CN206125920U - Unmanned aerial vehicle rotor quick assembly disassembly structure - Google Patents
Unmanned aerial vehicle rotor quick assembly disassembly structure Download PDFInfo
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- CN206125920U CN206125920U CN201621045241.9U CN201621045241U CN206125920U CN 206125920 U CN206125920 U CN 206125920U CN 201621045241 U CN201621045241 U CN 201621045241U CN 206125920 U CN206125920 U CN 206125920U
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- support
- support arm
- aerial vehicle
- unmanned aerial
- rotor
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Abstract
The utility model provides an unmanned aerial vehicle rotor quick assembly disassembly structure, it includes support, support arm, screw cap, the support is fixed in the unmanned aerial vehicle main part, the support arm is connected with unmanned aerial vehicle's rotor, screw cap is used for fixed connection support arm and support, the inside of support is provided with the location of the key open on the support arm have with location of the key assorted notch, after the support arm inserted support one end, the accessible location of the key was connected with the notch cooperation, reticulation cap internal surface is equipped with the internal thread, the support surface be equipped with with the external screw thread that the internal thread matches, screw cap passes through internal thread, external screw thread and the support arm is accomplished and is connected, will the support arm gets up with the leg joint. The utility model provides an unmanned aerial vehicle rotor quick assembly disassembly structure can let rotor and fuselage separate, breaks the whole up into parts, separately packs the effectual space that utilizes for more convenient of transportation.
Description
Technical field
This utility model is related to unmanned plane mounting technique field, particularly a kind of unmanned plane rotor fast assembling disassembling structure.
Background technology
The mode of folding rotor being used multi-rotor unmanned aerial vehicle in the market, as this connected mode is caused more
Rotor and fuselage itself are separated, and still occupy very big space, this to unmanned plane packaging and transport bring very
Big difficulty.In order to preferably adapt to development of the market to unmanned plane, on the premise of unmanned plane performance is guaranteed, using this fast
Fast attaching/detaching apparatus so that rotor can be separated with unmanned aerial vehicle body so that preferably can save in product packaging and transportation
Save space, improves packaging and the efficiency transported.
Utility model content
To solve above-mentioned technical problem, this utility model provides a kind of unmanned plane rotor fast assembling disassembling structure, and which includes
Support, support arm, thread cap, the support are fixed in unmanned plane main body, and the support arm is connected with the rotor of unmanned plane, the spiral shell
Stricture of vagina cap is used to be fixedly connected support arm and support；
The support includes a cylindrical hollow configuration, and the support arm is the cylinder matched with the cylindrical hollow configuration
Structure；
The support is internally provided with key mapping, is provided with the notch matched with the key mapping on the support arm, described
Behind support arm insertion support one end, can be connected with notch by key mapping；
Reticulate pattern cap inner surface is provided with female thread, and the rack outer surface is provided with the external screw thread matched with the female thread, institute
State thread cap to complete to be connected with the support arm by the female thread, external screw thread, the support arm and support are coupled together.
This utility model has the advantages that：
The unmanned plane rotor fast assembling disassembling structure that this utility model is provided can allow rotor to separate with fuselage, break the whole up into parts,
Separately pack, effective utilization space so that transport is more convenient.
Certainly, implement arbitrary product of the present utility model to it is not absolutely required to while reaching all the above advantage.
Description of the drawings
In order to be illustrated more clearly that the technical scheme of this utility model embodiment, below will be to making required for embodiment description
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present utility model,
For those of ordinary skill in the art, on the premise of not paying creative work, can be with according to these accompanying drawings acquisitions
Other accompanying drawings.
The unmanned plane rotor fast assembling disassembling structure schematic diagram that Fig. 1 is provided for this utility model.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only this utility model a part of embodiment, rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under the premise of creative work is made
The all other embodiment for being obtained, belongs to the scope of this utility model protection.
This utility model embodiment provides a kind of unmanned plane rotor fast assembling disassembling structure, as shown in Figures 1 and 2, its bag
Support 1, support arm 3, thread cap 2 are included, the support 1 is fixed in unmanned plane main body, the support arm 3 is connected with the rotor of unmanned plane
Connect, the thread cap 2 is used to be fixedly connected support arm 3 and support 1；
The support 1 includes a cylindrical hollow configuration, and the support arm 3 is the post matched with the cylindrical hollow configuration
Body structure；
The support 1 is internally provided with key mapping, is provided with the notch matched with the key mapping, institute on the support arm 3
After stating 1 one end of the insertion support of support arm 3, can be connected with notch by key mapping；
2 inner surface of reticulate pattern cap is provided with female thread, and 1 outer surface of the support is provided with the external screw thread matched with the female thread,
The thread cap 2 completes to be connected with the support arm 3 by the female thread, external screw thread, and the support arm 3 has been connected with support 1
Come.
The unmanned plane rotor fast assembling disassembling structure that this utility model is provided can allow rotor to separate with fuselage, break the whole up into parts,
Separately pack, effective utilization space so that transport is more convenient.
This utility model preferred embodiment disclosed above is only intended to help and illustrates this utility model.Preferred embodiment is simultaneously
Without all of details of detailed descriptionthe, it is only described specific embodiment also not limit the utility model.Obviously, according to this theory
The content of bright book, can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to preferably
Principle of the present utility model and practical application are explained, so that skilled artisan can be best understood by and utilize this
Utility model.This utility model is only limited by claims and its four corner and equivalent.
Claims (1)
1. a kind of unmanned plane rotor fast assembling disassembling structure, it is characterised in that including support, support arm, thread cap, the support is fixed
In unmanned plane main body, the support arm is connected with the rotor of unmanned plane, and the thread cap is used to be fixedly connected support arm and support；
The support includes a cylindrical hollow configuration, and the support arm is the cylinder knot matched with the cylindrical hollow configuration
Structure；
The support is internally provided with key mapping, is provided with the notch matched with the key mapping, the support arm on the support arm
Behind insertion support one end, can be connected with notch by key mapping；
Reticulate pattern cap inner surface is provided with female thread, and the rack outer surface is provided with the external screw thread matched with the female thread, the spiral shell
Stricture of vagina cap completes to be connected with the support arm by the female thread, external screw thread, and the support arm and support are coupled together.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621045241.9U CN206125920U (en) | 2016-09-08 | 2016-09-08 | Unmanned aerial vehicle rotor quick assembly disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621045241.9U CN206125920U (en) | 2016-09-08 | 2016-09-08 | Unmanned aerial vehicle rotor quick assembly disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206125920U true CN206125920U (en) | 2017-04-26 |
Family
ID=58570486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621045241.9U Active CN206125920U (en) | 2016-09-08 | 2016-09-08 | Unmanned aerial vehicle rotor quick assembly disassembly structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206125920U (en) |
-
2016
- 2016-09-08 CN CN201621045241.9U patent/CN206125920U/en active Active
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