CN205872483U - Unmanned aerial vehicle load upset jack - Google Patents
Unmanned aerial vehicle load upset jack Download PDFInfo
- Publication number
- CN205872483U CN205872483U CN201620770268.8U CN201620770268U CN205872483U CN 205872483 U CN205872483 U CN 205872483U CN 201620770268 U CN201620770268 U CN 201620770268U CN 205872483 U CN205872483 U CN 205872483U
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- upset
- installing plate
- load
- mounting base
- shaft
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Abstract
The utility model discloses an unmanned aerial vehicle load upset jack not only can realize the effective use of load, can in time retrieve when not using, effectively protects task load. Including fixing mounting plate on the fuselage, upset mounting panel, servo motor, mounting plate be hollow structure, and the upset mounting panel inlays the middle part of establishing at mounting plate, and the bottom of upset mounting panel is passed through the hinge and is connected with mounting plate's bottom, and the both sides of upset mounting panel are respectively through fix a position spool and mounting plate's both sides rotation is connected, task load and shock mitigation system through mounting screw on the upset mounting panel, servo motor rotates with one side positioning shaft connected and drive location axle, the upset mounting panel relative mounting plate rotate, the one end of driven shaft mount pad is equipped with spacing post, the axle forms certain contained angle between the two in spacing post and the driven shaft mount pad, spacing post is prescribed a limit to the location axle control and is overturn the mounting panel and overturn to the target location, task load is showed and is carried out operation outside the cabin.
Description
Technical field
This utility model relates to unmanned plane mechanical structure system, particularly relates to a kind of SUAV load upset radio and tape player
Structure, is particularly well-suited to the load installation system of Small and micro-satellite, mainly mission payload is carried out folding and unfolding design.
Background technology
The at present unmanned plane of China, great majority belong to Small and micro-satellite, can band load weight little, free space is narrow,
And the mission payload carried often is exposed to nacelle exterior, it is unfavorable for it is carried out efficient recovery and protection.
Need a kind of system can either conveniently installed and mission payload can be carried out effective folding and unfolding at present badly, but this load
The mesh such as the design of lotus extension and retraction system requires height, has both needed it lightweight, and space is little, in addition it is also necessary to realize simple to operate, and safety is high
, design requirement is difficult to realize.
Utility model content
For the problems referred to above, the purpose of this utility model is the one retractable general load microminiature upset provided
Jack, this mechanism can be controlled by automatic pilot, autonomous flight and manual flight can control load folding and unfolding, not only
It is capable of effective use of load, can reclaim in time when not in use simultaneously, mission payload is effectively protected.
A kind of SUAV load upset jack, including the mounting base being fixed on fuselage, upset installing plate,
Servomotor, described mounting base is hollow structure, and described upset installing plate is embedded at the middle part of described mounting base, described in turn over
The bottom turning installing plate is connected with the bottom of described mounting base by hinge, and the both sides of described upset installing plate are respectively by fixed
Position axle is rotationally connected with the both sides of described mounting base；
Mission payload and shock mitigation system are arranged on described upset installing plate by screw, described servomotor and side institute
Stating locating shaft connect and drive described locating shaft to rotate, described upset installing plate rotates relative to described mounting base, described driven
One end of axle mounting seat is provided with limited post, and described limited post forms an angle with axle shape therebetween in driven shaft mounting seat, institute
Stating the limited post restriction described locating shaft described upset installing plate of control to overturn to target location, described mission payload shows and carries out
Machine extravehicular work.
Further, described locating shaft includes driving shaft and driven shaft, is pacified by driving shaft mounting seat and driven shaft respectively
Dress bearing is fixed, and described driving shaft mounting seat is fixed on described upset installing plate, and described driven shaft erection support is fixed on institute
State on mounting base；Described driving shaft and described driven shaft are connected with each other by axle sleeve.
Further, being located at the described driving shaft of described upset installing plate both sides, wherein the described driving shaft of side passes through
Fix seat with the servomotor being located on described upset installing plate to be connected.
Further, the central rotating shaft of described hinge is arranged with spring.
Further, described mission payload is fixed on described upset installing plate by amortisseur.
A kind of SUAV load upset jack that this utility model provides, by the cabin at SUAV
On set up the mounting base of hollow structure, in this mounting base, be embedded upset installing plate, this upset installing plate arranged and appoints
Business load, the locating shaft that the hinge that arranged by one end of upset of upset installing plate and both sides are arranged realizes, and private takes motor driving
Locating shaft rotates, upset installing plate upset, is located at mission payload thereon and tilts out cabin, carries out machine extravehicular work, work as operation
After, then upset installing plate is gone back in cabin, mission payload backs up into cabin the most simultaneously.This mechanism can not only conveniently appoint
The installation of business load and use, effectively can protect mission payload when being made without machine extravehicular work and using simultaneously
Protect, improve the service life of mission payload.And this structure not only light weight, volume is little, and gondola load is replaceable, and shape is permissible
Design according to cabin section, reliable and stable, safe and feasible.
Use the SUAV load upset jack that this utility model provides, unmanned plane can be made to launch recovery
During, load is recycled in the section of cabin, and protection load reduces external environment to be affected mission payload.This design is taken off at unmanned plane
Before can change installed load at any time, convenient and swift, footprint is little, lightweight, economically feasible, is greatly promoted the whole of unmanned plane
Body performance, security performance and reliability, play a key effect in unmanned aerial vehicle design.
Meanwhile, this device all uses carbon fiber to make, lightweight, takes up room little, simple to operate, easy to use, suitable
Strong by property, any mission payload can be used, be arranged under any environment appearance space, according to load cabin condition load shape i.e.
Can.Meanwhile, this utility model scientific structure design is reasonable, and safely and effectively, cost is relatively low, has the wide market demand, it is easy to
Popularization and application.
Accompanying drawing explanation
The top view of the SUAV load upset jack that Fig. 1 provides for this utility model；
The side view of the SUAV load upset jack that Fig. 2 provides for this utility model；
1. mounting base, 2. upset installing plate, 3. seat fixed by servomotor, 4. hinge, 5. mission payload, 6. limited post,
7. driving shaft, 8. driven shaft, 9. driving shaft mounting seat, 10. driven shaft mounting seat, 11. axle sleeves, 12. servomotors, 13. springs,
14. amortisseurs.
Detailed description of the invention
Below in conjunction with the accompanying drawings embodiment of the present utility model is illustrated.
As depicted in figs. 1 and 2, a kind of SUAV load upset jack, including the hollow being fixed on fuselage
The mounting base 1 of structure, is similar to doorframe structure, and upset installing plate 2 is embedded at the middle part of mounting base 1, upset installing plate 2
Bottom is rotationally connected by the bottom of hinge 4 with mounting base 1, and the both sides of upset installing plate 2 are respectively by locating shaft and installation
The both sides of base plate 1 are rotationally connected；
Locating shaft includes driving shaft 7 and driven shaft 8, and the driving shaft 7 of side is located at upset by driving shaft mounting seat 9 and installs
On plate 2, driven shaft 8 is located on mounting base 1 by driven shaft mounting seat 10, is connected by axle sleeve 11 therebetween, opposite side
Driving shaft 7 be directly connected to servomotor 12, servomotor 12 by servomotor fix seat 3 be located at upset installing plate 2 on,
And drive the driving shaft 7 of this side to rotate, and then upset installing plate 2 is driven to rotate.
Mission payload 5 is located at the surface of upset installing plate 2, and upset installing plate 2 is mounted opposite base plate 1 and rotates, and the two is formed
Certain angle, the size of this angle determines corner dimension according to size and the size of mission payload 5.One end of locating shaft is provided with limit
Position post 6, this limited post 6 limits locating shaft control upset installing plate 2 and is fixed on target location, and now, the driven shaft 8 after upset blocks
In mounting seat, servomotor 12 does not stresses, it is ensured that the safety that mechanism is overall, the most described mission payload 5 is recycled to cabin section
In, upset installing plate 2 puts down and falls in driven shaft 8 mounting seat, and the most described mission payload 5 shows and carries out making outside cabin
Industry.
Hinge 4 cental axial position connected between upset installing plate 2 therein and mounting base 1 is provided with spring 13, this bullet
Spring 13 can promote the upset installing plate 2 needing Guan Bi more easily to return back to make position.Meanwhile, mounting base 1 limits
Position and fixed installation, upset installing plate 2 mission payload 5 is installed after in spring 13 axle rotate, driven shaft 8 and driving shaft 7
Playing the effect of spacing and fixing upset installing plate 2, limited post 6 plays and limits the effect that driving shaft 7 protects steering wheel not stress, with
Time rotate driving shaft at servomotor 12 and realize the upset of payload platform for 7 times so that load carries out folding and unfolding.Carry to improve task
The lotus 5 steadiness in rotation process, is fixed on mission payload 5 on upset installing plate 2 by amortisseur 14.
Assembling according to above-mentioned utility model content, use ground station control, earth station provides pwm signal, to control
Described mission payload 5 switching mechanism folding and unfolding.
Above, although illustrate several embodiment of the present utility model, but these embodiments are intended only as example
Propose, be not intended to limit scope of the present utility model.For the embodiment that these are new, it is possible to enter in other various modes
Row is implemented, in the range of without departing from main idea of the present utility model, it is possible to carry out various omission, displacement and change.These are implemented
Mode and its deformation, while being contained in scope or spirit of the present utility model, be also contained in described in claims
In utility model and equivalency range thereof.
Claims (5)
1. a SUAV load upset jack, it is characterised in that include mounting base, the upset being located on cabin
Installing plate, servomotor, described mounting base is hollow structure, and described upset installing plate is embedded in described mounting base
Portion, the bottom of described upset installing plate is connected with the bottom of described mounting base by hinge, the both sides of described upset installing plate
It is rotationally connected by the both sides of locating shaft with described mounting base respectively；
Mission payload and shock mitigation system are arranged on described upset installing plate by screw, and described servomotor is fixed with described in side
Position axle connects and drives described locating shaft to rotate, and described upset installing plate rotates relative to described mounting base, and driven shaft installs the end
One end of seat is provided with limited post, and described limited post forms an angle with axle shape therebetween in described driven shaft mounting seat, institute
Stating the limited post restriction described locating shaft described upset installing plate of control and be fixed on target location, described mission payload shows and carries out
Machine extravehicular work.
A kind of SUAV load upset jack the most according to claim 1, it is characterised in that described locating shaft
Including driving shaft and driven shaft, fixed by driving shaft mounting seat and driven shaft erection support respectively, described driving shaft mounting seat
Being located on described upset installing plate, described driven shaft erection support is located on described mounting base；Described driving shaft and described from
Moving axis is connected with each other by axle sleeve.
A kind of SUAV load upset jack the most according to claim 2, it is characterised in that turn over described in being located at
Turn the described driving shaft of installing plate both sides, wherein the described driving shaft of side by with the servo being located on described upset installing plate
Motor fixing seat connects.
A kind of SUAV load upset jack the most according to claim 1, it is characterised in that described hinge
Spring it is arranged with on central rotating shaft.
A kind of SUAV load upset jack the most according to claim 1, it is characterised in that described task carries
Lotus is fixed on described upset installing plate by amortisseur.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620770268.8U CN205872483U (en) | 2016-07-20 | 2016-07-20 | Unmanned aerial vehicle load upset jack |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620770268.8U CN205872483U (en) | 2016-07-20 | 2016-07-20 | Unmanned aerial vehicle load upset jack |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205872483U true CN205872483U (en) | 2017-01-11 |
Family
ID=57697892
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620770268.8U Active CN205872483U (en) | 2016-07-20 | 2016-07-20 | Unmanned aerial vehicle load upset jack |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205872483U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106719230A (en) * | 2017-03-13 | 2017-05-31 | 广东工业大学 | Aquatic products cultivates unmanned plane automatically |
-
2016
- 2016-07-20 CN CN201620770268.8U patent/CN205872483U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106719230A (en) * | 2017-03-13 | 2017-05-31 | 广东工业大学 | Aquatic products cultivates unmanned plane automatically |
| CN106719230B (en) * | 2017-03-13 | 2023-02-10 | 广东工业大学 | Automatic aquaculture unmanned aerial vehicle |
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| GR01 | Patent grant |