CN203417466U - Infrared induction remote control all-in-one aircraft - Google Patents
Infrared induction remote control all-in-one aircraft Download PDFInfo
- Publication number
- CN203417466U CN203417466U CN201320512462.2U CN201320512462U CN203417466U CN 203417466 U CN203417466 U CN 203417466U CN 201320512462 U CN201320512462 U CN 201320512462U CN 203417466 U CN203417466 U CN 203417466U
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- China
- Prior art keywords
- infrared induction
- rotating shaft
- infrared
- base
- remote control
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Abstract
The utility model discloses an infrared induction remote control all-in-one aircraft. The infrared induction remote control all-in-one aircraft comprises a base, a power module arranged in the base, an infrared induction assembly and a power source, wherein the power module, the infrared induction assembly and the power source are arranged in the base, two coaxial propeller assemblies are arranged above the base and connected with the power module in the base through a first rotating shaft and a second rotating shaft which are concentric and arranged together in a sleeved mode, and the rotating directions of the two propeller assemblies are opposite. The infrared induction remote control all-in-one aircraft further comprises a remote control and an integrated circuit board arranged in the base, wherein the power module, the infrared induction assembly and the power source are electrically connected the integrated circuit board, and a power source receiving switch is arranged between the integrated circuit board and the power source. According to the infrared induction remote control all-in-one aircraft, infrared induction and remote control are integrated, infrared induction flying or infrared remote control flying can be chosen automatically, and the infrared induction remote control all-in-one aircraft is convenient to operate. The infrared induction remote control all-in-one aircraft is reasonable in structural arrangement.
Description
Technical field
The utility model relates to vehicle technology field, particularly a kind of infrared induction remote-control integral aircraft.
Background technology
Aircraft is to be manufactured, can fly away from ground, in space flight, also can be controlled by people the apparatus flying object of flight by the mankind.On market, occur numerous aircraft of admiring for consumer, extensively popular, its basic principle is to adopt the rotation of screw assembly and produce lift, and aircraft is risen in the air.At present, known aircraft is divided into single purpose flying vehicle that infrared induction drives flight or infrared remote control driving flight.Due to existing aircraft function singleness, cause being difficult to realize the flight effect under various conditions, playing method is dull, and limitation is larger, is difficult to control.
Utility model content
The purpose of this utility model is for the defect of prior art and deficiency, and a kind of simple and reasonable, easy to operate infrared induction remote-control integral aircraft is provided.
For achieving the above object, the utility model is by the following technical solutions:
A kind of infrared induction remote-control integral aircraft described in the utility model, comprise base, be located at the power plant module in base, infrared induction assembly and power supply, described infrared induction assembly comprises infrared receiving tube and infrared transmitting tube A, described base top is provided with two coaxial screw assemblies, described two screw assemblies respectively by two with one heart and the first rotating shaft being mutually set-located, the second rotating shaft is connected with the power plant module in base, the direction of rotation of described two screw assemblies is contrary, also comprise remote controller and be located at the surface-mounted integrated circuit in base, described power plant module, infrared receiving tube, infrared transmitting tube A and power supply are electrically connected to described surface-mounted integrated circuit respectively, between described surface-mounted integrated circuit and described power supply, be provided with reception power switch, the battery that is provided with control chip in described remote controller and is electrically connected to control chip, between described control chip and battery, be provided with emission power switch, described remote controller is provided with the infrared transmitting tube B being electrically connected to control chip respectively, left and right turn knob, main throttle potentiometer and mode conversion switch.
Further, described power plant module comprises electric machine assembly, and by the transmission component of extremely described the first rotating shaft of transmission of power, the second rotating shaft, described electric machine assembly comprises the first motor, the second motor, described transmission component comprises the first gear train, the second gear train, wherein the first motor is by first rotating shaft that is in transmission connection of the first gear train, and the second motor is by second rotating shaft that is in transmission connection of the second gear train.
Further, described two screw assemblies comprise upper bracket, are fixed on upper fan blade, the lower carriage on upper bracket and are fixed on the lower fan blade on lower carriage, and described upper bracket fixed cover is located in the first rotating shaft, and described lower carriage fixed cover is located in the second rotating shaft.
Further, described surface-mounted integrated circuit, control chip are IC integrated chip.
Further, described power supply is battery.
The beneficial effects of the utility model are: surface-mounted integrated circuit and remote controller are set, and power plant module, infrared receiving tube, infrared transmitting tube A and power supply are electrically connected to described surface-mounted integrated circuit respectively, emission power switch, infrared transmitting tube B, left and right turn knob, main throttle potentiometer and mode conversion switch are set on remote controller, make the utility model integrate infrared induction and remote control, pass through mode conversion switch, can independently select infrared induction flight or infrared remote control flight, easy to operate, interesting enhancing.The utility model structure arranges rationally.
Accompanying drawing explanation
Fig. 1 is overall structure schematic diagram of the present utility model;
Fig. 2 is the utility model signal transmission circuit figure;
Fig. 3 is the utility model signal receiving circuit figure.
In figure:
1, base; 2, power supply; 3, infrared receiving tube; 4, infrared transmitting tube A; 5, the first rotating shaft; 6, the second rotating shaft; 7, remote controller; 8, surface-mounted integrated circuit; 9, accept power switch; 10, emission power switch; 11, infrared transmitting tube B; 12, left and right turn knob; 13, main throttle potentiometer; 14, mode conversion switch; 15, the first motor; 16, the second motor; 151, the first gear train; 161, the second gear train; 17, upper bracket; 171, upper fan blade; 18, lower carriage; 181, lower fan blade, 19, control chip; 20, battery.
The specific embodiment
Below in conjunction with accompanying drawing, the utility model is further described.
A kind of infrared induction remote-control integral aircraft as shown in Figure 1 to Figure 3, comprise base 1, be located at the power plant module in base 1, infrared induction assembly and power supply 2, described infrared induction assembly comprises infrared receiving tube 3 and infrared transmitting tube A4, described base 1 top is provided with two coaxial screw assemblies, described two screw assemblies respectively by two with one heart and the first rotating shaft 5 being mutually set-located, the second rotating shaft 6 is connected with the power plant module in base 1, the direction of rotation of described two screw assemblies is contrary, also comprise remote controller 7 and be located at the surface-mounted integrated circuit 8 in base 1, described power plant module, infrared receiving tube 3, infrared transmitting tube A4 and power supply 2 are electrically connected to described surface-mounted integrated circuit 8 respectively, between described surface-mounted integrated circuit 8 and described power supply 2, be provided with and receive power switch 9, the battery 20 that is provided with control chip 19 in described remote controller 7 and is electrically connected to control chip 19, between described control chip 19 and battery 20, be provided with emission power switch 10, described remote controller 7 is provided with the infrared transmitting tube B11 being electrically connected to control chip 19 respectively, left and right turn knob 12, main throttle potentiometer 13 and mode conversion switch 14.
The above forms agent structure of the present utility model.
Operation principle of the present utility model is: open simultaneously and receive power switch 9 and emission power switch 10, by the specific coding of infrared transmitting tube B11 transmitting 38KHZ, infrared receiving tube 3 received encoded signals, and this code signal is fed back to surface-mounted integrated circuit 8, and make the utility model automatically to code, 8 pairs of code signals of surface-mounted integrated circuit carry out PWM adjusting, and control power plant module work, and then drive two screw assemblies to rotate, and produce rising power, complete the variation of state of flight.Press mode conversion switch 14, make the utility model work in remote control distributor pattern, first promote main throttle potentiometer 13 to highest point, be pushed into again lowest part, make infrared receiving key 3 signal be detected, and then push away slowly main throttle potentiometer 13, make aircraft produce remote control distributor effect, promote left and right turn knob 12, can make the utility model left rotation and right rotation; Press mode conversion switch 14, make the utility model work in infrared induction offline mode, now the infrared transmitting tube B11 of remote controller 7 does not work, infrared transmitting tube A transmitting 38KHZ carrier wave, infrared receiving tube 3 detects after specific carrier data, and now the utility model is realized induction flight.
Described power plant module comprises electric machine assembly, and by the transmission component of extremely described the first rotating shaft 5 of transmission of power, the second rotating shaft 6, described electric machine assembly comprises the first motor 15, the second motor 16, described transmission component comprises the first gear train 151, the second gear train 161, wherein the first motor 15 is in transmission connection the first rotating shaft 5, the second motors 16 by second rotating shaft 6 that is in transmission connection of the second gear train 161 by the first gear train 151.Described two screw assemblies comprise upper bracket 17, are fixed on upper fan blade 171, the lower carriage 18 on upper bracket 17 and are fixed on the lower fan blade 181 on lower carriage 18, described upper bracket 17 fixed covers are located in the first rotating shaft 5, and described lower carriage 18 fixed covers are located in the second rotating shaft 6
By surface-mounted integrated circuit 8, controlled the switched in opposite of the first motor 15 and the second motor 16, when electric machine assembly rotates, the first motor 15 reaches the first rotating shaft 5 by the first gear train 151 by power, the second motor 16 reaches the second rotating shaft 6 by the second gear train 161 by power, now goes up fan blade 171 and lower fan blade 181 direction of rotation.The screw assembly that two groups of direction of rotation are set can not rotate base awing, and flying power is stronger, and flight effect is also better.
Described surface-mounted integrated circuit 8, control chip 19 are IC integrated chip.Described power supply 2 is battery.
The above is only better embodiment of the present utility model, and the equivalence of doing according to structure, feature and principle described in the utility model patent claim therefore all changes or modifies, and is included in the utility model patent claim.
Claims (5)
1. an infrared induction remote-control integral aircraft, comprise base (1), be located at the power plant module in base (1), infrared induction assembly and power supply (2), described infrared induction assembly comprises infrared receiving tube (3) and infrared transmitting tube A (4), described base (1) top is provided with two coaxial screw assemblies, described two screw assemblies respectively by two with one heart and the first rotating shaft (5) being mutually set-located, the second rotating shaft (6) is connected with the power plant module in base (1), the direction of rotation of described two screw assemblies is contrary, it is characterized in that: also comprise remote controller (7) and be located at the surface-mounted integrated circuit (8) in base (1), described power plant module, infrared receiving tube (3), infrared transmitting tube A (4) and power supply (2) are electrically connected to described surface-mounted integrated circuit (8) respectively, between described surface-mounted integrated circuit (8) and described power supply (2), be provided with and receive power switch (9), the battery (20) that is provided with control chip (19) in described remote controller (7) and is electrically connected to control chip (19), between described control chip (19) and battery (20), be provided with emission power switch (10), described remote controller (7) is provided with the infrared transmitting tube B (11) being electrically connected to control chip (19) respectively, left and right turn knob (12), main throttle potentiometer (13) and mode conversion switch (14).
2. infrared induction remote-control integral aircraft according to claim 1, it is characterized in that: described power plant module comprises electric machine assembly, and by extremely described the first rotating shaft (5) of transmission of power, the transmission component of the second rotating shaft (6), described electric machine assembly comprises the first motor (15), the second motor (16), described transmission component comprises the first gear train (151), the second gear train (161), wherein the first motor (15) is by the first gear train (151) the first rotating shaft (5) that is in transmission connection, the second motor (16) is by the second gear train (161) the second rotating shaft (6) that is in transmission connection.
3. infrared induction remote-control integral aircraft according to claim 1, it is characterized in that: described two screw assemblies comprise upper bracket (17), are fixed on upper fan blade (171), the lower carriage (18) on upper bracket (17) and are fixed on the lower fan blade (181) on lower carriage (18), it is upper that described upper bracket (17) fixed cover is located at the first rotating shaft (5), and described lower carriage (18) fixed cover is located in the second rotating shaft (6).
4. infrared induction remote-control integral aircraft according to claim 1, is characterized in that: described surface-mounted integrated circuit (8), control chip (19) are IC integrated chip.
5. infrared induction remote-control integral aircraft according to claim 1, is characterized in that: described power supply (2) is battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320512462.2U CN203417466U (en) | 2013-08-19 | 2013-08-19 | Infrared induction remote control all-in-one aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320512462.2U CN203417466U (en) | 2013-08-19 | 2013-08-19 | Infrared induction remote control all-in-one aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203417466U true CN203417466U (en) | 2014-02-05 |
Family
ID=50016573
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320512462.2U Expired - Fee Related CN203417466U (en) | 2013-08-19 | 2013-08-19 | Infrared induction remote control all-in-one aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203417466U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103816671A (en) * | 2014-02-26 | 2014-05-28 | 中山市泰宝电子科技有限公司 | Infrared induction toy aircraft structure and application |
| CN104784938A (en) * | 2015-04-14 | 2015-07-22 | 广东奥飞动漫文化股份有限公司 | Toy car double-mode inductive control system |
| CN105749563A (en) * | 2016-04-25 | 2016-07-13 | 电子科技大学中山学院 | Wearable model airplane wireless remote control system |
-
2013
- 2013-08-19 CN CN201320512462.2U patent/CN203417466U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103816671A (en) * | 2014-02-26 | 2014-05-28 | 中山市泰宝电子科技有限公司 | Infrared induction toy aircraft structure and application |
| CN104784938A (en) * | 2015-04-14 | 2015-07-22 | 广东奥飞动漫文化股份有限公司 | Toy car double-mode inductive control system |
| CN105749563A (en) * | 2016-04-25 | 2016-07-13 | 电子科技大学中山学院 | Wearable model airplane wireless remote control system |
| CN105749563B (en) * | 2016-04-25 | 2017-11-07 | 电子科技大学中山学院 | Wearable model airplane wireless remote control 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 |
Granted publication date: 20140205 Termination date: 20150819 |
|
| EXPY | Termination of patent right or utility model |