CN113859559A - Real-time data acquisition system - Google Patents
Real-time data acquisition system Download PDFInfo
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- CN113859559A CN113859559A CN202111168218.4A CN202111168218A CN113859559A CN 113859559 A CN113859559 A CN 113859559A CN 202111168218 A CN202111168218 A CN 202111168218A CN 113859559 A CN113859559 A CN 113859559A
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- 230000001681 protective effect Effects 0.000 claims abstract description 32
- 230000007246 mechanism Effects 0.000 claims abstract description 21
- 238000001125 extrusion Methods 0.000 claims abstract description 5
- 230000006698 induction Effects 0.000 claims description 18
- 230000005540 biological transmission Effects 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 6
- 230000008054 signal transmission Effects 0.000 claims description 5
- 230000002567 autonomic effect Effects 0.000 claims description 3
- 229920002635 polyurethane Polymers 0.000 claims description 3
- 239000004814 polyurethane Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 230000003139 buffering effect Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000872 buffer Substances 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 230000002633 protecting effect Effects 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
- G05D1/0022—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement characterised by the communication link
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The invention discloses a real-time data acquisition system which comprises a machine body, wherein four flying propeller mechanisms are arranged on the outer side of the machine body, protective rings are arranged on the outer sides of the four flying propeller mechanisms, the protective rings are fixedly connected with the machine body, a control module is arranged on the inner side of the machine body, the control module is in signal connection with the flying propeller mechanisms, and an autonomous protective assembly is arranged on the outer side of each protective ring; carry out data acquisition by data acquisition module, preserve the data that data acquisition module collected through first storage module and second storage module, the extrusion of outer guard circle, the outer guard circle cushions once, the motor starts, make the gag lever post rotatory, remove the restriction to the impact plate, make the impact plate can deviate from deviating from the groove, act on the impact, make the impact plate can apply a reaction force and give the impact, the spring cushions simultaneously, the loss that the organism received has been reduced, carry out the secondary protection, it is good to make the organism protective effect, ensure that unmanned aerial vehicle stably carries out data acquisition work.
Description
Technical Field
The invention relates to the technical field of data acquisition protection devices, in particular to a real-time data acquisition system.
Background
Miniature rotor unmanned aerial vehicle observes and controls communication system to ground control system and machine year, and ground control system can monitor and command control to unmanned aerial vehicle's flight gesture, and machine year observes and controls communication system and mainly carries out data acquisition to inertial sensor, ultrasonic ranging appearance etc. under unmanned aerial vehicle flight state to give ground control system to these data transfer.
The unmanned aerial vehicle that has at present uses under some narrow and small tunnel environment, and some can set up protection machanism in the unmanned aerial vehicle outside, and guarantee unmanned aerial vehicle stably carries out data acquisition work, but this layer of protection machanism only plays the effect of buffering, and is lower to the effect of unmanned aerial vehicle protection.
Disclosure of Invention
The present invention is directed to a real-time data acquisition system to solve the above problems.
In order to achieve the purpose, the invention provides the following technical scheme:
a real-time data acquisition system comprises a machine body, wherein four flying propeller mechanisms are arranged on the outer side of the machine body, protective rings are arranged on the outer sides of the four flying propeller mechanisms, the protective rings are fixedly connected with the machine body, a control module is arranged on the inner side of the machine body, the control module is in signal connection with the flying propeller mechanisms, an autonomous protective component is arranged on the outer side of the protective rings, the autonomous protective component comprises an outer protective ring, an impact plate, two fixed sleeves and two motors, connecting rods are connected in the two fixed sleeves in a sliding mode and used for achieving the purpose of positioning, limiting rods are fixedly connected to output ends of the two motors, and the limiting rods are inserted in the impact plate and used for achieving the purpose of limiting; an induction coil is arranged on the outer side of the impact plate, and a proximity sensor corresponding to the induction coil is fixedly connected in the outer protection coil and used for detecting whether the outer protection coil collides or not; the control module is in signal connection with the proximity sensor and the motor.
As a still further scheme of the invention: the internal side of the machine body is provided with a data acquisition module, an information transmission module, a first storage module and a second storage module, the data acquisition module is in signal connection with the control module, and the information transmission module is in signal connection with the first storage module and the second storage module.
As a still further scheme of the invention: the outer protective ring is made of polyurethane, and is provided with a disengaging groove matched with the impact plate.
As a still further scheme of the invention: the two fixed sleeves are fixed in the outer protection ring, the connecting rod is fixed on the impact plate, one end of the connecting rod is fixedly connected with a limiting plate, and the limiting plate slides in the fixed sleeves.
As a still further scheme of the invention: the inner side of the fixed sleeve is provided with a spring, one end of the spring is fixed in the fixed sleeve, and the other end of the spring is fixed on the limiting plate.
As a still further scheme of the invention: the two motors are respectively distributed on the outer sides of the two fixed sleeves, and the motors are fixed in the outer protection ring.
As a still further scheme of the invention: the impact plate is provided with two limiting grooves, the two limiting rods are respectively located in the two limiting grooves, the limiting grooves are provided with two transverse grooves, and the two transverse grooves are respectively communicated with the two limiting grooves.
As a still further scheme of the invention: the number of the proximity sensors is twelve, each proximity sensor is arranged in the outer protection ring, the proximity sensors are uniformly distributed in the outer protection ring, and the induction ring is fixedly connected with the outer protection ring.
As a further aspect of the present invention, a real-time data acquisition system comprises the following steps:
a: the aircraft body takes off under the action of the flight propeller mechanism, data acquisition is carried out by the data acquisition module, data collected by the data acquisition module are stored by the first storage module and the second storage module, and finally, the acquired data information can be transmitted by the information transmission module.
B: at the in-process that the organism plays to fly and carries out data acquisition, if the phenomenon of collision appears, then the action force can be exerted to the outer guard circle to the impactor, outer guard circle extrusion this moment makes the position change of induction coil, contact proximity sensor, proximity sensor receives the signal and gives the motor with signal transmission, the motor starts, make the gag lever post rotatory, relieve the restriction to the impact plate, make the impact plate can deviate from deviating from the groove, act on the impactor, make the impact plate can exert a reaction force and give the impactor, the loss that the organism received has been reduced.
Compared with the prior art, the invention has the beneficial effects that:
1. independently the protection component includes outer guard circle through the setting, the kickboard, two fixed covers and two motors, fly to carry out data acquisition's in-process at the organism, if the phenomenon of collision appears, then the impact can exert the effort to outer guard circle, outer guard circle extrusion this moment, outer guard circle cushions once, make the position change of induction coil, contact proximity sensor, proximity sensor receives the signal and gives the motor with the signal transmission, the motor starts, make the gag lever post rotatory, remove the restriction to the kickboard, make the kickboard deviate from the groove, act on the impact, make the kickboard can exert a reaction force and give the impact, the spring cushions simultaneously, the loss that the organism received has been reduced, carry out the secondary protection, make the organism protecting effect good, guarantee unmanned aerial vehicle stably carries out data acquisition work.
2. Through the fixed cover and the connecting rod that set up, when the impingement plate moved, can slide in fixed cover by the connecting rod, can fix a position the impingement plate position of moving to the impingement plate when not using, can compress in outer guard circle under the effect of spring, did not influence the volume of organism, made the effectual that the device used.
3. Through all being equipped with three proximity sensor in every outer guard circle, three proximity sensor evenly distributed makes proximity sensor distribute in every even position point department of outer guard circle, if outer guard circle atress, easily makes proximity sensor received signal, and the control motor starts, realizes the purpose of autonomic protection.
Drawings
FIG. 1 is a schematic diagram of a real-time data acquisition system;
FIG. 2 is a schematic diagram of the internal structure of a body of a real-time data acquisition system;
FIG. 3 is a system diagram of a real-time data acquisition system;
FIG. 4 is a schematic diagram of an autonomous protective assembly in a real-time data acquisition system;
FIG. 5 is a schematic structural diagram of an outer guard ring in a real-time data acquisition system;
FIG. 6 is a schematic diagram of a stop lever in a real-time data acquisition system;
fig. 7 is a schematic view of the structure inside the stationary sheath of the real-time data acquisition system.
In the figure: 1. a body; 11. a control module; 12. a data acquisition module; 13. an information transmission module; 14. a first storage module; 15. a second storage module; 2. a flight paddle mechanism; 21. a guard ring; 3. an autonomous protective component; 31. an outer guard ring; 311. taking out of the groove; 32. an impact plate; 321. a limiting groove; 322. a transverse groove; 33. fixing a sleeve; 34. a connecting rod; 341. a limiting plate; 35. a spring; 4. an induction coil; 5. a proximity sensor; 6. a motor; 61. a limiting rod.
Detailed Description
Referring to fig. 1 to 7, in the embodiment of the present invention, a real-time data acquisition system includes a machine body 1, four flight propeller mechanisms 2 are disposed outside the machine body 1, guard rings 21 are disposed outside the four flight propeller mechanisms 2, the guard rings 21 are fixedly connected to the machine body 1, a control module 11 is disposed inside the machine body 1, the control module 11 is in signal connection with the flight propeller mechanisms 2, an autonomous protection component 3 is disposed outside the guard rings 21, the autonomous protection component 3 includes an outer guard ring 31, an impact plate 32, two fixed sleeves 33 and two motors 6, a connecting rod 34 is slidably connected in the two fixed sleeves 33 for achieving a positioning purpose, a limiting rod 61 is fixedly connected to output ends of the two motors 6, and the limiting rod 61 is inserted in the impact plate 32 for achieving a limiting purpose; an induction coil 4 is arranged on the outer side of the impact plate 32, and a proximity sensor 5 corresponding to the induction coil 4 is fixedly connected in the outer protection ring 31 and used for detecting whether the outer protection ring 31 collides or not; the control module 11 is in signal connection with the proximity sensor 5 and the motor 6.
In fig. 2 and 3: the inner side of the machine body 1 is provided with a control module 11, the control module 11 is in signal connection with a flight propeller mechanism 2 and is respectively used for controlling the flight and landing of the machine body 1 by opening and closing the flight propeller mechanism 2, the control module 11 is in signal connection with a proximity sensor 5 and a motor 6, the inner side of the machine body 1 is provided with a data acquisition module 12, an information transmission module 13, a first storage module 14 and a second storage module 15, the data acquisition module 12 is in signal connection with the control module 11, the information transmission module 13 is in signal connection with the first storage module 14 and the second storage module 15, the machine body 1 takes off under the action of the flight propeller mechanism 2 and carries out data acquisition by the data acquisition module 12, the data acquired by the data acquisition module 12 is stored by the first storage module 14 and the second storage module 15, and finally the acquired data information can be transmitted by the information transmission module 13, the first storage module 14 and the second storage module 15 can store collected data information, the storage capacity is large, the use effect of the machine body 1 can be improved, and the information transmission module 13 can transmit the data to the ground control system.
In fig. 1, 4, 5, 6 and 7: the outer sides of four flight propeller mechanisms 2 are respectively provided with a protective ring 21, the protective rings 21 are fixedly connected with a machine body 1, the protective rings 21 protect the flight propeller mechanisms 2, the outer sides of the protective rings 21 are provided with an independent protective component 3, the independent protective component 3 comprises an outer protective ring 31, an impact plate 32, two fixed sleeves 33 and two motors 6, the outer protective ring 31 is made of polyurethane, the outer protective ring 31 is provided with a stripping groove 311 matched with the impact plate 32, if the machine body 1 is used, the phenomenon of collision occurs, the outer protective ring 31 can perform primary buffering, the impact plate 32 is stripped from the stripping groove 311 to perform secondary buffering, the connecting rods 34 are respectively and slidably connected in the two fixed sleeves 33 for realizing the positioning purpose, the two fixed sleeves 33 are respectively fixed in the outer protective ring 31, the connecting rods 34 are fixed on the impact plate 32, one end of each connecting rod 34 is fixedly connected with a limiting plate 341, the limiting plate 341 slides in the fixed sleeves 33, the inner side of the fixed sleeve 33 is provided with a spring 35, one end of the spring 35 is fixed in the fixed sleeve 33, the other end of the spring 35 is fixed on the limit plate 341, when the impact plate 32 is separated, the connecting rod 34 can move in the fixed sleeve 33, the limit plate 341 limits the moving position of the connecting rod 34, the connecting rod 34 slides in the fixed sleeve 33, the moving position of the impact plate 32 can be located, the machine body 1 is stably used, the impact plate 32 moves when the spring 35 is reset, namely, the purpose of secondary protection is realized on the machine body 1, and when the impact plate 32 is not used, the impact plate can be compressed in the outer protection ring 31 under the action of the spring 35, the volume of the machine body 1 is not influenced, the using effect of the device is good, the number of the proximity sensors 5 is twelve, three proximity sensors 5 are arranged in each outer protection ring 31, the three proximity sensors 5 are uniformly distributed in the outer protection ring 31, and the induction ring 4 is fixedly connected with the outer protection ring 31, an induction coil 4 is arranged on the outer side of the impact plate 32, the induction coil 4 is made of elastic materials, and a proximity sensor 5 corresponding to the induction coil 4 is fixedly connected in the outer protection ring 31 and used for detecting whether the outer protection ring 31 collides or not; the control module 11 is in signal connection with the proximity sensors 5 and the motors 6, the proximity sensors 5 are used for receiving signals and feeding the signals back to the motors 6, so that the motors 6 are started when the motors 6 need to be used, three proximity sensors 5 are arranged in each outer protection ring 31, the three proximity sensors 5 are uniformly distributed in the outer protection ring 31, the proximity sensors 5 are distributed at each uniform position of the outer protection ring 31, if the outer protection ring 31 is stressed, the proximity sensors 5 are easy to receive the signals, the motors 6 are controlled to be started, the purpose of autonomous protection is realized, the output ends of the two motors 6 are fixedly connected with limit rods 61, the limit rods 61 are inserted in the impact plate 32 and used for realizing the purpose of limiting, the two motors 6 are respectively distributed outside the two fixed sleeves 33, the motors 6 are fixed in the outer protection ring 31, the impact plate 32 is provided with two limit grooves 321, the two limiting rods 61 are respectively positioned in the two limiting grooves 321, the limiting grooves 321 are provided with two transverse grooves 322, the two transverse grooves 322 are respectively communicated with the two limiting grooves 321, when the motor 6 is started, the limiting rods 61 can rotationally move out of the limiting grooves 321, when the connecting rod 34 corresponds to the transverse grooves 322, the limiting rods 61 remove the limitation on the impact plate 32, the impact plate 32 can be separated from the separating grooves 311 and acts on an impact object, the impact plate 32 can apply a reaction force to the impact object, meanwhile, the spring 35 buffers, the loss of the machine body 1 is reduced, secondary protection is performed, the protection effect of the machine body 1 is good, the data acquisition work of the unmanned aerial vehicle is guaranteed, when the impact plate 32 retracts, the limiting rods 61 are rotated into the limiting grooves 321 to limit the position of the impact plate 32, and simultaneously, the impact plate 32 can be stably positioned in the outer protection ring 31 under the action of the spring 35, the impact plate 32 is hidden in the outer protective ring 31, the volume of the machine body 1 is not affected, and the transportation and carrying of the machine body 1 are facilitated.
As shown in fig. 1 to 7, the present invention further provides a method for using a real-time data acquisition system, which comprises the following specific steps:
a: the aircraft body 1 takes off under the action of the flight oar mechanism 2, data acquisition is carried out by the data acquisition module 12, data collected by the data acquisition module 12 are stored by the first storage module 14 and the second storage module 15, and finally, the acquired data information can be transmitted by the information transmission module 13.
B: in-process that takes off at organism 1 and carry out data acquisition, if the phenomenon of collision appears, then the action force can be applyed to outer guard circle 31 to the rammer, outer guard circle 31 extrusion this moment, make the position change of induction coil 4, contact proximity sensor 5, proximity sensor 5 receives the signal and gives motor 6 with signal transmission, motor 6 starts, make gag lever post 61 rotatory, remove the restriction to impact plate 32, make impact plate 32 can deviate from deviating from groove 311, act on the rammer, make impact plate 32 can apply a reaction force and give the rammer, the loss that organism 1 received has been reduced.
The working principle of the invention is as follows: when the airplane body takes off for data acquisition, the impact object can apply acting force on the outer protective ring 31 if a collision phenomenon occurs in the process of taking off the airplane body 1 for data acquisition, the outer protective ring 31 is extruded at the moment, the outer protective ring 31 is buffered for one time, so that the position of the induction ring 4 is changed and the airplane body contacts the proximity sensor 5, proximity sensor 5 receives the signal and gives motor 6 with the signal transmission, motor 6 starts, it is rotatory to drive gag lever post 61, make gag lever post 61 can rotary motion go out spacing groove 321, when connecting rod 34 corresponds with transverse groove 322, gag lever post 61 removes the restriction to impact plate 32, make impact plate 32 deviate from separating from groove 311 under the effect of spring 35, act on the rammer, make impact plate 32 can apply a reaction force for the rammer, spring 35 cushions simultaneously, the loss that organism 1 received has been reduced, carry out secondary protection, make organism 1 protect effectually, when impact plate 32 retracts, rotate gag lever post 61 to in the spacing groove 321, the position of impact plate 32 is being restricted, simultaneously under the effect of spring 35, can make impact plate 32 stable being located outer guard circle 31, can not influence the volume of organism 1.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention are equivalent to or changed within the technical scope of the present invention.
Claims (9)
1. The utility model provides a real-time data acquisition system, includes organism (1), the organism (1) outside is equipped with four flight oar mechanisms (2), four the flight oar mechanism (2) outside all is equipped with guard ring (21), guard ring (21) with organism (1) fixed connection, organism (1) inboard is equipped with control module (11), control module (11) with flight oar mechanism (2) signal connection, its characterized in that, the guard ring (21) outside is equipped with autonomic protection component (3), autonomic protection component (3) include outer guard ring (31), impingement plate (32), two fixed covers (33) and two motors (6), two equal sliding connection has connecting rod (34) in fixed cover (33) for realize the purpose of location, two equal fixedly connected with gag lever post (61) of motor (6) output, the limiting rod (61) is inserted into the impact plate (32) and used for limiting;
an induction coil (4) is arranged on the outer side of the impact plate (32), and a proximity sensor (5) corresponding to the induction coil (4) is fixedly connected in the outer protection coil (31) and is used for detecting whether the outer protection coil (31) collides or not;
the control module (11) is in signal connection with the proximity sensor (5) and the motor (6).
2. A real-time data acquisition system according to claim 1, wherein a data acquisition module (12), an information transmission module (13), a first storage module (14) and a second storage module (15) are arranged inside the machine body (1), the data acquisition module (12) is in signal connection with the control module (11), and the information transmission module (13) is in signal connection with the first storage module (14) and the second storage module (15).
3. The real-time data acquisition system according to claim 1, wherein the outer protective ring (31) is made of polyurethane, and the outer protective ring (31) is provided with a release groove (311) matched with the impact plate (32).
4. A real-time data acquisition system according to claim 1, wherein both said covers (33) are fixed inside said outer shield (31), and said connecting rod (34) is fixed on said impact plate (32), and one end of said connecting rod (34) is fixedly connected with a limit plate (341), and said limit plate (341) slides inside said covers (33).
5. A real-time data acquisition system according to claim 4, wherein a spring (35) is arranged inside the fixed sleeve (33), one end of the spring (35) is fixed in the fixed sleeve (33), and the other end of the spring (35) is fixed on the limit plate (341).
6. A real-time data acquisition system according to claim 1, characterized in that said two motors (6) are respectively distributed outside said two fixed housings (33) and said motors (6) are fixed inside said outer protective ring (31).
7. The real-time data acquisition system according to claim 1, wherein the impact plate (32) is provided with two limiting grooves (321), the two limiting rods (61) are respectively located in the two limiting grooves (321), the limiting grooves (321) are provided with two transverse grooves (322), and the two transverse grooves (322) are respectively communicated with the two limiting grooves (321).
8. A real-time data acquisition system according to claim 1, wherein the number of the proximity sensors (5) is twelve, three proximity sensors (5) are arranged in each outer guard ring (31), the three proximity sensors (5) are uniformly distributed in the outer guard ring (31), and the induction ring (4) is fixedly connected with the outer guard ring (31).
9. A real-time data acquisition system according to any one of claims 1 to 8, wherein: the using steps are as follows:
a: the aircraft body (1) takes off under the action of the flight propeller mechanism (2), data acquisition is carried out by the data acquisition module (12), data collected by the data acquisition module (12) are stored by the first storage module (14) and the second storage module (15), and finally, the acquired data information can be transmitted by the information transmission module (13);
b: in the process of taking off and carrying out data acquisition at organism (1), if the phenomenon of collision appears, then the acting force can be applyed to outer guard circle (31) to the rammer, outer guard circle (31) extrusion this moment, make the position change of induction coil (4), contact proximity sensor (5), proximity sensor (5) receive the signal and give motor (6) with the signal transmission, motor (6) start, make gag lever post (61) rotatory, remove the restriction to impact plate (32), make impact plate (32) can deviate from disengagement groove (311), act on the rammer, make impact plate (32) can apply a reaction force for the rammer, the loss that organism (1) received has been reduced.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111168218.4A CN113859559A (en) | 2021-10-08 | 2021-10-08 | Real-time data acquisition system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111168218.4A CN113859559A (en) | 2021-10-08 | 2021-10-08 | Real-time data acquisition system |
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| Publication Number | Publication Date |
|---|---|
| CN113859559A true CN113859559A (en) | 2021-12-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111168218.4A Withdrawn CN113859559A (en) | 2021-10-08 | 2021-10-08 | Real-time data acquisition system |
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| CN (1) | CN113859559A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802783A (en) * | 2022-03-01 | 2022-07-29 | 东莞市酷得智能科技有限公司 | Intelligent anti-collision unmanned aerial vehicle |
-
2021
- 2021-10-08 CN CN202111168218.4A patent/CN113859559A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802783A (en) * | 2022-03-01 | 2022-07-29 | 东莞市酷得智能科技有限公司 | Intelligent anti-collision unmanned aerial vehicle |
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Application publication date: 20211231 |
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