4 rotor leaf are installed in the outboard end of the rotor support 2
Piece 4, the rotor blade 4 are arranged on the rotating shaft outer wall of rotor motor 3, and the rotor blade 4 is angularly around corresponding rotor motor 3
Rotating shaft center line one week, a pair of upper magnetic sheets 7 for including beam, institute are respectively installed before and after the bottom of unmanned plane main body 1
Stating inverted U-shaped landing gear 6 has a pair, and respectively there are a pair of lower magnetic sheets 8 for including beam on the top of the inverted U-shaped landing gear 6 with including
The upper magnetic sheet 7 of beam is corresponding.
The application provides a kind of specific embodiment, a kind of split type unmanned plane of good damping effect, including unmanned plane main body
1st, rotor support 2, rotor motor 3, rotor blade 4, inverted U-shaped landing gear 6, the upper magnetic sheet 7 for including beam and beam is included
Lower magnetic sheet 8, for the unmanned plane main body 1 to be box-like, the front and rear side of the unmanned plane main body is installed with infrared inductor, if
Putting inductor can be monitored with surrounding environment, and the front and rear sides of the unmanned plane main body 1 are respectively provided with a rotor support 2,
Rotor motor 3 is installed, the corresponding 2-4 rotor blade 4 of each rotor motor 3 is described in the outboard end of the rotor support 2
Rotor blade 4 is arranged on the rotating shaft outer wall of rotor motor 3, and the rotor blade 4 is angularly around the rotating shaft for corresponding to rotor motor 3
Center line one week, a pair of upper magnetic sheets 7 for including beam, the inverted U-shaped drop are respectively installed before and after the bottom of unmanned plane main body 1
Falling frame 6 has a pair, and a damping sucker is respectively fixedly mounted in the both ends of the inverted U-shaped landing gear, sets damping sucker to reduce
Impacted caused by landing, the top of the inverted U-shaped landing gear 6 respectively there are a pair of lower magnetic sheets 8 for including beam and includes damping
The upper magnetic sheet 7 of pad is corresponding.
The above described is only a preferred embodiment of the present invention, it is not the limit for making any other form to the present invention
System, and any modification made according to technical spirit of the invention or equivalent variations, still fall within present invention model claimed
Enclose.
Claims (3)
1. a kind of split type unmanned plane of good damping effect, including unmanned plane main body（1）, rotor support（2）, rotor motor（3）、
Rotor blade（4）, inverted U-shaped landing gear（6）, include the upper magnetic sheet of beam（7）With the lower magnetic sheet for including beam（8）, it is special
Sign is：The unmanned plane main body（1）To be box-like, the unmanned plane main body（1）Front and rear sides one rotor branch is respectively installed
Frame（2）, the rotor support（2）Outboard end on rotor motor is installed（3）, each rotor motor（3）Corresponding 2-4 rotation
Wing blade（4）, the rotor blade（4）Installed in rotor motor（3）Rotating shaft outer wall, the rotor blade（4）Angularly around
Corresponding rotor motor（3）Rotating shaft center line one week, the unmanned plane main body（1）A pair are respectively provided with before and after bottom and is included and is subtracted
Shake the upper magnetic sheet of pad（7）, the inverted U-shaped landing gear（6）Have a pair, the inverted U-shaped landing gear（6）Top respectively have a pair and include
The lower magnetic sheet of beam（8）Upper magnetic sheet with including beam（7）It is corresponding.
A kind of 2. split type unmanned plane of good damping effect according to claim 1, it is characterised in that：The unmanned owner
Body（1）Front-end and back-end are mounted on infrared inductor（5）.
A kind of 3. split type unmanned plane of good damping effect according to claim 1, it is characterised in that：The inverted U-shaped drop
Fall frame（6）Both ends respectively be fixedly mounted a damping sucker（9）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710877279.5A CN107600416A (en) | 2017-09-25 | 2017-09-25 | A kind of split type unmanned plane of good damping effect |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710877279.5A CN107600416A (en) | 2017-09-25 | 2017-09-25 | A kind of split type unmanned plane of good damping effect |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107600416A true CN107600416A (en) | 2018-01-19 |
Family
ID=61058509
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710877279.5A Pending CN107600416A (en) | 2017-09-25 | 2017-09-25 | A kind of split type unmanned plane of good damping effect |
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| CN (1) | CN107600416A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204236773U (en) * | 2014-11-25 | 2015-04-01 | 南京机电职业技术学院 | A kind of transport Circular article rotary wind type unmanned plane |
| CN204688411U (en) * | 2015-06-01 | 2015-10-07 | 金陵科技学院 | A kind of bird transport unmanned plane |
| CN204776013U (en) * | 2015-06-04 | 2015-11-18 | 东莞中寰智能航空科技有限公司 | Six unmanned aerial vehicle |
| CN206141815U (en) * | 2016-10-08 | 2017-05-03 | 深圳市赛亿科技开发有限公司 | Unmanned aerial vehicle foot rest with descending cushioning effect |
| CN106697269A (en) * | 2015-07-21 | 2017-05-24 | 天津晓奇科技发展有限公司 | Multi-rotor unmanned aerial vehicle carbon tube damping and shock absorption undercarriage |
-
2017
- 2017-09-25 CN CN201710877279.5A patent/CN107600416A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204236773U (en) * | 2014-11-25 | 2015-04-01 | 南京机电职业技术学院 | A kind of transport Circular article rotary wind type unmanned plane |
| CN204688411U (en) * | 2015-06-01 | 2015-10-07 | 金陵科技学院 | A kind of bird transport unmanned plane |
| CN204776013U (en) * | 2015-06-04 | 2015-11-18 | 东莞中寰智能航空科技有限公司 | Six unmanned aerial vehicle |
| CN106697269A (en) * | 2015-07-21 | 2017-05-24 | 天津晓奇科技发展有限公司 | Multi-rotor unmanned aerial vehicle carbon tube damping and shock absorption undercarriage |
| CN206141815U (en) * | 2016-10-08 | 2017-05-03 | 深圳市赛亿科技开发有限公司 | Unmanned aerial vehicle foot rest with descending cushioning effect |
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| Date | Code | Title | Description |
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| 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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180119 |