CN204399477U - Adsorbable multifunction micro flight instruments - Google Patents
Adsorbable multifunction micro flight instruments Download PDFInfo
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- CN204399477U CN204399477U CN201420758856.0U CN201420758856U CN204399477U CN 204399477 U CN204399477 U CN 204399477U CN 201420758856 U CN201420758856 U CN 201420758856U CN 204399477 U CN204399477 U CN 204399477U
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Abstract
The utility model discloses a kind of adsorbable multifunction micro flight instruments, comprise body, rotor, vacuum pump, upper suction tray, side suction tray, side draught supporting leg, solar panel, camera, control module and remote manipulator, wherein rotor is connected with body by bracing frame, rotor orders about motion by motor, upper suction tray is located on the panel on body top, side suction tray is connected with body by sucker stand, vacuum pump is located at the below of body, vacuum pump is connected with upper suction tray and side suction tray by pipeline, vacuum pump is exhausted upper suction tray and side suction tray, the upper end of side draught supporting leg is connected with body, side draught supporting leg is connected with steering wheel, by the folding of servos control side draught supporting leg, beneficial effect: the work of detection and examination time expand making aircraft, economize energy, can be applicable to dual-use field, actual application value is large.
Description
Technical field
The utility model relates to a kind of flight instruments, particularly the adsorbable multifunction micro flight instruments of one.
Background technology
At present, a series of fields such as public sphere safety, national defense safety, Environmental security and dangerous operation make majority state in the world more and more pay attention to airflight device, especially micro-miniaturisation, intelligentized flight instruments, research and develop many moneys flight instruments both at home and abroad, such as, the fly flying robot of Harvard University's development; The novel flying robot of one of Lausanne, SUI federal Institute of Technology exploitation; Canada Company develops a flying robot being named as " scouter "; A kind of can the flight in the sky that Shenyang Inst of Automation, Chinese Academy of Sciences develops simultaneously can the snake-shaped robot of shape in mapping ensemble, and this robot can use common automobile gasoline, 70 kilometers per hour of scooter time the fastest.
Although have developed many moneys airflight device both at home and abroad, be generally used in multiple field, there are following problems:
1, structure design is unreasonable, some the two is only integrated by climbing robot and flying robot on hardware, and have ignored uniting two into one functionally, makes the structure distribution of flying robot unreasonable, can not reach corresponding using function;
2, the physical construction of similar adsorbable flight instruments when side draught is fixed sturcture, cause the oversize of aircraft, center-of-gravity regulating balance difficulties, cause mechanism stressed unreasonable, and be a support in support place, cause the problem that there will be structural instability when wall adsorption;
3, common absorption flying machine man-hour, its electricity expended cannot supplement immediately, if electricity exhausts, cannot continue to use;
4, existing most flying robot mainly utilizes people for remote manipulation, and main view flight attitude and the flight surrounding environment relying on people, significantly limit the flight range of flying robot;
5, existing adsorbable flying robot is when adsorbing, and in order to keep adsorption affinity can expend electricity always, reason does not consider that adsorption plant there is no need to work always.
Summary of the invention
Main purpose of the present utility model is to solve the more problem that existing micro air device in use exists and the adsorbable multifunction micro flight instruments of one provided.
The adsorbable multifunction micro flight instruments that the utility model provides comprises body, rotor, vacuum pump, upper suction tray, side suction tray, side draught supporting leg, solar panel, camera, control module and remote manipulator, wherein rotor is connected with body by bracing frame, rotor orders about motion by motor, upper suction tray is located on the panel on body top, side suction tray is connected with body by sucker stand, vacuum pump is located at the below of body, vacuum pump is connected with upper suction tray and side suction tray by pipeline, vacuum pump is exhausted upper suction tray and side suction tray, the upper end of side draught supporting leg is connected with body, side draught supporting leg is connected with steering wheel, by the folding of servos control side draught supporting leg, on the panel that camera is installed in body top respectively and sucker stand, solar panel is around on the support body of body, solar panel provides electric power to the single chip control module in control module and vacuum pump, control module is located in the support body inner chamber of body, order about the motor of rotor, order about the steering wheel of side draught supporting leg, vacuum pump and camera control work by control module, remote manipulator instruction control module works.
Rotor is provided with four, is equipped with alighting gear below each rotor.
The bracing frame that rotor is connected with body is provided with electronic governor, and electronic governor is connected with the motor ordering about rotor, and electronic governor controls the work of motor.
The flat board of side draught supporting leg end is fixed with cohesive material.
Vacuum pump, upper suction tray and side suction tray composition adsorption plant, vacuum pump is connected with upper suction tray and side suction tray respectively by pipeline, connecting line is provided with the first electromagnetic valve, second electromagnetic valve and the first relay, connecting line is also provided with the first check valve and the second check valve, single chip control module in control module is connected with vacuum pump by circuit, connection line is provided with the second relay, single chip control module controls the first relay and the second relay instruction first electromagnetic valve and the second electromagnetic valve folding, thus control vacuum pump, the work of upper suction tray and side suction tray.
Control module includes single chip control module, fly control plate and wireless digital transmission module, wherein wireless digital transmission module respectively with fly to control plate and single chip control module is connected, fly to control plate be connected with the steering wheel controlling the folding of side draught supporting leg and control the work of steering wheel, fly control plate and control single chip control module control adsorption plant work while steering wheel drives side draught supporting leg to run, single chip control module respectively with the baroceptor in upper suction tray and side suction tray, multifunction detecting module is connected with vacuum pump, single chip control module controls baroceptor, the work of multifunction detecting module and vacuum pump, multifunction detecting module is connected to Temperature Humidity Sensor, Smoke Sensor and dust degree sensor.
Body is also provided with remote control, remote control comprises camera, telltale, remote manipulator, Infrared remote controller, wireless video transmission module and image pick-up card, wherein remote manipulator controls the flight of body, the work of absorption and camera, camera can be real-time transmitted to wireless video transmission module image under the instruction of remote manipulator, wireless video transmission module is real-time transmitted to image pick-up card the information received, image pick-up card is shown the information received in real time by telltale, the work of the wireless digital transmission module in Infrared remote controller instruction control module.
Principle of work of the present utility model:
Send order with the matching used remote manipulator of the utility model to the flight instruments that the utility model provides and realize the control of airflight attitude and the function of multi-faceted absorption, described in specific as follows:
Flying in control module is controlled plate and is used for the state of kinematic motion of perception flight instruments and attitude.Flying to control plate drives steering wheel to realize the flexible of side draught supporting leg.Baroceptor is placed in suction tray and side suction tray the pressure measured in suction tray and side suction tray, and is transferred in single chip control module by pressure data signal.Single chip control module controls vacuum pump, for realizing multi-faceted adsorption function.Multifunction detecting module is driven by single chip control module and surveyed data is sent to upper computer through wireless digital transmission module.
When steering wheel is in initial position, side draught supporting leg is in contraction state, and when opening side draught function, remote manipulator sends signal control steering wheel and rotates 90 degree, and now side draught supporting leg launches, thus near vertical wall.Side draught function needs to be realized by side draught supporting leg.The side draught functional realiey step of flight instruments is as follows: when flight instruments is near vertical metope, signal is sent by Infrared remote controller, single chip control module controls the first relay and the second relay makes the first electromagnetic valve and the second electromagnetic valve action, first electromagnetic valve connects side suction tray and vacuum pump, and second electromagnetic valve makes suction tray communicate with air thus realize the pressure release at top simultaneously.Operator manipulation remote manipulator, makes steering wheel rotate 90 °, becomes state straight down.Make flight instruments become horizontal attitude, thus make flight instruments stay in vertical wall, now operator controls rotor motor stalling.
Flight instruments is drawn through journey performing step as follows:
When inhaling on flight instruments needs, wall above operator control flight instruments upwards flies.Send start signal by Infrared remote controller to vacuum pump simultaneously, wireless digital transmission module is sent to single chip control module process after receiving signal, single chip control module I/O mouth controls the first relay and the second relay closes, vacuum pump is connected main power source and is started working, and realizes air suction function.When upper suction tray touches upper wall surface, upper suction tray inside starts to reach negative pressure, and whole flight instruments will be close to wall, and now operator remote manipulator sends signal control rotor motor stalling.When whole flight instruments is in adsorbed state, multifunction detecting module is started working.Multifunction detecting model calling has multiple sensors, comprises DHT11 type Temperature Humidity Sensor module, MQ-2 smog degree sensor, Japanese Sharp GP2Y1010AU0F dust degree sensor.All the sensors is driven by single chip control module and reads surveyed data, is sent to telltale by over-over mode.Thus the functions such as aerial temperature and humidity measurement, fire alarm, environmental quality monitoring can be realized.
The Batch Adsorption functional realiey step of flight instruments during being adsorbed in wall is: by calculating, obtain the air pressure higher limit of suction tray inside, side when flight instruments can reliably adsorb.During stable absorption, the atmospheric pressure value in the suction tray of side is less than this higher limit, now can close vacuum pump.In the process of absorption, baroceptor is equipped with in suction tray inside, side, and baroceptor is driven by single chip control module and reads data.Because gas circuit end is equipped with the first check valve and the second check valve, then only have suction tray inner gas leakage in side that side suction tray air pressure inside value can be caused to raise gradually.When reaching the higher limit of setting, single chip control module exports control signal and opens vacuum pump, thus offside suction tray is exhausted and makes the atmospheric pressure value of suction tray inside, side decline, when lower than certain setting value less than higher limit, single chip control module exports control signal and vacuum-pump power supply is disconnected, and vacuum pump stops extracting air.The function according to the absorption of side suction tray inner air atmospheric pressure value automatic intermittent is realized with this, thus greatly reduce the running time of vacuum pump, and then the consumption of current of vacuum pump is significantly reduced, to save more electricity to be supplied to arrangement for detecting and control system, the time of work of detection and examination is finally made significantly to extend.
The beneficial effects of the utility model:
1, have employed supporting leg mechanism during the utility model side draught, improve stability during side draught, in addition, before realizing side draught function, keep the contraction state of supporting leg, which enhance the disguise of flight;
2, the utility model makes full use of solar power, makes the work of detection and examination time expand of aircraft, economize energy;
3, the utility model have employed batchwise adsorption pattern in absorption detecting process, considerably increases the lasting detecting ability of aircraft;
4, the utility model flying robot is based on four rotors, flight stability, and simultaneously with image real-time transmission system, can realize not controlling and detecting in operator's long-distance flight within the vision, can be applicable to dual-use field, actual application value is large.
Accompanying drawing explanation
Fig. 1 is the utility model integral structure schematic diagram.
Fig. 2 is the utility model local structure schematic diagrams.
Fig. 3 is adsorption plant structural representation described in the utility model.
Fig. 4 is control module structured flowchart described in the utility model.
Fig. 5 is remote control structured flowchart described in the utility model.
1, body 2, rotor 3, vacuum pump 4, upper suction tray 5, side suction tray
6, side draught supporting leg 7, solar panel 8, camera 9, control module
10, remote manipulator 11, bracing frame 12, motor 13, panel 14, sucker stand
15, steering wheel 16, alighting gear 17, electronic governor 20, first electromagnetic valve 21, second electromagnetic valve
22, the first relay 23, first check valve 24, second check valve 25, second relay
30, single chip control module 31, fly control plate 32, wireless digital transmission module
33, baroceptor 34, multifunction detecting module 35, Temperature Humidity Sensor
36, Smoke Sensor 37, dust degree sensor 40, telltale
41, Infrared remote controller 42, wireless video transmission module 43, image pick-up card.
Detailed description of the invention
Refer to shown in Fig. 1, Fig. 2, Fig. 3, Fig. 4 and Fig. 5:
The adsorbable multifunction micro flight instruments that the utility model provides comprises body 1, rotor 2, vacuum pump 3, upper suction tray 4, side suction tray 5, side draught supporting leg 6, solar panel 7, camera 8, control module 9 and remote manipulator 10, wherein rotor 2 is connected with body 1 by bracing frame 11, rotor 2 orders about motion by motor 12, upper suction tray 4 is located on the panel 13 on body 1 top, side suction tray 5 is connected with body 1 by sucker stand 14, vacuum pump 3 is located at the below of body 1, vacuum pump 3 is connected with upper suction tray 4 and side suction tray 5 by pipeline, vacuum pump 3 is exhausted upper suction tray 4 and side suction tray 5, the upper end of side draught supporting leg 6 is connected with body 1, side draught supporting leg 6 is connected with steering wheel 15, the folding of side draught supporting leg 6 is controlled by steering wheel 15, on the panel 13 that camera 8 is installed in body 1 top respectively and sucker stand 14, solar panel 7 is around on the support body of body 1, solar panel 7 is around on the support body of body 1, solar panel 7 provides electric power to the single chip control module 30 in control module 9 and vacuum pump 3, control module 9 is located in the support body inner chamber of body 1, order about the motor 12 of rotor 2, order about the steering wheel 15 of side draught supporting leg 6, vacuum pump 3 and camera 8 control work by control module 9, remote manipulator 10 instruction control module 9 works.
Rotor 2 is provided with four, is equipped with alighting gear 16 below each rotor 2.
The bracing frame 11 that rotor 2 is connected with body 1 is provided with electronic governor 17, and electronic governor 17 is connected with the motor 12 ordering about rotor 2, and electronic governor 17 controls the work of motor 12.
The flat board of side draught supporting leg 6 end is fixed with cohesive material.
Vacuum pump 3, upper suction tray 4 and side suction tray 5 form adsorption plant, vacuum pump 3 is connected with upper suction tray 4 and side suction tray 5 respectively by pipeline, connecting line is provided with the first electromagnetic valve 20, second electromagnetic valve 21 and the first relay 22, connecting line is also provided with the first check valve 23 and the second check valve 24, single chip control module 30 in control module 9 is connected with vacuum pump 3 by circuit, connection line is provided with the second relay 25, single chip control module 30 controls the first relay 22 and the second relay 25 instruction first electromagnetic valve 20 and the second electromagnetic valve 21 folding, thus control vacuum pump 3, the work of upper suction tray 4 and side suction tray 5.
Control module 9 includes single chip control module 30, fly control plate 31 and wireless digital transmission module 32, wherein wireless digital transmission module 32 respectively with fly to control plate 31 and single chip control module 30 is connected, fly to control plate 31 be connected with the steering wheel 15 controlling the folding of side draught supporting leg 6 and control the work of steering wheel 15, fly control plate 31 control steering wheel 15 drive side draught supporting leg 6 run while single chip control module 30 control adsorption plant work, single chip control module 30 respectively with the baroceptor 33 in upper suction tray 4 and side suction tray 5, multifunction detecting module 34 is connected with vacuum pump 3, single chip control module 30 controls baroceptor 33, the work of multifunction detecting module 34 and vacuum pump 3, multifunction detecting module 34 is connected to Temperature Humidity Sensor 35, Smoke Sensor 36 and dust degree sensor 37.
Body 1 is also provided with remote control, remote control comprises camera 8, telltale 40, remote manipulator 10, Infrared remote controller 41, wireless video transmission module 42 and image pick-up card 43, wherein remote manipulator 10 controls the flight of body 1, the work of absorption and camera 8, camera 8 can be real-time transmitted to wireless video transmission module 42 image under the instruction of remote manipulator 10, wireless video transmission module 42 is real-time transmitted to image pick-up card 43 the information received, image pick-up card 43 is shown the information received in real time by telltale 40, the work of the wireless digital transmission module 32 in Infrared remote controller 41 instruction control module 9.
Principle of work of the present utility model:
Send order with the matching used remote manipulator of the utility model 10 to the flight instruments that the utility model provides and realize the control of airflight attitude and the function of multi-faceted absorption, described in specific as follows:
Flying in control module 9 is controlled plate 31 and is used for the state of kinematic motion of perception flight instruments and attitude.Flying to control plate 31 drives steering wheel 15 to realize the flexible of side draught supporting leg 6.Baroceptor 33 is placed in suction tray 4 and side suction tray 5 pressure measured in suction tray 4 and side suction tray 5, and is transferred in single chip control module 30 by pressure data signal.Single chip control module 30 controls vacuum pump 3, for realizing multi-faceted adsorption function.Multifunction detecting module 34 is driven by single chip control module 30 and surveyed data is sent to upper computer through wireless digital transmission module 32.
When steering wheel 15 is in initial position, side draught supporting leg 6 is in contraction state, and when opening side draught function, remote manipulator 10 sends signal control steering wheel 15 and rotates 90 degree, and now side draught supporting leg 6 launches, thus near vertical wall.Side draught function needs to be realized by side draught supporting leg 6.The side draught functional realiey step of flight instruments is as follows: when flight instruments is near vertical metope, signal is sent by Infrared remote controller 41, single chip control module 30 controls the first relay 22 and the second relay 25 makes the first electromagnetic valve 20 and the second electromagnetic valve 21 action, first electromagnetic valve 20 connects side suction tray 5 and vacuum pump 3, and second electromagnetic valve 21 makes suction tray 4 communicate with air thus realize the pressure release at top simultaneously.Operator manipulation remote manipulator 10, makes steering wheel 15 rotate 90 °, becomes state straight down.Make flight instruments become horizontal attitude, thus make flight instruments stay in vertical wall, now operator controls motor 12 stall of rotor 2.
Flight instruments is drawn through journey performing step as follows:
When inhaling on flight instruments needs, wall above operator control flight instruments upwards flies.Send start signal to vacuum pump 3 by Infrared remote controller 41 simultaneously, wireless digital transmission module 32 is sent to single chip control module 30 and is processed after receiving signal, single chip control module 30I/O mouth controls the first relay 22 and the second relay 25 closes, vacuum pump 3 is connected main power source and is started working, and realizes air suction function.When upper suction tray 4 touches upper wall surface, upper suction tray 4 inside starts to reach negative pressure, and whole flight instruments will be close to wall, and now operator remote manipulator 10 sends motor 12 stall of signal control rotor 2.When whole flight instruments is in adsorbed state, multifunction detecting module 34 is started working.Multifunction detecting module 34 is connected with multiple sensors, comprises DHT11 type Temperature Humidity Sensor 35 module, MQ-2 Smoke Sensor 36, Japanese Sharp GP2Y1010AU0F dust degree sensor 37 etc.All the sensors is driven by single chip control module 30 and reads surveyed data, is sent to telltale 40 by over-over mode.Thus the functions such as aerial temperature and humidity measurement, fire alarm, environmental quality monitoring can be realized.
The Batch Adsorption functional realiey step of flight instruments during being adsorbed in wall is: by calculating, obtain the air pressure higher limit of suction tray 5 inside in side when flight instruments can reliably adsorb.During stable absorption, the atmospheric pressure value in side suction tray 5 is less than this higher limit, now can close vacuum pump 3.In the process of absorption, baroceptor 33 is equipped with in side suction tray 5 inside, and baroceptor 33 is driven by single chip control module 30 and reads data.Because gas circuit end is equipped with the first check valve 23 and the second check valve 24, then only have the inner gas leakage of side suction tray 5 that side suction tray 5 air pressure inside value can be caused to raise gradually.When reaching the higher limit of setting, single chip control module 30 exports control signal and opens vacuum pump 3, thus offside suction tray 5 is exhausted and makes the atmospheric pressure value of side suction tray 5 inside decline, when lower than certain setting value less than higher limit, single chip control module 30 exports control signal and is disconnected by vacuum pump 3 power supply, and vacuum pump 3 stops extracting air.The function according to the absorption of side suction tray 5 inner air atmospheric pressure value automatic intermittent is realized with this, thus greatly reduce the running time of vacuum pump 3, and then the consumption of current of vacuum pump 3 is significantly reduced, to save more electricity to be supplied to arrangement for detecting and control system, the time of work of detection and examination is finally made significantly to extend.
Claims (7)
1. an adsorbable multifunction micro flight instruments, it is characterized in that: comprise body, rotor, vacuum pump, upper suction tray, side suction tray, side draught supporting leg, solar panel, camera, control module and remote manipulator, wherein rotor is connected with body by bracing frame, rotor orders about motion by motor, upper suction tray is located on the panel on body top, side suction tray is connected with body by sucker stand, vacuum pump is located at the below of body, vacuum pump is connected with upper suction tray and side suction tray by pipeline, vacuum pump is exhausted upper suction tray and side suction tray, the upper end of side draught supporting leg is connected with body, side draught supporting leg is connected with steering wheel, by the folding of servos control side draught supporting leg, on the panel that camera is installed in body top respectively and sucker stand, solar panel is around on the support body of body, solar panel provides electric power to the single chip control module in control module and vacuum pump, control module is located in the support body inner chamber of body, order about the motor of rotor, order about the steering wheel of side draught supporting leg, vacuum pump and camera control work by control module, remote manipulator instruction control module works.
2. the adsorbable multifunction micro flight instruments of one according to claim 1, is characterized in that: described rotor is provided with four, is equipped with alighting gear below each rotor.
3. the adsorbable multifunction micro flight instruments of one according to claim 1, it is characterized in that: the bracing frame that described rotor is connected with body is provided with electronic governor, electronic governor is connected with the motor ordering about rotor, and electronic governor controls the work of motor.
4. the adsorbable multifunction micro flight instruments of one according to claim 1, is characterized in that: the flat board of described side draught supporting leg end is fixed with cohesive material.
5. the adsorbable multifunction micro flight instruments of one according to claim 1, it is characterized in that: described vacuum pump, upper suction tray and side suction tray composition adsorption plant, vacuum pump is connected with upper suction tray and side suction tray respectively by pipeline, connecting line is provided with the first electromagnetic valve, second electromagnetic valve and the first relay, connecting line is also provided with the first check valve and the second check valve, single chip control module in control module is connected with vacuum pump by circuit, connection line is provided with the second relay, single chip control module controls the first relay and the second relay instruction first electromagnetic valve and the second electromagnetic valve folding, thus control vacuum pump, the work of upper suction tray and side suction tray.
6. the adsorbable multifunction micro flight instruments of one according to claim 1, it is characterized in that: described control module includes single chip control module, fly control plate and wireless digital transmission module, wherein wireless digital transmission module respectively with fly to control plate and single chip control module is connected, fly to control plate be connected with the steering wheel controlling the folding of side draught supporting leg and control the work of steering wheel, fly control plate and control single chip control module control adsorption plant work while steering wheel drives side draught supporting leg to run, single chip control module respectively with the baroceptor in upper suction tray and side suction tray, multifunction detecting module is connected with vacuum pump, single chip control module controls baroceptor, the work of multifunction detecting module and vacuum pump, multifunction detecting module is connected to Temperature Humidity Sensor, Smoke Sensor and dust degree sensor.
7. the adsorbable multifunction micro flight instruments of one according to claim 1, it is characterized in that: described body is also provided with remote control, remote control comprises camera, telltale, remote manipulator, Infrared remote controller, wireless video transmission module and image pick-up card, wherein remote manipulator controls the flight of body, the work of absorption and camera, camera can be real-time transmitted to wireless video transmission module image under the instruction of remote manipulator, wireless video transmission module is real-time transmitted to image pick-up card the information received, image pick-up card is shown the information received in real time by telltale, the work of the wireless digital transmission module in Infrared remote controller instruction control module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201420758856.0U CN204399477U (en) | 2014-12-04 | 2014-12-04 | Adsorbable multifunction micro flight instruments |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420758856.0U CN204399477U (en) | 2014-12-04 | 2014-12-04 | Adsorbable multifunction micro flight instruments |
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| CN204399477U true CN204399477U (en) | 2015-06-17 |
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| CN201420758856.0U Withdrawn - After Issue CN204399477U (en) | 2014-12-04 | 2014-12-04 | Adsorbable multifunction micro flight instruments |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104443391A (en) * | 2014-12-04 | 2015-03-25 | 吉林大学 | Adsorbable multifunctional micro flight device |
| CN105527382A (en) * | 2016-01-05 | 2016-04-27 | 杭州潮流玩具有限公司 | Flyable air detection equipment and mobile terminal applying flyable air detection equipment |
| CN105539825A (en) * | 2015-12-30 | 2016-05-04 | 天津皓新艺科技有限公司 | Monitoring air vehicle |
| CN105905288A (en) * | 2016-04-27 | 2016-08-31 | 中国电子科技集团公司第二十八研究所 | Bionic suspension-based energy-saving multi-rotor unmanned aerial vehicle device |
| CN110329495A (en) * | 2019-06-28 | 2019-10-15 | 杭州电子科技大学 | A kind of unmanned plane absorption stop device and its parking scheme |
-
2014
- 2014-12-04 CN CN201420758856.0U patent/CN204399477U/en not_active Withdrawn - After Issue
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104443391A (en) * | 2014-12-04 | 2015-03-25 | 吉林大学 | Adsorbable multifunctional micro flight device |
| CN104443391B (en) * | 2014-12-04 | 2016-05-18 | 吉林大学 | Adsorbable multifunction micro flight instruments |
| CN105539825A (en) * | 2015-12-30 | 2016-05-04 | 天津皓新艺科技有限公司 | Monitoring air vehicle |
| CN105527382A (en) * | 2016-01-05 | 2016-04-27 | 杭州潮流玩具有限公司 | Flyable air detection equipment and mobile terminal applying flyable air detection equipment |
| CN105527382B (en) * | 2016-01-05 | 2018-03-02 | 杭州潮流玩具有限公司 | A kind of fly able air detection equipment and use its mobile terminal |
| CN105905288A (en) * | 2016-04-27 | 2016-08-31 | 中国电子科技集团公司第二十八研究所 | Bionic suspension-based energy-saving multi-rotor unmanned aerial vehicle device |
| CN105905288B (en) * | 2016-04-27 | 2018-03-06 | 中国电子科技集团公司第二十八研究所 | A kind of energy-conservation multi-rotor unmanned aerial vehicle device based on bionical suspension |
| CN110329495A (en) * | 2019-06-28 | 2019-10-15 | 杭州电子科技大学 | A kind of unmanned plane absorption stop device and its parking scheme |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20150617 Effective date of abandoning: 20160518 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |