CN208149610U - A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure - Google Patents
A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure Download PDFInfo
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- CN208149610U CN208149610U CN201820648988.6U CN201820648988U CN208149610U CN 208149610 U CN208149610 U CN 208149610U CN 201820648988 U CN201820648988 U CN 201820648988U CN 208149610 U CN208149610 U CN 208149610U
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- motor
- rotor
- motor fixing
- fixing sleeve
- fixing seat
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- 230000003139 buffering effect Effects 0.000 claims description 9
- 230000005611 electricity Effects 0.000 claims description 6
- 239000007787 solid Substances 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 3
- 239000000428 dust Substances 0.000 description 3
- 230000006641 stabilisation Effects 0.000 description 3
- 238000011105 stabilization Methods 0.000 description 3
- 230000007812 deficiency Effects 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003716 rejuvenation Effects 0.000 description 1
Abstract
The utility model discloses a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure, which includes motor fixing seat, motor Quick Release body, rotor motor and motor fixing sleeve；The inside of motor fixing seat forms the fixation cavity of rotor motor, and rotor motor is arranged in motor fixing sleeve, and what rotor motor and motor fixing sleeve were formed is integrally placed in fixed cavity；Motor Quick Release body is connected to the downside of motor fixing seat, and the through-hole stretched out for rotor motor turning end is provided at the top of motor fixing seat.This patent is made of motor fixing seat, motor Quick Release body, rotor motor and motor fixing sleeve, and rotor motor is set in fixed cavity by motor fixing sleeve；It, which is implemented, is relatively easy to, and is always not in gap around motor since motor fixing sleeve is close proximity in fixed cavity, thus will not occur unnecessary shaking after long-time use because of gap.
Description
Technical field
The utility model relates to unmanned plane rotor motor Quick Release fields, are especially a kind of multi-rotor unmanned aerial vehicle rotor motor
Quick-disassembly structure.
Background technique
Currently, unmanned plane using very extensive, can be widely used in land utilization dynamic monitors, mineral resources exploration,
The fields such as geological environment and disaster prospecting, cadastration, map rejuvenation.However, unmanned plane refers to power device, behaviour is not carried
Make the aircraft of personnel, can autonomous or remote control distributor, can disposably or repeatedly recycle use, scientific research field, civil field and
Military field has been widely used.Unmanned plane mainly includes fixed-wing unmanned plane and rotor wing unmanned aerial vehicle, with fixed-wing unmanned plane phase
Than rotor wing unmanned aerial vehicle has many advantages, such as that structure is simple, controls flexible, easy to operate, VTOL.However in rotor wing unmanned aerial vehicle,
Rotor motor usually requires corresponding fixed mechanism to support.
It is found by retrieval, the utility model of patent No. CN201720579651.X discloses a kind of multi-rotor unmanned aerial vehicle rotation
Wing motor quick-disassembly structure, including motor mount, rotor motor and spring, the motor mount inside bottom are equipped with spring base
One, the motor mount inner sidewall is equipped with card slot, and contact is equipped in the card slot, and the rotor motor lower end is equipped with spring
Seat two, the rotor motor outside are symmetrically arranged with two elastic pieces, and the elastic piece end is equipped with back-off, and the rotor motor is logical
It crosses back-off to be clamped with card slot, the spring one end is connect with spring base one, and other end is connect with spring base two.
However the analysis found that, for existing rotor motor quick-disassembly structure, since itself is using back-off and bullet
Spring cooperation buckle, it is therefore desirable to which more component is just able to achieve；And gap is also easy to produce around motor, easily occur after the time is slightly long
Motor shakes.
Utility model content
Therefore, in order to solve above-mentioned deficiency, the utility model provides a kind of multi-rotor unmanned aerial vehicle rotor motor Quick Release herein
Structure；It after this patent improves, is made of motor fixing seat, motor Quick Release body, rotor motor and motor fixing sleeve, relative to existing
For some rotor motor quick-disassembly structures, this patent is to be set to rotor motor in fixed cavity by motor fixing sleeve；Its
It implements and is relatively easy to, be always not in gap around motor since motor fixing sleeve is close proximity in fixed cavity, because
And will not occur unnecessary shaking after long-time use because of gap.
The utility model is realized in this way constructing a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure, feature exists
In：The quick-disassembly structure includes motor fixing seat, motor Quick Release body, rotor motor and motor fixing sleeve；Motor fixing seat it is interior
Portion forms the fixation cavity of rotor motor, and rotor motor is arranged in motor fixing sleeve, and rotor motor and motor fixing sleeve are formed
Be integrally placed in fixed cavity；Motor Quick Release body is connected to the downside of motor fixing seat, is provided at the top of motor fixing seat
The through-hole stretched out for rotor motor turning end.This patent improve after, by motor fixing seat, motor Quick Release body, rotor motor with
And motor fixing sleeve composition, for existing rotor motor quick-disassembly structure, this patent is that rotor motor is passed through motor
Fixing sleeve is set in fixed cavity；It, which is implemented, is relatively easy to, since motor fixing sleeve is close proximity in fixed cavity, electricity
Always be not in gap around machine, thus will not occur unnecessary shaking after long-time use because of gap.
As an improvement of the above technical solution, a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure, feature exist
In：The upper end of motor Quick Release body is connected by hinge the side of part and motor fixing seat along connection；The lower end of motor Quick Release body with
It is fixed between the lower end edge of motor fixing seat by bolt assembly.When dismantling rotor motor, first looser a bolt component, opens electricity
Motor fixing sleeve is carried out assembly and disassembly manually by machine Quick Release body.
As an improvement of the above technical solution, a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure, feature exist
In：Fixing the corresponding inner wall of cavity has internal screw thread, and the lateral surface of motor fixing sleeve has external screw thread corresponding with internal screw thread,
The lower end of motor fixing sleeve is formed with turning end.So after opening motor Quick Release body, assembled either manually or by turning end
With disassembly motor fixing sleeve, and motor fixing sleeve is the contact by external screw thread with internal screw thread to reach mutually tight in this patent
Solid, it also can guarantee the stabilization of motor after long-time use.
As an improvement of the above technical solution, a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure, feature exist
In：Groove is provided at the top of motor fixing seat, groove has been embedded in buffering spongy layer.When by motor fixing sleeve by rotor motor
After being sent into fixed cavity, buffering spongy layer can carry out buffer protection to the top of rotor motor, prevent the top of rotor motor
It is contacted with the inside top of motor fixing seat and generates damage, and buffering spongy layer can also prevent dust to be mixed into.
The utility model has the following advantages that：The utility model provides a kind of multi-rotor unmanned aerial vehicle rotor by improving herein
Motor quick-disassembly structure has the following advantages that as shown in Figure 1-Figure 3；
Advantage 1：The quick-disassembly structure includes motor fixing seat, motor Quick Release body, rotor motor and motor fixing sleeve；Motor
The inside of fixing seat forms the fixation cavity of rotor motor, and rotor motor is arranged in motor fixing sleeve, rotor motor and motor
What fixing sleeve was formed is integrally placed in fixed cavity；Motor Quick Release body is connected to the downside of motor fixing seat, motor fixing seat
Top be provided with for rotor motor turning end stretch out through-hole.This patent improve after, by motor fixing seat, motor Quick Release body,
Rotor motor and motor fixing sleeve composition, for existing rotor motor quick-disassembly structure, this patent is by rotor electricity
Machine is set in fixed cavity by motor fixing sleeve；It, which is implemented, is relatively easy to, since motor fixing sleeve is to be close proximity to admittedly
Determine in cavity, be always not in gap around motor, thus will not occur because of gap after long-time use unnecessary
It shakes.
Advantage 2：A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure described in the utility model, in order to guarantee motor Quick Release
The rotation of body flexibly and is quickly opened, and the upper end of motor Quick Release body can be connected by hinge to the side of part and motor fixing seat
Along connection；It is fixed between the lower end of motor Quick Release body and the lower end edge of motor fixing seat by bolt assembly；In disassembly rotor electricity
When machine, first looser a bolt component, opens motor Quick Release body, and motor fixing sleeve is carried out assembly and disassembly manually.
Advantage 3：A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure described in the utility model, fixed cavity are corresponding interior
Wall surface has internal screw thread, and the lateral surface of motor fixing sleeve has external screw thread corresponding with internal screw thread, the lower end one of motor fixing sleeve
Body is formed with turning end；So after opening motor Quick Release body, carry out assembly and disassembly motor fixing sleeve either manually or by turning end, and
And motor fixing sleeve is that the contact by external screw thread with internal screw thread mutually fastens to reach in this patent, after long-time use
It can guarantee the stabilization of motor.
Advantage 4：A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure described in the utility model, the top of motor fixing seat
It is provided with groove, groove has been embedded in buffering spongy layer；After rotor motor is sent into fixed cavity by motor fixing sleeve, delay
Buffer protection can be carried out to the top of rotor motor by rushing spongy layer, be prevented in the top of rotor motor and the top of motor fixing seat
Side contacts and generate damage, and buffer spongy layer dust can also be prevented to be mixed into.
Detailed description of the invention
Fig. 1 is the whole implementation schematic diagram of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure described in the utility model；
Fig. 2 is motor fixing seat and motor Quick Release body portion schematic diagram in the utility model；
Fig. 3 is the schematic diagram of motor fixing sleeve described in the utility model.
Wherein：Motor fixing seat 1, motor Quick Release body 2, rotor motor 3, motor fixing sleeve 4, fixed cavity 5, hinge connection
Part 6, side is along 7, lower end edge 8, bolt assembly 9, internal screw thread 10, external screw thread 11, turning end 12, through-hole 13, groove 14, buffering sea
Continuous layer 15, the inside top 16 of motor fixing seat.
Specific embodiment
The utility model is described in detail below in conjunction with attached drawing 1- Fig. 3, to the skill in the utility model embodiment
Art scheme is clearly and completely described, it is clear that and the described embodiments are only a part of the embodiments of the utility model, and
The embodiment being not all of.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creativeness
Every other embodiment obtained, fall within the protection scope of the utility model under the premise of labour.
The utility model provides a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure by improving herein, such as Fig. 1-Fig. 3
It is shown, it can be practiced as follows；The quick-disassembly structure includes motor fixing seat 1, motor Quick Release body 2, rotor motor 3
And motor fixing sleeve 4；The inside of motor fixing seat 1 forms the fixation cavity 5 of rotor motor 3, and rotor motor 3 is arranged in motor
In fixing sleeve 4, what rotor motor 3 and motor fixing sleeve 4 were formed is integrally placed in fixed cavity 5；Motor Quick Release body 2 is connected to electricity
The downside of machine fixing seat 1, the top of motor fixing seat 1 are provided with the through-hole 13 stretched out for 3 turning end of rotor motor.
After this patent improves, it is made of motor fixing seat 1, motor Quick Release body 2, rotor motor 3 and motor fixing sleeve 4,
For existing rotor motor quick-disassembly structure, this patent is that rotor motor 3 is set to fixation by motor fixing sleeve 4
In cavity 5；It, which is implemented, is relatively easy to, since motor fixing sleeve 4 is close proximity in fixed cavity 5, around motor always not
It will appear gap, thus will not occur unnecessary shaking after long-time use because of gap.
On the other hand, a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure described in the utility model, in order to guarantee motor
The rotation of Quick Release body 2 flexibly and is quickly opened, and the upper end of motor Quick Release body 2 can be connected by hinge part 6 and fixed with motor
The side of seat 1 is along 7 connections；It is solid by bolt assembly 9 between the lower end of motor Quick Release body 2 and the lower end edge 8 of motor fixing seat 1
It is fixed；When dismantling rotor motor 3, first looser a bolt component 9, opens motor Quick Release body 2, motor fixing sleeve 4 is carried out group manually
Assembly and disassembly.
On the other hand, a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure described in the utility model, fixed cavity 5 are corresponding
Inner wall there is internal screw thread 10, the lateral surface of motor fixing sleeve 4 has external screw thread 11 corresponding with internal screw thread 10, and motor is fixed
The lower end of set 4 is formed with turning end 12；So after opening motor Quick Release body 2, assembled either manually or by turning end 12 and
Motor fixing sleeve 4 is dismantled, and motor fixing sleeve 4 is to reach phase with the contact of internal screw thread 10 by external screw thread 11 in this patent
It mutually fastens, also can guarantee the stabilization of motor after long-time use.
On the other hand, a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure described in the utility model, motor fixing seat 1
Top is provided with groove 14, and groove 14 has been embedded in buffering spongy layer 15；It is solid when being sent into rotor motor 3 by motor fixing sleeve 4
After determining in cavity 5, buffering spongy layer 15 can carry out buffer protection to the top of rotor motor 3, prevent the top of rotor motor 3 with
The inside top 16 of motor fixing seat 1 contacts and generates damage, and buffering spongy layer 15 can also prevent dust to be mixed into.
The foregoing description of the disclosed embodiments can be realized professional and technical personnel in the field or using originally practical new
Type.Various modifications to these embodiments will be readily apparent to those skilled in the art, and determine herein
The General Principle of justice can be realized in other embodiments without departing from the spirit or scope of the present utility model.Cause
This, the present invention will not be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The widest scope consistent with features of novelty.
Claims (4)
1. a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure, it is characterised in that：The quick-disassembly structure includes motor fixing seat
（1）, motor Quick Release body（2）, rotor motor（3）And motor fixing sleeve（4）；Motor fixing seat（1）Inside formed rotor electricity
Machine（3）Fixation cavity（5）, rotor motor（3）It is arranged in motor fixing sleeve（4）In, rotor motor（3）With motor fixing sleeve
（4）What is formed is integrally placed at fixed cavity（5）It is interior；Motor Quick Release body（2）It is connected to motor fixing seat（1）Downside, motor
Fixing seat（1）Top be provided with for rotor motor（3）The through-hole that turning end is stretched out（13）.
2. a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure according to claim 1, it is characterised in that：Motor Quick Release body
（2）Upper end be connected by hinge part（6）With motor fixing seat（1）Side edge（7）Connection；Motor Quick Release body（2）Lower end
With motor fixing seat（1）Lower end edge（8）Between pass through bolt assembly（9）It is fixed.
3. a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure according to claim 1, it is characterised in that：Fixed cavity
（5）Corresponding inner wall has internal screw thread（10）, motor fixing sleeve（4）Lateral surface have and internal screw thread（10）Corresponding outer spiral shell
Line（11）, motor fixing sleeve（4）Lower end be formed with turning end（12）.
4. a kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure according to claim 1 or claim 2, it is characterised in that：Motor is solid
Reservation（1）Top be provided with groove（14）, groove（14）It has been embedded in buffering spongy layer（15）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820648988.6U CN208149610U (en) | 2018-05-03 | 2018-05-03 | A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820648988.6U CN208149610U (en) | 2018-05-03 | 2018-05-03 | A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208149610U true CN208149610U (en) | 2018-11-27 |
Family
ID=64377553
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820648988.6U Expired - Fee Related CN208149610U (en) | 2018-05-03 | 2018-05-03 | A kind of multi-rotor unmanned aerial vehicle rotor motor quick-disassembly structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208149610U (en) |
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2018
- 2018-05-03 CN CN201820648988.6U patent/CN208149610U/en not_active Expired - Fee Related
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| 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: 20181127 |