CN205418094U - Push -button aircraft - Google Patents
Push -button aircraft Download PDFInfo
- Publication number
- CN205418094U CN205418094U CN201620214582.8U CN201620214582U CN205418094U CN 205418094 U CN205418094 U CN 205418094U CN 201620214582 U CN201620214582 U CN 201620214582U CN 205418094 U CN205418094 U CN 205418094U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- rotor
- push
- definition camera
- utility
- 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
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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
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The utility model discloses a push -button aircraft, including fuselage, high definition camera, rotor, wireless communication module, singlechip and battery, the undercarriage is installed to the bottom of fuselage, and solar cell panel has been laid to the top of fuselage, the battery that solar cell panel passes through in intelligent charging and discharging module and the fuselage is connected, the output of intelligent charging and discharging module respectively with singlechip and control module's input electric connection, high definition camera and singlechip electric connection install wireless communication module on the singlechip, the both sides of fuselage are fixed with lateral part rotor mast, and the afterbody of fuselage is fixed with afterbody rotor mast, all install two rotors through the connecting piece on lateral part rotor mast and the afterbody rotor mast, and the upper and lower both ends of two same pivots of rotor installation. The utility model provides the stability of fuselage has been guaranteed simultaneously to the high flexibility and the flying speed of fuselage, avoids the vibrations of fuselage to exert an influence to the shooting.
Description
Technical field
The utility model relates to aircraft field, specifically a kind of push-button aircraft.
Background technology
(TaiWan, China is referred to as unmanned vehicle to push-button aircraft, English: UnmannedAerialVehicle, abbreviation: UAV, or UnmannedAircraftSystem, abbreviation: UAS) be commonly called as unmanned plane, unmanned airborne vehicle, referring broadly to need not various remote control or the autonomous intelligence airborne vehicle that driver's boarding is driven.This life circle, advanced person's unmanned plane was the most military, was used for scouting, observation and high-risk strike mission etc..Unmanned plane but more is for fields such as police, city management, agricultural, geology, meteorology, electric power, rescue and relief works, and my people's button aircraft very flexible the most existing, stability is the highest, the picture quality that impact is taken photo by plane.
Summary of the invention
The deficiency existed for above-mentioned prior art, the purpose of this utility model is to provide a kind of push-button aircraft.
To achieve these goals, the utility model be the technical scheme is that
nullA kind of push-button aircraft，Including fuselage、High-definition camera、Rotor、Wireless communication module、Single-chip microcomputer and battery，The bottom of described fuselage is provided with undercarriage，Fuselage overlaid with solar panel，Described solar panel is connected with the battery in fuselage by intelligent recharge and discharge module，The output of intelligent recharge and discharge module is electrically connected with the input of single-chip microcomputer and control module respectively，The bottom of the front end of described fuselage is fixed with support，High-definition camera is installed on support，Described high-definition camera is electrically connected with single-chip microcomputer，Wireless communication module is installed on single-chip microcomputer，The both sides of described fuselage are fixed with sidepiece rotor bar，The afterbody of fuselage is fixed with anti-torque rotor bar，All by connector, two rotors are installed on described sidepiece rotor bar and anti-torque rotor bar，And the two ends up and down of two rotor same rotating shafts of installation.
Further, described high-definition camera is rack-mount by rotary shaft.
Further, the rotating shaft in described connector is provided with shock-absorbing ball.
Further, the rotor below the rotor above described connector and connector is symmetrical.
Use after technique scheme, the utility model the most advantageously:
Push-button aircraft described in the utility model, by being all provided with two laterally zygomorphic rotors at the afterbody of the both sides of fuselage, improve flexibility and the flying speed of fuselage, ensure that the stability of fuselage simultaneously, the vibrations avoiding fuselage produce impact to shooting, by being arranged above solar panel at fuselage, save the energy.
Accompanying drawing explanation
With embodiment, the utility model is further illustrated below in conjunction with the accompanying drawings:
Fig. 1 is structural representation of the present utility model；
Fig. 2 is system block diagram of the present utility model.
In reference: 1-fuselage；2-undercarriage；3-high-definition camera；4-support；5-connector；6-sidepiece rotor bar；7-solar panel；8-anti-torque rotor bar；9-rotor；10-wireless communication module；11-single-chip microcomputer；12-control module；13-intelligent recharge and discharge module；14-battery.
Detailed description of the invention
The following stated is only preferred embodiment of the present utility model, the most therefore limits protection domain of the present utility model.
nullEmbodiment，As shown in Figure 1-2，A kind of push-button aircraft，Including fuselage 1、High-definition camera 3、Rotor 9、Wireless communication module 10、Single-chip microcomputer 11 and battery 14，The bottom of fuselage 1 is provided with undercarriage 2，Fuselage 1 overlaid with solar panel 7，Solar panel 7 is connected with the battery 14 in fuselage 1 by intelligent recharge and discharge module 13，The output of intelligent recharge and discharge module 13 is electrically connected with the input of single-chip microcomputer 11 and control module 12 respectively，The bottom of the front end of fuselage 1 is fixed with support 4，High-definition camera 3 is installed on support 4，High-definition camera 3 is arranged on support 4 by rotary shaft，High-definition camera 3 is electrically connected with single-chip microcomputer 11，Wireless communication module 10 is installed on single-chip microcomputer 11，The both sides of fuselage 1 are fixed with sidepiece rotor bar 6，The afterbody of fuselage 1 is fixed with anti-torque rotor bar 8，All by connector 5, two rotors 9 are installed on sidepiece rotor bar 6 and anti-torque rotor bar 8，And two rotors 9 install the two ends up and down of same rotating shaft，In rotating shaft in connector 5, shock-absorbing ball is installed.
Operation principle: during use, by respectively installing two rotors 9 in the both sides of fuselage 1 and afterbody, the flying speed making airborne vehicle is very fast, flexibility is higher simultaneously, owing to two rotors 9 are symmetrical above and below, under the effect of air-flow, it is ensured that the stability of fuselage 1, can be generated electricity by solar panel 7 simultaneously, save the energy.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and in the case of without departing substantially from spirit or essential attributes of the present utility model, it is possible to realize the utility model in other specific forms.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that all changes fallen in the implication of equivalency and scope of claim included in the utility model.Should not be considered as limiting involved claim by any reference in claim.
The above; it is only preferred embodiment of the present utility model; not in order to limit the utility model, every any trickle amendment, equivalent and improvement made above example according to technical spirit of the present utility model, within should be included in the protection domain of technical solutions of the utility model.
Claims (4)
- null1. a push-button aircraft，It is characterized in that: include fuselage (1)、High-definition camera (3)、Rotor (9)、Wireless communication module (10)、Single-chip microcomputer (11) and battery (14)，The bottom of fuselage (1) is provided with undercarriage (2)，Fuselage (1) overlaid with solar panel (7)，Solar panel (7) is connected with the battery (14) in fuselage (1) by intelligent recharge and discharge module (13)，The output of intelligent recharge and discharge module (13) is electrically connected with the input of single-chip microcomputer (11) and control module (12) respectively，The bottom of the front end of fuselage (1) is fixed with support (4)，High-definition camera (3) is installed on support (4)，High-definition camera (3) is electrically connected with single-chip microcomputer (11)，Wireless communication module (10) is installed on single-chip microcomputer (11)，The both sides of fuselage (1) are fixed with sidepiece rotor bar (6)，The afterbody of fuselage (1) is fixed with anti-torque rotor bar (8)，All by connector (5), two rotors (9) are installed on sidepiece rotor bar (6) and anti-torque rotor bar (8)，And two rotors (9) install the two ends up and down of same rotating shaft.
- A kind of push-button aircraft the most according to claim 1, it is characterised in that: described high-definition camera (3) is arranged on support (4) by rotary shaft.
- A kind of push-button aircraft the most according to claim 1, it is characterised in that: in the rotating shaft in described connector (5), shock-absorbing ball is installed.
- A kind of push-button aircraft the most according to claim 1, it is characterised in that: the rotor (9) of described connector (5) top is symmetrical with the rotor (9) of connector (5) lower section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620214582.8U CN205418094U (en) | 2016-03-18 | 2016-03-18 | Push -button aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620214582.8U CN205418094U (en) | 2016-03-18 | 2016-03-18 | Push -button aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205418094U true CN205418094U (en) | 2016-08-03 |
Family
ID=56519510
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620214582.8U Expired - Fee Related CN205418094U (en) | 2016-03-18 | 2016-03-18 | Push -button aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205418094U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081077A (en) * | 2016-08-23 | 2016-11-09 | 成都翼高九天科技有限公司 | A kind of can the shockproof flight instruments of multiple-effect of flying for long time |
| CN106275397A (en) * | 2016-08-23 | 2017-01-04 | 成都翼高九天科技有限公司 | A kind of can the minute vehicle of automatic power |
| CN114180047A (en) * | 2021-12-11 | 2022-03-15 | 迈动互联(北京)信息科技有限公司 | Smart city recognition device based on artificial intelligence and recognition method thereof |
-
2016
- 2016-03-18 CN CN201620214582.8U patent/CN205418094U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081077A (en) * | 2016-08-23 | 2016-11-09 | 成都翼高九天科技有限公司 | A kind of can the shockproof flight instruments of multiple-effect of flying for long time |
| CN106275397A (en) * | 2016-08-23 | 2017-01-04 | 成都翼高九天科技有限公司 | A kind of can the minute vehicle of automatic power |
| CN114180047A (en) * | 2021-12-11 | 2022-03-15 | 迈动互联(北京)信息科技有限公司 | Smart city recognition device based on artificial intelligence and recognition method thereof |
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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: 20160803 Termination date: 20170318 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |