CN204473153U - The fixed sturcture that a kind of multi-rotor aerocraft electricity is adjusted - Google Patents
The fixed sturcture that a kind of multi-rotor aerocraft electricity is adjusted Download PDFInfo
- Publication number
- CN204473153U CN204473153U CN201520086619.9U CN201520086619U CN204473153U CN 204473153 U CN204473153 U CN 204473153U CN 201520086619 U CN201520086619 U CN 201520086619U CN 204473153 U CN204473153 U CN 204473153U
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- CN
- China
- Prior art keywords
- rotor aerocraft
- main body
- electricity
- described main
- fixed sturcture
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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.)
- Expired - Fee Related
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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The utility model discloses the fixed sturcture that a kind of multi-rotor aerocraft electricity is adjusted, comprise main body; Described main body side is connected with multi-rotor aerocraft support level, and opposite side is connected with multi-rotor aerocraft motor is vertical, is provided with and puts the downside that cavity, cavity that electricity adjusts are positioned at described main body and multi-rotor aerocraft motor junction in described main body.Multi-rotor aerocraft support, multi-rotor aerocraft motor, multi-rotor aerocraft electricity are adjusted and are fixedly connected with by main body by the utility model, reach effect that is fixing and protection multi-rotor aerocraft electricity tune, fixation is played to multi-rotor aerocraft motor simultaneously; After fixing, profile is neatly generous, without repetition and waste band, avoids waste of material cost-saving.
Description
Technical field
The utility model belongs to multi-rotor aerocraft technical field, in particular to the fixed sturcture that a kind of multi-rotor aerocraft electricity is adjusted.
Background technology
In recent years, the advantages such as the region that multi-rotor aerocraft much cannot arrive because of its cost is low, efficiency-cost ratio is high, no one was injured risk and can setting foot in, be with a wide range of applications in dual-use field, as low-altitude reconnaissance, meteorological exploration, aerial photography, traffic patrolling etc.
As accompanying drawing 1, shown in 2, the electricity of existing multi-rotor aerocraft adjusts fixed form to be substantially all increase by one piece of carbon plate in motor bottom, then 11 direct VELCRO are adjusted to be pasted onto below carbon plate electricity, and fixed by band colligation, shortcoming fixing is like this complicated operation, contour structures is affected after fixing, each dismounting all needs band to cut, new band need be used when again fixing, cause waste of material, cost increases, and as run into misty rain weather during flight, electricity adjusts 11 to be easy to damage, once the aircraft bombing that has an accident, damaging easily appears in the direct Crater face of exposed motor outside.
Summary of the invention
Goal of the invention: for the deficiencies in the prior art, the utility model provides a kind of multi-rotor aerocraft fixed sturcture that electricity is adjusted, and fixed form is succinct, saves material, and can play a very good protection to electricity tune.
Technical scheme: the fixed sturcture that multi-rotor aerocraft electricity described in the utility model is adjusted, comprises main body; Described main body side is provided with the groove one for being connected with multi-rotor aerocraft support level, and opposite side is provided with for the groove two that be connected vertical with multi-rotor aerocraft motor, is provided with the cavity put electricity and adjust in the below of groove two; Described main body is connected side higher than the side be connected with multi-rotor aerocraft support with multi-rotor aerocraft motor.
Improve such scheme further, described main body is the main body that injection moulding is made.
Described main body both sides are triangular shape.
Described main body is the main body adopting waterproof material to make.
Described main body side is provided with through hole.
Beneficial effect: compared with prior art, advantage of the present utility model: the utility model is the agent structure adopting injection moulding to make, makes simple; By main body, multi-rotor aerocraft support, multi-rotor aerocraft motor, multi-rotor aerocraft electricity are adjusted and be fixedly connected with, reach the fixing and electric effect adjusted of protection multi-rotor aerocraft, fixation is played to multi-rotor aerocraft motor simultaneously; After fixing, profile is neatly generous, without repetition and waste band, avoids waste of material cost-saving; Employing waterproof material is made, and plays the effect of waterproofing protection.
Accompanying drawing explanation
Fig. 1 is the lateral plan that in prior art, multi-rotor aerocraft electricity adjusts fixed sturcture.
Fig. 2 is the elevation view that in prior art, multi-rotor aerocraft electricity adjusts fixed sturcture.
Fig. 3 is lateral plan of the present utility model.
Fig. 4 is block diagram of the present utility model.
Detailed description of the invention
Below by accompanying drawing, technical solutions of the utility model are described in detail, but protection domain of the present utility model is not limited to described embodiment.
Embodiment 1: as accompanying drawing 3, the fixed sturcture that multi-rotor aerocraft electricity shown in Fig. 4 is adjusted, for integrated body 20 structure that injection moulding is made, main body 20 both sides are triangular shape, main body 20 side is connected with multi-rotor aerocraft support level, multi-rotor aerocraft support stretches in the groove 1 of main body side, main body 20 opposite side is connected with multi-rotor aerocraft motor is vertical, multi-rotor aerocraft motor extend in the groove 2 22 of main body opposite side from top to bottom, main body is connected the height of side higher than the side that is connected with multi-rotor aerocraft support with multi-rotor aerocraft motor, play and better protective effect is fixed to multi-rotor aerocraft motor, in main body 20, the below of groove 2 22 is provided with the cavity 23 put multi-rotor aerocraft electricity and adjust, being adjusted by multi-rotor aerocraft electricity is placed in cavity, well fixing and protective effect is played to it, the side of main body 20 is provided with through hole 24.
As mentioned above, although represented with reference to specific preferred embodiment and described the utility model, it shall not be construed as the restriction to the utility model self.Under the spirit and scope prerequisite of the present utility model not departing from claims definition, various change can be made in the form and details to it.
Claims (5)
1. a fixed sturcture for multi-rotor aerocraft electricity tune, is characterized in that: comprise main body; Described main body side is provided with the groove one for being connected with multi-rotor aerocraft support level, and opposite side is provided with for the groove two that be connected vertical with multi-rotor aerocraft motor, is provided with the cavity put electricity and adjust in the below of groove two; Described main body is connected side higher than the side be connected with multi-rotor aerocraft support with multi-rotor aerocraft motor.
2. the fixed sturcture of multi-rotor aerocraft electricity tune according to claim 1, is characterized in that: described main body is the main body that injection moulding is made.
3. the fixed sturcture of multi-rotor aerocraft electricity tune according to claim 1, is characterized in that: described main body both sides are triangular shape.
4. the fixed sturcture of multi-rotor aerocraft electricity tune according to claim 1, is characterized in that: described main body is the main body adopting waterproof material to make.
5. the fixed sturcture of multi-rotor aerocraft electricity tune according to claim 1, is characterized in that: described main body side is provided with through hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520086619.9U CN204473153U (en) | 2015-02-06 | 2015-02-06 | The fixed sturcture that a kind of multi-rotor aerocraft electricity is adjusted |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520086619.9U CN204473153U (en) | 2015-02-06 | 2015-02-06 | The fixed sturcture that a kind of multi-rotor aerocraft electricity is adjusted |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204473153U true CN204473153U (en) | 2015-07-15 |
Family
ID=53628944
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520086619.9U Expired - Fee Related CN204473153U (en) | 2015-02-06 | 2015-02-06 | The fixed sturcture that a kind of multi-rotor aerocraft electricity is adjusted |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204473153U (en) |
-
2015
- 2015-02-06 CN CN201520086619.9U patent/CN204473153U/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 |
Granted publication date: 20150715 Termination date: 20190206 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |