CN207516831U9 - A kind of interaction four-axle aircraft - Google Patents
A kind of interaction four-axle aircraft Download PDFInfo
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- CN207516831U9 CN207516831U9 CN201721595515.6U CN201721595515U CN207516831U9 CN 207516831 U9 CN207516831 U9 CN 207516831U9 CN 201721595515 U CN201721595515 U CN 201721595515U CN 207516831 U9 CN207516831 U9 CN 207516831U9
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- 230000003993 interaction Effects 0.000 title claims abstract description 35
- 238000004891 communication Methods 0.000 claims abstract description 10
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 10
- 229910052744 lithium Inorganic materials 0.000 claims description 10
- 230000004888 barrier function Effects 0.000 description 28
- 230000008859 change Effects 0.000 description 14
- 238000000034 method Methods 0.000 description 12
- 230000008569 process Effects 0.000 description 4
- 230000001681 protective effect Effects 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000002452 interceptive effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000002688 persistence Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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Abstract
The utility model relates to a kind of interaction four-axle aircrafts, including main stand, control module, power module and power plant module, the power module is located at the bottom of main stand, the power plant module is arranged around power module, control module includes control mainboard, module and bottom is laterally followed to follow module, control mainboard is located in power plant module, control mainboard is equipped with MCU Main Processing Unit, attitude transducer gyroscope, baroceptor and 2.4G wireless communication module, module is laterally followed to be located at the side of main stand, bottom follows module to be located at the bottom of main stand, laterally follow module, bottom follows module to be electrically connected respectively with control mainboard, by laterally following module and bottom that module is followed to realize Intelligent gesture control, reduce hand difficulty, it does not need to control using remote controler, enhance playability With interactivity.
Description
Technical field
The utility model relates to vehicle technology field, espespecially a kind of interaction four-axle aircraft.
Background technique
As people are to the pay attention to day by day of Intelligent life, the relevant technology of four-axle aircraft (also referred to as unmanned plane) is widely used in the field of toys, creates various types of Intelligent flight toys, and existing toy four-axle aircraft is complicated for operation, lack interaction, playability is not high.
Utility model content
To solve the above problems, the utility model provides a kind of interaction four-axle aircraft easy to operate, playing method is various, playability is high.
To achieve the above object, the utility model adopts the following technical scheme is: a kind of interaction four-axle aircraft, including aircraft body, it is characterised in that: the aircraft body side is equipped with and laterally follows module, and the aircraft body bottom is equipped with bottom and follows module.
Preferably, it is described that laterally to follow module include infrared receiving tube, infrared transmitting tube, infrared receiver pipe sleeve and infrared emission pipe sleeve, two infrared transmitting tube horizontal alignments are located at the side of aircraft body, the infrared receiving tube is located at the top of infrared transmitting tube, the infrared transmitting tube, infrared receiving tube are electrically connected with aircraft body respectively, the infrared receiver pipe sleeve is set on infrared receiving tube, and the infrared transmitting tube is respectively sleeved on infrared transmitting tube.
Preferably, it includes infrared receiving tube, infrared transmitting tube, infrared receiver pipe sleeve and infrared emission pipe sleeve that the bottom, which follows module, the infrared transmitting tube and infrared receiving tube are located at the bottom of aircraft body and are electrically connected with aircraft body, the infrared receiver pipe sleeve is set on infrared receiving tube, and the infrared emission pipe sleeve is set on infrared transmitting tube.Infrared emission pipe sleeve can be reduced the scattering of infrared ray, the infrared ray for issuing infrared transmitting tube can only go out have directionality from the outlet of infrared emission pipe sleeve, infrared receiver pipe sleeve can be reduced the receiving area of infrared receiving tube, reflected signal can only be received, the judgement precision and accuracy of control module are improved.
Preferably, the aircraft body includes main stand, control mainboard, power module and power plant module, the power module is located at the bottom of main stand, the power plant module is arranged around power module, the control module with laterally module is followed to follow module to be electrically connected with bottom, the control control module is located in power plant module, and the side for laterally module being followed to be located at main stand, the bottom follows module to be located at the bottom of main stand.
Preferably, the control module is equipped with MCU Main Processing Unit, attitude transducer gyroscope, baroceptor and wireless communication module, and attitude transducer gyroscope, baroceptor and the wireless communication module are electrically connected with MCU Main Processing Unit respectively.
Preferably, the main stand includes upper cover and bottom case, and the upper cover is connected together with bottom case, and the lower section of the bottom case is equipped with erecting bed, and the erecting bed is surrounded by pillar, card slot is equipped in the erecting bed, is equipped with mounting hole in the pillar.
Preferably, the power module includes lithium battery and charging terminal, and the lithium battery is located in card slot, and the charging terminal is located at the inside of erecting bed, and the charging terminal and lithium battery are electrically connected.
Preferably, the power plant module includes motor, motor cover and propeller, four motors are respectively provided in four pillars, four angles of the motor cover are equipped with through-hole and corresponding with four motors respectively, the motor cover lid is located on bottom case, and one end of the motor shaft of four motors passes through through-hole and connect with propeller rotational.
Preferably, it further include LED strip lamp, the shape of the LED strip lamp is identical as the section shape of main stand, and the LED strip lamp is sticked in the inner wall of main stand, the LED strip lamp and control mainboard are electrically connected, since visual persistence forms aperture under interaction four-axle aircraft spin flight.
A kind of interactive method of interaction four-axle aircraft gesture control according to claim 1, includes the following steps
Step 1: after wireless communication module is to code success, aircraft body height-lock control normal in rotary manner；
Step 2: the bottom of module and bottom is laterally followed to follow module obstacle scanning in turn by side, emit infrared signal, when in the horizontal direction 360 degree without in the scanning process of dead angle, scanning to front has obstacle, barrier is locked in a certain direction, in the case of indoors, for the distance change of scanning between 40cm~60cm, aircraft will follow barrier to fly；Between 30cm~40cm, aircraft will hover in the sky the distance change of scanning；The record of scanning changes within the scope of 20cm~30cm, and aircraft will be at a slow speed far from barrier, and the distance change of scanning is less than 20cm, and aircraft will be rapidly directed away from barrier, have protective effect；In the horizontal direction realize follow, hover, impetus；
Step 3: when the infrared emission signal for receiving the front left and right sides for laterally following module, aircraft locks barrier direction on certain angle, when receiving left-side signal, right-side signal is not received, and aircraft can spin to the left, until locking direction, when receiving right-side signal, left-side signal is not received, and aircraft can spin to the right, until locking direction, so that angle in the horizontal direction follows；
Step 4: following module by the bottom of bottom, emit infrared signal, and during bottom scan, scanning has obstacle to bottom, and for the distance change of scanning between 40cm~60cm, aircraft will follow the variation in vertical direction of bottom barrier.The distance of scanning is between 30cm~40cm, aircraft will hover in the sky, the distance of scanning is between 20cm~30cm, barrier will push aircraft to rise at a slow speed, the distance of scanning is less than between 20cm, barrier quickly will push aircraft to rise, and realize following, hovering, pushing in vertical direction.
The utility model has the beneficial effects that: the utility model is by laterally following module and bottom that module is followed to realize Intelligent gesture control, overcome the complicated control method of existing four-axle aircraft, reduce the upper hand difficulty of four-axle aircraft, it does not need to control using remote controler, realize four axis aircraft gesture controls, including obstacle, it follows, enhance playability and interactivity, using the spacing system of rotary infrared Scanning Detction, accomplish 360 degree without the infrared obstacle detection in dead angle, using two infrared transmitting tubes and infrared sensor composition is infrared follows module on UFO four-axle aircraft, it is infrared that module is followed to emit signal towards UFO aircraft horizontal direction, so that UFO four-axle aircraft is greatly promoted the judgement precision for interacting playing method and accuracy and effectively reduces cost, it is different from the existing toy four-axle aircraft in market completely Single remote control playing method, than other infrared spacing modes and application, cost is lower, reliability it is higher and movement differentiate it is more acurrate.
Detailed description of the invention
Fig. 1 is the stereoscopic schematic diagram of the utility model.
Fig. 2 is the main view diagrammatic cross-section of the utility model.
Fig. 3 is the configuration schematic diagram of the utility model.
Fig. 4 is the main view of the utility model.
Fig. 5 is that the lateral of the utility model follows module principle figure.
Fig. 6 is the working principle diagram of the utility model.
Description of symbols: 1. main stands；11. upper cover；12. bottom case；121. erecting bed；122. pillar；2. control mainboard；21.MCU main control unit；3. side is to following module；31. infrared receiving tube；32. infrared transmitting tube；33. infrared receiver pipe sleeve；34. infrared emission pipe sleeve；4. bottom follows module；5. power module；51. lithium battery；52. charging terminal；6. power plant module；61. motor；62. motor cover；63. propeller；7.LED lamp；8. reflecting surface；9. current-limiting resistance.
Specific embodiment
It please refers to shown in Fig. 1-6, the utility model is about a kind of interaction four-axle aircraft, including aircraft body, the aircraft body side laterally follows module equipped with parallel with aircraft body direction front end face, laterally module is followed to be located at aircraft body front end face center, the aircraft body bottom, which is equipped with, follows module with the aircraft body direction vertically disposed bottom of bottom face, and bottom follows module to be located at aircraft body bottom face center position to the rear.Aircraft body includes main stand 1, control mainboard, power module 5 and power plant module 6; the shape of the main stand 1 is the UFO structure of hollow out; including upper cover 11 and bottom case 12; upper cover 11 and bottom case 12 constitute protective cover, have protection safety effect, and the upper cover 11 is connected together with bottom case 12; the lower section of the bottom case 12 is equipped with erecting bed 121; the erecting bed 121 is surrounded by four pillars 122, and card slot is equipped in the erecting bed 121, is equipped with mounting hole in four pillars 122；The power module 5 includes lithium battery 51 and charging terminal 52, and the lithium battery 51 is located in card slot, and the charging terminal 52 is located at the side of erecting bed 121, and the charging terminal 52 is electrically connected with lithium battery 51；The power plant module 6 includes motor 61, motor cover 62 and propeller 63, propeller 63 provides lifting power, four motors 61 are respectively provided in four pillars 122, four angles of the motor cover 62 are equipped with through-hole and corresponding with four motors 61 respectively, fixture block is respectively equipped on four angles of the motor cover 62, the motor cover 62 is fastened on bottom case 12 by fixture block, circular through hole and corresponding with motor 61 is respectively equipped on four angles of the control mainboard 2, the control mainboard 2 is located in motor cover 62, 61 axis of motor on the motor 61 sequentially passes through control mainboard 2 with motor cover 62 to connect with propeller 63, the control mainboard 2 is equipped with MCU Main Processing Unit 21, attitude transducer gyroscope, baroceptor and wireless communication module The side for laterally module 3 being followed to be located at main stand 1, the bottom follows module 4 to be located at the bottom of main stand 1, and the attitude transducer gyroscope, baroceptor and wireless communication module laterally follow module 3, bottom that module 4 is followed to be electrically connected respectively with MCU Main Processing Unit 21.
Preferably, it is described that module 3 is laterally followed to include infrared receiving tube 31, infrared transmitting tube 32, infrared receiver pipe sleeve 33 and infrared emission pipe sleeve 34, two 32 horizontal alignments of infrared transmitting tube are located at the side of erecting bed 121, the infrared receiving tube 31 is located at the top of two infrared transmitting tubes 32, infrared sensor is respectively equipped in the infrared receiving tube 31 and infrared transmitting tube 32, the infrared receiver pipe sleeve 33 is set on infrared receiving tube 31, two infrared transmitting tubes 32 are respectively sleeved on two infrared transmitting tubes 32, infrared emission pipe sleeve 34 can be reduced the scattering of infrared ray, the infrared ray for issuing infrared transmitting tube 32 can only go out have directionality from the outlet of infrared emission pipe sleeve 34, infrared receiver pipe sleeve 33 can be reduced connecing for infrared receiving tube 31 Area is received, reflected signal can only be received, improve the judgement precision and accuracy of control module.
Preferably, it includes infrared receiving tube 31 that the bottom, which follows module 4, infrared transmitting tube 32, infrared receiver pipe sleeve 33 and infrared emission pipe sleeve 34, the infrared transmitting tube 32 is located at the bottom of erecting bed 121 with infrared receiving tube 31, infrared sensor is respectively equipped in the infrared receiving tube 31 and infrared transmitting tube 32, the infrared receiver pipe sleeve 33 is set on infrared receiving tube 31, the infrared emission pipe sleeve 34 is set on infrared transmitting tube 32, infrared emission pipe sleeve 34 can be reduced the scattering of infrared ray, the infrared ray for issuing infrared transmitting tube 32 can only go out have directionality from the outlet of infrared emission pipe sleeve 34, infrared receiver pipe sleeve 33 can be reduced the receiving area of infrared receiving tube 31, reflected signal can only be received, improve the judgement precision and standard of control module True property.
Preferably, it further include LED strip lamp 7, the shape of the LED strip lamp 7 is identical as the section shape of main stand 1, and the LED strip lamp 7 is sticked in the inner wall of main stand 1, the LED strip lamp 7 is electrically connected with control mainboard 2, forms aperture under interaction four-axle aircraft spin flight.
Working principle: four-axle aircraft is interacted by gesture control, after wireless communication module is to code success, effect height-lock control normal in rotary manner by control mainboard 2, by laterally following module 3 to follow 4 realization level of module to follow function with vertical interaction function and angle with bottom.
Module and bottom is laterally followed to follow the control principle of module: IO1 mouthfuls of control infrared transmitting tubes of AD pin of MCU Main Processing Unit 21, the encoded signal of output, emitted by infrared transmitting tube 32, as shown in Figure 5, the power supply of infrared transmitting tube 32 is stable VDD, the current-limiting resistance 9 of infrared emission is fixed resistance value, it can be deduced that it is stable for emitting the transmission power intensity of signal；IO2 mouthfuls of the AD pin of MCU Main Processing Unit 21, acquire 31 signal pins voltage of infrared receiving tube, in the absence of reflecting surface 8, infrared receiving tube 31 is in off state, and the voltage of the IO2 detection of AD pin is VDD, in the presence of reflecting surface 9, reflecting surface 9 with laterally to follow module or bottom to follow closer at a distance from module, the signal of reflection is stronger, and 31 on-state rate of infrared receiving tube is higher, and the IO2 of AD pin voltage detected is lower；Conversely, reflecting surface 9 with laterally to follow module or bottom to follow remoter at a distance from module, the signal of reflection is weaker, and 31 on-state rate of infrared receiving tube is lower, and the IO2 of AD pin voltage detected is higher；In conclusion can be determined that the presence or absence of reflecting surface 9 by the IO2 voltage detected of AD pin, if the variation of the distance between aircraft body and reflecting surface 9 can be can detecte out in the presence of reflecting surface 9 by the voltage change of the IO2 of AD pin；Indoors under environment, module and bottom is laterally followed to follow the effective reflective distance 60cm of module, when reflective distance can follow in 40cm~60cm. four-axle aircraft the movement of reflecting surface；When reflecting surface apart from red in 30cm-40cm, four-axle aircraft is in floating state, and as reflective distance 20cm~30cm, four-axle aircraft can be at a slow speed far from reflecting surface.When reflective distance is less than 20cm, four-axle aircraft is rapidly directed away from reflecting surface.Reflecting surface 8 can be a plane, be also possible to the three-dimensional object with several faces or animal or human body.
Laterally module is followed to be located at aircraft body left and right ends, and there are two infrared emission end (infrared transmitting tubes) respectively, when infrared inductor (infrared receiving tube) receives the signal of two infrared transmitting tubes simultaneously, four-axle aircraft can lock the direction of barrier；When infrared inductor receives left side infrared emission signal, the right infrared emission signal is not received, and four-axle aircraft can left-handed, locks angle when receiving the signal for controlling two transmitting tubes simultaneously；When infrared inductor receives the right infrared emission signal, do not receive left side infrared emission signal, four-axle aircraft can dextrorotation, lock angle when receiving the signal of two transmitting tubes in left and right simultaneously；To realize that angle follows function.
The utility model uses the spacing system of rotary infrared Scanning Detction, accomplishes 360 degree without the infrared obstacle detection in dead angle, and effectively reduces cost；And laterally follow module on four-axle aircraft using two infrared transmitting tubes and an infrared sensor composition, module is laterally followed to emit signal towards aircraft horizontal direction, four-axle aircraft is set to greatly promote the judgement precision and accuracy of interaction playing method, specific interaction follows feature operation mode as follows with angle:
Interaction function: obstacle scanning is carried out by laterally following the infrared transmitting tube 32 of module 3 to emit infrared signal, when in the horizontal direction 360 degree without in the scanning process of dead angle, scanning to front has obstacle, locks barrier in a certain direction and basis makes different reactions at a distance from barrier.In the case of indoors, for the distance change of scanning within the scope of 40cm~60cm, interaction four-axle aircraft will follow barrier to fly；When the distance change of scanning is within the scope of 30cm~40cm, interaction four-axle aircraft will hover in the sky；When the distance change of scanning is within the scope of 20cm~30cm, interaction four-axle aircraft will be at a slow speed far from barrier；When the distance change of scanning is less than 20cm, interaction four-axle aircraft will be rapidly directed away from barrier；Protective effect is played, realization follows in the horizontal direction, hovering or impetus.
It follows the infrared transmitting tube 32 of module 4 to emit infrared signal by bottom to be scanned, when during the scanning process, scanning has obstacle to bottom, locking barrier in a certain direction, simultaneously basis makes different reactions at a distance from barrier.When the distance change of scanning is within the scope of 40cm~60cm, interaction four-axle aircraft will follow bottom barrier to fly in vertical direction；When the distance of scanning is within the scope of 30cm~40cm, interaction four-axle aircraft will hover in the sky；When the distance of scanning is within the scope of 20cm~30cm, barrier will push at a slow speed interaction four-axle aircraft to rise；When the distance of scanning is less than 20cm, barrier will quickly push interaction four-axle aircraft to rise.Realize following in vertical direction, hovering or impetus.
Angle follows function: when the infrared receiving tube 31 for laterally following module 3 while the signal that is issued of infrared transmitting tube 32 for receiving the left and right sides, interaction four-axle aircraft lock barrier direction on certain angle.When receiving left-side signal, when not receiving right-side signal, interaction four-axle aircraft can spin to the left, lock angle when receiving the signal of two transmitting tubes in left and right simultaneously；When receiving right-side signal, when not receiving left-side signal, interaction four-axle aircraft can spin to the right, lock angle when receiving the signal of two transmitting tubes in left and right simultaneously, to realize that angle follows in the horizontal direction.
A kind of interactive method of interaction four-axle aircraft gesture control according to claim 1, includes the following steps
Step 1: after after wireless communication module is to code success, aircraft body height-lock control normal in rotary manner, specially MCU Main Processing Unit are adjusted through attitude algorithm, PID, the calculating such as high algorithm fusion is determined in air pressure, the normal height-lock control of aircraft body is controlled；
Step 2: the bottom of module and bottom is laterally followed to follow module obstacle scanning in turn by side, emit infrared signal, when in the horizontal direction 360 degree without in the scanning process of dead angle, scanning to front has obstacle, barrier is locked in a certain direction, in the case of indoors, for the distance change of scanning between 40cm~60cm, aircraft will follow barrier to fly；Between 30cm~40cm, aircraft will hover in the sky the distance change of scanning；The record of scanning changes within the scope of 20cm~30cm, and aircraft will be at a slow speed far from barrier, and the distance change of scanning is less than 20cm, and aircraft will be rapidly directed away from barrier, have protective effect；In the horizontal direction realize follow, hover, impetus；
Step 3: when the infrared emission signal for receiving the front left and right sides for laterally following module, aircraft locks barrier direction on certain angle, when receiving left-side signal, right-side signal is not received, and aircraft can spin to the left, until locking direction, when receiving right-side signal, left-side signal is not received, and aircraft can spin to the right, until locking direction, so that angle in the horizontal direction follows；
Step 4: following module by the bottom of bottom, emit infrared signal, and during bottom scan, scanning has obstacle to bottom, and for the distance change of scanning between 40cm~60cm, aircraft will follow the variation in vertical direction of bottom barrier.The distance of scanning is between 30cm~40cm, aircraft will hover in the sky, the distance of scanning is between 20cm~30cm, barrier will push aircraft to rise at a slow speed, the distance of scanning is less than between 20cm, barrier quickly will push aircraft to rise, and realize following, hovering, pushing in vertical direction.
Embodiment of above is only that preferred embodiments of the present invention are described; not the scope of the utility model is defined; under the premise of not departing from the spirit of the design of the utility model; the various changes and improvements that this field ordinary engineering and technical personnel makes the technical solution of the utility model should all be fallen into the protection scope of claims determination of the utility model.
Claims (8)
1. a kind of interaction four-axle aircraft, including aircraft body, it is characterized by: the aircraft body side, which is equipped with, laterally follows module, the aircraft body bottom is equipped with bottom and follows module, the aircraft body includes main stand, control mainboard, power module and power plant module, the power module is located at the bottom of main stand, the power plant module is arranged around power module, the control mainboard with laterally module is followed to follow module to be electrically connected with bottom, the control mainboard is located in power plant module, the side for laterally module being followed to be located at main stand, the bottom follows module to be located at the bottom of main stand.
2. interaction four-axle aircraft according to claim 1, it is characterized by: described, laterally to follow module include infrared receiving tube, infrared transmitting tube, infrared receiver pipe sleeve and infrared emission pipe sleeve, two infrared transmitting tube horizontal alignments are located at the side of aircraft body, the infrared receiving tube is located at the top of infrared transmitting tube, the infrared transmitting tube, infrared receiving tube are electrically connected with aircraft body respectively, the infrared receiver pipe sleeve is set on infrared receiving tube, and the infrared transmitting tube is respectively sleeved on infrared transmitting tube.
3. interaction four-axle aircraft according to claim 1, it is characterized by: it includes infrared receiving tube, infrared transmitting tube, infrared receiver pipe sleeve and infrared emission pipe sleeve that the bottom, which follows module, the infrared transmitting tube and infrared receiving tube are located at the bottom of aircraft body and are electrically connected with aircraft body, the infrared receiver pipe sleeve is set on infrared receiving tube, and the infrared emission pipe sleeve is set on infrared transmitting tube.
4. interaction four-axle aircraft according to claim 1, it is characterized by: the control mainboard is equipped with MCU Main Processing Unit, attitude transducer gyroscope, baroceptor and wireless communication module, attitude transducer gyroscope, baroceptor and the wireless communication module are electrically connected with MCU Main Processing Unit respectively.
5. interaction four-axle aircraft according to claim 1, it is characterized by: the main stand includes upper cover and bottom case, the upper cover is connected together with bottom case, the lower section of the bottom case is equipped with erecting bed, the erecting bed is surrounded by pillar, it is equipped with card slot in the erecting bed, is equipped with mounting hole in the pillar.
6. interaction four-axle aircraft according to claim 1, it is characterised in that: the power module includes lithium battery and charging terminal, and the lithium battery is located in card slot, and the charging terminal is located at the inside of erecting bed, and the charging terminal and lithium battery are electrically connected.
7. interaction four-axle aircraft according to claim 1, it is characterized by: the power plant module includes motor, motor cover and propeller, the motor is respectively provided in pillar, four angles of the motor cover are equipped with through-hole and corresponding with motor respectively, the motor cover lid is located on bottom case, and one end of the motor shaft of the motor passes through through-hole and connect with propeller rotational.
8. interaction four-axle aircraft according to claim 1, it is characterised in that: further include LED strip lamp, the LED strip lamp is sticked in the inner wall of main stand, and the LED strip lamp and control mainboard are electrically connected.
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| CN201721595515.6U CN207516831U9 (en) | 2017-11-25 | 2017-11-25 | A kind of interaction four-axle aircraft |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201721595515.6U CN207516831U9 (en) | 2017-11-25 | 2017-11-25 | A kind of interaction four-axle aircraft |
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| CN207516831U CN207516831U (en) | 2018-06-19 |
| CN207516831U9 true CN207516831U9 (en) | 2019-11-01 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD1001009S1 (en) | 2021-06-09 | 2023-10-10 | Amax Group Usa, Llc | Quadcopter |
| USD1003214S1 (en) | 2021-06-09 | 2023-10-31 | Amax Group Usa, Llc | Quadcopter |
| USD1010004S1 (en) | 2019-11-04 | 2024-01-02 | Amax Group Usa, Llc | Flying toy |
| USD1035787S1 (en) | 2022-06-24 | 2024-07-16 | Amax Group Usa, Llc | Flying toy |
| US12121826B2 (en) | 2020-05-28 | 2024-10-22 | Amax Group Usa, Llc | Hand gesture controlled flying toy |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN211685615U (en) * | 2020-01-03 | 2020-10-16 | 仿翼(北京)科技有限公司 | Flapping wing aircraft |
-
2017
- 2017-11-25 CN CN201721595515.6U patent/CN207516831U9/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD1010004S1 (en) | 2019-11-04 | 2024-01-02 | Amax Group Usa, Llc | Flying toy |
| US12121826B2 (en) | 2020-05-28 | 2024-10-22 | Amax Group Usa, Llc | Hand gesture controlled flying toy |
| USD1001009S1 (en) | 2021-06-09 | 2023-10-10 | Amax Group Usa, Llc | Quadcopter |
| USD1003214S1 (en) | 2021-06-09 | 2023-10-31 | Amax Group Usa, Llc | Quadcopter |
| USD1035787S1 (en) | 2022-06-24 | 2024-07-16 | Amax Group Usa, Llc | Flying toy |
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| Publication number | Publication date |
|---|---|
| CN207516831U (en) | 2018-06-19 |
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Correction item: Claims Correct: Correct False: error Number: 25-01 Page: full text Volume: 34 |
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Effective date of registration: 20201029 Address after: 3 / F, 8 Muling street, Gangzi village, Changping Town, Dongguan City, Guangdong Province Patentee after: Dongguan tesmai Electronic Technology Co.,Ltd. Address before: Changping Zhen Gang Zi Cun Mu Ling Jie 523000 Guangdong city in Dongguan Province, the third floor of No. 8 A Patentee before: DONGGUAN ZHONGQIAN ELECTRONICS Co.,Ltd. |