CN204801444U - A wheel for unmanned aerial vehicle - Google Patents
A wheel for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN204801444U CN204801444U CN201520519888.XU CN201520519888U CN204801444U CN 204801444 U CN204801444 U CN 204801444U CN 201520519888 U CN201520519888 U CN 201520519888U CN 204801444 U CN204801444 U CN 204801444U
- Authority
- CN
- China
- Prior art keywords
- runner
- wheel
- pivot shaft
- back shaft
- aerial vehicle
- 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 belongs to the technical field of the wheel, concretely relates to a wheel for unmanned aerial vehicle, include runner and the supporting mechanism of being connected with the runner, the supporting mechanism sets up in the runner top surface outside, and the runner is the hollow, the supporting mechanism includes back shaft, vice back shaft, and leading wheel, the upper end of this back shaft is provided with the connector of central counter roll, and the lower extreme of back shaft is connected with vice back shaft, connects the leading wheel through vice back shaft, and this leading wheel sets up in the top surface guide way of runner, the bottom surface of runner is provided with a plurality of latches, can intervene the power supply and provide the long -time road surface power that traveles, realize the dual -purpose function of unmanned aerial vehicle dead circuit, the hollow department of runner gushes and places the power supply, through setting up the latch in the bottom surface, connects the power supply, just so can drive the wheel rotation, provides the power that unmanned aerial vehicle gos forward, this a wheel for unmanned aerial vehicle in the aspect of the support, adopts the even support of off -axial, sets up and is supporting epaxial bumper shock absorber for it is more steady to travel.
Description
Technical field
The utility model belongs to wheel technical field, is specifically related to a kind of wheel for unmanned plane.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Without driving compartment on machine, but the equipment such as autopilot, process controller, information collecting device are installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, it is followed the tracks of, locates, remote control, remote measurement and digital communication.Can take off as conventional airplane or launch with booster rocket down wireless electric-controlled, also can be taken to by machine tool and throw in flight in the air.
Unmanned plane at least comprises fuselage, driving engine, mast and oar clamp pin axle.Wherein, what mast and oar clamp pin axle were arranged on unmanned aerial vehicle body is end, and driving engine is arranged on the inside of unmanned aerial vehicle body, thinks that the rotor wing rotation without other provides power.
If existing unmanned plane is provided with wheel, its wheel is all conventional wheel, wheel does not arrange power, just play a supportive role in ground glide process before take-off or after landing, the power of long-term road traveling cannot be met, this causes existing unmanned plane to fly aloft, does not possess the multifunctional usage of road surface carrier.
Utility model content
The purpose of this utility model overcomes existing unmanned plane wheel not arrange the problem that propulsion source cannot provide road traveling power for a long time.
For this reason, the utility model provides a kind of wheel for unmanned plane, the supporting mechanism comprising runner and be connected with runner, described supporting mechanism is arranged at outside runner end face, runner is hollow, and this runner end face is provided with U-shaped guide groove, and the notch of this guide groove is towards the axle center of runner;
Described supporting mechanism comprises pivot shaft, secondary pivot shaft, and track adjusting wheel;
The upper end of this pivot shaft is provided with the communication port of center pivot, and the lower end of pivot shaft is connected with secondary pivot shaft, and connect track adjusting wheel by secondary pivot shaft, this track adjusting wheel is arranged in the end face guide groove of runner;
The bottom surface of described runner is provided with multiple latch, and this latch, arranges in center radiation for axle center with the bottom center of runner.
Pivot shaft outside the end face being arranged at runner is at least provided with 3, and corresponding track adjusting wheel is at least provided with 3.
Described pivot shaft is provided with 3, and corresponding track adjusting wheel is provided with 3, and with the axle center of the end face of runner for summit is the distribution of even angle.
The lower end of described pivot shaft is also provided with bumper, and the lower end of this bumper is connected with secondary pivot shaft.
The beneficial effects of the utility model: this wheel for unmanned plane that the utility model provides, propulsion source can be got involved long-time road traveling power is provided, realize the function that unmanned plane dead circuit is dual-purpose, runner hollow position gushes to place propulsion source, by being arranged on the latch of bottom surface, connects propulsion source, so just wheel turns can be driven, there is provided the power that unmanned plane advances, this structural dynamic conversion efficiency is high, and structure is simple; This is used for the wheel of unmanned plane, in support, adopts axle outer support, arranges at least three strong points, support uniformly, be arranged on the bumper on pivot shaft in addition, makes traveling more steady.
Below with reference to accompanying drawing, the utility model is described in further details.
Accompanying drawing explanation
Fig. 1 is the wheel front sectional drawing for unmanned plane.
Fig. 2 is the wheel end face schematic diagram for unmanned plane.
Fig. 3 is the wheel schematic bottom view for unmanned plane.
Fig. 4 is supporting mechanism schematic diagram.
Fig. 5 is latch structural scheme of mechanism.
In figure: 1, runner; 2, pivot shaft; 3, bumper; 4, latch; 5, secondary pivot shaft; 6, track adjusting wheel; 7, center pivot; 8, U-shaped guide groove.
Detailed description of the invention
Reaching for setting forth the utility model further the technological means and effect that predetermined object takes, below in conjunction with drawings and Examples to detailed description of the invention of the present utility model, architectural feature and effect thereof, being described in detail as follows.
Embodiment 1:
In order to solve existing unmanned plane wheel, the problem that propulsion source cannot provide road traveling power for a long time is not set, the utility model provides a kind of as shown in Figure 1 for the wheel of unmanned plane, the supporting mechanism comprising runner 1 and be connected with runner 1, described supporting mechanism is arranged at outside runner 1 end face, runner 1 is hollow, this runner 1 end face is provided with U-shaped guide groove 8, and the notch of this guide groove 8 is towards the axle center of runner 1;
Described supporting mechanism comprises pivot shaft 2, secondary pivot shaft 5, and track adjusting wheel 6;
As shown in Figure 2, the upper end of this pivot shaft 2 is provided with the communication port of center pivot 7, and the lower end of pivot shaft 2 is connected with secondary pivot shaft 5, connects track adjusting wheel 6 by secondary pivot shaft 5, and this track adjusting wheel 6 is arranged in the end face guide groove 8 of runner 1;
As shown in Fig. 3,5, the bottom surface of above-mentioned runner 1 is provided with multiple latch 4, and this latch 4, arranges in center radiation for axle center with the bottom center of runner 1.
This is used for the wheel of unmanned plane, propulsion source can be got involved long-time road traveling power is provided, realize the function that unmanned plane dead circuit is dual-purpose, runner 1 hollow position is used for placing propulsion source, by being arranged on the latch 4 of bottom surface, connects propulsion source, so just wheel turns can be driven, there is provided the power that unmanned plane advances, this structural dynamic conversion efficiency is high, and structure is simple; This is used for the wheel of unmanned plane, in support, adopts axle outer support, arranges at least three strong points, support uniformly, be arranged on the bumper 3 on pivot shaft 2 in addition, makes traveling more steady.
Embodiment 2:
The above-mentioned wheel for unmanned plane, the pivot shaft 2 outside the end face being arranged at runner 1 is at least provided with 3, and corresponding track adjusting wheel 6 is at least provided with 3; Make the support of pivot shaft 2 pairs of runners 1 more stable like this, the pivot shaft 2 of setting is more much more stable with corresponding track adjusting wheel 6.
As shown in Figure 4, described pivot shaft 2 is provided with 3, corresponding track adjusting wheel 6 is provided with 3, and with the axle center of the end face of runner 1 for the angle that summit is every two pivot shafts 2 of even angle distribution is 120 °, take full advantage of triangle stability so specific, support for runner 1 is highly stable, the pillar stiffener fuselage that unmanned plane can be stable in traveling process.
The lower end of above-mentioned pivot shaft 2 is also provided with bumper 3, and the lower end of this bumper 3 is connected use with secondary pivot shaft 5, has good cushioning effect, unmanned plane is advanced more steady; And the installation of bumper 3 adopts the mode of clamping, disassemble conveniently, for safeguarding that wheel is also very easy to.
Above content is in conjunction with concrete preferred implementation further detailed description of the utility model, can not assert that concrete enforcement of the present utility model is confined to these explanations.For the utility model person of an ordinary skill in the technical field, without departing from the concept of the premise utility, some simple deduction or replace can also be made, all should be considered as belonging to protection domain of the present utility model.
Claims (4)
1. the wheel for unmanned plane, the supporting mechanism comprising runner (1) and be connected with runner (1), it is characterized in that: described supporting mechanism is arranged at outside runner (1) end face, runner (1) is hollow, this runner (1) end face is provided with U-shaped guide groove (8), and the notch of this guide groove (8) is towards the axle center of runner (1);
Described supporting mechanism comprises pivot shaft (2), secondary pivot shaft (5), and track adjusting wheel (6);
The upper end of this pivot shaft (2) is provided with the communication port of center pivot (7), the lower end of pivot shaft (2) is connected with secondary pivot shaft (5), connect track adjusting wheel (6) by secondary pivot shaft (5), this track adjusting wheel (6) is arranged in the end face guide groove (8) of runner (1);
The bottom surface of described runner (1) is provided with multiple latch (4), and this latch (4), arranges in center radiation for axle center with the bottom center of runner (1).
2. as claimed in claim 1 for the wheel of unmanned plane, it is characterized in that: the pivot shaft (2) outside the end face being arranged at runner (1) is at least provided with 3, corresponding track adjusting wheel (6) is at least provided with 3.
3. as claimed in claim 1 or 2 for the wheel of unmanned plane, it is characterized in that: described pivot shaft (2) is provided with 3, corresponding track adjusting wheel (6) is provided with 3, and be summit with the axle center of the end face of runner (1) is the distribution of even angle.
4. as claimed in claim 1 for the wheel of unmanned plane, it is characterized in that: the lower end of described pivot shaft (2) is also provided with bumper (3), the lower end of this bumper (3) is connected with secondary pivot shaft (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520519888.XU CN204801444U (en) | 2015-07-17 | 2015-07-17 | A wheel for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520519888.XU CN204801444U (en) | 2015-07-17 | 2015-07-17 | A wheel for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204801444U true CN204801444U (en) | 2015-11-25 |
Family
ID=54586330
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520519888.XU Expired - Fee Related CN204801444U (en) | 2015-07-17 | 2015-07-17 | A wheel for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204801444U (en) |
-
2015
- 2015-07-17 CN CN201520519888.XU patent/CN204801444U/en not_active Expired - Fee Related
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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: 20151125 Termination date: 20160717 |