CN209392737U - A kind of infrared induction aircraft interacting control - Google Patents

Abstract

The utility model relates to aerobat toy technical fields, the infrared induction aircraft of control can be interacted more particularly to one kind, including pedestal and the shield for covering at pedestal, the pedestal, which extends outwardly, several linking arms, flying power component is mounted on several linking arms, it is set to several the first infrared emission sensors for being used to incude simultaneously avoidant disorder object of pedestal and linking arm dislocation, being set to base bottom, at least one is used to incude simultaneously the second infrared emission sensor of avoidant disorder object and the infrared receiver sensor of at least one, it is provided with positioned at infrared receiver sensor side and stirs controller, the controller of stirring is connected with control panel；The utility model can realize interactive effect by induction gesture；Be additionally provided with stir controller can operate control aircraft fly along flight path, to improve whole interest.

Description

A kind of infrared induction aircraft interacting control

Technical field

The utility model relates to aerobat toy technical field, the infrared induction that can interact control more particularly to one kind flies Row device.

Background technique

Existing flying toy mostly uses greatly the mode of remote controler to be controlled, interactive insufficient, inconvenient for operation. Occur a kind of toy aircraft on the market at present, it, can automatic sensing by being provided with height infra-red ray detection device in bottom The height of current flight toy and adjust wing, flying toy can be made to maintain certain height according to the fluctuating on ground, and nothing Height control need to be carried out using remote controler in real time, it is easy to operate.

But these flying toys have the disadvantage that 1, aircraft can only be adjusted automatically in flying height, control The forward-reverse of flying toy still needs to be controlled using remote controler.2, the taking off, close of aircraft, pattern switching be still It needs to be controlled using remote controler.3, above-mentioned aerobat toy, infrared height detecting device are all set in aircraft object for appreciation The bottom centre of tool, when need aircraft bottom assemble accessory when (such as aircraft bottom installation suspension type camera shooting Head), height detecting device will be blocked, to can not the height of flying toy be detected and be adjusted, and due to red Outer height detecting device is all set in the bottom centre of aerobat toy, and the height of reflection is aircraft bottom centre distance The height on ground can not reflect the height of entire aircraft, longer for flight arm flying toy (such as fuselage is longer Helicopter flight device, the four-axle aircraft extended around), if only distance of the sense aircraft bottom centre apart from ground, When flying toy tilts, certain parts of toy are still likely to be encountered the barriers such as ground.

In the prior art, Chinese Patent Application No. 201520794316.2 disclose a kind of based on infrared induction technology Flying toy device, control flying toy can be facilitated to open, close, cut by the movement that gestures detection mechanism detects user Mold changing formula can detecte user in the hand motion of side by being provided with obstacle infrared probe in host body side surface, in this way, User without using remote controler can lifting to flying toy, move forward and backward, motor pattern controls, playability is significantly It improves；Moreover, the infrared height detection probe of the utility model is set on the bottom of flight arm, the entirety of aircraft can be incuded Highly, the part of flying toy and ground or bar contact are avoided, while the installation of flying toy bottom accessory will not be interfered.

In addition, Chinese Patent Application No. is 201720979071.X, a kind of anticollision aircraft is disclosed, it is desirable to provide a kind of It can reduce aircraft contact or anticollision aircraft the case where when impacting object and aircraft are fallen causes damage, skill Art programme element is, including aircraft body, and aircraft body installation is there are four individual motor, and four individual motors are and respectively The connection of fan blade power device, four individual motors access control unit, and the two sides of aircraft body are symmetrical arranged useful In be mounted on the protective cover for being provide with fan blade power device, two protective covers for detecting whether have object close to protective cover simultaneously The switching signal of the infrared inductor of output switching signal and receiving infrared-ray inductor is to control the start and stop of driving motor Controller.

It is disadvantageous in that for existing for above-mentioned existing flying toy, it cannot be simultaneously to multiple faces in flight course Or multiple positions carry out induction barrier, are easy to stop flight after colliding barrier in flight course and fall, to subtract The low interest of aircraft；It flies in addition, also fixed flight path can not be arranged to aircraft, to reduce flight The playability and interactivity of device.

Utility model content

To solve the above problems, the utility model, which provides one kind, to realize interactive effect by induction gesture；In addition it is arranged It stirs controller and can operate control aircraft and fly along flight path, so that improves whole interest interacts control Infrared induction aircraft.

The technical scheme adopted by the utility model is a kind of infrared induction aircraft that can interact control, including pedestal With the shield for covering at pedestal, which, which extends outwardly, several linking arms, is mounted on flying power on several linking arms Component is set to several the first infrared emission sensors for being used to incude simultaneously avoidant disorder object of pedestal and linking arm dislocation, if Being placed in base bottom, at least one is infrared at least one for incuding simultaneously the second infrared emission sensor of avoidant disorder object Receiving sensor is provided with positioned at infrared receiver sensor side and stirs controller, and the controller of stirring is connected with control electricity Plate, the control panel setting is set to the power supply in pedestal positioned at control panel side for power supply in base interior, described Control panel and flying power component, the first infrared emission sensor, the second infrared emission sensor and infrared receiver sensor Electrical connection.

Further improvement of these options is that the pedestal top is equipped with protection cap and encapsulates power supply and control panel.

Further improvement of these options is, the shield include with the integrally formed lower cover of pedestal, be fastened on The upper outlet body on lower cover top, the upper outlet body and lower cover offer several grids；The upper outlet body is equipped with male earner.

Further improvement of these options is that the linking arm is uniformly arranged on outside pedestal there are four setting.

Further improvement of these options is that the flying power component includes being installed on linking arm and and control panel Connected driving motor, is installed on the flight blade at driving motor driving end, and the several groups flying power component is synchronous drives Dynamic setting.

Further improvement of these options is that the first infrared emission sensor is set to pedestal there are two setting It misplaces with linking arm, the transmitting terminal of the first infrared emission sensor is toward outside pedestal.

Further improvement of these options is to be misplaced there are four the first infrared emission sensor is set with linking arm It is arranged and is evenly arranged in four side of pedestal.

Further improvement of these options is that the second infrared emission sensor is respectively provided with infrared receiver sensor It is one, the transmitting terminal of the second infrared emission sensor and the receiving end of infrared receiver sensor are arranged downward.

Further improvement of these options is that the controller of stirring is connected with control panel, in the control panel If stirring controller control aircraft equipped with dry run path program and flying along flight path.

Further improvement of these options is the interface being provided in the control panel for power supply source charging.

The utility model has the following beneficial effects:

On the one hand, pedestal and shield are set, made the encapsulation installation of the control panels such as control panel and power supply by pedestal With, it is easy for installation, the installation effect of matrix is also functioned to, protection can be played during aircraft flight by the effect of shield Effect, preventing aircraft to be collided in flight course causes to damage, and protecting effect is good；Second aspect extends on the base There is linking arm, flying power component is set on the connecting arm, plays flight driving effect particular by flying power component, makes Aircraft can smooth flight, interest is strong；The several of the third aspect, pedestal and linking arm dislocation are used to incude and avoid barrier The first infrared emission sensor of object is hindered to pass through transmitting during aircraft flight using the emission sensor shifted to install Sensor sensing periphery barrier or gesture can be realized when sensing gesture or barrier and avoid flight effect, so as to Realize that multi-person interactive is played use, interest is strong；Fourth aspect is at least arranged one for incuding and avoiding barrier in base bottom The the second infrared emission sensor and the infrared receiver sensor of at least one for hindering object, receive first by infrared receiver sensor The signal issued with the second infrared emission sensor is easy to implement interactive playing to control aircraft avoidant disorder object, interest Taste is high；5th aspect, by the setting of the second infrared transmitter in lower surface, effect is to prevent aircraft from falling, and can also be led to Receiving and distributing will definitely its picking-up；6th aspect, infrared receiver sensor side, which is provided with, stirs controller, stirs controller connection control Battery plate is provided with flight path in control panel, stirs controller by operation during aircraft flight to control flight Device is along the flight path flight set, to further increase interest；In terms of 7th, it is provided in pedestal winged for controlling The control panel of row device work, is set to the power supply in pedestal positioned at control panel side for power supply, the control panel with Flying power component, the first infrared emission sensor, the second infrared emission sensor and the electrical connection of infrared receiver sensor, specifically It is the control action that emission sensor and receiving sensor are realized by control panel, to realize that aircraft can encounter barrier Avoidance effect is realized when hindering.

In the utility model, periphery barrier is incuded when by the way that multiple infrared transmitters are arranged to aircraft flight, thus It can guarantee the avoiding barrier in flight course, while can also realize interactive effect by induction gesture；It is additionally provided with and dials Movement controller can operate control aircraft and fly along flight path, to improve whole interest.

Detailed description of the invention

Fig. 1 is the schematic perspective view of the utility model；

Fig. 2 is the schematic perspective view at another visual angle of the utility model；

Fig. 3 is the overlooking structure diagram of the utility model；

Fig. 4 is the A-A sectional view of Fig. 3；

Fig. 5 is the stereoscopic schematic diagram that the utility model removes upper cover body.

Description of symbols: description of symbols: aircraft 100, pedestal 110, protection cap 111, shield 120, lower cover Body 121, upper outlet body 122, male earner 123, linking arm 130, flying power component 140, driving motor 141, flight blade 142, One infrared emission sensor 150, infrared receiver sensor 170, stirs controller 180, control at second infrared emission sensor 160 Battery plate 190 processed, interface 191, power supply 200.

Specific embodiment

The utility model is further described below in conjunction with attached drawing.

As shown in fig. 1~fig. 5, a kind of infrared induction aircraft 100 interacting control, including pedestal 110 and cover at The shield 120 of pedestal 110, which, which extends outwardly, several linking arms 130, is mounted on several linking arms 130 winged Action edge component 140, be set to that pedestal 110 and linking arm 130 misplace is several first red for incude simultaneously avoidant disorder object Outer emission sensor 150 is set at least one second infrared emission for being used to incude simultaneously avoidant disorder object of 110 bottom of pedestal and passes The infrared receiver sensor 170 of sensor 160 and at least one is provided with positioned at 170 side of infrared receiver sensor and stirs control Device 180, the controller 180 of stirring are connected with control panel 190, and the control panel 190 is arranged inside pedestal 110, if It is placed in the power supply 200 in pedestal 110 positioned at 190 side of control panel for power supply, the control panel 190 and flying power group Part 140, the first infrared emission sensor 150, the second infrared emission sensor 160 and infrared receiver sensor 170 are electrically connected.

110 top of pedestal is equipped with protection cap 111 and encapsulates power supply 200 and control panel 190, passes through 111 pairs of electricity of protection cap Source 200 and control panel 190 play the role of packaging protection, improve the protecting effect to control unit, protecting effect is good, flight Stability is good.

Shield 120 include with the integrally formed lower cover 121 of pedestal 110, be fastened on the upper outlet body on 121 top of lower cover 122, the upper outlet body 122 offers several grids with lower cover 121, can save raw material using integrally formed cover, Good forming effect, while protecting effect is good, and 122 protecting effect of upper outlet body on top is good, the effect that grid is arranged facilitates flight The flight of Power Component 140, which drives, to be used, while buffer function can be also played when being collided, and improves protecting effect.

Upper outlet body 122 is equipped with male earner 123, and whole entertaining can be improved in the effect that male earner 123 is arranged on upper outlet body 122 Property, it can be the discovery that be seen to be in 100 flight course of aircraft and be flown by male earner 123 in driving aircraft 100, it can be into one Step improves whole interest.

There are four linking arm 130 is set, it is uniformly arranged on outside pedestal 110, is further improved to, the flying power group Part 140 includes the driving motor 141 for being installed on linking arm 130 and being connected with control panel 190, is installed on the drive of driving motor 141 The flight blade 142 of moved end, the several groups flying power component 140 are synchronous driving setting, are flown particular by four Power Component 140 fly, guarantee aircraft 100 can smooth flight, it is more stable in flight course, using driving motor 141 Flight blade 142 is driven to realize flight, degree of having a smooth flight is high, highly reliable.

In the present embodiment 1, the first infrared emission sensor 150 is set to pedestal 110 and linking arm 130 there are two setting Two the first infrared emissions are arranged toward outside pedestal 110 in dislocation, the transmitting terminal of the first infrared emission sensor 150 The effect of sensor 150 can realize interactive effect in 100 flight course of aircraft, facilitate avoidant disorder object, practicability compared with By force.

In the present embodiment 2, the difference is that, the first infrared emission sensor 150 is equipped with four with above-described embodiment 1 It is a, 110 4 side of pedestal is shifted to install and is evenly arranged in linking arm 130, it is more steady in flight course for acting on, Multiple faces can be carried out with induction avoidant disorder object, flight interaction is more preferable, and interest is stronger.

Second infrared emission sensor 160 is disposed as one with infrared receiver sensor 170, the second infrared emission sensing The transmitting terminal of device 160 and the receiving end of infrared receiver sensor 170 are arranged downward, are sensed by the infrared emission being arranged downward The effect of device can be in flight course by holding up so that aircraft 100 flies higher, and interest is strong, in addition, being connect by infrared It receives sensor 170 and receives the signal that emission sensor issues, avoid to control aircraft 100 by control panel 190 and realize.

Controller 180 is stirred to be connected with control panel 190, if being equipped with dry run path program in the control panel 190, It stirs controller 180 and controls aircraft 100 along the flight of flight path, specifically in actual use, settable a plurality of flight rail Sequence of threads stirs controller 180 by operation and controls aircraft 100 along the flight of flight path, and such as: controller 180 is stirred in operation 1 time, aircraft 100 along stir operator flight one circle or multi-turn；Operation stir controller 180 2 times, aircraft 100 turn over It struggles against one or many；Operation is stirred controller 180 3 times, and aircraft 100 rapidly go up and down 1 time or multiple；Certainly it is also not limited to Other interaction movements, are arranged according to flight path program.

It is provided with the interface 191 to charge for power supply source 200 in control panel 190, is also set on control panel 190 certainly It is equipped with switch, charging is connected by interface 191 and is used, it is easy to use.

On the one hand, pedestal 110 and shield 120 are set, controlled control panel 190 and power supply 200 etc. by pedestal 110 The encapsulation of battery plate 190 is installed and used, easy for installation, is also functioned to the installation effect of matrix, can flown by the effect of shield 120 It plays a protective role in 100 flight course of device, preventing aircraft 100 to be collided in flight course causes to damage, protection effect Fruit is good；Second aspect is extended with linking arm 130 on pedestal 110, and flying power component 140, tool are arranged on linking arm 130 Body is to play flight driving effect by flying power component 140, enables 100 smooth flight of aircraft, and interest is strong；The Three aspects, pedestal 110 and linking arm 130 misplace several for incuding the first infrared emission sensor of simultaneously avoidant disorder object 150, using the emission sensor shifted to install, periphery obstacle is incuded by emission sensor in 100 flight course of aircraft Object or gesture can be realized when sensing gesture or barrier and avoid flight effect, so that can realize that multi-person interactive is played makes With interest is strong；Fourth aspect is at least arranged one for incude the second infrared of simultaneously avoidant disorder object in 110 bottom of pedestal The infrared receiver sensor 170 of emission sensor 160 and at least one receives first and the by infrared receiver sensor 170 The signal that two infrared emission sensors 160 are issued is easy to implement interactive playing to control 100 avoidant disorder object of aircraft, Interest is high；5th aspect, by the setting of the second infrared transmitter in lower surface, effect is to prevent aircraft 100 from falling, It can be held up by gesture；6th aspect, 170 side of infrared receiver sensor, which is provided with, stirs controller 180, stirs control Device 180 connects control panel 190, is provided with flight path in control panel 190, passes through behaviour in 100 flight course of aircraft Controller 180 is stirred to control aircraft 100 along the flight path flight set, to further increase interest；The In terms of seven, it is provided with the control panel 190 for controlling the work of aircraft 100 in pedestal 110, is set in pedestal 110 and is located at Power supply 200 of 190 side of control panel for power supply, the control panel 190 and flying power component 140, the first infrared hair It penetrates sensor 150, the second infrared emission sensor 160 and infrared receiver sensor 170 to be electrically connected, particular by control panel 190 realize the control action of emission sensor and receiving sensor, to realize that aircraft 100 being capable of the realization when encountering obstacle Avoidance effect.

In the utility model, periphery barrier is incuded when by the way that multiple infrared transmitters are arranged to 100 flight of aircraft, from And it can guarantee the avoiding barrier in flight course, while can also realize interactive effect by induction gesture；It is additionally provided with Stir controller 180 can operate control aircraft 100 fly along flight path, to improve whole interest.

Above-described embodiments merely represent several embodiments of the utility model, the description thereof is more specific and detailed, But it should not be understood as limiting the scope of the patent of the utility model.It should be pointed out that for the common of this field For technical staff, without departing from the concept of the premise utility, various modifications and improvements can be made, these all belong to In the protection scope of the utility model.Therefore, the scope of protection shall be subject to the appended claims for the utility model patent.

Claims (9)

1. the infrared induction aircraft that one kind can interact control, it is characterised in that: including pedestal and the shield for covering at pedestal, The pedestal, which extends outwardly, several linking arms, and flying power component is mounted on several linking arms, be set to pedestal with connect Several the first infrared emission sensors for being used to incude simultaneously avoidant disorder object of arm dislocation are set at least one use of base bottom In induction and the second infrared emission sensor and the infrared receiver sensor of at least one of avoidant disorder object, it is located at infrared receiver Sensor side, which is provided with, stirs controller, and the controller of stirring is connected with control panel, and the control panel is arranged in base Seat is internal, is set to the power supply in pedestal positioned at control panel side for power supply, the control panel and flying power component, First infrared emission sensor, the second infrared emission sensor and infrared receiver sensor electrical connection, it is described stir controller with Control panel is connected, if being equipped with dry run path program in the control panel, stirs controller control aircraft along flight rail Line flight.

2. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: on the pedestal Portion is equipped with protection cap and encapsulates power supply and control panel.

3. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: the shield Including with the integrally formed lower cover of pedestal, be fastened on the upper outlet body on lower cover top, the upper outlet body is opened up with lower cover There are several grids；The upper outlet body is equipped with male earner.

4. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: the linking arm If there are four, it is uniformly arranged on outside pedestal.

5. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: the flight is dynamic Power component includes the driving motor for being installed on linking arm and being connected with control panel, is installed on the flight leaf at driving motor driving end Piece, the several groups flying power component are synchronous driving setting.

6. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: described first is red There are two outer emission sensor is set, it is set to pedestal and linking arm misplaces, the transmitting terminal of the first infrared emission sensor Toward outside pedestal.

7. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: described first is red There are four outer emission sensor is set, is shifted to install with linking arm and be evenly arranged in four side of pedestal.

8. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: described second is red Outer emission sensor and infrared receiver sensor are disposed as one, the transmitting terminal and infrared receiver of the second infrared emission sensor The receiving end of sensor is arranged downward.

9. the infrared induction aircraft that one kind according to claim 1 can interact control, it is characterised in that: the control electricity The interface for power supply source charging is provided in plate.