CN204937518U - A kind of multi-rotor aerocraft motor base - Google Patents
A kind of multi-rotor aerocraft motor base Download PDFInfo
- Publication number
- CN204937518U CN204937518U CN201520312271.0U CN201520312271U CN204937518U CN 204937518 U CN204937518 U CN 204937518U CN 201520312271 U CN201520312271 U CN 201520312271U CN 204937518 U CN204937518 U CN 204937518U
- Authority
- CN
- China
- Prior art keywords
- motor
- base
- rotor aerocraft
- utility
- model
- 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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Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The utility model relates to a kind of multi-rotor aerocraft motor base, is arranged on aircraft carbon fiber pipe, for laying motor; Comprise base; The both sides of described base are respectively arranged with two bolts hole, and the bolt hole of both sides be arranged in parallel; The middle part of described base is provided with the screw hole of at least three circle distribution; The utility model is by motor bottom mounting seat, more steady when motor is run, and facilitates installation and removal.
Description
Technical field
The utility model relates to aircraft field, refers in particular to a kind of multi-rotor aerocraft motor base.
Background technology
Aircraft is rotated by driven by motor wing and realizes flight, and therefore carry-on motor should ensure motor horizontal positioned when mounted, and when ensureing that motor runs again, stable generation is rocked; But existing carry-on motor is installed and extremely bothered, and can not ensure the stationarity of motor, and for this reason, we have developed a kind of multi-rotor aerocraft motor base, are arranged on motor bottom, more steady when motor is run, and facilitate installation and removal.
Utility model content
The utility model object provides a kind of multi-rotor aerocraft motor base to overcome the deficiencies in the prior art, is arranged on motor bottom, more steady when motor is run, and facilitate installation and removal.
For achieving the above object, the technical solution adopted in the utility model is: a kind of multi-rotor aerocraft motor base, is arranged on aircraft carbon fiber pipe, for laying motor; Comprise base; The both sides of described base are respectively arranged with two bolts hole, and the bolt hole of both sides be arranged in parallel; The middle part of described base is provided with the screw hole of at least three circle distribution.
Preferably, the middle part of described base is provided with knock hole.
Due to the utilization of technique scheme, the utility model compared with prior art has following advantages:
Multi-rotor aerocraft motor base described in the utility model is arranged on motor bottom, more steady when motor is run, and facilitates installation and removal.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, technical solutions of the utility model are described further:
Accompanying drawing 1 is the birds-eye view of multi-rotor aerocraft motor base described in the utility model;
Accompanying drawing 2 is the operating diagram of multi-rotor aerocraft motor base described in the utility model;
Wherein: 1, base; 11, bolt hole; 12, screw hole; 13, knock hole; 2, motor; 3, carbon fiber pipe; 4, clevis bolt.
Detailed description of the invention
Below in conjunction with drawings and the specific embodiments, the utility model is described in further detail.
Accompanying drawing 1-2 multi-rotor aerocraft motor base described in the utility model, is arranged on aircraft carbon fiber pipe 3, for laying motor 2; Comprise base 1; The both sides of described base 1 are respectively arranged with two bolts hole 11, and the bolt hole 11 of both sides be arranged in parallel; The middle part of described base 1 is provided with knock hole 13 and eight screw holes 12 of circle distribution centered by knock hole 13; During work, described base 1 is fixed on carbon fiber pipe 3 through bolt hole 11 by clevis bolt 4, and adjusts the levelness of base 1 by level indicator; The afterbody of described motor 2 is arranged in knock hole 13, makes the center of gravity of motor 2 consistent with the center of gravity of base 1, and ensure that the levelness of motor 2 simultaneously, and described motor 2 is fixed on base 1 by bolts through bolt holes 12.
Due to the utilization of technique scheme, the utility model compared with prior art has following advantages:
Multi-rotor aerocraft motor base described in the utility model is arranged on motor bottom, more steady when motor is run, and facilitates installation and removal.
Below be only embody rule example of the present utility model, protection domain of the present utility model is not constituted any limitation.The technical scheme that all employing equivalents or equivalence are replaced and formed, all drops within the utility model rights protection scope
.
Claims (2)
1. a multi-rotor aerocraft motor base, is characterized in that: be arranged on aircraft carbon fiber pipe, for laying motor; Comprise base; The both sides of described base are respectively arranged with two bolts hole, and the bolt hole of both sides be arranged in parallel; The middle part of described base is provided with the screw hole of at least three circle distribution.
2. multi-rotor aerocraft motor base according to claim 1, is characterized in that: the middle part of described base is provided with knock hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520312271.0U CN204937518U (en) | 2015-05-14 | 2015-05-14 | A kind of multi-rotor aerocraft motor base |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520312271.0U CN204937518U (en) | 2015-05-14 | 2015-05-14 | A kind of multi-rotor aerocraft motor base |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204937518U true CN204937518U (en) | 2016-01-06 |
Family
ID=55004963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520312271.0U Expired - Fee Related CN204937518U (en) | 2015-05-14 | 2015-05-14 | A kind of multi-rotor aerocraft motor base |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204937518U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908954A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Multi-rotor aircraft motor base |
| CN106275459A (en) * | 2016-08-31 | 2017-01-04 | 深圳市莲花百川科技有限公司 | A kind of easy assembling type motor of many rotors |
-
2015
- 2015-05-14 CN CN201520312271.0U patent/CN204937518U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908954A (en) * | 2015-05-14 | 2015-09-16 | 苏州绿农航空植保科技有限公司 | Multi-rotor aircraft motor base |
| CN106275459A (en) * | 2016-08-31 | 2017-01-04 | 深圳市莲花百川科技有限公司 | A kind of easy assembling type motor of many rotors |
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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: 20160106 Termination date: 20200514 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |