CN206437215U - Rotatably compress formula Quick Release oar - Google Patents
Rotatably compress formula Quick Release oar Download PDFInfo
- Publication number
- CN206437215U CN206437215U CN201621447495.3U CN201621447495U CN206437215U CN 206437215 U CN206437215 U CN 206437215U CN 201621447495 U CN201621447495 U CN 201621447495U CN 206437215 U CN206437215 U CN 206437215U
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- CN
- China
- Prior art keywords
- propeller
- deck
- briquetting
- oar
- quick release
- 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
Formula Quick Release oar is rotatably compressed the utility model discloses one kind.The formula Quick Release oar of the present utility model that rotatably compresses includes：Pushpin, rotation briquetting, rotating dog, propeller, propeller deck, bullet block and spring；Wherein, pushpin is set in the briquetting boss hole of rotation briquetting according to mode that can be up and down in the briquetting boss hole of rotation briquetting, rotation briquetting is locked in the high spot of propeller deck one end in the way of it can be rotated around rotating dog by rotating dog, propeller is disposed in propeller deck, and bullet block is arranged in the deck boss hole with propeller deck according to mode that can be up and down in deck boss hole；And spring is set in the endoporus of bullet block.
Description
Technical field
The utility model is related to the oar in unmanned plane field, more particularly, to unmanned plane；Specifically, the utility model is related to
And one kind rotatably compresses formula Quick Release oar.
Background technology
Unmanned plane market is more and more burning hoter, is also increasingly received by many people.Travelled outdoors boat using unmanned plane
, it is necessary to often dismantle propeller to facilitate transport during bat.Existing unmanned plane propeller leans on screw locking substantially with motor, dismounts numerous
It is trivial, and often dismounting is easily caused screw cunning tooth, causes unnecessary risk.
Moreover, existing rotary clamping mode up and down has used easy generation diastema long, so as to influence the flight of unmanned plane
Performance.
Therefore, those skilled in the art is directed to developing a kind of convenient dismounting, will not cause and tear risk open by mistake and avoid
Influence the technical scheme of the flying quality of unmanned plane.
Utility model content
In view of the drawbacks described above of prior art, technical problem to be solved in the utility model is to provide one kind and conveniently torn open
Unload, will not cause and tear risk open by mistake and avoid influenceing the flying quality of unmanned plane to rotatably compress formula Quick Release oar.
To achieve the above object, the utility model rotatably compresses formula Quick Release oar there is provided one kind, including：Pushpin, rotation
Briquetting, rotating dog, propeller, propeller deck, bullet block and spring；Wherein, pushpin according to can rotation briquetting briquetting
Up and down mode is set in the briquetting boss hole of rotation briquetting in boss hole, and rotation briquetting around rotating dog according to can revolve
The mode turned is locked in the high spot of propeller deck one end by rotating dog, and propeller is disposed in propeller deck, bullet block
According to can be up and down in deck boss hole mode be arranged in the deck boss hole with propeller deck；And spring housing
In the endoporus for being located at bullet block.
To achieve the above object, the utility model additionally provides a kind of described assembling side for rotatably compressing formula Quick Release oar
Method, it is characterised in that including：Propeller slide fit is put into propeller deck, the endoporus and propeller card of propeller deck is utilized
Two locating shafts in seat plane are positioned to propeller；The other end for pinning rotation briquetting rotates to rotation briquetting,
The rotation briquetting other end is set to be stuck in neck；Bullet block is upspring, be arranged in the groove in rotation briquetting, to limit rotation briquetting
Motion, has pressuring action to propeller to limit propeller to prevent propeller from ejecting using briquetting is rotated.
To achieve the above object, the utility model additionally provides a kind of described dismounting side for rotatably compressing formula Quick Release oar
Method, it is characterised in that including：Downwards by the pushpin being sheathed on rotation briquetting, promote bullet block to move down, depart from bullet block
Briquetting is rotated, restriction effect of the bullet block to rotation briquetting is released, the other end for pinning rotation briquetting is rotated, and makes rotation briquetting
The end region of propeller is marked, pressuring action of the rotation briquetting to propeller is released, takes out propeller.
Compared with prior art, the utility model can greatly improve the disassembly efficiency of propeller, facilitate the fortune of unmanned plane
It is defeated, and the utility model is by compression power restriction propeller, the diastema between limited reduction propeller and deck, to unmanned plane
Flying quality does not influence, and safe.
The technique effect of design of the present utility model, concrete structure and generation is made furtherly below with reference to accompanying drawing
It is bright, to be fully understood from the purpose of this utility model, feature and effect.
Brief description of the drawings
With reference to accompanying drawing, and by reference to following detailed description, it will more easily have more complete to the utility model
Understand and its adjoint advantages and features is more easily understood, wherein：
Fig. 1 is the decomposing schematic representation for rotatably compressing formula Quick Release oar according to the utility model preferred embodiment.
Fig. 2 is illustrated according to the assembling of the part-structure for rotatably compressing formula Quick Release oar of the utility model preferred embodiment
Figure.
Fig. 3 is shown according to another assembling of the part-structure for rotatably compressing formula Quick Release oar of the utility model preferred embodiment
It is intended to.
Fig. 4 is the part-structure of the part-structure for rotatably compressing formula Quick Release oar according to the utility model preferred embodiment
Sectional view.
It should be noted that accompanying drawing is used to illustrate the utility model, and unrestricted the utility model.Note, represent structure
Accompanying drawing may be not necessarily drawn to scale.Also, in accompanying drawing, same or similar element indicates same or similar mark
Number.
Embodiment
Fig. 1 is the decomposing schematic representation for rotatably compressing formula Quick Release oar according to the utility model preferred embodiment, and Fig. 2 is basis
The assembling schematic diagram of the part-structure for rotatably compressing formula Quick Release oar of the utility model preferred embodiment, Fig. 3 is according to this practicality
Another assembling schematic diagram of the part-structure for rotatably compressing formula Quick Release oar of new preferred embodiment, Fig. 4 is new according to this practicality
The sectional view of the part-structure of the part-structure for rotatably compressing formula Quick Release oar of type preferred embodiment.
As shown in Figure 1, Figure 2, Figure 3 and Figure 4, formula Quick Release oar bag is rotatably compressed according to the utility model preferred embodiment
Include：Pushpin 1, rotation briquetting 2, rotating dog 3, propeller 4, propeller deck 5, bullet block 6 and spring 7.
Wherein, pushpin 1 is set in rotation according to mode that can be up and down in the briquetting boss hole of rotation briquetting 2
In the briquetting boss hole of briquetting 2, rotation briquetting 2 is locked in propeller in the way of it can be rotated around rotating dog 3 by rotating dog 3
The high spot of the one end of deck 5, propeller 4 is disposed in propeller deck 5, and bullet block 6 is according on can be in deck boss hole
Lower movable mode is arranged in the deck boss hole with propeller deck 5；And spring 7 is set in the endoporus of bullet block 6.
For the assembling for rotatably compressing formula Quick Release oar according to the utility model preferred embodiment, following steps can be taken
Suddenly：
The slide fit of propeller 4 is put into propeller deck 5, the endoporus and the plane of propeller deck 5 of propeller deck 5 is utilized
On two locating shafts propeller 4 is positioned；The other end for pinning rotation briquetting 2 rotates to rotation briquetting 2, makes rotation
Turn the other end of briquetting 2 to be stuck in neck；Bullet block 6 is upspring, be arranged in the groove in rotation briquetting 2, to limit rotation briquetting 2
Motion, has pressuring action to limit propeller 4 to prevent propeller 4 from ejecting using briquetting 2 is rotated to propeller 4.
For the dismounting for rotatably compressing formula Quick Release oar according to the utility model preferred embodiment, following steps can be taken
Suddenly：
Downwards by the pushpin 1 being sheathed on rotation briquetting 2, promote bullet block 6 to move down, bullet block 6 is departed from rotation pressure
Block 2, releases the restriction effect of bullet 6 pairs of rotation briquettings 2 of block, and the other end for installing rotation briquetting 2 is rotated, and makes rotation briquetting 2
The end region of propeller 4 is marked, pressuring action of the rotation briquetting 2 to propeller 4 is released, takes out propeller 4.
Compared with prior art, the utility model can greatly improve the disassembly efficiency of propeller, facilitate the fortune of unmanned plane
It is defeated, and the utility model is by compression power restriction propeller, the diastema between limited reduction propeller and deck, to unmanned plane
Flying quality does not influence, and safe.
Preferred embodiment of the present utility model has shown and described in described above, as previously described, it should be understood that this practicality is new
Type is not limited to form disclosed herein, is not to be taken as the exclusion to other embodiment, and available for various other groups
Close, change and environment, and above-mentioned teaching or the technology of association area can be passed through in utility model contemplated scope described herein
Or knowledge is modified.And the change and change that those skilled in the art are carried out do not depart from spirit and scope of the present utility model, then
All should be in the protection domain of the utility model appended claims.
Claims (1)
1. one kind rotatably compresses formula Quick Release oar, it is characterised in that including：Pushpin, rotation briquetting, rotating dog, propeller, spiral
Oar deck, bullet block and spring；Wherein, pushpin according to can in the briquetting boss hole of rotation briquetting up and down mode set
In the briquetting boss hole for being located at rotation briquetting, rotation briquetting is locked in spiral shell in the way of it can be rotated around rotating dog by rotating dog
The high spot of oar deck one end is revolved, propeller is disposed in propeller deck, bullet block is according on can be in deck boss hole
Lower movable mode is arranged in the deck boss hole with propeller deck；And spring is set in the endoporus of bullet block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621447495.3U CN206437215U (en) | 2016-12-27 | 2016-12-27 | Rotatably compress formula Quick Release oar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621447495.3U CN206437215U (en) | 2016-12-27 | 2016-12-27 | Rotatably compress formula Quick Release oar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206437215U true CN206437215U (en) | 2017-08-25 |
Family
ID=59642049
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621447495.3U Expired - Fee Related CN206437215U (en) | 2016-12-27 | 2016-12-27 | Rotatably compress formula Quick Release oar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206437215U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109969389A (en) * | 2017-12-28 | 2019-07-05 | 昆山优尼电能运动科技有限公司 | A kind of blade connection structure |
| CN111655579A (en) * | 2019-05-17 | 2020-09-11 | 深圳市大疆创新科技有限公司 | Quick detach coupling assembling, power component, power suit and unmanned aerial vehicle |
-
2016
- 2016-12-27 CN CN201621447495.3U patent/CN206437215U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109969389A (en) * | 2017-12-28 | 2019-07-05 | 昆山优尼电能运动科技有限公司 | A kind of blade connection structure |
| CN111655579A (en) * | 2019-05-17 | 2020-09-11 | 深圳市大疆创新科技有限公司 | Quick detach coupling assembling, power component, power suit and unmanned aerial vehicle |
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Legal Events
| 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: 20170825 Termination date: 20201227 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |