CN204297076U - A kind of six axle aircraft - Google Patents
A kind of six axle aircraft Download PDFInfo
- Publication number
- CN204297076U CN204297076U CN201420600595.XU CN201420600595U CN204297076U CN 204297076 U CN204297076 U CN 204297076U CN 201420600595 U CN201420600595 U CN 201420600595U CN 204297076 U CN204297076 U CN 204297076U
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- CN
- China
- Prior art keywords
- fuselage
- aircraft
- remote controller
- engine installation
- pcb board
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Abstract
The utility model relates to a kind of six axle aircraft, the remote controller comprising aircraft body and match with it, it is characterized in that, described aircraft body comprises fuselage, described fuselage upper end is connected with housing, described housing lower end is provided with alighting gear, described fuselage is provided with printed electronic circuit pcb board, described pcb board is provided with photosensor, described remote controller is provided with the luminotron matched with photosensor, described fuselage is connected with some rotors by strut bar, described rotor comprises engine installation, described engine installation is connected with blade, described pcb board is electrically connected with engine installation.The beneficial effects of the utility model are: reasonable in design, by adjusting the yaw maneuver of aircraft of the orientation enhancement of rotor, can arbitrarily angledly overturn, the flight of aircraft, rotation and stop is controlled by the adjustment of remote controller transmitted beam, need not frequent manually operated while do not affect again other operating functions of remote controller, handled easily, enhances the interest of toy.
Description
Technical field
The utility model relates to a kind of six axle aircraft.
Background technology
Along with the development of science and technology, aerobat toy more and more receives the concern of people, and this is because aerobat toy has flexibly small and exquisite, can realize Long-distance Control, workable, interesting high, and it can be good at the coordination ability of tempering toy operation person.But although current existing aerobat toy is of a great variety, there is yaw maneuver poor, structure design is single, needs remote controller frequently, the shortcomings such as operation easier is large.
Utility model content
The purpose of this utility model is to provide a kind of six axle aircraft, to overcome currently available technology above shortcomings.
The purpose of this utility model is achieved through the following technical solutions:
A kind of six axle aircraft, the remote controller comprising aircraft body and match with it, described aircraft body comprises fuselage, described fuselage upper end is connected with housing, described housing lower end is provided with alighting gear, described fuselage is provided with pcb board, described pcb board is provided with photosensor, described remote controller is provided with the luminotron matched with described photosensor, described fuselage is connected with some rotors by strut bar, described rotor comprises engine installation, described engine installation is electrically connected with pcb board, described engine installation is connected with blade, the upper cover that described engine installation comprises lower cover and is connected with described lower cover, cover under described and be provided with motor cabinet, described motor cabinet two ends are provided with lubricating cup one and lubricating cup two, described motor cabinet is provided with motor, described motor is N50 motor, described motor is connected with transmission gear, described transmission gear is connected with pipe link, described pipe link extends to outside upper cover, described pipe link is connected with blade.
Further, described strut bar is respectively equipped with the white lamp of high brightness and high brightness green light.
Further, described fuselage is provided with housing, and described housing comprises pathfinder two generation shell one and pathfinder two generation shell two.
Further, described fuselage material is the one in polyamide PA, polycarbonate, polyoxygenated polyformaldehyde POM and alloy aluminum.
Further, the material of described alighting gear and strut bar is alloy aluminum.
Further, the quantity of the engine installation of described aircraft, pipe link and blade is six.
The beneficial effects of the utility model are: reasonable in design, by adjusting the yaw maneuver of aircraft of the orientation enhancement of rotor, can arbitrarily angledly overturn, the flight of aircraft, rotation and stop is controlled by the adjustment of remote controller transmitted beam, need not frequent manually operated while do not affect again other operating functions of remote controller, handled easily, enhances the interest of toy.
Accompanying drawing explanation
Below in order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment below, apparently, accompanying drawing in the following describes is only some embodiments of the application, 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 the schematic diagram of a kind of six axle aircraft described in the utility model embodiment;
Fig. 2 is the schematic diagram of the pathfinder two generation housing one of a kind of six axle aircraft described in the utility model embodiment;
Fig. 3 is the schematic diagram of the pathfinder two generation housing two of a kind of six axle aircraft described in the utility model embodiment;
Fig. 4 is the fuselage schematic diagram of a kind of six axle aircraft described in the utility model embodiment;
Fig. 5 is the rotor structure exploded perspective view of a kind of six axle aircraft described in the utility model embodiment;
Fig. 6 is the rotor schematic diagram of a kind of six axle aircraft described in the utility model embodiment;
Horizontality schematic diagram when Fig. 7 is the one six axle aircraft flight described in the utility model embodiment;
Fig. 8 rotates 45 ° of schematic diagrams when being the one six axle aircraft flight described in the utility model embodiment;
Fig. 9 rotates 180 ° of schematic diagrams when being the one six axle aircraft flight described in the utility model embodiment.
In figure:
1, pcb board; 2, housing; 3, alighting gear; 4, strut bar; 5, motor; 6, transmission gear; 7, motor cabinet; 8, lubricating cup one; 9, lower cover; 10, upper cover; 11, pipe link; 12, blade; 13, lubricating cup two.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain, all belongs to the scope of protection of the invention.
One six axle aircraft as shown in figures 1 to 6, the remote controller comprising aircraft body and match with it, described aircraft body comprises fuselage, described fuselage material is polyamide PA, polycarbonate, one in polyoxygenated polyformaldehyde POM and alloy aluminum, described fuselage upper end is connected with housing 2, described housing 2 comprises pathfinder two generation housing one and pathfinder two generation housing two, housing can arbitrarily be changed, described housing 2 lower end is provided with alighting gear 3, described fuselage is provided with pcb board 1, described pcb board is provided with photosensor, described remote controller is provided with the luminotron matched with described photosensor, described fuselage is connected with six rotors by six strut bars 4, described strut bar 4 is separated by 60 ° and is evenly distributed in same plane, described strut bar 4 is provided with the white lamp of some high brightness and high brightness green light, described rotor is provided with engine installation, described engine installation comprises motor cabinet 7, described motor cabinet two ends are provided with lubricating cup 1 and lubricating cup 2 13, described motor cabinet 7 is provided with motor 5, described motor is N50 motor, described motor 5 is connected with transmission gear 6, described transmission gear 6 is connected with pipe link 11, described pipe link 11 extends to outside upper cover 10, described pipe link 11 is connected with blade 12, described pcb board 1 is electrically connected with engine installation.
During concrete use, one six axle aircraft as Figure 7-9, six axle aircraft are placed in smooth broad vacant lot, transmitted control signal by remote controller, described control signal is electric signal or optical signal, described optical signal is light beam, pcb board 1 reception control signal, described control signal comprises rising, decline, upset, advance, retreat, left lateral and right lateral etc., motor 5 is transferred to after pcb board 1 Received signal strength, due to the N50 motor that motor 5 is high rotating speed height torsion, it provide stronger power, enhance the speed maneuver of six axle aircraft, described motor 5 starts immediately and is with nutating gear 6 to rotate, because transmission gear 6 is connected with pipe link 11, therefore pipe link 11 also synchronously rotates, blade 12 is driven to rotate while pipe link 11 rotates, during aircraft takeoff, be positioned at fuselage front left, rear left, right side blade 12 is cw rotating forward, be positioned at fuselage front right, rear right, left side blade 12 is conter clockwise reversion, after aircraft successfully flies up, can aloft stop certain altitude position, when aircraft overturns, by remote controller, upset control signal is sent to pcb board 1, after pcb board 1 analyzing and processing, this signal is sent to motor 5, motor 5 is with nutating gear 6 to rotate, transmission gear 6 drives pipe link 11 to rotate again, aircraft can be made to enter rollover states from horizontality by the rotating speed of the rotation direction and control motor 5 that change different rotor, enhance the yaw maneuver of six axle aircraft, if aircraft is when night flying, send signal by remote controller the high brightness be positioned on aircraft support bar and high brightness green light are opened, play illuminating effect, aircraft can carry out normal flight at night.
The utility model is not limited to above-mentioned preferred forms; anyone can draw other various forms of products under enlightenment of the present utility model; no matter but any change is done in its shape or structure; every have identical with the application or akin technical scheme, all drops within protection domain of the present utility model.
Claims (5)
1. an axle aircraft, the remote controller comprising aircraft body and match with it, it is characterized in that, described aircraft body comprises fuselage, described fuselage upper end is connected with housing (2), described housing (2) lower end is provided with alighting gear (3), described fuselage is provided with printed electronic circuit pcb board (1), described pcb board (1) is provided with photosensor, described remote controller is provided with the luminotron matched with described photosensor, described fuselage is connected with six rotors by strut bar (4), described rotor comprises engine installation, described engine installation is electrically connected with pcb board (1), described engine installation is connected with blade (12), the upper cover (10) that described engine installation comprises lower cover (9) and is connected with described lower cover (9), described lower cover (9) is provided with motor cabinet (7), described motor cabinet (7) is respectively equipped with lubricating cup one (8) and lubricating cup two (13) in two ends up and down, described motor cabinet (7) is provided with motor (5), described motor (5) is N50 motor, described motor (5) is connected with transmission gear (6), described transmission gear (6) is connected with pipe link (11), described pipe link extends to upper cover (10) outward, described pipe link (11) is connected with blade (12).
2. six axle aircraft according to claim 1, is characterized in that, described strut bar (4) are respectively equipped with the white lamp of high brightness and high brightness green light.
3. six axle aircraft according to claim 2, is characterized in that, described housing (2) comprises pathfinder two generation shell one and pathfinder two generation shell two.
4. six axle aircraft according to claim 3, is characterized in that, described fuselage material is the one in polyamide PA, polycarbonate, polyoxygenated polyformaldehyde POM and alloy aluminum.
5. six axle aircraft according to claim 4, is characterized in that, the material of described alighting gear (3) and strut bar (4) is alloy aluminum.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420600595.XU CN204297076U (en) | 2014-10-16 | 2014-10-16 | A kind of six axle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420600595.XU CN204297076U (en) | 2014-10-16 | 2014-10-16 | A kind of six axle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204297076U true CN204297076U (en) | 2015-04-29 |
Family
ID=53102639
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420600595.XU Expired - Fee Related CN204297076U (en) | 2014-10-16 | 2014-10-16 | A kind of six axle aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204297076U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986341A (en) * | 2015-06-04 | 2015-10-21 | 深圳一电科技有限公司 | Aircraft side turning prevention method and device |
| CN106403958A (en) * | 2016-10-27 | 2017-02-15 | 广东容祺智能科技有限公司 | Unmanned plane aircraft intelligent course indication system |
| CN107085433A (en) * | 2016-02-16 | 2017-08-22 | 松下电器（美国）知识产权公司 | Emission control device, unmanned vehicle and light-emitting control method |
| CN110152318A (en) * | 2019-04-30 | 2019-08-23 | 汕头市鹏瑞电子科技有限公司 | A kind of brick-type construction toy telecar |
-
2014
- 2014-10-16 CN CN201420600595.XU patent/CN204297076U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986341A (en) * | 2015-06-04 | 2015-10-21 | 深圳一电科技有限公司 | Aircraft side turning prevention method and device |
| CN104986341B (en) * | 2015-06-04 | 2018-01-19 | 深圳一电航空技术有限公司 | aircraft anti-rollover method and device |
| CN107085433A (en) * | 2016-02-16 | 2017-08-22 | 松下电器（美国）知识产权公司 | Emission control device, unmanned vehicle and light-emitting control method |
| CN107085433B (en) * | 2016-02-16 | 2021-08-10 | 松下电器（美国）知识产权公司 | Light emission control device, unmanned aerial vehicle, and light emission control method |
| CN106403958A (en) * | 2016-10-27 | 2017-02-15 | 广东容祺智能科技有限公司 | Unmanned plane aircraft intelligent course indication system |
| CN106403958B (en) * | 2016-10-27 | 2019-04-02 | 广东容祺智能科技有限公司 | A kind of unmanned plane during flying device intelligence bearing indication system |
| CN110152318A (en) * | 2019-04-30 | 2019-08-23 | 汕头市鹏瑞电子科技有限公司 | A kind of brick-type construction toy telecar |
| CN110152318B (en) * | 2019-04-30 | 2020-12-25 | 广东星堡电子科技有限公司 | Toy telecar is assembled to cordwood system |
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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: 20150429 Termination date: 20161016 |