CN102886148A - Toy aircraft capable of stopping in air - Google Patents
Toy aircraft capable of stopping in air Download PDFInfo
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- CN102886148A CN102886148A CN2012104111381A CN201210411138A CN102886148A CN 102886148 A CN102886148 A CN 102886148A CN 2012104111381 A CN2012104111381 A CN 2012104111381A CN 201210411138 A CN201210411138 A CN 201210411138A CN 102886148 A CN102886148 A CN 102886148A
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Abstract
The invention provides a toy aircraft capable of stopping in air. The toy aircraft comprises a remote controller and an aircraft, wherein the remote controller comprises an operation mechanism and a transmission circuit, wherein the aircraft comprises a remote control receiving circuit and a control circuit, and the remote controller is provided with a light emitting tube used for emitting a conical light beam capable of covering and irradiating a body of the aircraft; the control circuit of the aircraft identifies the up and down movement of the aircraft in the conical light beam according to the input signals of photosensitive elements at different positions of the body of the aircraft so as to adjust output control signals and control the lifting of the aircraft. According to the toy aircraft, the aircraft is captured and stops in air by utilizing the light beam, so that the use is intuitive and easy, and the remote control interestingness of the toy is improved.
Description
Technical field
The present invention relates to a kind of toy, be specially a kind of remote control electric aircraft.
Background technology
Electronic class aerobat toy such as helicopter, flying saucer, the flight balls etc. of going straight up to comprise remote controller and aircraft, adopt radio or infra-red remote control.Wherein remote controller comprises operation push-button or action bars, coding circuit and radiating circuit, and operator's both hands operate at remote controller, forms coded message by coding circuit and launches by radiating circuit.The control circuit of aircraft comprises receiving circuit, decoding circuit, drive circuit and execution unit.Receiving circuit receives remote controller and transmits, decoding draws remote information through decoding circuit, by drive circuit control execution unit, make aircraft finish exercises, as rising, decline, left/right rotation to, advance, retreat (or halting), unsettled etc.
Vacant state wherein, it is the important relatively difficulty that also realizes, existing toy aircraft, if in the middle of the process of straighforward operation, make aircraft unsettled rest on aerial, mostly need ceaselessly rising and the decline button (or action bars) of remote controller, trimming movement by continuous rising and decline makes aircraft be in the state of dynamic equilibrium, realize aircraft relatively unsettled stop aloft, this operation is very hard, difficulty is very large, for the less children of age, is difficult to realize.Some aircraft improves, and makes the main screw of aircraft with certain rotating speed (can be described as unsettled rotating speed) work when vacant state, and the lift that screw produces just equals the weight of aircraft, makes aircraft keep unsettled aloft.But in actual the use, because operating voltage changes and the impact of various factors, be difficult to the stable of hold mode, and, from physical theory, even the lift that screw produces just equals the weight of aircraft, also just make aircraft keep original motion state, occur rising or descending if aircraft is subject to the impact of air-flow, then at this moment aircraft can become at the uniform velocity rising or descend, and can't keep the static unsettled of aircraft.
Summary of the invention
The present invention seeks to purpose is to disclose a kind of remote control electric aircraft that can unsettledly rest in the air, particularly can unsettledly rest on aerial ad-hoc location.
The present invention includes remote controller and aircraft, remote controller can be the various remote controllers of prior art, include remote-control gear and remote controlled transmitting circuit, aircraft includes with the remote-control receiving circuit of remote controller cooperating, remote control circuit and is used for driving the lifting executing agency that aircraft is done lifting action, it is characterized in that: also be provided with luminous tube at remote controller, be used for launching and a branch ofly can cover the cone-shaped beam that shines aircraft fuselage; Up and down diverse location at the above-below direction of aircraft fuselage is provided with two light-sensitive elements that are used for receiving cone-shaped beam at least; Light-sensitive element is connected to the input of unsettled control circuit, and the output of unsettled control circuit is connected to lifting executing agency; Unsettled control circuit is used for according to the up and down variation of the input signal of the light-sensitive element of diverse location, identify the change in location that aircraft moves up and down in cone-shaped beam, and adjust the output control signal according to change in location, control aircraft by lifting executing agency and do lifting action.
The cone-shaped beam of remote controller emission can adopt the luminous tube electrified light emitting to produce optically focused through concentration structure again and form, and this belongs to electrooptics aspect common technology, such as common LED flashlight.
The cone-shaped beam of remote controller emission can be visible light beam or infrared beam, perhaps comprises simultaneously both beam combinations.Its operation principle is the same, different just luminous tubes, and supporting light-sensitive element on the aircraft.In fact a lot of light-sensitive elements can be suitable for visible light and infrared ray simultaneously, and just the filter of light-sensitive element front is different.Adopt visible light beam can see light beam, operation control is more directly perceived and easier, is fit to children's use that various crowds comprise little age; Use the infrared beam interference free performance better, but cannot see light beam, have some difficulty, if but the operator understands infrared ray also is straightline propagation, just can hold with angle the range of exposures of cone-shaped beam, can realize equally.When illumination beam adopts visible light beam, interference for fear of ambient light, light beam should not adopt white light, adopt the light beam of ruddiness or green glow or blue light or purple light first-selectedly, to improve anti-interference, correspondingly be added with redness or optical filter green or blue or purple in the light-sensitive element front of aircraft.Also can launch infrared beam and realize controlling function, adopt infrared optical sensor to receive on the aircraft, launch simultaneously visible light beam and come the location for the operator, and both optically focused are become with a branch of cone-shaped beam together, reach again easy-operating advantage directly perceived of existing anti-interference.
How to identify aircraft for unsettled control circuit and move up and down and adjust the output control signal in cone-shaped beam, the present invention discloses following two kinds of technical schemes:
The first scheme is: unsettled control circuit at the light-sensitive element of the diverse location of aircraft above-below direction simultaneously by the prerequisite that cone-shaped beam shone under, the different conditions that breaks away from the cone-shaped beam irradiation according to the light-sensitive element of diverse location up and down, identify the change in location that aircraft moves up and down in cone-shaped beam, and adjust the output control signal with this, control aircraft by lifting executing agency and carry out lifting action.
First scheme is: unsettled control circuit at the light-sensitive element of the diverse location of aircraft above-below direction simultaneously by the prerequisite that cone-shaped beam shone under, different conditions and precedence according to the up and down light-sensitive element disengaging cone-shaped beam irradiation of diverse location, identify change in location and pace of change that aircraft moves up and down in cone-shaped beam, and adjust the output control signal with this, carry out lifting action by lifting actuating mechanism controls aircraft with friction speed.
Toy aircraft of the present invention can be in conjunction with various remote controls and the control technology of existing remotely-piloted vehicle, aircraft is risen, descends, turns to, advances, retreats other remote control controls of (or halting) with existing techniques in realizing, and realize making the unsettled aerial specific region (also being the zone of irradiation that cone-shaped beam is covered) that rests on of aircraft with technology of the present invention.Carrying out the aircraft rising, descend, advance, retreat, when other remote controls such as turning to, unsettled control circuit does not start work, do not affect other straighforward operations, and when needs make aircraft unsettled, the cone-shaped beam of remote controller emission is shone on the aircraft fuselage, the unsettled control circuit of aircraft will be according to the variation of the input signal of light-sensitive element on the fuselage diverse location, identify the change in location that aircraft moves up and down in cone-shaped beam, because rising or descend, certain factor detaches the shadow surface of cone-shaped beam when aircraft, when namely producing change in location, unsettled control circuit will be according to this change in location adjustment output control signal, control aircraft by lifting executing agency and do the reverse adjustment action that descends or rise, thereby make aircraft all the time by in the unsettled ad-hoc location that rests on the cone-shaped beam shadow surface of control.
The advantage that the present invention has is: 1, the operator need not the frequent manual operation by button or the action bars of remote controller, but adopts a branch of light beam to control aircraft, can control easily just that aircraft is unsettled to be rested in the air, uses not only intuitively but also easy.2, can control the height of the unsettled stop of aircraft by adjusting up and down the cone-shaped beam of remote controller emission, cone-shaped beam is pointed to where aircraft just rests on the there, not only convenient but also to increase the remote control of toy interesting.3, do not affect original straighforward operation.
Description of drawingsFig. 1 is operation principle schematic diagram of the present invention.Fig. 2 is that light-sensitive element is arranged on carry-on schematic diagram.Fig. 3 is the circuit diagram of a kind of circuit of aircraft of the present invention.
The specific embodimentThe below to how implementing the present invention describes with reference to the accompanying drawings.
Need to prove, the object of the invention is to disclose a kind of dependence cone-shaped beam and control the skyborne technology of the unsettled stop of aircraft, relevant remote control and execution technique for aircraft, as adopt infrared remote control or wireless remotecontrol realize aircraft rising, descend, advance, retreat, left/right rotation to action, belong to existing toy remote control technology.For realizing correlation technique of the present invention, such as the lifting executing agency of aircraft, cooperate main screw to drive aircraft by motor and carry out rising and down maneuver, also belong to existing toy technique.The unsettled control circuit of aircraft of the present invention, it both can be an independent circuits, also can combine with the remote control circuit of the original telecontrol engineering of aircraft, and, control circuit is except receiving, identify, judge and control the part of output to signal, general also including carried out power amplification for use in the drive circuit that drives executing agency's action to the output control signal, and this also belongs to the general knowledge of prior art.Some basic functions of circuit involved in the present invention, comprise the reception of light and detection, to modulus (A/D) conversion of voltage signal and computing relatively, by adjusting operating voltage or PWM pulsewidth modulation the adjustment of machine operation power and rotating speed is controlled, comprise how adopting single-chip microprocessor MCU or microprocessor or other circuit modes according to operation principle of the present invention and logic is designed concrete unsettled control circuit and program is carried out work, the common technology that yet belongs to electronic technology field and toy remote control does not do being described in detail here.Single-chip microprocessor MCU 1 in the accompanying drawing of the embodiment of the invention does not have any specific (special) requirements, can adopt various general MCU models.And for simplicity, the circuit diagram of the application's accompanying drawing only draws with the relevant element of operation principle, other circuit parts such as power supply, filtering, clock, reset, anti-interference, the interlock circuits such as the power amplification of output and driving belong to general knowledge, also do not draw.
Fig. 1 is operation principle schematic diagram of the present invention.The present invention includes remote controller 1 and aircraft 2, remote controller 1 can be to adopt the various remote controllers of existing telecontrol engineering to be the basis, include remote-control gear (such as button or action bars) and remote controlled transmitting circuit, adopt infrared ray or radio remote control technology, aircraft 2 include with the remote-control receiving circuit of remote controller cooperating, remote control circuit and be used for driving aircraft do lifting, advance and retreat or left/right rotation to etc. the various executing agencies of remote control actions, this is prior art.
The present invention also is provided with luminous tube on remote controller 1, be used for launching a branch of light beam 3 that can shine on aircraft 2 fuselages.Light beam 3 is a branch of cone-shaped beams that present the low-angle diffusion.(cone-shaped beam is sometimes also referred to as light beam in the present specification).In use, cone-shaped beam 3 is faced toward aircraft 2, the shadow surface of cone-shaped beam, (also being hot spot) can all shine a face of right aircraft 2 fuselages, namely covers irradiation.Cone-shaped beam can adopt power drives luminous tube such as the luminous again process of LED concentration structure to carry out optically focused and form cone-shaped beam, (some LED luminous tube itself is just with concentration structure), belong to electrooptical technology commonly used, can adopt or the various compact LED flashlights with optically focused of reference.The angle of departure of cone-shaped beam, too small meeting make the shadow surface of cone-shaped beam too small, are difficult to aircraft is covered irradiation; The excessive shadow surface of cone-shaped beam that can make again is excessive, and brightness is too small and command range is diminished, and causes the up and down fluctuation range of aircraft in cone-shaped beam excessive; Only, be to make the shadow surface of cone-shaped beam equal or be slightly larger than the fuselage of aircraft at remote control distance; Usually, the transmission angle is comparatively suitable at several years to tens degree.
Up and down diverse location at the above-below direction of the fuselage 4 of aircraft 2 is provided with two light-sensitive elements that are used for receiving cone-shaped beam at least, such as two light-sensitive element G1 and the G2 of Fig. 2.Light-sensitive element generally is installed in the side of aircraft fuselage, on trailing flank, so that work is easily shone by cone-shaped beam the time.The light-sensitive element front generally also is added with the optical filter that matches with cone-shaped beam, is red visible light such as cone-shaped beam, just cooperates Red lightscreening plate, (some light-sensitive element self is with optical filter).
Realize a kind of aircraft circuit of the present invention such as Fig. 3, light-sensitive element G1, G2 respectively series resistance R1, R2 consist of 2 road light beam receiving circuits, unsettled control circuit mainly is made of single-chip microprocessor MCU 1 grade, (MCU1 also can utilize the single-chip microcomputer of original remote control circuit), the output of light-sensitive element G1 and G2 is connected to input IO1 and the IO2 of unsettled control circuit, and the output of unsettled control circuit is connected to lifting executing agency.In the time will making aircraft unsettled, the operator aims at aircraft with the cone-shaped beam of remote controller luminous tube emission, the shadow surface that also is about to cone-shaped beam covers the light-sensitive element that shines on the aircraft fuselage, (can be described as aircraft is caught), because occurring rising or descending, various factors detaches the shadow surface of cone-shaped beam when aircraft, when namely producing change in location, can produce different variations at the light-sensitive element G1 of above-below direction diverse location and the input signal of G2, unsettled control circuit is according to the variation of the input signal of G1 and G2, identify the situation of the change in location that aircraft moves up and down in cone-shaped beam, and adjust the output control signal according to the situation of this change in location, control aircraft by lifting executing agency and do the reverse adjustment action that descends or rise, aircraft is captured all the time is controlled in the shadow surface of cone-shaped beam, realize making the unsettled purpose that rests on cone-shaped beam indication ad-hoc location of aircraft.
How to identify aircraft for unsettled control circuit and move up and down and adjust the output control signal in cone-shaped beam, the present invention discloses following two kinds of technical schemes.
The first scheme is: unsettled control circuit at the light-sensitive element of the diverse location of aircraft above-below direction simultaneously by the prerequisite that cone-shaped beam shone under, the different conditions that breaks away from the cone-shaped beam irradiation according to the light-sensitive element of diverse location up and down, identify the change in location (also being the different conditions that the position changes) that aircraft moves up and down in cone-shaped beam, and adjust the output control signal with this, control aircraft by lifting executing agency and carry out lifting action.Concrete operation principle and control procedure are: 1, when there not being cone-shaped beam to shine on the aircraft fuselage, G1 and G2 are not shone by light beam entirely, the dark resistance of G1 and G2 is very large, at this moment the input IO1 of single-chip microprocessor MCU 1 and IO2 input low level signal simultaneously, (also namely be lower than threshold level, threshold level is greater than the level of IO1 and IO2 input under the naturally light, can obtain by adjusting R1 and R2, also can arrange at MCU1), at this moment not output of unsettled control circuit, aircraft keeps original motion state, does not also affect other straighforward operations.2, when covering cone-shaped beam, the operator shines on the aircraft fuselage, G1 and G2 are simultaneously by irradiation that light beam covers, the light resistance of G1 and G2 is very little, at this moment the input IO1 of single-chip microprocessor MCU 1 and IO2 input high level signal simultaneously, the identification control function on work of unsettled control circuit, the main screw of the output control signal control lifting executing agency of unsettled control circuit rotates with certain rotating speed (also being unsettled rotating speed), and the lift that screw is produced probably equals the gravity of aircraft.This state can be described as trap state.But trap state is also unstable, and unsettled rotating speed can not guarantee really unsettled resting in the air of aircraft, and various factors all may make aircraft occur rising or descending such as the inertia motion of voltage pulsation, interference in air flow or aircraft self.3, such as, certain factor has caused aircraft to rise and has departed from gradually the shadow surface of cone-shaped beam, when the light-sensitive element G1 of the top of aircraft fuselage above-below direction breaks away from the cone-shaped beam shadow surface, at this moment light-sensitive element G1 breaks away from illumination and G2 also is subject to illumination, IO1 input becomes first low level and the IO2 input still is high level, at this moment the output control signal of unsettled control circuit will be turned down the rotating speed of the main screw of (perhaps turning off) lifting executing agency, aircraft is descended, until aircraft comes back to the shadow surface the inside of cone-shaped beam, G1 is shone by light beam again, and the output control signal of unsettled control circuit is controlled the rotating speed that trap state is got back to by lifting executing agency again.4, the shadow surface that has departed from gradually cone-shaped beam if certain factor has caused aircraft to descend, when the light-sensitive element G2 of the bottom of aircraft fuselage above-below direction breaks away from the cone-shaped beam shadow surface, at this moment light-sensitive element G2 breaks away from illumination and G1 also is subject to illumination, IO2 input becomes first low level and the IO1 input still is high level, at this moment the output control signal of unsettled control circuit will be heightened the rotating speed of the main screw of (perhaps transferring to full power operation) lifting executing agency, aircraft is risen, until aircraft comes back to the shadow surface the inside of cone-shaped beam, G2 is shone by light beam again, and the output control signal of unsettled control circuit is controlled the rotating speed that trap state is got back to by lifting executing agency again.
First scheme is the further optimization of the first scheme: unsettled control circuit at the light-sensitive element of the diverse location of aircraft above-below direction simultaneously by the prerequisite that cone-shaped beam shone under, different conditions and precedence according to the up and down light-sensitive element disengaging cone-shaped beam irradiation of diverse location, identify change in location and pace of change that aircraft moves up and down in cone-shaped beam, and adjust the output control signal with this, carry out lifting action by lifting actuating mechanism controls aircraft with friction speed.State the first scheme part in front of its operation principle and the control procedure similar, the 1st kind of situation wherein, do not have namely that cone-shaped beam shines on the aircraft fuselage, G1 and G2 be by situation that light beam shone entirely, with the 2nd kind of situation, be cone-shaped beam cover shine on the aircraft fuselage, G1 and G2 be simultaneously by the situation of irradiation that light beam covers, the work of unsettled control circuit is described the same with the first scheme under the both of these case.Just the rising or descend and during disengaging cone-shaped beam shadow surface when aircraft of difference, the identification of unsettled control circuit is different with control, be specially: 5, in aforementioned the 3rd kind of situation, namely when aircraft rises so that light-sensitive element G1 has just broken away from illumination that G2 also is subject to illumination, the output control signal of unsettled control circuit will be turned down with less amplitude the rotating speed of the main screw of lifting executing agency, aircraft is slowly descended, slowly get back to cone-shaped beam shadow surface the inside; If G2 also and then broke away from illumination after G1 broke away from illumination in this case, also be that the IO2 input also and then became low level after the input of IO1 became first low level, illustrate that the aircraft rate of climb is very fast, then the output control signal of unsettled control circuit will be turned down with larger amplitude the rotating speed of the main screw of (perhaps turning off) lifting executing agency, make the aircraft fast-descending, get back to quickly cone-shaped beam shadow surface the inside.6, in aforementioned the 4th kind of situation, namely descend and make light-sensitive element G2 just break away from illumination and G1 when also being subject to illumination when aircraft, the output control signal of unsettled control circuit will be heightened with less amplitude the rotating speed of the main screw of lifting executing agency, make the aircraft climbed, slowly get back to cone-shaped beam shadow surface the inside; If G1 also and then broke away from illumination after G2 broke away from illumination in this case, also be that the IO1 input also and then became low level after the input of IO2 became first low level, illustrate that the aircraft decrease speed is very fast, then the output control signal of unsettled control circuit will be heightened with larger amplitude the rotating speed of the main screw of (perhaps directly heightening to full power operation) lifting executing agency, make the aircraft fast rise, get back to quickly cone-shaped beam shadow surface the inside.This scheme can make the adjustment of aircraft more timely and effective, thereby makes the up and down fluctuation of aircraft less.
To sum up state, aircraft of the present invention is under trap state, even owing to various factors causes rising or descending, also always fluctuate up and down round the shadow surface of cone-shaped beam, rest on the ad-hoc location at cone-shaped beam shadow surface place, similarly be to be caught in the light beam the inside by cone-shaped beam, realize the object of the invention.
The embodiment of Fig. 2 and Fig. 3, diverse location at the above-below direction of same side, to carry out work with two light-sensitive elements, this is the minimum number that the identification aircraft moves up and down, if increase the quantity of light-sensitive element, obviously also can according to the same principle realization to the identification that aircraft moves, just increase material.
Obviously, light-sensitive element is arranged on a certain side of aircraft fuselage, just the cone-shaped beam of remote controller emission can be shone this face and realize control of the present invention, such as, light-sensitive element is arranged on the trailing flank of aircraft fuselage, just can controls from behind aircraft and carry out unsettled.And if it is unsettled to wish can both to control aircraft from all directions, can all be provided with two light-sensitive elements at the above-below direction of a plurality of sides of aircraft fuselage (such as front, rear, left and right on four sides), the position arranges as G1, the G2 of Fig. 2, again the output-parallel of each light-sensitive element of top is accessed the IO1 of unsettled control circuit, IO2 with the unsettled control circuit of each light-sensitive element of bottom access in parallel, be used for receiving in each side cone-shaped beam, so that cone-shaped beam can both effectively be received in each side and control the unsettled stop of aircraft.Light resistance and the dark resistance of light-sensitive element differ greatly, and general direct parallel connection can work, the resistance of in case of necessity capable of regulating series connection, or add buffer circuit for the output of each light-sensitive element.
Remote controller also can include modulation circuit, makes the cone-shaped beam band of its emission be useful on jamproof modulation intelligence.Come modulated beam of light such as adopting oscillating circuit to produce high frequency waves, perhaps adopt coding circuit to produce coded message and come modulated beam of light.Correspondingly on aircraft with the demodulator circuit that modulation intelligence is carried out demodulation.This belongs to the conventional means of remote control.But it is not to carry remote information that light beam of the present invention adopts the purpose of modulation intelligence modulation, but: 1, better improve anti-interference, avoid the interference of ambient light; 2, different cone-shaped beams can not interfered with each other each other.
Claims (6)
- One kind can unsettled stop toy aircraft, comprise remote controller and aircraft; Remote controller includes remote-control gear and remote controlled transmitting circuit, and aircraft includes with the remote-control receiving circuit of remote controller cooperating, remote control circuit and lifting executing agency; It is characterized in that: also be provided with luminous tube at remote controller, be used for launching and a branch ofly can cover the cone-shaped beam that shines aircraft fuselage; Up and down diverse location at aircraft fuselage is provided with two light-sensitive elements that are used for receiving cone-shaped beam at least; Light-sensitive element is connected to the input of unsettled control circuit, and the output of unsettled control circuit is connected to lifting executing agency; Described unsettled control circuit is according to the up and down variation of the input signal of the light-sensitive element of diverse location, identify the change in location that aircraft moves up and down in cone-shaped beam, and according to change in location adjustment output control signal, carry out lifting action by lifting actuating mechanism controls aircraft.
- 2. a kind of toy aircraft that can unsettled stop according to claim 1 is characterized in that: described cone-shaped beam, adopt visible light beam or infrared beam; When adopting visible light beam, adopt the light beam of ruddiness or green glow or blue light or purple light.
- 3. according to claim 1 or a kind of toy aircraft that can unsettled stop claimed in claim 2, it is characterized in that: described remote controller, also include be used to the modulation circuit that makes cone-shaped beam with anti-interference modulation intelligence, described aircraft also includes the demodulator circuit that modulation intelligence is carried out demodulation.
- 4. a kind of toy aircraft that can unsettled stop according to claim 1, it is characterized in that: described unsettled control circuit at the light-sensitive element of the diverse location of aircraft above-below direction simultaneously by the prerequisite that cone-shaped beam shone under, the different conditions that breaks away from the cone-shaped beam irradiation according to the light-sensitive element of diverse location up and down, identify the change in location that aircraft moves up and down in cone-shaped beam, and adjust the output control signal with this, control aircraft by lifting executing agency and carry out lifting action.
- 5. according to claim 1 or a kind of toy aircraft that can unsettled stop claimed in claim 4, it is characterized in that: described unsettled control circuit at the light-sensitive element of the diverse location of aircraft above-below direction simultaneously by the prerequisite that cone-shaped beam shone under, different conditions and precedence according to the up and down light-sensitive element disengaging cone-shaped beam irradiation of diverse location, identify change in location and pace of change that aircraft moves up and down in cone-shaped beam, and adjust the output control signal with this, carry out lifting action by lifting actuating mechanism controls aircraft with friction speed.
- 6. according to claim 1 to the described a kind of toy aircraft that can unsettled stop of one of claim 5, it is characterized in that: on a plurality of sides of the fuselage of described aircraft, all be provided with two light-sensitive elements at diverse location up and down, the output-parallel of each light-sensitive element of each top, side accesses an input of unsettled control circuit, and the output-parallel of each light-sensitive element of each side bottom accesses another input of unsettled control circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210411138.1A CN102886148B (en) | 2012-09-21 | 2012-10-25 | Toy aircraft capable of stopping in air |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210360596.7 | 2012-09-21 | ||
| CN201210360596 | 2012-09-21 | ||
| CN201210411138.1A CN102886148B (en) | 2012-09-21 | 2012-10-25 | Toy aircraft capable of stopping in air |
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| Publication Number | Publication Date |
|---|---|
| CN102886148A true CN102886148A (en) | 2013-01-23 |
| CN102886148B CN102886148B (en) | 2014-09-17 |
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| CN201210390693.0A Active CN103657113B (en) | 2012-09-21 | 2012-10-16 | Adopt the method that mobile beam controls electronic toy |
| CN 201220527193 Expired - Lifetime CN202961875U (en) | 2012-09-21 | 2012-10-16 | Electric toy car adopting light-beam remote control |
| CN201210390701.1A Expired - Fee Related CN102861441B (en) | 2012-09-21 | 2012-10-16 | Electronic toy car remotely controlled by light beams |
| CN201210390705.XA Expired - Fee Related CN102861443B (en) | 2012-09-21 | 2012-10-16 | toy aircraft employing light-beam remote control |
| CN201210390718.7A Active CN102861444B (en) | 2012-09-21 | 2012-10-16 | Remote control electronic toy adopting light-beam remote control |
| CN 201220527190 Expired - Lifetime CN202961878U (en) | 2012-09-21 | 2012-10-16 | Toy aircraft adopting light-beam remote control |
| CN201210411139.6A Expired - Fee Related CN102880189B (en) | 2012-09-21 | 2012-10-25 | Method for hovering toy aircraft in air |
| CN201210411138.1A Expired - Fee Related CN102886148B (en) | 2012-09-21 | 2012-10-25 | Toy aircraft capable of stopping in air |
| CN 201220549393 Expired - Lifetime CN202961881U (en) | 2012-09-21 | 2012-10-25 | Toy aircraft capable of being suspended and stayed in air |
| CN201310427799.8A Pending CN103520935A (en) | 2012-09-21 | 2013-09-21 | Two-player adversarial remote control electric toy |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201210390693.0A Active CN103657113B (en) | 2012-09-21 | 2012-10-16 | Adopt the method that mobile beam controls electronic toy |
| CN 201220527193 Expired - Lifetime CN202961875U (en) | 2012-09-21 | 2012-10-16 | Electric toy car adopting light-beam remote control |
| CN201210390701.1A Expired - Fee Related CN102861441B (en) | 2012-09-21 | 2012-10-16 | Electronic toy car remotely controlled by light beams |
| CN201210390705.XA Expired - Fee Related CN102861443B (en) | 2012-09-21 | 2012-10-16 | toy aircraft employing light-beam remote control |
| CN201210390718.7A Active CN102861444B (en) | 2012-09-21 | 2012-10-16 | Remote control electronic toy adopting light-beam remote control |
| CN 201220527190 Expired - Lifetime CN202961878U (en) | 2012-09-21 | 2012-10-16 | Toy aircraft adopting light-beam remote control |
| CN201210411139.6A Expired - Fee Related CN102880189B (en) | 2012-09-21 | 2012-10-25 | Method for hovering toy aircraft in air |
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| CN201310427799.8A Pending CN103520935A (en) | 2012-09-21 | 2013-09-21 | Two-player adversarial remote control electric toy |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103520935A (en) * | 2012-09-21 | 2014-01-22 | 徐志强 | Two-player adversarial remote control electric toy |
| CN105984592A (en) * | 2015-01-27 | 2016-10-05 | 张斌 | Electric helicopter |
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|---|---|---|---|---|
| CN105100439A (en) * | 2015-06-18 | 2015-11-25 | 广州飞米电子科技有限公司 | Operation control method and device |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020106966A1 (en) * | 2001-02-08 | 2002-08-08 | Oscar Jimenez | Radio-controlled toy blimp with infrared beam weapons for staging a gun battle |
| CN2657746Y (en) * | 2003-10-09 | 2004-11-24 | 刘菊兰 | Controller of light-operated toy |
| US20070026757A1 (en) * | 2005-07-29 | 2007-02-01 | Yu Tian | Method and device for checking plane's entry into a dive and anti-dive devices for planes using the same |
| CN202387227U (en) * | 2011-12-10 | 2012-08-22 | 厦门新泰阳网络科技有限公司 | Robot toy |
| CN202961881U (en) * | 2012-09-21 | 2013-06-05 | 徐志强 | Toy aircraft capable of being suspended and stayed in air |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4201012A (en) * | 1978-04-13 | 1980-05-06 | Marshall Harry L | Remote control vehicle |
| JPS63186496U (en) * | 1987-05-22 | 1988-11-30 | ||
| CN2284089Y (en) * | 1996-12-04 | 1998-06-17 | 黄幸美 | Controller of remote-control toy |
| DE19983441B4 (en) * | 1998-08-07 | 2010-12-23 | Mattel, Inc., El Segundo | Toy vehicle with pivotally mounted side wheels |
| CN2408933Y (en) * | 1998-10-27 | 2000-12-06 | 吴宗祥 | Light remote-controlled electric toy |
| JP2000325671A (en) * | 1999-05-19 | 2000-11-28 | Hiroboo Kk | Remote control car |
| JP3756015B2 (en) * | 1999-06-02 | 2006-03-15 | 株式会社トミー | Remote control toy |
| FR2840541B1 (en) * | 2002-06-11 | 2005-02-25 | Janick Simeray | MOTORIZED MOTORIZED TOY WITH REMOTE CONTROL |
| CN2691671Y (en) * | 2003-10-21 | 2005-04-13 | 方凯 | Digital ratio remote control equipment |
| CN1631478A (en) * | 2003-12-24 | 2005-06-29 | 徐洋 | Remote control infrared fight model tank with large ratio |
| US7344430B2 (en) * | 2005-05-12 | 2008-03-18 | Hasty Christopher M | Remote/occupant controlled toy vehicle |
| US20070018041A1 (en) * | 2005-07-07 | 2007-01-25 | Butler Ernest M | Model aircraft |
| CN200948361Y (en) * | 2006-09-10 | 2007-09-19 | 周银东 | Laser remote control toy car |
| JP2009101127A (en) * | 2007-10-05 | 2009-05-14 | Tomy Co Ltd | Control device for steering running toy and running toy |
| CN201194120Y (en) * | 2008-03-25 | 2009-02-11 | 中山市东升镇高级中学 | Computer answering machine |
| CN101816838B (en) * | 2010-01-19 | 2012-03-21 | 广东群兴玩具股份有限公司 | Infrared control running toy |
| WO2012012883A1 (en) * | 2010-07-30 | 2012-02-02 | Thinking Technology | Improved remote controlled toy |
| CN102005113A (en) * | 2010-11-11 | 2011-04-06 | 广东欧珀电子工业有限公司 | Anti-interference infrared remote control signal receiving circuit |
| US20120122367A1 (en) * | 2010-11-16 | 2012-05-17 | Michael Sivan | Advanced Light Beam Remote Control |
| CN102847322A (en) * | 2012-09-15 | 2013-01-02 | 徐志强 | Low-power consumption remote control method of electric toy |
| CN102847323A (en) * | 2012-09-15 | 2013-01-02 | 徐志强 | Remote control electric toy employing efficient energy-saving remote control mode |
-
2012
- 2012-10-16 CN CN201210390693.0A patent/CN103657113B/en active Active
- 2012-10-16 CN CN 201220527193 patent/CN202961875U/en not_active Expired - Lifetime
- 2012-10-16 CN CN201210390701.1A patent/CN102861441B/en not_active Expired - Fee Related
- 2012-10-16 CN CN201210390705.XA patent/CN102861443B/en not_active Expired - Fee Related
- 2012-10-16 CN CN201210390718.7A patent/CN102861444B/en active Active
- 2012-10-16 CN CN 201220527190 patent/CN202961878U/en not_active Expired - Lifetime
- 2012-10-25 CN CN201210411139.6A patent/CN102880189B/en not_active Expired - Fee Related
- 2012-10-25 CN CN201210411138.1A patent/CN102886148B/en not_active Expired - Fee Related
- 2012-10-25 CN CN 201220549393 patent/CN202961881U/en not_active Expired - Lifetime
-
2013
- 2013-09-21 CN CN201310427799.8A patent/CN103520935A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020106966A1 (en) * | 2001-02-08 | 2002-08-08 | Oscar Jimenez | Radio-controlled toy blimp with infrared beam weapons for staging a gun battle |
| CN2657746Y (en) * | 2003-10-09 | 2004-11-24 | 刘菊兰 | Controller of light-operated toy |
| US20070026757A1 (en) * | 2005-07-29 | 2007-02-01 | Yu Tian | Method and device for checking plane's entry into a dive and anti-dive devices for planes using the same |
| CN202387227U (en) * | 2011-12-10 | 2012-08-22 | 厦门新泰阳网络科技有限公司 | Robot toy |
| CN202961881U (en) * | 2012-09-21 | 2013-06-05 | 徐志强 | Toy aircraft capable of being suspended and stayed in air |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103520935A (en) * | 2012-09-21 | 2014-01-22 | 徐志强 | Two-player adversarial remote control electric toy |
| CN105984592A (en) * | 2015-01-27 | 2016-10-05 | 张斌 | Electric helicopter |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102861441A (en) | 2013-01-09 |
| CN202961875U (en) | 2013-06-05 |
| CN102886148B (en) | 2014-09-17 |
| CN103520935A (en) | 2014-01-22 |
| CN103657113B (en) | 2016-02-24 |
| CN102861444A (en) | 2013-01-09 |
| CN103657113A (en) | 2014-03-26 |
| CN102880189B (en) | 2015-02-11 |
| CN102861443A (en) | 2013-01-09 |
| CN102880189A (en) | 2013-01-16 |
| CN202961878U (en) | 2013-06-05 |
| CN202961881U (en) | 2013-06-05 |
| CN102861444B (en) | 2014-12-03 |
| CN102861441B (en) | 2014-10-22 |
| CN102861443B (en) | 2015-01-14 |
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