CN204871614U - Battery embeds multiaxis aircraft - Google Patents
Battery embeds multiaxis aircraft Download PDFInfo
- Publication number
- CN204871614U CN204871614U CN201520493234.4U CN201520493234U CN204871614U CN 204871614 U CN204871614 U CN 204871614U CN 201520493234 U CN201520493234 U CN 201520493234U CN 204871614 U CN204871614 U CN 204871614U
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- CN
- China
- Prior art keywords
- horn
- battery
- aircraft
- motor
- utility
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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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Classifications
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- 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
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model provides a battery embeds multiaxis aircraft, including control module, horn installation department, whereabouts frame and a plurality of horn subassembly, control module installs in the top of horn installation department, and the whereabouts frame is fixed in the below of horn installation department, and the horn subassembly includes horn, motor cabinet, motor, paddle and battery, and the horn outwards extends from the horn installation department to be connected to the motor through the motor cabinet, the paddle is installed on the motor, and the battery is placed in the horn, and is connected to the the control unit of motor through the wire. The utility model discloses an in the horn of battery embeds multiaxis aircraft through the multiaxis aircraft of placing the battery, make the aircraft have more spaces to come other effective equipment carries of carry, shorten the distance of battery to the motor of horn end, practiced thrift the cost of wire, the whole evenly distributed of messenger's battery makes the aircraft focus more accurate on arriving whole aircraft, and the security is better.
Description
Technical field
The utility model relates to aircraft field, and in particular to the built-in Multi-axis aircraft of a kind of battery.
Background technology
In the prior art, the battery of Multi-axis aircraft is all the middle position being directly bundled in aircraft, or by the special battery compartment made by carry on board the aircraft.Because battery is placed on the middle position of aircraft, need the motor by long lead, electric energy being transmitted to horn end from battery, the conduction of long distance will be consumed energy consumption and need higher wire cost.In addition, because battery volume, weight are large, greatly occupy the load space of aircraft, and the weight of battery occupy significant proportion in whole aircraft, therefore need center-of-gravity regulating well that aircraft just can be made to keep balance in aircraft central authorities.
Utility model content
The purpose of this utility model is to provide a kind of battery built-in Multi-axis aircraft.
The utility model embodiment provides a kind of battery built-in Multi-axis aircraft, comprise control module, horn installation portion, land frame and multiple horn assembly, described control module is installed on the top of described horn installation portion, described land frame is fixed on the below of described horn installation portion, described horn assembly comprises horn, motor cabinet, motor, blade, and battery, described horn stretches out from described horn installation portion, and be connected to described motor by described motor cabinet, described blade is arranged on described motor, it is characterized in that, described battery is placed in described horn, and be wired to the control unit of described motor.
Preferably, described multiple horn of described multiple horn assembly to be symmetrically distributed on described installation portion and to stretch out with radial.
Preferably, the identical described battery of quantity is placed with in described multiple horn of described multiple horn assembly.
Preferably, described wire is copper conductor.
In the horn of the built-in Multi-axis aircraft of battery of the present utility model by the Multi-axis aircraft by battery placement, the position of script carry battery on aircraft is abdicated, aircraft is had, and other effective equipment carry of carry is carried out in more space, such as, and airborne tripod head etc.; Because battery is placed on horn inside, shorten the distance of battery to the motor of horn end, without the need to long lead conduction, decrease the electric energy loss caused because of long lead conduction, greatly saved the cost of wire simultaneously; In addition, by evenly placing the battery of equal number in each horn, make cell integratedly to be evenly distributed on whole aircraft, so again without the need to adjusting battery center of gravity on board the aircraft, make aircraft center of gravity more accurate, safety is better; By battery is built into horn, make aircraft without the need to customized design battery compartment, monnolithic case is more succinct, attractive in appearance.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is schematic perspective view of the present utility model;
Fig. 2 is the schematic perspective view of horn assembly of the present utility model;
Fig. 3 is the cutaway view along the line of A-A shown in Fig. 2.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Fig. 1 is schematic perspective view of the present utility model.As shown in Figure 1, Multi-axis aircraft of the present utility model comprises control module 1, horn installation portion 2, is fixed on land frame 3 below horn installation portion 2 and multiple horn assembly.Control module 1 is installed on above horn installation portion 2, in order to control the state of flight of Multi-axis aircraft.In the embodiment shown in Fig. 1, Multi-axis aircraft is six axle aircraft, so have six horn assemblies, in other embodiments, Multi-axis aircraft has the horn assembly of other quantity, and the utility model is not as limit.
Fig. 2 is the schematic perspective view of horn assembly of the present utility model, and Fig. 3 is the cutaway view along the line of A-A shown in Fig. 2.As shown in Figure 2, horn assembly comprises horn 4, motor cabinet 5, motor 6 and blade 7.Horn 4 stretches out from horn installation portion 2, and is connected to motor 6 by motor cabinet 5.Blade 7 is arranged on motor 6.Six horns 4 to be symmetrically distributed on installation portion 2 and to stretch out with radial.As shown in Figure 3, battery 41 is placed in horn 4, is connected to the control unit 61 of motor 6 by wire 42.When after energising, motor 6 drives blade 7 to rotate, thus Multi-axis aircraft is flown.
Further, in the horn 4 of six horn assemblies, be all evenly placed with the identical battery of quantity 41, make cell integrated being evenly distributed on whole aircraft.
Further, wire 42 is copper conductor.
Advantageously, in the horn of the built-in Multi-axis aircraft of battery of the present utility model by the Multi-axis aircraft by battery placement, abdicated the position of script carry battery on aircraft, aircraft is had, and other effective equipment carry of carry is carried out in more space, such as, airborne tripod head etc.; Because battery is placed on horn inside, shorten the distance of battery to the motor of horn end, without the need to long lead conduction, decrease the electric energy loss caused because of long lead conduction, greatly saved the cost of wire simultaneously; In addition, by evenly placing the battery of equal number in each horn, make cell integratedly to be evenly distributed on whole aircraft, so again without the need to adjusting battery center of gravity on board the aircraft, make aircraft center of gravity more accurate, safety is better; By battery is built into horn, make aircraft without the need to customized design battery compartment, monnolithic case is more succinct, attractive in appearance.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (4)
1. the built-in Multi-axis aircraft of battery, comprise control module, horn installation portion, land frame and multiple horn assembly, described control module is installed on the top of described horn installation portion, described land frame is fixed on the below of described horn installation portion, described horn assembly comprises horn, motor cabinet, motor, blade, and battery, described horn stretches out from described horn installation portion, and be connected to described motor by described motor cabinet, described blade is arranged on described motor, it is characterized in that, described battery is placed in described horn, and be wired to the control unit of described motor.
2. the built-in Multi-axis aircraft of battery as claimed in claim 1, is characterized in that, described multiple horn of described multiple horn assembly to be symmetrically distributed on described installation portion and to stretch out with radial.
3. the built-in Multi-axis aircraft of battery as claimed in claim 1, is characterized in that, be placed with the identical described battery of quantity in described multiple horn of described multiple horn assembly.
4. the built-in Multi-axis aircraft of battery as claimed in claim 1, it is characterized in that, described wire is copper conductor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520493234.4U CN204871614U (en) | 2015-07-09 | 2015-07-09 | Battery embeds multiaxis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520493234.4U CN204871614U (en) | 2015-07-09 | 2015-07-09 | Battery embeds multiaxis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204871614U true CN204871614U (en) | 2015-12-16 |
Family
ID=54816019
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520493234.4U Expired - Fee Related CN204871614U (en) | 2015-07-09 | 2015-07-09 | Battery embeds multiaxis aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204871614U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN107396491A (en) * | 2017-07-11 | 2017-11-24 | 广东容祺智能科技有限公司 | A kind of course lamp driving of unmanned plane body and control system |
| CN108829129A (en) * | 2018-06-04 | 2018-11-16 | 成都天麒科技有限公司 | A kind of quadrotor plant protection drone flight balance adjusting method |
| CN110475719A (en) * | 2017-04-07 | 2019-11-19 | 马克·H·汉纳 | Distributed battery aircraft and its method of supplying power to |
| CN112498672A (en) * | 2020-11-03 | 2021-03-16 | 中国直升机设计研究所 | Unmanned aerial vehicle |
-
2015
- 2015-07-09 CN CN201520493234.4U patent/CN204871614U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN110475719A (en) * | 2017-04-07 | 2019-11-19 | 马克·H·汉纳 | Distributed battery aircraft and its method of supplying power to |
| US11811224B2 (en) | 2017-04-07 | 2023-11-07 | Mark Holbrook Hanna | Distributed-battery aerial vehicle and a powering method therefor |
| CN107396491A (en) * | 2017-07-11 | 2017-11-24 | 广东容祺智能科技有限公司 | A kind of course lamp driving of unmanned plane body and control system |
| CN108829129A (en) * | 2018-06-04 | 2018-11-16 | 成都天麒科技有限公司 | A kind of quadrotor plant protection drone flight balance adjusting method |
| CN112498672A (en) * | 2020-11-03 | 2021-03-16 | 中国直升机设计研究所 | Unmanned aerial vehicle |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151216 Termination date: 20190709 |