CN103816671A - Infrared induction toy aircraft structure and application - Google Patents
Infrared induction toy aircraft structure and application Download PDFInfo
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- CN103816671A CN103816671A CN201410068143.6A CN201410068143A CN103816671A CN 103816671 A CN103816671 A CN 103816671A CN 201410068143 A CN201410068143 A CN 201410068143A CN 103816671 A CN103816671 A CN 103816671A
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- 230000006698 induction Effects 0.000 title claims abstract description 19
- 238000001514 detection method Methods 0.000 claims abstract description 11
- 238000000034 method Methods 0.000 claims abstract description 8
- 230000004888 barrier function Effects 0.000 claims description 26
- 208000032364 Undersensing Diseases 0.000 claims description 3
- 230000002452 interceptive effect Effects 0.000 description 9
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
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Abstract
The invention discloses an infrared induction toy aircraft structure which comprises a helicopter aircraft body. An infrared emission receiving detection mechanism used for detecting obstacles below an aircraft is arranged at the bottom of the helicopter aircraft body, the infrared emission receiving detection mechanism is provided with a plurality of emission ends and one or more corresponding receiving ends, the emission ends point to a plurality of different angles under or below the aircraft body, and a movement mechanism driving the helicopter aircraft body to ascend, descend, advance and retreat is arranged on the helicopter aircraft body. In the use process, when the obstacles exist correspondingly below the helicopter aircraft, the detection mechanism feeds back obstacle information to a master control circuit arranged in the aircraft body, and the master control circuit controls the movement mechanism to move and to carry out evasion movement in the other direction.
Description
Technical field
The present invention relates to a kind of toy aircraft, especially a kind of toy aircraft of infrared induction and application thereof.
Background technology
At present, general remote toy aircraft, be conventionally merely able to by remote controller realize aircraft front and back, move up and down, cannot by realize better interactive.
To this, in the formerly open file that the applicant is CN202128908U at notification number, a kind of infrared induction toy driven helicopter is disclosed, this toy aircraft is by infrared emission and the reception of bottom, voluntarily judgement detect and realize lifting, this aircraft is interactive better, firmly gets child's welcome.
But this product can only be realized again upper and lower lifting conversely, cannot realize as telecontrolled aircraft front and back drive.
Summary of the invention
In order to solve the above problems, the object of the present invention is to provide a kind of result of use good, interactive stronger infrared induction toy aircraft structure and application thereof.
The present invention solves the technical scheme that its problem adopts:
A kind of toy aircraft structure of infrared induction, comprise driven helicopter main body, the bottom of driven helicopter main body is provided with for detection of the infrared emission of aircraft below barrier and receives testing agency, infrared emission receives testing agency multiple transmitting terminals and one or above corresponding receiving terminal, transmitting terminal points to multiple different angles of aircraft body below and oblique below, in driven helicopter main body, be provided with and drive its lifting, the motion moving forward and backward, when use, when there is barrier the corresponding oblique below of driven helicopter, testing agency feeds back to obstacle information the governor circuit being built in aircraft body, by governor circuit controlled motion mechanism action, hide motion to other direction.
Further, described receiving terminal is one, is the common receiving terminal of all transmitting terminals, sends signal and runs into the signal that barrier reflects for receiving transmitting terminal, simple and reasonable, with low cost.Preferably, described receiving terminal is one, for the common receiving terminal of all transmitting terminals, each transmitting terminal is according to the time interval circulation transmitting infrared signal of setting, the infrared signal that receiving terminal received in the corresponding time period, be judged as the reflected signal of this direction transmitting terminal, supply with governor circuit and use.
Further, described transmitting terminal has five, under one of them points to, other four become 90 degree between adjacent, and point to respectively the oblique below of aircraft body, the signal of the transmitting terminal under sensing, for detection of height, refers to signal oliquely downward, can substantially cover oblique below and the side surrounding position thereof of aircraft body.
Further, refer to have on transmitting terminal oliquely downward make the gathering sill that points to separately, receiving terminal is arranged in a sleeve, to avoid interference each other.
Further, receiving terminal is arranged on the middle position between multiple transmitting terminals, compact conformation, reasonable.
A kind of toy aircraft control method of the toy aircraft structure that is applied to described infrared induction, in driven helicopter running, in the time running into barrier, the motion of driven helicopter moves to another one direction, when user using hand or grip thing as barrier, near the oblique below of driven helicopter, the infrared signal reflection that the corresponding transmitting terminal of the infrared emission reception testing agency of driven helicopter sends, after being received by receiving terminal, and through governor circuit processing, by governor circuit controlled motion mechanism action, hide motion to other direction.In addition, for the signal under pointing to, in driven helicopter running, below not detecting, ground or barrier in the situation that, lifting force declines, aircraft is descending, in the time ground or barrier being detected, represent to have dropped to certain height, motion acts accordingly, raise, so basic circulation.Therefore, hide and the functions such as lifting by left and right, can realize interactive better, for example, when the small volume of this aircraft, can be by player's hand as barrier, drive action, can make aircraft in player's left and right, front, front and back, tiltedly on, tiltedly under, the flight of lifting etc., interactive splendid.
Apply a toy aircraft for the toy aircraft structure of described infrared induction, driven helicopter has upper strata blade motor, lower floor's blade motor and tail motor, and infrared emission reception testing agency is arranged on the bottom of aircraft body.
Apply a toy aircraft for described control method, driven helicopter has upper strata blade motor, lower floor's blade motor and tail motor and is arranged on the bottom of aircraft body.
The invention has the beneficial effects as follows: the infrared signal transmitting terminal that is provided with the multiple different angles of corresponding aircraft body below tiltedly in the bottom of driven helicopter, can detect barrier and the height of diverse location, by the governor circuit of aircraft, realize all around of aircraft, tiltedly upper, tiltedly under, the motion of lifting, interactive splendid.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described.
Fig. 1 is the embodiment stereogram one of aircraft of the present invention;
Fig. 2 is the embodiment stereogram two of aircraft of the present invention;
Fig. 3 is the reference view one that infrared emission of the present invention receives testing agency;
Fig. 4 is the reference view two that infrared emission of the present invention receives testing agency;
Fig. 5 is the reference view three that infrared emission of the present invention receives testing agency;
Fig. 6 is the reference view four that infrared emission of the present invention receives testing agency;
Fig. 7 is the physical circuit figure of aircraft embodiment governor circuit of the present invention;
The manipulation reference view that Fig. 8,9,10 is aircraft of the present invention.
The specific embodiment
With reference to Fig. 1-Fig. 6, the toy aircraft structure of a kind of infrared induction of the present invention, comprise driven helicopter main body 1, the bottom of driven helicopter main body 1 is provided with for detection of the infrared emission of aircraft below barrier and receives testing agency 2, infrared emission receives testing agency 2 multiple transmitting terminals (22, 23) and one or above corresponding receiving terminal 20, wherein, there is transmitting terminal 22 to point to tiltedly multiple different angles of below (barrier for detection of side and tiltedly) of aircraft body 1, there is transmitting terminal 23 to point to the below (for detection of height) of main body, in driven helicopter main body 1, be provided with and drive its lifting, the motion 3 moving forward and backward, when use, when there is barrier the corresponding oblique below of driven helicopter, testing agency feeds back to obstacle information the governor circuit being built in aircraft body, by governor circuit controlled motion mechanism action, hide motion to other direction, in the time that below drops to certain altitude, under again receiving when signal, again move upward.
Preferably, described receiving terminal 20 is one, is the common receiving terminal of all transmitting terminals 22,23, sends signal and runs into signal that barrier reflects and the altitude signal of transmitting terminal 23 for receiving transmitting terminal 22, simple and reasonable, with low cost.
Further, each transmitting terminal 22,23 is according to the time interval circulation transmitting infrared signal of setting, and receiving terminal 20, in the infrared signal that the corresponding time period receives, is judged as the reflected signal of this direction transmitting terminal, supply governor circuit uses, and is the detection method of polling type.
With reference to figure 3,4,5,6, as an embodiment, described finger transmitting terminal 22 oliquely downward has four, between adjacent, become 90 degree, and point to respectively the oblique below of aircraft body 1, oblique below and the side surrounding position thereof that can substantially cover aircraft body 1, the transmitting terminal 23 under sensing is one.On transmitting terminal 22, have and make the gathering sill 220 that points to separately, receiving terminal 20 is arranged in a sleeve 200, to avoid interference each other.This transmitting terminal 22 can be arranged on same pedestal with receiving terminal, also can be arranged on respectively on the diverse location of aircraft body 1.Preferably, receiving terminal is arranged on the middle position between multiple transmitting terminals 22, compact conformation, reasonable.
Toy aircraft control method of the present invention, be applied to the toy aircraft structure of described infrared induction, driven helicopter is in running, in the time running into barrier, the motion of driven helicopter moves to another one direction, when user using hand or grip thing as barrier, near the below of driven helicopter or tiltedly, the infrared signal reflection that the corresponding transmitting terminal of the infrared emission reception testing agency of driven helicopter sends, after being received by receiving terminal, and through governor circuit processing, by governor circuit controlled motion mechanism action, hide motion to other direction.Preferably, in driven helicopter running, in the situation that barrier not detected and below not detecting when the bottom surface in certain altitude or barrier, lifting force declines, aircraft is descending, when detecting that apart from ground, below or below barrier, lower than certain altitude, motion acts accordingly, raise, so basic circulation.The motor pattern that aircraft is hidden in conjunction with lifting, left-right and front-back is interactive good.
Further, this toy aircraft, has upper strata blade motor, lower floor's blade motor and tail motor, and infrared emission reception testing agency is arranged on the bottom of aircraft body.
In addition, with reference to Fig. 7, take the circuit of the toy helicopter that adopted in the present invention as embodiment, illustrate its governor circuit, this governor circuit comprises power supply and mu balanced circuit, circuit for controlling motor, infrared receiving circuit, infrared emission signal processing circuit, signal processing and Electric Machine Control treatment circuit and gyroscope circuit.The parts of transmitting terminal are in infrared emission signal processing circuit, and the parts of receiving terminal get final product in infrared receiving circuit, narrate no longer one by one at this.
With reference to figure 8-10, aircraft of the present invention can be as shown in the figure, when as Fig. 9, barrier is detected in its aircraft front lower place, pass through motion, motion backward, as Figure 10, when detecting, skew back below moves barrier to opposite side, can realize interactive better, for example, when the small volume of this aircraft, can, by player's hand as barrier, drive action, can make aircraft in player's left and right, front, front and back, tiltedly on, oblique upper and lower liter, decline and fly, interactive splendid.
Certainly, the invention is not limited to above-mentioned embodiment, as long as it reaches technique effect of the present invention with essentially identical means, all should belong to protection scope of the present invention.
Claims (10)
1. the toy aircraft structure of an infrared induction, it is characterized in that: comprise driven helicopter main body, the bottom of driven helicopter main body is provided with for detection of the infrared emission of aircraft below barrier and receives testing agency, infrared emission receives testing agency multiple transmitting terminals and one or above corresponding receiving terminal, transmitting terminal points to multiple different angles of aircraft body below and oblique below, in aircraft body, be provided with and drive its lifting, the motion moving forward and backward, when use, when there is barrier the corresponding oblique below of aircraft, testing agency feeds back to obstacle information the governor circuit being built in aircraft body, by governor circuit controlled motion mechanism action, hide motion to other direction.
2. the toy aircraft structure of a kind of infrared induction according to claim 1, is characterized in that: described receiving terminal is one, is the common receiving terminal of all transmitting terminals, sends for receiving transmitting terminal the signal that signal reflects.
3. the toy aircraft structure of a kind of infrared induction according to claim 2, it is characterized in that: described receiving terminal is one, for the common receiving terminal of all transmitting terminals, each transmitting terminal is according to the time interval circulation transmitting infrared signal of setting, the infrared signal that receiving terminal received in the corresponding time period, be judged as the reflected signal of this direction transmitting terminal, supply with governor circuit and use.
4. the toy aircraft structure of a kind of infrared induction according to claim 1, is characterized in that: described transmitting terminal has five, and under one of them points to, other four become 90 degree between adjacent, and point to respectively the oblique below of aircraft body.
5. the toy aircraft structure of a kind of infrared induction according to claim 1, is characterized in that: refer to have on transmitting terminal oliquely downward make the gathering sill that points to separately, receiving terminal is arranged in a sleeve.
6. according to the toy aircraft structure of a kind of infrared induction described in claim 1,2,3,4 or 5, it is characterized in that: receiving terminal is arranged on the middle position between multiple transmitting terminals.
7. one kind is applied to the toy aircraft control method of the toy aircraft structure of the arbitrary described infrared induction of claim 1-6, it is characterized in that: in driven helicopter running, in the time running into barrier, the motion of driven helicopter moves to another one direction, when user using hand or grip thing as barrier, near the oblique below of driven helicopter, the infrared signal reflection that the corresponding transmitting terminal of the infrared emission reception testing agency of driven helicopter sends, after being received by receiving terminal, and through governor circuit processing, by governor circuit controlled motion mechanism action, hide motion to other direction, the signal of the transmitting terminal under sensing is for detection of the height of aircraft.
8. toy aircraft control method according to claim 7, it is characterized in that: in driven helicopter running, when aircraft falls higher than certain altitude, under the signal of transmitting terminal under not detecting, lifting force declines, aircraft is descending, in the time barrier being detected, motion acts accordingly, and raises, so basic circulation.
9. the toy aircraft of the toy aircraft structure of the arbitrary described infrared induction of application rights requirement 1-6, it is characterized in that: driven helicopter has upper strata blade motor, lower floor's blade motor and tail motor, infrared emission reception testing agency is arranged on the bottom of driven helicopter main body.
10. application rights requires a toy aircraft for control method described in 7 or 8, it is characterized in that: driven helicopter has upper strata blade motor, lower floor's blade motor and tail motor and be arranged on the bottom of driven helicopter main body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410068143.6A CN103816671B (en) | 2014-02-26 | 2014-02-26 | The toy aircraft structure of infrared induction and application |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410068143.6A CN103816671B (en) | 2014-02-26 | 2014-02-26 | The toy aircraft structure of infrared induction and application |
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| Publication Number | Publication Date |
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| CN103816671A true CN103816671A (en) | 2014-05-28 |
| CN103816671B CN103816671B (en) | 2017-03-29 |
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| CN201410068143.6A Active CN103816671B (en) | 2014-02-26 | 2014-02-26 | The toy aircraft structure of infrared induction and application |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104056456A (en) * | 2014-06-11 | 2014-09-24 | 赵旭 | Infrared ray sensing toy aircraft structure and application of infrared ray sensing toy aircraft structure |
| CN104645626A (en) * | 2014-12-01 | 2015-05-27 | 赵旭 | Infrared gesture-sensing toy structure and application thereof |
| CN109592024A (en) * | 2016-07-05 | 2019-04-09 | 金福珍 | A kind of Intelligent unattended machine |
| CN111679691A (en) * | 2020-07-16 | 2020-09-18 | 深圳市澳玛禾经贸有限公司 | Obstacle avoidance control system and method for aircraft and aircraft |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104056456A (en) * | 2014-06-11 | 2014-09-24 | 赵旭 | Infrared ray sensing toy aircraft structure and application of infrared ray sensing toy aircraft structure |
| CN104645626A (en) * | 2014-12-01 | 2015-05-27 | 赵旭 | Infrared gesture-sensing toy structure and application thereof |
| CN104645626B (en) * | 2014-12-01 | 2017-12-29 | 赵旭 | A kind of infrared gesture induction formula toy structure and its application |
| CN109592024A (en) * | 2016-07-05 | 2019-04-09 | 金福珍 | A kind of Intelligent unattended machine |
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| CN111679691A (en) * | 2020-07-16 | 2020-09-18 | 深圳市澳玛禾经贸有限公司 | Obstacle avoidance control system and method for aircraft and aircraft |
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|---|---|
| CN103816671B (en) | 2017-03-29 |
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Effective date of registration: 20180201 Address after: 528400 the first to four floors of changguan Road, 48, West District, Zhongshan, Guangdong Patentee after: ZHONGSHAN LUCKEY ELECTRONIC TECHNOLOGY Co.,Ltd. Address before: 528400 Zhongshan Province, West Palm Rainbow Building 602, room 4, 3 Patentee before: Zhongshan Taibao Electronics Co.,Ltd. |
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Effective date of registration: 20240608 Address after: 518101, Building 219, Ningchang Building, Xin2, Xicheng Industrial Zone, Longteng Community, Xixiang Street, Bao'an District, Shenzhen City, Guangdong Province Patentee after: Shenzhen Zongheng Core Technology Co.,Ltd. Country or region after: China Address before: 528400, 1st to 4th floors, No. 48 Changguan Road, West District, Zhongshan City, Guangdong Province Patentee before: ZHONGSHAN LUCKEY ELECTRONIC TECHNOLOGY Co.,Ltd. Country or region before: China |