CN205602097U - Unmanned plant protection machine shock attenuation undercarriage - Google Patents
Unmanned plant protection machine shock attenuation undercarriage Download PDFInfo
- Publication number
- CN205602097U CN205602097U CN201620299447.8U CN201620299447U CN205602097U CN 205602097 U CN205602097 U CN 205602097U CN 201620299447 U CN201620299447 U CN 201620299447U CN 205602097 U CN205602097 U CN 205602097U
- Authority
- CN
- China
- Prior art keywords
- undercarriage
- guide cylinder
- unmanned
- free end
- utility
- 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
- 230000035939 shock Effects 0.000 title abstract 3
- 238000013016 damping Methods 0.000 claims description 12
- 230000002349 favourable effect Effects 0.000 abstract 1
- 238000005507 spraying Methods 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000011010 flushing procedure Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- -1 seed Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Catching Or Destruction (AREA)
- Vibration Dampers (AREA)
Abstract
The utility model discloses an unmanned plant protection machine shock attenuation undercarriage belongs to unmanned plant protection machine subassembly technical field, including the undercarriage mount pad, the guide cylinder is installed to undercarriage mount pad below, in the guide cylinder from last down in proper order the holding have elastomeric element and bracing piece, the free end of bracing piece is followed wear out the guide cylinder bottom, the free end of bracing piece is connected with second grade buffer. The utility model discloses satisfied the requirement of unmanned aerial vehicle to the undercarriage shock -absorbing capacity with simple reliable structure, the reliability is high, and the stable performance is favorable to improving the security that unmanned aerial vehicle landed.
Description
Technical field
This utility model relates to unmanned fog machine component technology field, particularly to a kind of unmanned fog machine damping
Undercarriage.
Background technology
Unmanned fog machine, as the term suggests be for agriculture and forestry plant protection operation UAV, this type without
People's aircraft has flying platform (fixed-wing, single rotor, many rotors), GPS to fly control, spraying mechanism three part group
Become, fly control by ground remote control or GPS, realize spraying operation, can be with spraying agent, seed, powder
Deng.
In recent years, being widely used of small-sized depopulated helicopter, such as multi-rotor aerocraft, it is mainly used in
The places such as the service of crops pesticide spraying, Aerial photography, forest fire protection tour, public security monitoring.Undercarriage is
The vitals of unmanned plane, existing unmanned plane undercarriage major part is made up of two, left and right support bar, this
Kind undercarriage, without buffer gear, can only ensure that the high perpendicular of near-earth tens centimetres falls, just can make fuselage
Do not damaged.
Utility model content
This utility model provide a kind of unmanned fog machine damping undercarriage, solve existing unmanned fog machine due to
The problem that undercarriage is bad without damping or damping effect and makes fuselage easily damage.
For solving above-mentioned technical problem, the technical solution of the utility model is:
A kind of unmanned fog machine damping undercarriage, including undercarriage mounting seat, below described undercarriage mounting seat
Guide cylinder is installed, in described guide cylinder, is equipped with elastomeric element and support bar the most successively, described
The free end of strut passes bottom described guide cylinder, and the free end of described support bar connects has level 2 buffering to fill
Put.
Wherein it is preferred to, described secondary buffer device includes fixing seat, connecting rod and wheel mounting rod, described
Fixed seating is located at the outside of described guide cylinder bottom, and one end of described wheel mounting rod is provided with wheel, institute
The other end stating wheel mounting rod is provided with U-shape structure, and one end of described connecting rod is hinged with described fixing seat, institute
The other end stating connecting rod is hinged with the top of described U-shape structure, and the free end of described support bar is U-shaped with described
The bottom of structure is hinged.
Wherein it is preferred to, described elastomeric element is the spring of the most collinear gauge structure of multiple connection.
Wherein it is preferred to, described spring uses the most tapered mode to lay.
The beneficial effects of the utility model:
1. this utility model meets the unmanned plane requirement to undercarriage shock-absorbing capacity with simple and reliable structure, can
High by property, stable performance, be conducive to improving the safety of UAV Landing.
2. the present invention provides elastic force by modified line diameter spring, and simple in construction, assembly work amount are little, reduce system
Cause this, be not only suitable for unmanned plane and closely land, be applicable to again relatively rise from landing, applied widely.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below by right
In embodiment or description of the prior art, the required accompanying drawing used is briefly described, it should be apparent that below,
Accompanying drawing in description is only embodiments more of the present utility model, for those of ordinary skill in the art,
On the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the structural representation of this utility model unmanned fog machine damping undercarriage.
In figure, 1. undercarriage mounting seat, 2. guide cylinder, 3. support bar, 4. fix seat, 5. connecting rod, 6. wheel peace
Dress bar, 7. wheel
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, to the technical side in this utility model embodiment
Case is clearly and completely described, it is clear that described embodiment is only that this utility model part is real
Execute example rather than whole embodiments.Based on the embodiment in this utility model, ordinary skill people
All other embodiments that member is obtained under not making creative work premise, broadly fall into this utility model
The scope of protection.
As it is shown in figure 1, the present embodiment provides a kind of unmanned fog machine damping undercarriage, install including undercarriage
Seat, is provided with guide cylinder, is equipped with elastomeric element in guide cylinder the most successively below undercarriage mounting seat
And support bar, the free end of support bar passes bottom guide cylinder, and the free end of support bar connects has two grades to delay
Flushing device.Elastomeric element has the effect of certain buffering to undercarriage, and two grades of level flushing devices further function as
Cushioning effect, undercarriage landing safety, improve the safety of UAV Landing.
Wherein, secondary buffer device includes fixing seat, connecting rod and wheel mounting rod, and fixed seating is located at guiding
The outside of cylinder bottom, one end of wheel mounting rod is provided with wheel, and the other end of wheel mounting rod is provided with U-shaped
Structure, one end of connecting rod is hinged with fixing seat, and the other end of connecting rod is hinged with the top of U-shape structure, supports
The free end of bar is hinged with the bottom of U-shape structure.
Wherein, elastomeric element is the spring (not shown) of two the most collinear gauge structures connected.Spring is adopted
Lay by the most tapered mode.Undercarriage have employed the spring in two kinds of footpaths the most collinear, normally rises
Being absorbed energy by hairspring when falling, if falling from side higher, then, after hairspring is compressed, bulky spring continues
The continuous energy that absorbs, the protection that this kind of design can provide higher height to fall with the lightest weight for unmanned plane.
In this utility model, the quantity of spring is also not limited thereto, and the most also can use many
Level line gauge structure, to adapt to surrounding, reaches optimal buffering effect.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model,
All within spirit of the present utility model and principle, any modification, equivalent substitution and improvement etc. made, all
Within protection domain of the present utility model should be included in.
Claims (4)
1. a unmanned fog machine damping undercarriage, it is characterised in that: include undercarriage mounting seat, described in rise and fall
Guide cylinder is installed below frame mounting seat, is equipped with elastomeric element in described guide cylinder the most successively and props up
Strut, the free end of described support bar passes bottom described guide cylinder, and the free end of described support bar connects
There is secondary buffer device.
One the most according to claim 1 unmanned fog machine damping undercarriage, it is characterised in that: described two
Level buffer unit includes fixing seat, connecting rod and wheel mounting rod, and described fixed seating is located at the bottom of described guide cylinder
The outside of end, one end of described wheel mounting rod is provided with wheel, and the other end of described wheel mounting rod is provided with
U-shape structure, one end of described connecting rod is hinged with described fixing seat, and the other end of described connecting rod is U-shaped with described
The top of structure is hinged, and the free end of described support bar is hinged with the bottom of described U-shape structure.
One the most according to claim 1 unmanned fog machine damping undercarriage, it is characterised in that: described bullet
Property parts are the spring of the most collinear gauge structure of multiple connection.
One the most according to claim 3 unmanned fog machine damping undercarriage, it is characterised in that: described bullet
Spring uses the most tapered mode to lay.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620299447.8U CN205602097U (en) | 2016-04-12 | 2016-04-12 | Unmanned plant protection machine shock attenuation undercarriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620299447.8U CN205602097U (en) | 2016-04-12 | 2016-04-12 | Unmanned plant protection machine shock attenuation undercarriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205602097U true CN205602097U (en) | 2016-09-28 |
Family
ID=56972578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620299447.8U Expired - Fee Related CN205602097U (en) | 2016-04-12 | 2016-04-12 | Unmanned plant protection machine shock attenuation undercarriage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205602097U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639314A (en) * | 2018-05-14 | 2018-10-12 | 郑州晨昱硕电子科技有限公司 | A kind of plant protection drone undercarriage with pooling feature |
-
2016
- 2016-04-12 CN CN201620299447.8U patent/CN205602097U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639314A (en) * | 2018-05-14 | 2018-10-12 | 郑州晨昱硕电子科技有限公司 | A kind of plant protection drone undercarriage with pooling feature |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ES2688609T3 (en) | Landing gear upright extender | |
| CN204822065U (en) | Unmanned aerial vehicle's undercarriage | |
| CN101973393A (en) | High-strength cage-type undercarriage of unmanned helicopter | |
| CN202783777U (en) | Unmanned aerial vehicle undercarriage | |
| CN108357667B (en) | Buffer-type undercarriage for rotary wind type unmanned plane | |
| CN205602097U (en) | Unmanned plant protection machine shock attenuation undercarriage | |
| CN206841708U (en) | A kind of vapour-pressure type multi-rotor unmanned aerial vehicle undercarriage | |
| CN106143881A (en) | A kind of unmanned plane deceleration damping undercarriage | |
| US20140097293A1 (en) | Airplane Shock Absorbing Suspension | |
| CN204916167U (en) | Many rotor unmanned aerial vehicle carbon pipe damping shock attenuation undercarriage | |
| CN106347638B (en) | A kind of unmanned helicopter undercarriage | |
| CN203652104U (en) | Damping landing gear of unmanned plane | |
| CN112249311A (en) | Be used for plant protection to spray buffering auxiliary device for unmanned aerial vehicle | |
| CN109808873A (en) | A kind of straight line self-locking tail portion folding and unfolding buffer unit | |
| CN206307266U (en) | A kind of multi-rotor unmanned aerial vehicle double damping undercarriage | |
| CN205418079U (en) | Tertiary buffering undercarriage of unmanned plant protection machine | |
| CN108502149A (en) | One kind being used for plant protection drone rack damping device | |
| CN103523230A (en) | Landing assistant parachute of unmanned aerial vehicle | |
| CN206218211U (en) | Undercarriage and aircraft | |
| CN206351777U (en) | A kind of unmanned plane deceleration damping undercarriage | |
| CN207580159U (en) | A kind of novel damping unmanned plane | |
| CN211033007U (en) | Pure electric manned aircraft | |
| CN210555562U (en) | Unmanned aerial vehicle shock attenuation undercarriage | |
| CN211442742U (en) | Unmanned aerial vehicle aerial survey equipment protection device | |
| CN208412108U (en) | A kind of unmanned helicopter buffer-type undercarriage |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160928 |