CN206679250U - A kind of unmanned plane undercarriage - Google Patents
A kind of unmanned plane undercarriage Download PDFInfo
- Publication number
- CN206679250U CN206679250U CN201720307421.8U CN201720307421U CN206679250U CN 206679250 U CN206679250 U CN 206679250U CN 201720307421 U CN201720307421 U CN 201720307421U CN 206679250 U CN206679250 U CN 206679250U
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- CN
- China
- Prior art keywords
- support bar
- unmanned plane
- spring
- connecting seat
- bonded
- 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
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Abstract
The utility model discloses a kind of unmanned plane undercarriage, including connecting seat, riffled tube, first support bar, spring, second support bar, bearing, luminescent powder and rotor wing unmanned aerial vehicle, the bottom of the rotor wing unmanned aerial vehicle is bonded the connecting seat, riffled tube described in the bottom weld of the connecting seat, the bottom thread of the riffled tube connects the top of the first support bar, the bottom of the first support bar is bonded the spring, and the bottom of the spring is bonded the top of the second support bar.The unmanned plane undercarriage, light weight, it is convenient for dismantlement work, vibration damping processing effectively can be carried out to unmanned plane when unmanned plane lands by spring, so as to effectively ensure security of the unmanned plane in landing, also, the luminescent powder in the bearing of the bottom of second support bar can provide illumination at night for undercarriage, consequently facilitating operating personnel understand the situation of rising and falling of unmanned plane.
Description
Technical field
A kind of unmanned plane undercarriage is the utility model is related to, specially a kind of unmanned plane undercarriage, belongs to unmanned machine equipment
Technical field.
Background technology
In recent years, unmanned air vehicle technique had the development advanced by leaps and bounds.Because its cost is low, mobility is good, survival ability
By force, the advantages that risk that no one was injured, unmanned plane occupies extremely important status in modern military war, in civil area
There is boundless prospect.Current unmanned plane mainly includes fixed-wing unmanned plane and rotor wing unmanned aerial vehicle.With fixed-wing nobody
Machine is compared, rotor wing unmanned aerial vehicle have the advantages that simple in construction, control flexibly, VTOL, can hover or inverted flight, clapped in aviation
Take the photograph, police service application etc. have a wide range of applications.
The undercarriage of rotor wing unmanned aerial vehicle is substantially fixed at present, and simple in construction, thus lacks effective damping
Effect, when unmanned plane is landed, larger vibration easily is produced to the internal structure of unmanned plane and unmanned plane is caused to damage, it is right
The technology of operating personnel has higher requirement, also, traditional unmanned plane lacks the lighting apparatus of correlation when using at night,
The lighting apparatus relied only on mostly on unmanned plane is illuminated, and lacks lighting apparatus on undercarriage, thus is not easy to operator
Member understands the situation of rising and falling of current unmanned plane.
The content of the invention
The purpose of this utility model is that to solve the above problems and provides a kind of unmanned plane undercarriage.
The utility model is achieved through the following technical solutions above-mentioned purpose：A kind of unmanned plane undercarriage, including connecting seat,
Riffled tube, first support bar, spring, second support bar, bearing, luminescent powder and rotor wing unmanned aerial vehicle, the rotor wing unmanned aerial vehicle
Bottom is bonded the connecting seat, riffled tube described in the bottom weld of the connecting seat, and the bottom thread of the riffled tube connects
The top of the first support bar is connect, the bottom of the first support bar is bonded the spring, the bottom bonding institute of the spring
The top of second support bar is stated, the bottom of the second support bar is bonded the bearing, and the inner side of the bearing is filled with described
Luminescent powder.
Preferably, the connecting seat, the riffled tube, the first support bar, the spring and described second
Strut is carbon fibre materials.
Preferably, the bearing is transparent rubber material.
Preferably, the luminescent powder is photo-induced energy storage luminescent powder.
Preferably, the side of the first support bar is provided with crisscross lines.
The beneficial effects of the utility model are：The unmanned plane undercarriage, it is simple in construction, be easy to implement, light weight, be easy into
Row dismantlement work, vibration damping processing effectively can be carried out to rotor wing unmanned aerial vehicle when rotor wing unmanned aerial vehicle lands by spring, so as to have
Effect ensures security of the unmanned plane in landing, also, the luminescent powder in the bearing of the bottom of second support bar can be at night
Illumination is provided for undercarriage, consequently facilitating operating personnel understand the situation of rising and falling of unmanned plane.
Brief description of the drawings
Fig. 1 is overall schematic of the present utility model；
Fig. 2 is the internal structure schematic diagram of bearing of the present utility model；
In figure：1st, connecting seat；2nd, riffled tube；3rd, first support bar；4th, spring；5th, second support bar；6th, bearing；7th, night
Light powder, 8, rotor wing unmanned aerial vehicle.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Refer to Fig. 1-2, a kind of unmanned plane undercarriage, including connecting seat 1, riffled tube 2, first support bar 3, spring 4,
Second support bar 5, bearing 6, luminescent powder 7 and rotor wing unmanned aerial vehicle 8, the bottom of the rotor wing unmanned aerial vehicle 8 are bonded the connecting seat 1,
Riffled tube 2 described in the bottom weld of the connecting seat 1, the bottom thread of the riffled tube 2 connect the first support bar 3
Top, the bottom of the first support bar 3 is bonded the spring 4, and the bottom of the spring 4 is bonded the second support bar 5
Top, the bottom of the second support bar 5 is bonded the bearing 6, and the inner side of the bearing 6 is filled with the luminescent powder 7.
The connecting seat 1, the riffled tube 2, the first support bar 3, the spring 4 and the second support bar
5 be carbon fibre materials, and the quality of the unmanned plane undercarriage is fully reduced with this, and ensures the firm of the unmanned plane undercarriage
Property.The bearing 6 is transparent rubber material, because bearing 6 is transparent rubber material, the photograph for the luminescent powder being easy to this in bearing
It is bright.The luminescent powder 7 is photo-induced energy storage luminescent powder, because luminescent powder 7 is photo-induced energy storage luminescent powder, by natural light, daylight
After the irradiation such as light, ultraviolet light, luminous energy is stored, after light irradiation is stopped, slowly being discharged in a manner of fluorescence
Come, so as to be lighted at night or dark, illumination is provided as undercarriage.The side of the first support bar 3 is provided with vertical
The wrong lines of traversed by, because the side of first support bar 3 is provided with crisscross lines, with this personnel easy to operation to first
Strut 3 is rotated and carries out disassembly and installation work to first support bar 3
It should be noted that the utility model is when in use, by spring 4 effectively when rotor wing unmanned aerial vehicle 8 lands pair
Unmanned plane carries out vibration damping processing, so as to effectively ensure security of the unmanned plane in landing, also, the bottom of second support bar 5
Luminescent powder 7 in the bearing 6 at end can provide illumination at night for undercarriage, consequently facilitating operating personnel understand rising and falling for unmanned plane
Situation.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (5)
- A kind of 1. unmanned plane undercarriage, it is characterised in that：Including connecting seat（1）, riffled tube（2）, first support bar（3）, bullet Spring（4）, second support bar（5）, bearing（6）, luminescent powder（7）And rotor wing unmanned aerial vehicle（8）, the rotor wing unmanned aerial vehicle（8）Bottom It is bonded the connecting seat（1）, the connecting seat（1）Bottom weld described in riffled tube（2）, the riffled tube（2）Bottom Portion is threadedly coupled the first support bar（3）Top, the first support bar（3）Bottom be bonded the spring（4）, it is described Spring（4）Bottom be bonded the second support bar（5）Top, the second support bar（5）Bottom be bonded the bearing （6）, the bearing（6）Inner side be filled with the luminescent powder（7）.
- A kind of 2. unmanned plane undercarriage according to claim 1, it is characterised in that：The connecting seat（1）, the internal thread Pipe（2）, the first support bar（3）, the spring（4）And the second support bar（5）It is carbon fibre materials.
- A kind of 3. unmanned plane undercarriage according to claim 1, it is characterised in that：The bearing（6）For transparent rubber material Matter.
- A kind of 4. unmanned plane undercarriage according to claim 1, it is characterised in that：The luminescent powder（7）For photo-induced energy storage Luminescent powder.
- A kind of 5. unmanned plane undercarriage according to claim 1, it is characterised in that：The first support bar（3）Side Provided with crisscross lines.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720307421.8U CN206679250U (en) | 2017-03-28 | 2017-03-28 | A kind of unmanned plane undercarriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720307421.8U CN206679250U (en) | 2017-03-28 | 2017-03-28 | A kind of unmanned plane undercarriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206679250U true CN206679250U (en) | 2017-11-28 |
Family
ID=60390145
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720307421.8U Expired - Fee Related CN206679250U (en) | 2017-03-28 | 2017-03-28 | A kind of unmanned plane undercarriage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206679250U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945444A (en) * | 2018-08-30 | 2018-12-07 | 无锡莱特杰米科技发展有限公司 | A kind of unmanned aerial photography machine of the wedding celebration with landing protection structure |
-
2017
- 2017-03-28 CN CN201720307421.8U patent/CN206679250U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945444A (en) * | 2018-08-30 | 2018-12-07 | 无锡莱特杰米科技发展有限公司 | A kind of unmanned aerial photography machine of the wedding celebration with landing protection structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171128 Termination date: 20180328 |
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| CF01 | Termination of patent right due to non-payment of annual fee |