CN112644685B - Power equipment RFID code recognition unmanned aerial vehicle - Google Patents

Power equipment RFID code recognition unmanned aerial vehicle Download PDF

Info

Publication number
CN112644685B
CN112644685B CN202011621322.XA CN202011621322A CN112644685B CN 112644685 B CN112644685 B CN 112644685B CN 202011621322 A CN202011621322 A CN 202011621322A CN 112644685 B CN112644685 B CN 112644685B
Authority
CN
China
Prior art keywords
aerial vehicle
unmanned aerial
limiting
identification
antenna
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202011621322.XA
Other languages
Chinese (zh)
Other versions
CN112644685A (en
Inventor
李小玉
贾伯岩
马天祥
景皓
张姿姿
段昕
贾静然
李丹
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
State Grid Corp of China SGCC
Electric Power Research Institute of State Grid Hebei Electric Power Co Ltd
State Grid Hebei Energy Technology Service Co Ltd
Original Assignee
State Grid Corp of China SGCC
Electric Power Research Institute of State Grid Hebei Electric Power Co Ltd
State Grid Hebei Energy Technology Service Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by State Grid Corp of China SGCC, Electric Power Research Institute of State Grid Hebei Electric Power Co Ltd, State Grid Hebei Energy Technology Service Co Ltd filed Critical State Grid Corp of China SGCC
Priority to CN202011621322.XA priority Critical patent/CN112644685B/en
Publication of CN112644685A publication Critical patent/CN112644685A/en
Application granted granted Critical
Publication of CN112644685B publication Critical patent/CN112644685B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06K—GRAPHICAL DATA READING; PRESENTATION OF DATA; RECORD CARRIERS; HANDLING RECORD CARRIERS
    • G06K7/00—Methods or arrangements for sensing record carriers, e.g. for reading patterns
    • G06K7/10—Methods or arrangements for sensing record carriers, e.g. for reading patterns by electromagnetic radiation, e.g. optical sensing; by corpuscular radiation
    • G06K7/10544—Methods or arrangements for sensing record carriers, e.g. for reading patterns by electromagnetic radiation, e.g. optical sensing; by corpuscular radiation by scanning of the records by radiation in the optical part of the electromagnetic spectrum
    • G06K7/10821—Methods or arrangements for sensing record carriers, e.g. for reading patterns by electromagnetic radiation, e.g. optical sensing; by corpuscular radiation by scanning of the records by radiation in the optical part of the electromagnetic spectrum further details of bar or optical code scanning devices
    • G06K7/10861—Methods or arrangements for sensing record carriers, e.g. for reading patterns by electromagnetic radiation, e.g. optical sensing; by corpuscular radiation by scanning of the records by radiation in the optical part of the electromagnetic spectrum further details of bar or optical code scanning devices sensing of data fields affixed to objects or articles, e.g. coded labels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications

Abstract

The invention provides an unmanned aerial vehicle for recognizing an RFID code of power equipment, and belongs to the field of power equipment recognition. Power equipment RFID sign indicating number discernment unmanned aerial vehicle includes unmanned aerial vehicle main part, two discernment antennas and control mechanism. Two discernment antennas are located respectively the both sides face of unmanned aerial vehicle main part, every the upper end of discernment antenna with the unmanned aerial vehicle main part is articulated, and the lower extreme is kept away from the unmanned aerial vehicle main part, so that the discernment face of discernment antenna is towards oblique top. Control mechanism connects in two between the discernment antenna for the drive is two the discernment antenna is kept away from the unmanned aerial vehicle main part is expanded, perhaps is close to two the unmanned aerial vehicle main part is closed and is closed. Power equipment RFID sign indicating number discernment unmanned aerial vehicle rises to the height of built on stilts equipment, expandes the discernment antenna of both sides through control mechanism, makes the discernment face of discernment antenna towards the RFID electronic tags on the built on stilts equipment, the RFID electronic tags of power equipment is built on stilts to discernment that can be quick, accurate.

Description

Power equipment RFID code recognition unmanned aerial vehicle
Technical Field
The invention belongs to the technical field of power equipment identification, and particularly relates to an unmanned aerial vehicle for power equipment RFID code identification.
Background
The RFID (Radio Frequency Identification) electronic tag is applied to outdoor overhead power equipment and used as an electronic nameplate of the equipment, so that the full life cycle management of the power equipment is realized. The existing RFID electronic tag identification equipment is generally handheld or fixedly installed ground equipment, an antenna of the existing RFID electronic tag identification equipment is installed on the handheld or fixed equipment along with the equipment, and due to the fact that the reading distance of the RFID electronic tag is limited, the existing identification equipment is prone to the technical problem that the antenna identification distance is not enough, and therefore identification cannot be achieved.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle for recognizing an RFID code of power equipment, which aims to solve the technical problem that the RFID electronic tag of overhead power equipment is difficult to recognize due to insufficient antenna recognition distance of the traditional recognition equipment in the prior art.
In order to achieve the above object, the present invention adopts a technical solution that an electric power device RFID code recognition unmanned aerial vehicle is provided, including:
an unmanned aerial vehicle main body;
the two identification antennas are respectively arranged on two side surfaces of the unmanned aerial vehicle main body, the upper end of each identification antenna is hinged with the unmanned aerial vehicle main body, and the lower end of each identification antenna is far away from the unmanned aerial vehicle main body, so that the identification surface of each identification antenna faces to the obliquely upper direction; and
control mechanism connects in two between the discernment antenna, be used for the drive two the discernment antenna is kept away from the unmanned aerial vehicle main part expandes, perhaps is close to two the unmanned aerial vehicle main part is received and is closed.
As another embodiment of the present application, the control mechanism includes:
the two ends of the elastic component are respectively connected with the two identification antennas so as to oppositely draw the two identification antennas to be folded; and
and the telescopic assembly is supported between the two identification antennas and used for pushing the two identification antennas to expand.
As another embodiment of the present application, the elastic member includes:
one end of the first connecting rod is connected with the identification antenna, and the other end of the first connecting rod is a first limiting end;
one end of the second connecting rod is connected with the other identification antenna, and the other end of the second connecting rod is a second limiting end; the second limiting end is opposite to the first limiting end;
the sleeve is sleeved on the first limiting end and the second limiting end;
the first elastic piece is arranged in the sleeve and used for pushing the first limiting end to the second limiting end; and
and the second elastic piece is arranged in the sleeve and used for pushing the second limiting end to the first limiting end.
As another embodiment of the application, a first limit plate is arranged in the sleeve, and the end head of the first limit end penetrates through the first limit plate in a sliding manner and is provided with a first limit cap; the first elastic piece is a first spring sleeved on the first limiting end, the first spring is located between the first limiting plate and the first limiting cap, and two ends of the first spring are respectively abutted to the first limiting plate and the first limiting cap.
As another embodiment of the application, a second limit plate is arranged in the sleeve, and the end head of the second limit end penetrates through the second limit plate in a sliding manner and is provided with a second limit cap; the second elastic piece is a second spring sleeved on the second limiting end, the second spring is located between the second limiting plate and the second limiting cap, and two ends of the second spring are respectively abutted to the second limiting plate and the second limiting cap.
As another embodiment of the present application, the main body of the unmanned aerial vehicle is provided with a limiting member, and the limiting member is provided with a vertical limiting chute;
the middle part of flexible subassembly with the sleeve pipe is worn to locate respectively in the spacing spout, and slide along vertical direction, the middle part of flexible subassembly is equipped with to press from both sides and establishes two first spacing rings of locating part both sides, be equipped with on the sleeve pipe and press from both sides and establish two second spacing rings of locating part both sides.
As another embodiment of the present application, a plurality of bar-shaped protruding portions are provided on the identification surface of the identification antenna, and a groove is formed between the adjacent bar-shaped protruding portions.
As another embodiment of this application, the side of unmanned aerial vehicle main part is equipped with and is used for taking in the state of closing the groove of accomodating of discernment antenna.
As another embodiment of the application, an adjusting seat is arranged on the side surface of the unmanned aerial vehicle main body, and the upper end of the identification antenna is hinged to the adjusting seat; the adjusting seat is vertically arranged in a sliding mode and can be locked, and the angle of the identification antenna is adjusted.
As another embodiment of this application, the side of unmanned aerial vehicle main part is equipped with vertical guide rail, adjust the seat be equipped with vertical guide rail complex guide slot, it is used for the top tight to adjust to be equipped with on the seat the jackscrew of vertical guide rail.
The power equipment RFID code recognition unmanned aerial vehicle provided by the embodiment of the invention has the beneficial effects that: compared with the prior art, the power equipment RFID code recognition unmanned aerial vehicle disclosed by the embodiment of the invention has the advantages that the main body of the unmanned aerial vehicle rises to the height of the overhead equipment, the recognition antennas on the two sides are unfolded through the control mechanism, so that the recognition surfaces of the recognition antennas face the RFID electronic tags on the overhead equipment, and the RFID electronic tags of the overhead power equipment can be quickly and accurately recognized.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings required to be used in the embodiments or the prior art description will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings may be obtained according to these drawings without inventive labor.
Fig. 1 is a front view of an electrical equipment RFID code identification drone provided in an embodiment of the present invention;
FIG. 2 is a cross-sectional view of the elastomeric component of FIG. 1;
FIG. 3 is a cross-sectional view taken at A-A of FIG. 1;
fig. 4 is a side view of the power equipment RFID code recognition drone of fig. 1;
FIG. 5 is a cross-sectional view of the identification antenna of FIG. 4;
fig. 6 is a side view of an RFID code recognition drone for a power device according to another embodiment of the present invention;
fig. 7 is a front view of the identification antenna of the power equipment RFID code identification drone in fig. 6 in an unfolded state.
Wherein, in the figures, the various reference numbers:
1-a main body of the unmanned aerial vehicle; 11-a receiving groove; 12-an adjusting seat; 13-vertical guide rails; 14-top thread; 2-identifying the antenna; 21-a boss; 22-a groove; 3-a control mechanism; 31-a resilient component; 311-first connecting rod; 3111-a first limit cap; 3112-a first magnet; 312-a second connecting rod; 3121-a second limit cap; 3122-a second magnet; 313-a cannula; 3131-a second stop collar; 3132-a first limiting plate; 3133-a second limiting plate; 314-a first spring; 315-a second spring; 32-a telescoping assembly; 321-a first stop collar; 4-a limiting part.
Detailed Description
In order to make the technical problems, technical solutions and advantageous effects to be solved by the present invention more clearly apparent, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or be indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or be indirectly connected to the other element.
It will be understood that the terms "length," "width," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like, as used herein, refer to an orientation or positional relationship indicated in the drawings, which is solely for the purpose of facilitating the description and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and is therefore not to be construed as limiting the invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "plurality" or "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1 to 7 together, the power equipment RFID code identification drone provided by the embodiment of the present invention will now be described. An electric power equipment RFID code discernment unmanned aerial vehicle includes: unmanned aerial vehicle main part 1, two discernment antennas 2 and control mechanism 3.
Two discernment antennas 2 divide the both sides face of locating unmanned aerial vehicle main part 1, and the upper end of every discernment antenna 2 is articulated with unmanned aerial vehicle main part 1, and unmanned aerial vehicle main part 1 is kept away from to the lower extreme to make discernment antenna 2's discernment face towards oblique top.
Control mechanism 3 connects between two discernment antennas 2 for two discernment antennas 2 are kept away from unmanned aerial vehicle main part 1 and are expanded, perhaps close to two unmanned aerial vehicle main parts 1 and receive.
Compared with the prior art, the power equipment RFID code recognition unmanned aerial vehicle disclosed by the embodiment of the invention has the advantages that the unmanned aerial vehicle main body 1 rises to the height of the overhead equipment, the recognition antennas 2 on the two sides are unfolded through the control mechanism 3, so that the recognition surfaces of the recognition antennas 2 face the RFID electronic tags on the overhead equipment, and the RFID electronic tags of the overhead power equipment can be rapidly and accurately recognized.
Of course, in the specific implementation, the power equipment RFID codeIdentificationThe operation of the drone is not limited thereto, and is only illustrated here.
In this embodiment, 1 top of unmanned aerial vehicle main part is the rotor, and the bottom is equipped with the frame and is used for installing discernment antenna 2 and control mechanism 3, specifically, unmanned aerial vehicle main part 1 can adopt four rotor unmanned aerial vehicle.
The identification antenna 2 has a swing arm at its upper end and an identification portion at its lower end. The recognition antenna 2 is hinged on the side of the unmanned aerial vehicle main body 1 through a swing arm, so that the recognition part can swing close to or away from the unmanned aerial vehicle main body 1. The identification part of the identification antenna 2 may be a conventional RFID tag antenna, or may be any of various special RFID tag antennas capable of increasing the identification distance.
The control mechanism 3 is mounted on the main body 1 of the drone and may take any form of actuation, such as electrical, hydraulic, etc. The control mechanism 3 can drive the two identification antennas 2 to be unfolded or folded by pushing and pulling.
Referring to fig. 1 to 3, as a specific implementation of the power equipment RFID code identification drone provided by the present invention, the control mechanism 3 includes: a resilient assembly 31 and a retraction assembly 32.
The two ends of the elastic component 31 are respectively connected with the two identification antennas 2, so as to pull the two identification antennas 2 to be folded in an opposite direction.
The telescopic assembly 32 is supported between the two identification antennas 2 for urging the two identification antennas 2 to be unfolded.
In this embodiment, when the telescopic component 32 is extended, the two identification antennas 2 are pushed to be unfolded, and when the two identification antennas 2 are unfolded, the elastic component 31 is stretched, so that the elastic component 31 generates an elastic force; when the telescopic element 32 is not extended any more, the elastic force of the elastic element 31 pulls the two identification antennas 2 towards each other, so that the two identification antennas 2 are folded.
In a specific implementation, the elastic member 31 may be a spring, a rubber strip, or the like, which is tensioned between the two identification antennas 2, or may be another structure having elasticity.
The telescopic assembly 32 may be an electric push rod or a hydraulic telescopic structure. The two ends of the telescopic component 32 are telescopic ends, and the two telescopic ends are respectively hinged with the two identification antennas 2.
Referring to fig. 1 to 3, as an embodiment of the power equipment RFID code identification drone provided by the present invention, the elastic component 31 includes: a first connecting rod 311, a second connecting rod 312, a sleeve 313, a first elastic member and a second elastic member.
One end of the first connecting rod 311 is connected to the identification antenna 2, and the other end is a first limiting end. One end of the second connecting rod 312 is connected to the other identification antenna 2, and the other end is a second limiting end; the second limiting end is opposite to the first limiting end. The sleeve 313 is sleeved on the first limit end and the second limit end. The first elastic element is arranged in the sleeve 313 and used for pushing the first limit end to the second limit end. The second elastic element is arranged in the sleeve 313 and used for pushing the second limit end to the first limit end.
In this embodiment, the sleeve 313 can guide the first limit end and the second limit end, and can protect the first elastic element and the first elastic element, so as to ensure stability and service life. The first elastic member pushes the first position-limiting end toward the second position-limiting end, so that the first connecting rod 311 drives the connected identification antenna 2 to fold. The second elastic member pushes the second position-limiting end toward the first position-limiting end, so that the second connecting rod 312 drives the connected identification antenna 2 to be folded.
In a specific implementation, the first connecting rod 311 may be a straight rod, one end of which is hinged to the identification antenna 2, and the other end of which is provided with an end cap with a large diameter to form a first limiting end. The second connecting rod 312 may be a straight rod, one end of which is hinged to the identification antenna 2, and the other end of which is provided with a large-diameter end cap to form a second limit end. The first elastic member and the second elastic member may employ a spring or other elastic member.
Referring to fig. 1 to 3, as an embodiment of the power equipment RFID code recognition drone provided by the present invention, a first limiting plate 3132 is disposed in the sleeve 313, and a tip of the first limiting end slides through the first limiting plate 3132 and is provided with a first limiting cap 3111; the first elastic element is a first spring 314 sleeved on the first limiting end, the first spring 314 is located between the first limiting plate 3132 and the first limiting cap 3111, and two ends of the first spring are respectively abutted against the first limiting plate 3132 and the first limiting cap 3111.
In this embodiment, one end of the first spring 314 abuts against the first stopper plate 3132, and the other end abuts against the first stopper cap 3111, and the first spring 314 pushes the first stopper end through the first stopper cap 3111.
In a specific implementation, the first restriction plate 3132 may be disposed at one end of the bushing 313 and provided with a through hole. The first stopper end passes through the through hole of the first stopper plate 3132. The end of the first limit end expands to form a first limit cap 3111. The first spring 314 is sleeved on the first limit end, and the outer diameter of the first spring 314 is smaller than the diameter of the first limit cap 3111, so that the first spring 314 abuts against the first limit cap 3111.
Referring to fig. 1 to 3, as an embodiment of the power equipment RFID code recognition drone provided by the present invention, a second limiting plate 3133 is disposed in the sleeve 313, and a tip of the second limiting end slides through the second limiting plate 3133 and is provided with a second limiting cap 3121; the second elastic element is a second spring 315 sleeved on the second limiting end, the second spring 315 is located between the second limiting plate 3133 and the second limiting cap 3121, and two ends of the second spring are respectively abutted against the second limiting plate 3133 and the second limiting cap 3121.
In this embodiment, one end of the second spring 315 abuts against the second stopper plate 3133, the other end abuts against the second stopper cap 3121, and the second spring 315 pushes the second stopper end through the second stopper cap 3121.
In a specific implementation, the second restriction plate 3133 may be disposed at one end of the bushing 313 and provided with a through hole. The second stopper end passes through the through hole of the second stopper plate 3133. The end of the second limiting end is expanded to form a second limiting cap 3121. The second spring 315 is sleeved on the second limit end, and the outer diameter of the second spring 315 is smaller than the diameter of the second limit cap 3121, so that the second spring 315 is abutted against the second limit cap 3121.
In a specific embodiment, a first magnet 3112 is arranged in the first limiting cap 3111 of the first limiting end, a second magnet 3122 is arranged in the second limiting cap 3121 of the second limiting end, and the first magnet 3112 and the second magnet 3122 have opposite and opposite magnetic poles. When the first limit cap 3111 and the second limit cap 3121 are closer, the first spring 314 and the second spring 315 have been stretched more and the elasticity is insufficient, and at this time, the first magnet 3112 and the second magnet 3122 can attract each other, increasing the driving force for the first limit end and the second limit end to move toward each other. The first magnet 3112 and the second magnet 3122 may each employ an electromagnet or a permanent magnet.
Referring to fig. 1 to 3, as a specific embodiment of the power equipment RFID code recognition unmanned aerial vehicle provided by the present invention, the unmanned aerial vehicle main body 1 is provided with a limiting member 4, and the limiting member 4 is provided with a vertical limiting sliding groove.
The middle portion of the telescopic assembly 32 and the sleeve 313 penetrate through the limiting sliding groove and slide along the vertical direction, two first limiting rings 321 clamped on two sides of the limiting member 4 are arranged in the middle portion of the telescopic assembly 32, and two second limiting rings 3131 clamped on two sides of the limiting member 4 are arranged on the sleeve 313.
In this embodiment, the limiting member 4 can limit the middle part of the telescopic assembly 32 and the position of the sleeve 313, so that the opening angles of the identification antennas 2 on the two sides of the main body 1 of the unmanned aerial vehicle are the same. Meanwhile, the middle part of the telescopic assembly 32 and the sleeve 313 can slide in the limit sliding groove, so that the telescopic assembly 32 and the elastic assembly 31 can smoothly drive the two identification antennas 2 to be unfolded and folded.
During concrete implementation, locating part 4 can adopt the vertical rectangular board of fixing on unmanned aerial vehicle main part 1, sets up vertical spacing spout on the rectangular board, and the width of spacing spout is the same with the width at the middle part of telescopic component 32 and sleeve pipe 313's external diameter. Two first limiting rings 321 with a larger diameter are processed in the middle of the telescopic assembly 32, and the two first limiting rings 321 are located at two sides of the limiting member 4 to clamp the limiting member 4 in the middle. Two second limiting rings 3131 with a larger diameter are formed on the outer circumference of the sleeve 313, and the two second limiting rings 3131 are located on two sides of the limiting member 4 to sandwich the limiting member 4.
Referring to fig. 4 to 6, as a specific embodiment of the power equipment RFID code identification drone provided by the present invention, a plurality of bar-shaped protruding portions 21 are provided on the identification surface of the identification antenna 2, and a groove 22 is formed between adjacent bar-shaped protruding portions 21.
In a specific implementation, the protruding portions 21 are in a horizontal strip shape, the adjacent protruding portions 21 are parallel to each other, the cross sections of the protruding portions 21 are in a trapezoid shape, and the adjacent protruding portions 21 form grooves 22 with inverted trapezoid or inverted triangle cross sections. The height of the protrusion 21 with respect to the bottom of the groove 22 is between 0.5 cm and 1 cm, preferably 0.6 cm, increasing the stability of the device.
Referring to fig. 4 and 6, as a specific embodiment of the power device RFID code recognition unmanned aerial vehicle provided by the present invention, a storage slot 11 for storing the identification antenna 2 in a storage state is disposed on a side surface of the main body 1 of the unmanned aerial vehicle.
In this embodiment, when discernment antenna 2 was received, the articulated shaft isotructure at the back and most structures of discernment antenna 2 all can be accomodate and receive groove 11, and protection discernment antenna 2 avoids damaging, the transportation after facilitating the use.
Referring to fig. 6 and 7, as a specific embodiment of the power equipment RFID code identification unmanned aerial vehicle provided by the present invention, an adjusting base 12 is disposed on a side surface of the main body 1 of the unmanned aerial vehicle, and an upper end of the identification antenna 2 is hinged to the adjusting base 12; the adjusting base 12 is vertically slidably disposed and lockable, and is used for adjusting the angle of the identification antenna 2.
In this embodiment, can slide down and adjust seat 12, then expand discernment antenna 2, make discernment antenna 2 can avoid sheltering from of structures such as the oar that revolves of top, conveniently discern the RFID electronic tags of antenna 2 discernment. By sliding the adjustment base 12 upward, the identification antenna 2 can be smoothly folded and stored in the storage groove 11.
During concrete implementation, the top of unmanned aerial vehicle main part 1 generally is oar rotating isotructure, and in order to guarantee the flight effect, the area that the oar rotating on the horizontal plane covers is great, leads to oar rotating isotructure to shelter from discernment antenna 2 easily. The general practice is to lengthen the identification antenna 2, so that the identification antenna 2 can exceed the coverage of the propeller and other structures after swinging and unfolding, but this will certainly increase the volume of the identification antenna 2, resulting in the increase of the volume of the whole device. This scheme is through lower slide adjusting seat 12, makes identification antenna 2 keep away from the oar isotructure at the 1 top of unmanned aerial vehicle main part, and then makes identification antenna 2 after the expansion avoid the sheltering from of the oar isotructure of top. The identification antenna 2 in fig. 7 is the position of the identification antenna 2 after the adjustment seat 12 slides down, the dotted line part in fig. 7 is the position of the identification antenna 2 after the adjustment seat 12 is unfolded at the top, and the comparison of the two shows that the identification antenna 2 after the adjustment seat 12 slides down can be opened to avoid the upper propeller and align to the RFID electronic tag on the overhead device obliquely above.
Referring to fig. 6 and 7, as a specific embodiment of the power equipment RFID code recognition unmanned aerial vehicle provided by the present invention, a vertical guide rail 13 is disposed on a side surface of the unmanned aerial vehicle main body 1, a guide groove matched with the vertical guide rail 13 is disposed on the adjusting seat 12, and a jackscrew 14 for tightly jacking the vertical guide rail 13 is disposed on the adjusting seat 12.
In this embodiment, the adjusting base 12 can be adjusted in the up-down direction along the vertical guide rail 13, and after the adjusting base 12 is adjusted in place, the adjusting base 12 and the vertical guide rail 13 can be locked by tightly pushing the vertical guide rail 13 through the jackscrew 14, so that the position of the identification antenna 2 is fixed.
In a specific implementation, the vertical guide rail 13 may be a guide rail with a dovetail-shaped cross section, a dovetail groove is disposed on the back surface of the corresponding adjusting seat 12, and the adjusting seat 12 is slidably mounted on the vertical guide rail 13 through the dovetail groove. The jackscrew 14 is arranged on the front surface of the adjusting seat 12, and the jackscrew 14 can be inserted into the guide groove of the adjusting seat 12 after being screwed tightly to jack the vertical guide rail 13 tightly.
The present invention is not limited to the above preferred embodiments, and any modifications, equivalent substitutions and improvements made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (9)

1. Power equipment RFID sign indicating number discernment unmanned aerial vehicle, its characterized in that includes:
an unmanned aerial vehicle main body;
the two identification antennas are respectively arranged on two side surfaces of the unmanned aerial vehicle main body, the upper end of each identification antenna is hinged with the unmanned aerial vehicle main body, and the lower end of each identification antenna is far away from the unmanned aerial vehicle main body, so that the identification surface of each identification antenna faces to the obliquely upper direction; and
the control mechanism is connected between the two identification antennas and used for driving the two identification antennas to be far away from the unmanned aerial vehicle main body to be unfolded or close to the two unmanned aerial vehicle main bodies to be folded;
a plurality of strip-shaped protruding portions are arranged on the identification surface of the identification antenna, and grooves are formed between every two adjacent strip-shaped protruding portions.
2. The power equipment RFID code recognition drone of claim 1, wherein the control mechanism includes:
the two ends of the elastic component are respectively connected with the two identification antennas so as to oppositely draw the two identification antennas to be folded; and
and the telescopic assembly is supported between the two identification antennas and used for pushing the two identification antennas to expand.
3. The power device RFID code recognition drone of claim 2, wherein the elastic component comprises:
one end of the first connecting rod is connected with the identification antenna, and the other end of the first connecting rod is a first limiting end;
one end of the second connecting rod is connected with the other identification antenna, and the other end of the second connecting rod is a second limiting end; the second limiting end is opposite to the first limiting end;
the sleeve is sleeved on the first limiting end and the second limiting end;
the first elastic piece is arranged in the sleeve and used for pushing the first limiting end to the second limiting end; and
and the second elastic piece is arranged in the sleeve and used for pushing the second limiting end to the first limiting end.
4. The power equipment RFID code recognition unmanned aerial vehicle of claim 3, wherein a first limiting plate is arranged in the sleeve, and a tip of the first limiting end slides through the first limiting plate and is provided with a first limiting cap; the first elastic piece is a first spring sleeved on the first limiting end, the first spring is located between the first limiting plate and the first limiting cap, and two ends of the first spring are respectively abutted to the first limiting plate and the first limiting cap.
5. The power equipment RFID code recognition unmanned aerial vehicle of claim 3, wherein a second limiting plate is arranged in the sleeve, and the end of the second limiting end slides through the second limiting plate and is provided with a second limiting cap; the second elastic piece is a second spring sleeved on the second limiting end, the second spring is located between the second limiting plate and the second limiting cap, and two ends of the second spring are respectively abutted to the second limiting plate and the second limiting cap.
6. The power equipment RFID code recognition unmanned aerial vehicle of claim 3, wherein the unmanned aerial vehicle main body is provided with a limiting piece, and the limiting piece is provided with a vertical limiting sliding groove;
the middle part of flexible subassembly with the sleeve pipe is worn to locate respectively in the spacing spout, and slide along vertical direction, the middle part of flexible subassembly is equipped with to press from both sides and establishes two first spacing rings of locating part both sides, be equipped with on the sleeve pipe and press from both sides and establish two second spacing rings of locating part both sides.
7. The power equipment RFID code recognition unmanned aerial vehicle of any one of claims 1 to 6, wherein a side surface of the unmanned aerial vehicle main body is provided with a storage groove for storing the recognition antenna in a folded state.
8. The power equipment RFID code recognition unmanned aerial vehicle of any one of claims 1 to 6, wherein a side surface of the unmanned aerial vehicle main body is provided with an adjusting seat, and an upper end of the recognition antenna is hinged to the adjusting seat; the adjusting seat is vertically arranged in a sliding mode and can be locked, and the angle of the identification antenna is adjusted.
9. The power equipment RFID code recognition unmanned aerial vehicle of claim 8, wherein a vertical guide rail is arranged on the side surface of the unmanned aerial vehicle main body, the adjusting seat is provided with a guide groove matched with the vertical guide rail, and a jackscrew for jacking the vertical guide rail is arranged on the adjusting seat'.
CN202011621322.XA 2020-12-30 2020-12-30 Power equipment RFID code recognition unmanned aerial vehicle Active CN112644685B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011621322.XA CN112644685B (en) 2020-12-30 2020-12-30 Power equipment RFID code recognition unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011621322.XA CN112644685B (en) 2020-12-30 2020-12-30 Power equipment RFID code recognition unmanned aerial vehicle

Publications (2)

Publication Number Publication Date
CN112644685A CN112644685A (en) 2021-04-13
CN112644685B true CN112644685B (en) 2022-06-10

Family

ID=75367372

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011621322.XA Active CN112644685B (en) 2020-12-30 2020-12-30 Power equipment RFID code recognition unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN112644685B (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140197280A1 (en) * 2011-11-22 2014-07-17 Donald Earl Smith Delta Wing Unmanned Aerial Vehicle (UAV) and Method of Manufacture of the Same
CN206806514U (en) * 2017-05-31 2017-12-26 合肥海天电子科技有限公司 A kind of type radio frequency identification intelligent antennas of new RFID I
CN108860602A (en) * 2018-06-05 2018-11-23 深圳市雷凌广通技术研发有限公司 A kind of unmanned plane of taking photo by plane with camera head protecting function
CN110329493A (en) * 2019-07-29 2019-10-15 江苏虹彩航空科技有限公司 A kind of monitoring unmanned equipment stable supporting device
CN211308978U (en) * 2019-08-28 2020-08-21 周志毅 A antenna mounting structure for forestry seeding unmanned aerial vehicle
CN111062454A (en) * 2019-11-28 2020-04-24 北京瑞芯谷科技有限公司 Tower pole inspection system
CN212074410U (en) * 2020-04-07 2020-12-04 深圳市云海方成科技有限公司 Anti-rollover unmanned aerial vehicle undercarriage with damping function

Also Published As

Publication number Publication date
CN112644685A (en) 2021-04-13

Similar Documents

Publication Publication Date Title
CN111819616A (en) Flexible display device
CN111819615B (en) Flexible display device
CN102916294B (en) Electronic installation
CN107545849A (en) Flexible display apparatus
CN112644685B (en) Power equipment RFID code recognition unmanned aerial vehicle
CN109933141B (en) Functional assembly, electronic device and control method thereof
CN110067805B (en) Rotating shaft, terminal equipment and rotating shaft control method
CN113923286A (en) Electronic device
CN109862148B (en) Functional assembly, mobile terminal and control method thereof
CN211738441U (en) Quick detach formula computer and display
CN110247151B (en) Antenna double-track sliding structure
CN105789813A (en) Expansion antenna device
CN213751192U (en) Entrance guard detector with power-off prevention function for intelligent supermarket
CN219833130U (en) Personnel basic information acquisition equipment
CN213212365U (en) GSM2G antenna with self-clamping shell structure
CN218330261U (en) Movable temperature monitoring device
CN112987864B (en) Storage module fixing device and operation method thereof
CN214253228U (en) Anti-static ultrahigh frequency reader-writer
CN108646059B (en) Overhead transmission line folding type insulating rod withstand voltage experiment support
CN219281442U (en) Anti-collision temporary protective enclosing wall
CN216490468U (en) Airport wireless communication handheld terminal equipment based on private network
CN213584142U (en) Handheld terminal of thing networking data acquisition
CN211826191U (en) Intelligent electric energy metering box
CN211580034U (en) Electronic device
CN219733041U (en) Building construction foundation pit guardrail

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant