CN205469825U - Novel aircraft - Google Patents
Novel aircraft Download PDFInfo
- Publication number
- CN205469825U CN205469825U CN201620043484.2U CN201620043484U CN205469825U CN 205469825 U CN205469825 U CN 205469825U CN 201620043484 U CN201620043484 U CN 201620043484U CN 205469825 U CN205469825 U CN 205469825U
- Authority
- CN
- China
- Prior art keywords
- centre frame
- frame
- course
- master control
- control center
- 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
Links
Abstract
The utility model discloses a novel aircraft, include: a machine support, the frame includes centre frame and rotor mounting bracket, centre frame and rotor mounting bracket are connected, be provided with master control center subassembly on the centre frame, be provided with the GPS module on the centre frame, GPS module arch is established on the centrally positioned frame to and be the interval setting between the subassembly of master control center. In this way, the utility model discloses novel aircraft can reduce the master control center and to GPS's interference, improve the unmanned aerial vehicle flight stability, reduces the unmanned aerial vehicle organism, safe and reliable.
Description
Technical field
This utility model relates to unmanned plane field, particularly relates to a kind of course of new aircraft.
Background technology
During aircraft flight out of doors, GPS's is precisely reliably key factor, all the time unmanned plane in order to cube little more flat, but this structure can cause gps signal the most disturbed.GPS module can be disturbed by Master Control Center, and the reliability disturbing the strongest then aircraft is the poorest.Therefore, existing unmanned plane is usually and reduces interference at GPS module overlying last layer copper film, ensures the reliability of unmanned plane during flying, but this infrastructure cost is higher, and copper film ruggedness is poor, it is impossible to meet use demand.
Summary of the invention
This utility model is mainly solving the technical problems that provide a kind of course of new aircraft, it is possible to reduces the Master Control Center interference to GPS, improves unmanned plane during flying stability, reduces unmanned plane body, safe and reliable.
For solving above-mentioned technical problem, the technical scheme that this utility model uses is: provide a kind of course of new aircraft, including: frame, described frame includes centre frame and rotor installing rack, described centre frame is connected with rotor installing rack, described centre frame is provided with Master Control Center assembly, described centre frame is provided with GPS module, described GPS module projection is arranged on centre frame, and and Master Control Center assembly between in spacing arrange.
In one preferred embodiment of this utility model, described Master Control Center assembly includes that multiple panel stacking gradually setting is connected and forms.
In one preferred embodiment of this utility model, arcuately, described GPS module is arranged at the top of centre frame to the cross section of described GPS module.
In one preferred embodiment of this utility model, described centre frame and rotor installing rack one connect molding, and described rotor installing rack is provided with 4 rotor installing holes.
In one preferred embodiment of this utility model, described rotor installing hole is uniformly distributed in interval around centre frame place circle, and described rotor installing hole is provided with rotor.
In one preferred embodiment of this utility model, the both sides up and down of described rotor installing hole are provided with guard, and described guard is covered in the both sides up and down of rotor.
The beneficial effects of the utility model are: this utility model course of new aircraft, it is possible to reduce the Master Control Center interference to GPS, improve unmanned plane during flying stability, reduce unmanned plane body, safe and reliable.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, in describing embodiment below, the required accompanying drawing used is briefly described, apparently, accompanying drawing in describing below is only embodiments more of the present utility model, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings, wherein:
Fig. 1 is the perspective view of this utility model course of new aircraft one preferred embodiment；
Fig. 2 is the front view of the course of new aircraft shown in Fig. 1；
Fig. 3 is the top view of the course of new aircraft shown in Fig. 2；
Fig. 4 is the internal structure schematic diagram of the course of new aircraft shown in Fig. 2；
In accompanying drawing, the labelling of each parts is as follows: 1, frame, and 2, centre frame, 3, rotor installing rack, 4, Master Control Center assembly, 5, GPS module, 6, rotor installing hole, 7, rotor, 8, guard.
Detailed description of the invention
Technical scheme in this utility model embodiment will be clearly and completely described below, it is clear that described embodiment is only a part of embodiment of the present utility model rather than whole embodiments.Based on the embodiment in this utility model, all other embodiments that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
Refer to Fig. 1, a kind of course of new aircraft, including: frame 1, described frame includes centre frame 2 and rotor installing rack 3, described centre frame 2 is connected with rotor installing rack 3, described centre frame 2 is provided with Master Control Center assembly 4, described centre frame 2 is provided with GPS module 5, described GPS module 5 projection is arranged on centre frame 2, and and Master Control Center assembly 4 between in spacing arrange.
Form it addition, described Master Control Center assembly 4 includes that multiple panel stacking gradually setting is connected.
It addition, the cross section of described GPS module 5 is arcuately, described GPS module 5 is arranged at the top of centre frame 2.
It addition, described centre frame 2 and rotor installing rack 3 one connect molding, described rotor installing rack 3 is provided with 4 rotor installing holes 6.
It addition, described rotor installing hole 6 is uniformly distributed in interval around centre frame 2 place circle, described rotor installing hole 3 is provided with rotor 7.
It addition, the both sides up and down of described rotor installing hole 3 are provided with guard 8, described guard 8 is covered in the both sides up and down of rotor 7.
This utility model course of new aircraft is by increasing the height of frame, the diameter reducing frame reduces aircraft volume, and GPS module is arranged away from Master Control Center assembly, reduces the Master Control Center assembly signal disturbing to GPS module, improve the reliability of aircraft.
It is different from prior art, this utility model course of new aircraft, it is possible to reduce the Master Control Center interference to GPS, improves unmanned plane during flying stability, reduce unmanned plane body, safe and reliable.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every equivalent structure utilizing this utility model description to be made or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical field, the most in like manner it is included in scope of patent protection of the present utility model.
Claims (6)
1. a course of new aircraft, it is characterized in that, including: frame, described frame includes centre frame and rotor installing rack, described centre frame is connected with rotor installing rack, described centre frame is provided with Master Control Center assembly, described centre frame is provided with GPS module, described GPS module projection is arranged on centre frame, and and Master Control Center assembly between in spacing arrange.
Course of new aircraft the most according to claim 1, it is characterised in that described Master Control Center assembly includes that multiple panel stacking gradually setting is connected and forms.
Course of new aircraft the most according to claim 2, it is characterised in that arcuately, described GPS module is arranged at the top of centre frame to the cross section of described GPS module.
Course of new aircraft the most according to claim 1, it is characterised in that described centre frame and rotor installing rack one connect molding, and described rotor installing rack is provided with 4 rotor installing holes.
Course of new aircraft the most according to claim 4, it is characterised in that described rotor installing hole is uniformly distributed in interval around centre frame place circle, and described rotor installing hole is provided with rotor.
Course of new aircraft the most according to claim 5, it is characterised in that the both sides up and down of described rotor installing hole are provided with guard, described guard is covered in the both sides up and down of rotor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620043484.2U CN205469825U (en) | 2016-01-18 | 2016-01-18 | Novel aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620043484.2U CN205469825U (en) | 2016-01-18 | 2016-01-18 | Novel aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205469825U true CN205469825U (en) | 2016-08-17 |
Family
ID=56670753
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620043484.2U Expired - Fee Related CN205469825U (en) | 2016-01-18 | 2016-01-18 | Novel aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205469825U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539848A (en) * | 2016-01-18 | 2016-05-04 | 无锡觅睿恪科技有限公司 | Novel flying pet |
| CN107176298A (en) * | 2017-05-28 | 2017-09-19 | 珠海磐磊智能科技有限公司 | Aircraft flight control method and aircraft |
-
2016
- 2016-01-18 CN CN201620043484.2U patent/CN205469825U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539848A (en) * | 2016-01-18 | 2016-05-04 | 无锡觅睿恪科技有限公司 | Novel flying pet |
| CN107176298A (en) * | 2017-05-28 | 2017-09-19 | 珠海磐磊智能科技有限公司 | Aircraft flight control method and aircraft |
| CN107176298B (en) * | 2017-05-28 | 2020-01-03 | 珠海磐磊智能科技有限公司 | Aircraft flight control method and aircraft |
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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: 20160817 Termination date: 20180118 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |