CN207157527U - Unmanned plane propeller fast-assembling buckle assembly - Google Patents
Unmanned plane propeller fast-assembling buckle assembly Download PDFInfo
- Publication number
- CN207157527U CN207157527U CN201721222868.1U CN201721222868U CN207157527U CN 207157527 U CN207157527 U CN 207157527U CN 201721222868 U CN201721222868 U CN 201721222868U CN 207157527 U CN207157527 U CN 207157527U
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- CN
- China
- Prior art keywords
- propeller
- block
- fixture
- output end
- unmanned plane
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- 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.)
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Abstract
The utility model discloses a kind of unmanned plane propeller fast-assembling buckle assembly, including the propeller fixture being arranged on propeller and the output end fixture being arranged in unmanned machine actuating device output end;Buckle projection is provided with the outer wall of the propeller fixture;Being shaped as of the output end fixture can accommodate the barrel-shaped of propeller fixture, the chute in the same direction with own axes is provided with the side wall of output end fixture, the block that can slide up and down is provided with chute, block is arranged with the block for driving up block, and the side of chute is provided with the stopper slot for accommodating buckle projection and being connected with chute.Propeller installation and dismounting speed are fast, efficiency high, greatly shorten the time before unmanned machine operation, binding site area is big, and structure is firm;Two two-way fixings of block are set in stopper slot, eliminate the diastema with drive device part after propeller installation, mounted configuration is stable, reduces unmanned plane during flying risk.
Description
Technical field
It the utility model is related to a kind of unmanned plane propeller fast-assembling buckle, more particularly to a kind of unmanned plane propeller quick-mounting clamp
Detain assembly.
Background technology
, it is necessary to which propeller is arranged on driving assembling device when using unmanned plane.Unmanned plane spiral of the prior art
Oar mounting structure is complicated, and coupling part is weak, and insufficient strength is, it is necessary to multiple steps could be completed to install or remove, installing/dismounting
Efficiency is low;And diastema after installing, cause propeller to produce vibration when rotating at a high speed, influence efficiency, or even de- oar phenomenon occurs,
De- oar is easier especially when drive device is slowed down suddenly.
Therefore, it is necessary to prior art is improved to solve above-mentioned technical problem.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of unmanned plane propeller fast-assembling buckle assembly, Ke Yishi
The Fast Installation of existing propeller or dismounting, and mounted configuration is stable.Realized in particular by following technical scheme:
Unmanned plane propeller fast-assembling buckle assembly of the present utility model, including the propeller fixture being arranged on propeller
With the output end fixture being arranged in unmanned machine actuating device output end;
Buckle projection is provided with the outer wall of the propeller fixture;
The output end fixture is shaped as accommodating the barrel-shaped of propeller fixture, in the side wall of output end fixture
The chute in the same direction with own axes is provided with, the block that can slide up and down is provided with chute, block is arranged with for upward
The block of block is driven, the side of chute is provided with the stopper slot for accommodating buckle projection and being connected with chute.
Further, buckle projection, chute, block, spring and the stopper slot are all symmetrical arranged two groups.
Further, the block stretches out to form block epitaxy part, the side wall of the output end fixture and bottom surface pair
Block epitaxy part is answered to stretch out to form block epitaxy part accommodating chamber, the spring is arranged at below block epitaxy part.
Further, the handle for being easy to drive block is provided with the outside of the block epitaxy part, the block epitaxy part accommodates
The elliptical hole passed through for handle is provided with the outer wall of chamber.
Further, the propeller fixture is the barrel shaped structure that Open Side Down.
Further, the output end fixture is provided with defeated for output end fixture to be fixed on into unmanned machine actuating device
The output end fixing hole gone out on end.
Further, the propeller fixing hole for being fixed on propeller is provided with the propeller fixture.
The beneficial effects of the utility model:Unmanned plane propeller fast-assembling buckle assembly of the present utility model, propeller installation
It is fast with dismounting speed, efficiency high, the time before unmanned machine operation is greatly shortened, binding site area is big, and structure is firm;
Two two-way fixings of block are set in stopper slot, eliminate the diastema with drive device part after propeller installation, peace
Stability Analysis of Structures after dress, reduce unmanned plane during flying risk;Other beneficial effects of the present utility model will combine to be implemented in detail below
Example is further detailed.
Brief description of the drawings
The utility model is further described with reference to the accompanying drawings and examples:
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of propeller fixture;
Fig. 3 is the structural representation of output end fixture;
Fig. 4 is that the utility model completes the view after fast-assembling;
In figure:1st, propeller fixture, 1-1, buckle projection, 1-2, propeller fixing hole;2nd, output end fixture, 2-1,
Output end fixing hole, 2-2, spring, 2-3, block epitaxy part, 2-4, block, 2-5, stopper slot, 2-6, handle, 2-7, ellipse are logical
Hole
Embodiment
As shown in the figure:Unmanned plane propeller fast-assembling buckle assembly in the present embodiment, including the spiral shell being arranged on propeller
Revolve oar fixture 1 and the output end fixture 2 being arranged in unmanned machine actuating device output end;
Buckle projection 1-1 is provided with the outer wall of the propeller fixture 1;
The output end fixture 2 is shaped as accommodating the barrel-shaped of propeller fixture 1, the side of output end fixture 2
The chute in the same direction with own axes is provided with wall, the block 2-4 that can slide up and down is provided with chute, block is arranged with use
In the spring 2-2 for driving up block, the side of chute is provided with for accommodating buckle projection 1-1 and being connected with chute spacing
Groove 2-5.
During installation, buckle projection 1-1 is moved down along chute and press against block 2-4 and overcome spring 2-2 elastic force downward
Motion expose stopper slot 2-5 lean on mouth after, rotating screw fixture 1 cause buckle projection 1-1 enter stopper slot 2-5 in after,
Block 2-4 is popped up under spring 2-2 elastic force effect and is blocked buckle projection 1-1, prevents propeller fixture 1 from turning round;Tear open
When unloading, block 2-4 is pressed downward, after opposite direction rotating screw fixture 1 causes buckle projection 1-1 to enter chute, you can quick
Extract propeller fixture 1.
In the present embodiment, buckle projection 1-1, chute, block 2-4, spring 2-2 and the stopper slot 2-4 are all symmetrical arranged
Two groups.Bidirectionally limited, structure is more stable, caused de- oar when being avoided that the unexpected reduction of speed of drive device.
In the present embodiment, the block 2-4 stretches out to form block epitaxy part 2-3, the side of the output end fixture 2
Wall and bottom surface correspond to block epitaxy part and stretch out to form block epitaxy part accommodating chamber, and the spring is arranged at block epitaxy part 2-
3 lower sections, it can be provided for installing spring 2-2 blind hole below block epitaxy part 2-3.It is easily installed spring.
In the present embodiment, the handle 2-6 for being easy to drive block, the block are provided with the outside of the block epitaxy part 2-3
The elliptical hole 2-7 passed through for handle is provided with the outer wall of epitaxy part accommodating chamber.Block is pressed downward when easy to disassemble.
In the present embodiment, the propeller fixture 1 is the barrel shaped structure that Open Side Down.Mitigate main screw lift, and not
Propeller fixture is influenceed to be fixed on propeller.
In the present embodiment, the output end fixture 2 is provided with for output end fixture 2 to be fixed on into unmanned plane driving
Output end fixing hole 2-1 in device output end.
In the present embodiment, it is provided with the propeller fixture 1 and consolidates for the propeller being fixed on propeller
Determine hole 1-2.
Finally illustrate, above example is only unrestricted to illustrate the technical solution of the utility model, although ginseng
The utility model is described in detail according to preferred embodiment, it will be understood by those within the art that, can be to this
The technical scheme of utility model is modified or equivalent substitution, without departing from the objective and model of technical solutions of the utility model
Enclose, it all should cover among right of the present utility model.
Claims (7)
- A kind of 1. unmanned plane propeller fast-assembling buckle assembly, it is characterised in that:Propeller including being arranged on propeller is fixed Part and the output end fixture being arranged in unmanned machine actuating device output end;Buckle projection is provided with the outer wall of the propeller fixture;The output end fixture is shaped as accommodating the barrel-shaped of propeller fixture, is set in the side wall of output end fixture There is the chute in the same direction with own axes, the block that can slide up and down is provided with chute, block is arranged with for driving up The block of block, the side of chute are provided with the stopper slot for accommodating buckle projection and being connected with chute.
- 2. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The buckle projection, cunning Groove, block, spring and stopper slot are all symmetrical arranged two groups.
- 3. unmanned plane propeller fast-assembling buckle assembly according to claim 2, it is characterised in that:The block stretches out Block epitaxy part is formed, the side wall of the output end fixture and bottom surface correspond to block epitaxy part and stretch out to form block extension Portion's accommodating chamber, the spring are arranged at below block epitaxy part.
- 4. unmanned plane propeller fast-assembling buckle assembly according to claim 3, it is characterised in that:Outside the block epitaxy part Side is provided with the handle for being easy to drive block, and the ellipse passed through for handle is provided with the outer wall of the block epitaxy part accommodating chamber Through hole.
- 5. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The propeller fixture For the barrel shaped structure that Open Side Down.
- 6. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The output end fixture Be provided with the output end fixing hole for output end fixture being fixed in unmanned machine actuating device output end.
- 7. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The propeller fixture On be provided with propeller fixing hole for being fixed on propeller.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721222868.1U CN207157527U (en) | 2017-09-22 | 2017-09-22 | Unmanned plane propeller fast-assembling buckle assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721222868.1U CN207157527U (en) | 2017-09-22 | 2017-09-22 | Unmanned plane propeller fast-assembling buckle assembly |
Publications (1)
Publication Number | Publication Date |
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CN207157527U true CN207157527U (en) | 2018-03-30 |
Family
ID=61723490
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201721222868.1U Expired - Fee Related CN207157527U (en) | 2017-09-22 | 2017-09-22 | Unmanned plane propeller fast-assembling buckle assembly |
Country Status (1)
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CN (1) | CN207157527U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112407300A (en) * | 2020-12-01 | 2021-02-26 | 广东历鼎龙动力科技有限公司 | Brushless motor used for plant protection unmanned aerial vehicle |
-
2017
- 2017-09-22 CN CN201721222868.1U patent/CN207157527U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112407300A (en) * | 2020-12-01 | 2021-02-26 | 广东历鼎龙动力科技有限公司 | Brushless motor used for plant protection 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 | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180330 Termination date: 20190922 |