CN207536122U - A kind of novel unmanned plane foot stool - Google Patents
A kind of novel unmanned plane foot stool Download PDFInfo
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- CN207536122U CN207536122U CN201721709211.8U CN201721709211U CN207536122U CN 207536122 U CN207536122 U CN 207536122U CN 201721709211 U CN201721709211 U CN 201721709211U CN 207536122 U CN207536122 U CN 207536122U
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- curved rod
- buffer
- unmanned plane
- mounting groove
- fixed
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Abstract
The utility model discloses a kind of novel unmanned plane foot stool, including fuselage, mounting portion, curved rod, mounting groove, buffer bar, buffer stopper, elastic membrane, spring, buffering ball；The bottom end of the fuselage both sides is fixed with mounting portion, and the both ends of each mounting portion are fixed with curved rod, are hollow-core construction inside curved rod, cushion pad is filled with, and the surrounding of the stress concentration point of curved rod offers grooving inside curved rod；The mounting groove is set on the bottom of curved rod, and the bottom end of mounting groove is provided with through-hole, and elastic membrane is fixed on inside mounting groove；One end of the buffer bar is equipped with buffer stopper, and the upper surface of buffer stopper is contacted with elastic membrane, and the bottom of buffer bar passes through, and spring pocket is on buffer bar, and spring is located between buffer stopper and installation groove bottom wall.The utility model structure novel, reasonable design, equipped with many places buffer damping mechanism, the body of effective protection unmanned plane is without damage, extends its service life.
Description
Technical field
The utility model is related to a kind of foot stool, more particularly to a kind of novel unmanned plane foot stool belongs to unmanned plane accessory technology
Field.
Background technology
Unmanned plane is to utilize radio robot and the not manned aircraft of presetting apparatus manipulation provided for oneself, civilian nothing
It is man-machine take photo by plane, there is more important application in agricultural, plant protection, the fields such as the disaster relief；The unmanned plane used at present especially miniature self-service
Machine, foot stool is not provided with buffer structure or buffer structure is unreasonable, and during landing or when unmanned plane failure is fallen, body is easy
Larger vibration is generated, can be damaged the electrical equipment on unmanned plane in this way, further influences the service life of unmanned plane.
Utility model content
The utility model aim is to provide a kind of novel unmanned plane foot stool, good buffer effect, so as to protect unmanned plane
Electrical equipment on fuselage is without damage, to solve drawbacks described above caused by the prior art.
In order to solve the above-mentioned technical problem, the utility model provides following technical solution：
A kind of novel unmanned plane foot stool, including fuselage, mounting portion, curved rod, mounting groove, buffer bar, buffer stopper, elasticity
Film, spring, buffering ball；The bottom end of the fuselage both sides is fixed with mounting portion, and the both ends of each mounting portion are fixed with curved rod, arc
It is hollow-core construction inside shape bar, filled with cushion pad inside curved rod, and the surrounding of the stress concentration point of curved rod is offered and cut
Slot；The mounting groove is set on the bottom of curved rod, and the bottom end of mounting groove is provided with through-hole, and elastic membrane is fixed on inside mounting groove；Institute
The one end for stating buffer bar is equipped with buffer stopper, and the upper surface of buffer stopper is contacted with elastic membrane, and the bottom of buffer bar passes through, spring pocket
On buffer bar, and spring is located between buffer stopper and installation groove bottom wall；Link block is installed at the top of the buffering ball, is delayed
The bottom for rushing ball is equipped with foot pad, and link block is fixed on the bottom end of buffer bar, and on the mounting groove above elastic membrane and buffers
The side of ball offers gas vent.
As a kind of optimal technical scheme of the utility model, the depth value of the grooving is three points of curved rod wall thickness value
One of.
As a kind of optimal technical scheme of the utility model, the buffering ball uses the rubber material of elastically deformable.
As a kind of optimal technical scheme of the utility model, the material of the cushion pad is expandability polyethylene.
As a kind of optimal technical scheme of the utility model, the foot pad is taper type structure.
Advantageous effect：Compared with traditional technology, a kind of novel unmanned plane foot rest structure of the utility model is novel, and design is closed
Reason, equipped with many places buffer damping mechanism, the body of effective protection unmanned plane is without damage, extends its service life.
Description of the drawings
Fig. 1 is a kind of general structure schematic diagram of novel unmanned plane foot stool of the utility model；
Fig. 2 is the partial enlarged view at A in Fig. 1；
Fig. 3 is the partial enlarged view at B in Fig. 1；
Wherein：1- fuselages, 2- mounting portions, 3- curved rods, 4- mounting grooves, 5- buffer bars, 6- buffer stoppers, 7- springs, 8- bullets
Property film, 9- buffering balls, 10- groovings, 11- cushion pads, 12- through-holes, 14- link blocks, 15- foots pad, 16- gas vents.
Specific embodiment
To be easy to understand technical means, creative features, achievable purpose and effectiveness of the utility model, below
With reference to specific embodiment, the utility model is expanded on further.
As shown in Figure 1-Figure 3, a kind of novel unmanned plane foot stool including fuselage 1, mounting portion 2, curved rod 3, mounting groove 4, delays
Jumper bar 5, buffer stopper 6, elastic membrane 8, spring 7, buffering ball 9；The bottom end of 1 both sides of fuselage is fixed with mounting portion 2, each to install
The both ends in portion 2 are fixed with curved rod 3, and 3 inside of curved rod is hollow-core construction, and 3 inside of curved rod is filled with cushion pad 11, and arc
The surrounding of the stress concentration point of bar 3 offers grooving 10；The mounting groove 4 is set on the bottom of curved rod 3, the bottom end of mounting groove 4
Through-hole 12 is provided with, elastic membrane 8 is fixed on inside mounting groove 4；One end of the buffer bar 5 is equipped with buffer stopper 6, buffer stopper 6
Upper surface is contacted with elastic membrane 8, and the bottom of buffer bar 5 passes through, and spring 7 is sleeved on buffer bar 5, and spring 7 is located at buffer stopper 6
Between 4 bottom wall of mounting groove；The top of the buffering ball 9 is equipped with link block 14, and the bottom of buffering ball 9 is equipped with foot pad 15,
Link block 14 is fixed on the bottom end of buffer bar 5, and on the mounting groove 4 of 8 top of the elastic membrane and side of buffering ball 9 offers
Gas vent 16.
Wherein, the depth value of the grooving 10 is 1/3rd of 3 wall thickness value of curved rod.
Wherein, the buffering ball 9 uses the rubber material of elastically deformable.
Wherein, the material of the cushion pad 11 is expandability polyethylene.
Wherein, the foot pad 15 is taper type structure.
In landing in a flash, by gravity, buffer bar 5 moves upwards unmanned plane, and buffer stopper 6 is upward by elastic membrane 8
Jacking, so as to which elastic membrane 8 filters out a part of vibration, the rubber buffer ball 9 of elastically deformable is deformed by gravity in addition, into
One step filters out vibration, and the foot pad 15 of taper type structure can ensure stability of the unmanned plane in static condition, when standing in addition
Due to 7 tension force effect of spring, buffer bar 5 moves down；When unmanned plane, which breaks down, quickly to fall, due in curved rod 3
On stress concentration point, curved rod 3 is hit to be broken grooving 10, while the buffering of the expandability polyethylene inside curved rod 3
Pad 11 further reduces impact force, protects the electrical equipment on unmanned plane body without damage.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned exemplary embodiment, and
And in the case of the spirit or essential attributes without departing substantially from the utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this practicality is new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that by containing in the equivalent requirements of the claims is fallen
All changes in justice and range are embraced therein.Any reference numeral in claim should not be considered as limitation
Involved claim.
Claims (5)
1. a kind of novel unmanned plane foot stool, including fuselage, mounting portion, curved rod, mounting groove, buffer bar, buffer stopper, spring, bullet
Property film, buffering ball；It is characterized in that：The bottom end of the fuselage both sides is fixed with mounting portion, and the both ends of each mounting portion are fixed with
Curved rod, curved rod inside are hollow-core construction, and cushion pad, and the surrounding of the stress concentration point of curved rod are filled with inside curved rod
Offer grooving；The mounting groove is set on the bottom of curved rod, and the bottom end of mounting groove is provided with through-hole, and elastic membrane is fixed on mounting groove
It is internal；One end of the buffer bar is equipped with buffer stopper, and the upper surface of buffer stopper is contacted with elastic membrane, and the bottom of buffer bar is worn
It crosses, spring pocket is on buffer bar, and spring is located between buffer stopper and installation groove bottom wall；It is equipped at the top of the buffering ball
Link block, the bottom of buffering ball are equipped with foot pad, and link block is fixed on the bottom end of buffer bar, and on the mounting groove above elastic membrane
And the side of buffering ball offers gas vent.
2. a kind of novel unmanned plane foot stool according to claim 1, it is characterised in that：The depth value of the grooving is arc
/ 3rd of bar wall thickness value.
3. a kind of novel unmanned plane foot stool according to claim 1, it is characterised in that：The buffering ball uses can elasticity change
The rubber material of shape.
4. a kind of novel unmanned plane foot stool according to claim 1, it is characterised in that：The material of the cushion pad is can send out
Property polyethylene.
5. a kind of novel unmanned plane foot stool according to claim 1, it is characterised in that：The foot pad is taper type structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721709211.8U CN207536122U (en) | 2017-12-11 | 2017-12-11 | A kind of novel unmanned plane foot stool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721709211.8U CN207536122U (en) | 2017-12-11 | 2017-12-11 | A kind of novel unmanned plane foot stool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207536122U true CN207536122U (en) | 2018-06-26 |
Family
ID=62617853
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721709211.8U Active CN207536122U (en) | 2017-12-11 | 2017-12-11 | A kind of novel unmanned plane foot stool |
Country Status (1)
| Country | Link |
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| CN (1) | CN207536122U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108995814A (en) * | 2018-08-27 | 2018-12-14 | 佛山科学技术学院 | A kind of sand prevention improvement unmanned plane seeding apparatus |
| CN111169663A (en) * | 2020-01-17 | 2020-05-19 | 北京时代精衡航天科技有限公司 | Deep space detection impact overload test and data wireless transmission measuring device |
-
2017
- 2017-12-11 CN CN201721709211.8U patent/CN207536122U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108995814A (en) * | 2018-08-27 | 2018-12-14 | 佛山科学技术学院 | A kind of sand prevention improvement unmanned plane seeding apparatus |
| CN111169663A (en) * | 2020-01-17 | 2020-05-19 | 北京时代精衡航天科技有限公司 | Deep space detection impact overload test and data wireless transmission measuring device |
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