CN116119063B - Mapping unmanned aerial vehicle energy supplementing relay platform and application method - Google Patents
Mapping unmanned aerial vehicle energy supplementing relay platform and application method Download PDFInfo
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- CN116119063B CN116119063B CN202211606782.4A CN202211606782A CN116119063B CN 116119063 B CN116119063 B CN 116119063B CN 202211606782 A CN202211606782 A CN 202211606782A CN 116119063 B CN116119063 B CN 116119063B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
- B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Anchoring
- B64F1/125—Mooring or ground handling devices for helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
Abstract
The invention relates to an unmanned aerial vehicle energy supplementing platform, in particular to an unmanned aerial vehicle energy supplementing relay platform for surveying and mapping. The main structure comprises: the device comprises a triangular bracket and a Y-shaped bracket fixed with the triangular bracket through a turntable, wherein bases are fixed at the two top ends of the Y-shaped bracket, and a screw box and a jaw driver are fixed on the bases; two U-shaped support module surround centre gripping unmanned aerial vehicle main part. The base is formed by welding three rods which are 120 degrees each other, and the chassis is light and stable for the traditional base; the triangular bracket and the Y-shaped bracket are provided with pins, so that the triangular bracket can be positioned at any position in space; the first clamp plate and the second clamp plate are mutually close to or separated from each other, so that the arcuate workpiece can be locked at an inclined position; the magnetic sheet corresponds to a magnetic field signal of the magnetic induction area, so that contact alignment between the electric connection copper sheet and the feeler lever can be realized, and the connection of an energy supplementing circuit is realized.
Description
Technical Field
The invention relates to an unmanned aerial vehicle energy supplementing platform, in particular to an unmanned aerial vehicle energy supplementing relay platform for surveying and mapping.
Background
The unmanned aerial vehicle aerial survey is a powerful supplement to the traditional aerial photogrammetry, has the characteristics of flexibility, high efficiency, rapidness, fineness, accuracy, low operation cost, wide application range, short production period and the like, has obvious advantages in the aspect of rapid acquisition of high-resolution images in small areas and difficult flying areas, has shown unique advantages along with the development of unmanned aerial vehicle and digital camera technologies, and combines unmanned aerial vehicle and aerial photogrammetry to enable unmanned aerial vehicle digital low-altitude remote sensing to become a brand-new development direction in the aerial remote sensing field, so that unmanned aerial vehicle aerial photography can be widely applied to the aspects of national major engineering construction, disaster emergency and treatment, homeland supervision, resource development, new rural areas, small town construction and the like, and has wide prospects in the aspects of basic surveying and mapping, land resource investigation and monitoring, land utilization dynamic monitoring, digital city construction, emergency relief and mapping data acquisition and the like.
However, the battery of the unmanned aerial vehicle has short endurance, and the endurance of the lithium battery of the unmanned aerial vehicle which is commonly used at present is only 30 minutes, so that the battery which is frequently replaced or the reciprocating charging is required for the large-area mapping of the unmanned aerial vehicle in the mapping work process of the unmanned aerial vehicle; this not only consumes a lot of manual management but also affects the efficiency of unmanned aerial vehicle mapping; the same purpose of 'unmanned' cannot be truly realized; therefore, a relay energy supplementing platform should be designed for the unmanned aerial vehicle for mapping.
Disclosure of Invention
The invention aims to provide an energy supplementing relay platform for a surveying and mapping unmanned aerial vehicle and a using method thereof, which are energy supplementing relay platforms pointed out in the background art, so as to provide battery electric energy supplementing for the surveying and mapping unmanned aerial vehicle.
The invention solves the technical problems as follows: the utility model provides a survey and drawing unmanned aerial vehicle benefit can relay platform, its main structure includes: the device comprises a triangular bracket and a Y-shaped bracket fixed with the triangular bracket through a turntable, wherein bases are fixed at the two top ends of the Y-shaped bracket, and a screw box and a jaw driver are fixed on the bases;
a screw rod is penetrated in the screw rod box, and a fluted disc is screwed in the screw rod; the top end of the screw rod is fixed at the middle position of the workpiece block, the upper end and the lower end of the workpiece block are hinged with a U-shaped bracket module through movable hinges, a threaded rod with a handle penetrates into the tail end of an arch-shaped workpiece of the U-shaped bracket module, the threaded rod with the handle is screwed into the tail end of the workpiece block, and a second spring seat is arranged between the tail end of the workpiece block and the lower part of the arch-shaped workpiece;
two U-shaped support module surround centre gripping unmanned aerial vehicle main part.
Further, the screw box is formed by: a hoop member is fixed in the Fang Xingqiang body, and an arc-shaped rack is arranged at the notch position of the hoop member; the center of the inner concave surface of the arc-shaped rack is fixedly provided with a biting tooth, and the outer convex surface of the arc-shaped rack is meshed with the gear; the gear is driven by a speed reducing motor arranged in the Fang Xingqiang body;
further, the hoop member and the arc-shaped rack form a hole groove, a screw rod penetrates into the hole groove, a screw rod groove is formed in the screw rod, and the screw rod groove is matched with the biting teeth.
Further, the clamp driver comprises: a first spring seat is fixed between the first clamp plate and the second clamp plate, a second driving motor is fixed on the first clamp plate, a rotating shaft of the second driving motor is a threaded rod, and the threaded rod penetrates through the first clamp plate and the first spring seat and is screwed with a thread groove formed in the second clamp plate; a first driving motor is fixed on one end of the first clamp plate, the rotating shaft of the first driving motor is a worm, the worm penetrates through the first clamp plate and the second clamp plate, and the worm is engaged with the fluted disc in a cross manner; the fluted disc is located between the first pincers board and the second pincers board.
Further, the U-shaped bracket module is formed by: a positioning rod is arranged at the concave center of the arched workpiece, rubber roller groups are respectively arranged at the two ends of the arched workpiece, and power transmission rods are respectively arranged at the two ends of the arched workpiece; the positioning rod is internally provided with an electric air rod, and the tail end of the electric air rod is provided with a magnetic sheet; the power transmission rod is inserted with a feeler lever, and a spring seat is abutted between the feeler lever and the power transmission rod.
Further, an electric copper sheet and a magnetic induction area are arranged on the outer wall of the unmanned aerial vehicle main body; the electric connection copper sheet is matched with the top end of the feeler lever; the magnetic induction area is matched with the magnetic sheet.
Further, a first circuit control unit is arranged in the unmanned aerial vehicle main body, and the first circuit control unit takes the magnetic induction area as a signal collecting end so as to control a rotor wing on the unmanned aerial vehicle main body to adjust the gesture; the circuit control unit also controls a wireless signal module and a positioning module; the Y-shaped support is provided with a second circuit control unit, and the second circuit control unit is also connected with a wireless signal module and a positioning module.
Further, a bearing is arranged in the turntable, and a Y-shaped bracket bottom rod piece is fixedly arranged in the bearing; the triangular bracket is formed by welding three rods which form an included angle of 120 degrees, and a circular groove is formed in the center point of the welding; a bearing is arranged in the circular groove; and the bearing is provided with a limiting bolt.
Further, the power supply rod is externally connected with a power supply input; the unmanned aerial vehicle main part select for use is coaxial unmanned aerial vehicle.
The invention has the beneficial effects that: the base is formed by welding three rods which are 120 degrees each other, and the chassis is light and stable for the traditional chassis; the triangular bracket and the Y-shaped bracket are provided with pins, so that the triangular bracket can be positioned at any position in space; the first clamp plate and the second clamp plate are mutually close to or separated from each other, so that the arcuate workpiece can be locked at an inclined position; the magnetic sheet corresponds to a magnetic field signal of the magnetic induction area, so that contact alignment between the electric connection copper sheet and the feeler lever can be realized, and the connection of an energy supplementing circuit is realized.
Drawings
Fig. 1 is a diagram illustrating an overall construction of an energy supplementing relay platform for a surveying and mapping unmanned aerial vehicle.
Fig. 2 is a top view of an energy supplementing relay platform of a surveying and mapping unmanned aerial vehicle.
Fig. 3 is a diagram of a fixture structure with an arcuate workpiece as a core of the unmanned aerial vehicle energy supplementing relay platform.
Fig. 4 is a front view of a fixture with an arcuate workpiece as a core for the unmanned aerial vehicle energy supplementing relay platform of the present invention.
Fig. 5 is a main body structure diagram of the unmanned aerial vehicle clamped by two arcuate workpieces of the energy supplementing relay platform of the unmanned aerial vehicle for surveying and mapping.
Fig. 6 is a schematic diagram of a clamp driver of the energy supplementing relay platform of the unmanned aerial vehicle.
Fig. 7 is an exploded view of an arcuate workpiece holder assembly of the unmanned aerial vehicle energy-compensating relay platform of the present invention.
Fig. 8 is a schematic diagram of a screw box principle of the energy supplementing relay platform of the surveying and mapping unmanned aerial vehicle.
Fig. 9 is a diagram of a coaxial unmanned aerial vehicle structure of the mapping unmanned aerial vehicle energy supplementing relay platform.
Fig. 10 is a block diagram of a positioning rod of the mapping unmanned aerial vehicle energy supplementing relay platform.
Fig. 11 is a diagram of a power transmission rod structure of the mapping unmanned aerial vehicle energy supplementing relay platform.
In the drawing, a 1-A bracket, a 2-turntable, a 3-Y bracket, a 4-screw box, a 41-square cavity, a 42-hoop piece, a 43-arc rack, a 431-biting tooth, a 44-gear, a 5-jaw driver, a 51-first jaw plate, a 52-second jaw plate, a 53-first spring seat, a 54-first driving motor, a 541-worm, a 6-second driving motor, a 61-threaded rod, a 7-fluted disc, an 8-threaded rod, a 81-threaded rod groove, a 9-workpiece block, a 10-movable hinge, a 11-arcuate workpiece, a 12-threaded rod, a 121-second spring seat, a 13-rubber roller group, a 14-power feeding rod, a 141-feeler lever, a 15-positioning rod, a 151-electric air lever, a 152-magnetic sheet, a 16-unmanned aerial vehicle body, a 161-power connection copper sheet, a 162-magnetic induction area and a 17-base are arranged.
Detailed Description
The following describes in detail the embodiments of the present invention with reference to fig. 1-11.
Examples: the energy supplementing relay platform of the unmanned aerial vehicle for surveying and mapping is characterized in that a Y-shaped bracket 3 is fixed with a triangular bracket 1 through a turntable 2, bases 17 are fixed at two top ends of the Y-shaped bracket 3, and a screw box 4 and a jaw driver 5 are fixed on the bases 17;
with reference to fig. 1, a bearing is arranged in the turntable 2, and a rod piece at the bottom of the Y-shaped bracket 3 is fixedly arranged in the bearing; the triangular bracket 1 is formed by welding three rods which form an included angle of 120 degrees, and a circular groove is formed in the center point of the welding; a bearing is arranged in the circular groove; the bearing is provided with a limiting bolt; the Y-shaped bracket 3 can be positioned at any angle and in any direction through the limiting bolt, so that the U-shaped bracket module works in cooperation with the following.
The screw box 4 is constituted as shown in fig. 8: the square cavity 41 is internally fixed with the anchor ear piece 42, the anchor ear piece 42 can limit the screw rod 8, so that the screw rod 8 can be inserted in the anchor ear piece 42 only in the horizontal direction, and obviously, lubricating grease can be added on the contact surface of the anchor ear piece 42 and the screw rod 8; a notch is arranged on the hoop member 42, and an arc-shaped rack 43 is arranged at the position of the notch; the two end surfaces provided with the arc-shaped racks 43 can be abutted against the notch surfaces of the hoop, the arc-shaped racks 43 play a limiting role in the rotation process, and the same arc-shaped racks 43 can also be covered on the outer wall of the hoop 42; the arc rack 43 is limited at this moment, and the gear motor controlled by the gear 44 is designed to limit, and the designed limiting structure is conventional, because the limiting structure is not recorded in the claims of the present application, the conventional limiting method adopts the counting control of the number of turns of the motor, and in general, the motor is set to be automatically stopped after the rated number of turns of the motor is turned.
In the structure, the arc-shaped rack 43 is fixed with the biting teeth 431 at the center of the inner concave surface, and the outer convex surface of the arc-shaped rack 43 is provided with the outer convex surface which is meshed with the gear 44; the gear 44 is driven by a gear motor built in the Fang Xingqiang body 41;
supplementary is required in connection with fig. 7 and 8: the hoop member 42 and the arc-shaped rack 43 form a hole groove, a screw rod 8 penetrates into the hole groove, a screw rod groove 81 is formed in the screw rod 8, and the screw rod groove 81 is matched with the biting teeth 431; it is apparent that the structural biting teeth 431 are capable of sliding in the screw grooves 81.
Obviously, the rotation of the screw rod 8 in a certain angle can be stirred through the driving of the gear motor, the certain angle is generally 5-15 degrees in a positive-negative interval, and the control on the inclination of the position of the arcuate workpiece 11 for clamping the unmanned aerial vehicle main body 16 can be realized through the small-angle rotation control of the screw rod 8.
The jaw driver 5 as shown in fig. 6 is constituted by: a first spring seat 53 is fixed between the first clamp plate 51 and the second clamp plate 52, and the first spring seat 53 has two functions, namely, a bridge for providing connection between the first clamp plate 51 and the second clamp plate 52 and an auxiliary force when the first clamp plate 51 and the second clamp plate 52 are far away; the first spring seat 53 is generally designed at a position near to one side of the first nipper 51, because the second driving motor 6 is fixed on the first nipper 51, and the rotating shaft of the second driving motor 6 is a threaded rod 61, and the threaded rod 61 penetrates through the first nipper 51 and the first spring seat 53 and is screwed with a thread groove provided on the second nipper 52; the above-described structure obviously constitutes that the second nipper 52 can be moved away from or close to the first nipper 51 when the second driving motor 6 is rotated in the forward or reverse direction, and is designed to lock or unlock the toothed disc 7; it is apparent that the toothed disc 7 is located between the first vise plate 51 and the second vise plate 52.
In addition, a first driving motor 54 is fixed at one end of the first nipper 51, the rotation shaft of the first driving motor 54 is a worm 541, the worm 541 penetrates through the first nipper 51 and the second nipper 52, and the worm 541 is engaged with the fluted disc 7 in a cross manner; it is obvious that the constitution of worm 541 and fluted disc 7 is a rotation that can change the transverse rotation force of worm 541 into longitudinal rotation to drive fluted disc 7's rotation, obviously the rotation of fluted disc 7 can control the horizontal flexible control of distance of work piece 9, thereby realizes that two pairs of arciform work pieces 11 that mirror image was arranged draw close or keep away from each other, and then reaches the purpose of centre gripping unmanned aerial vehicle main part 16.
As shown in fig. 3 and 7, a screw rod 8 penetrates through the screw rod box 4, and a fluted disc 7 is screwed on the screw rod 8; the top end of the screw rod 8 is fixed in the middle of the workpiece block 9, and the upper end and the lower end of the workpiece block 9 are hinged with U-shaped bracket modules through movable hinges 10; referring to fig. 4, a threaded rod 12 with a handle is penetrated into the tail end of the arched workpiece 11 of the U-shaped bracket module, the threaded rod 12 with the handle is screwed into the tail end of the workpiece block 9, and a second spring seat 121 is arranged between the tail end of the workpiece block 9 and the lower part of the arched workpiece 11; in the above-mentioned structure, it is apparent that when the arcuate workpieces 11 mounted at both ends of the U-shaped bracket module receive the start-stop impact of the unmanned aerial vehicle body 16, the arcuate workpieces 11 can be pressed toward the middle position of the workpiece block 9, so as to reduce the start-stop impact of the unmanned aerial vehicle body 16, that is, the above-mentioned movable hinge 10 and second spring seat 121 structure constitute a buffer device;
after the above-mentioned structure is distributed, two U-shaped support modules can be used for surrounding and clamping the unmanned aerial vehicle main body 16.
The U-shaped bracket module described above in connection with fig. 3 is formed by: the concave center of the arched workpiece 11 is provided with a positioning rod 15, two ends of the arched workpiece 11 are respectively provided with a rubber roller group 13, the rubber roller group 13 is generally preferably composed of 2-4 single rubber rollers, and two ends of the arched workpiece 11 are respectively provided with a power transmission rod 14; referring to fig. 11, a power input is connected to the power transmission rod 14, a contact rod 141 is inserted in the power transmission rod 14, a spring seat is abutted between the contact rod 141 and the power transmission rod 14, and the structure of the power transmission rod 14 can ensure that the abutted conductor does not generate virtual connection and ensures smooth conduction;
the positioning rod 15 contains an electric air rod 151, and a magnetic sheet 152 is arranged at the tail end of the electric air rod 151; by means of the telescopic control of the electric air rod 151, support can be provided when the magnetic sheet 152 and the magnetic induction area 162 are located; referring to fig. 9, an electric copper sheet 161 and a magnetic induction area 162 are arranged on the outer wall of the matched unmanned plane main body 16; and the said copper sheet 161 of electricity connects with top of the feeler lever 141 and matches; the magnetic induction zone 162 is matched with the magnetic sheet 152. Here, it is necessary to explain: there are many prior art solutions for interfacing the magnetic induction zone 162 with the magnetic sheet 152, as the prior art is not described in the claims herein, but in the specific implementation, my exemplifies two prior art: one can adopt an NFC structure, and the magnetic sheet 152 is a chip coil; the magnetic induction area 162 is a card reader, and obviously, when the chip coil is close to the card reader, the chip coil can receive data, and the same approach of the chip coil and the card reader can read, so that the position is correct; secondly, the magnetic induction area 162 is a conventional magnetic field detection chip module, and the magnetic sheet 152 is a simple permanent magnetic sheet, and it is obvious that when the permanent magnetic sheet is in central contact with the magnetic field detection chip module, the magnetic field is strongest; matching can also be achieved.
A first circuit control unit is arranged in the unmanned aerial vehicle main body 16, and the first circuit control unit takes the magnetic induction area 162 as a signal collecting end to control a rotor wing on the unmanned aerial vehicle main body 16 to adjust the gesture; the circuit control unit also controls a wireless signal module and a positioning module; the Y-shaped bracket 3 is provided with a second circuit control unit, and the second circuit control unit is also connected with a wireless signal module and a positioning module.
The first circuit control unit and the second circuit control unit need to cooperatively control each other, so that the unmanned aerial vehicle main body 16 can start and stop on a relay platform with the Y-shaped bracket 3 as a core; obviously, the electric control part is not developed in detail, and the prior art is mostly adopted for the structure of the electric control part; as to the core technical section other applications; it should be noted that the protection application is a mechanical structure part, and the circuit structure is a part of the application.
In addition, the unmanned aerial vehicle main body 16 is a coaxial unmanned aerial vehicle, because the platform can only be designed for the coaxial unmanned aerial vehicle structure, and the input four-axis aircraft cannot be suitable for the platform.
Fig. 2 shows a state diagram of an optimal bracket structure, wherein one supporting rod of the triangular bracket 1 is vertical to the Y-shaped bracket 3, and the structure is stable relative to the locking mode.
The application method of the mapping unmanned aerial vehicle energy supplementing relay platform comprises the following steps:
s1, firstly, placing the tripod 1 in a working area of a mapping unmanned aerial vehicle; the bottom of the optional A-frame 1 is provided with a fixing device which can lock the bottom, the optional structure is shown as a lockable roller in the figure 1 in the scheme, then the bottom end of the Y-shaped frame 3 is inserted into a bearing at the center of the A-frame 1, and a limit bolt is arranged, so that the Y-shaped frame 3 can be positioned and fixed on the A-frame 1;
s2, debugging whether the functions of the electric accessories are normal or not:
the first driving motor 54 is started to rotate forward, the normal function of the first driving motor is that the screw 541 can drive the fluted disc 7 to be screwed, the screwing of the fluted disc 7 is indirectly represented by that the screw rod 8 is ejected from the screw rod box 4 to the workpiece block 9, and the visual display is that the arciform workpieces 11 which are mirror symmetry are mutually closed; conversely, when the first driving motor 54 rotates reversely, the arcuate workpieces 11 which are mirror-symmetrical are visually displayed to be far away from each other;
the second driving motor 6 is started to rotate forward, and the normal function is to enable the second nipper 52 to ascend through the rotation of the threaded rod 61, so that the distance between the first nipper 51 and the second nipper 52 is shortened, and the function of clamping the fluted disc 7 is achieved; the second driving motor 6 rotates reversely, so that the second nipper 52 is lifted to release the fluted disc 7;
the gear 44 is started, and the gear motor rotates forwards or reversely, so that the screw rod 8 rotates in the hoop member 42 at a small angle, and the visual appearance is that the workpiece block 9 inclines at a certain angle on the base 17;
the electric air rod 151 in the positioning rod 15 is started, so that the rod piece of the electric air rod 151 can be ensured to freely stretch and retract;
s3, penetrating a power line from the base of the triangular bracket 1, penetrating out from the top of the triangular bracket 1, and then connecting the power line to a binding post of the power transmission rod 14; when the power supply connected to the power supply line is in an off state, the contact rod 141 is pressed by a finger, whether the contact rod can be pressed into the power transmission rod 14 body or not, and free ejection can be ensured after the contact rod is released;
s4, when the coaxial unmanned aerial vehicle sends out a low-electricity alarm in mapping work, a first circuit control unit is arranged in the unmanned aerial vehicle main body 16, and the wireless signal module is controlled to send out a signal to search for a positioning signal of a second circuit control unit on the relay platform; the two signals are matched with each other, at the moment, the unmanned aerial vehicle main body 16 controls the rotor wing to fly into the middle position of the arciform workpiece 11 in mirror image arrangement, at the moment, the first driving motor 54 is started to enable the arciform workpiece 11 in mirror image arrangement to be mutually close, in the process of closing, the unmanned aerial vehicle main body 16 is clamped through the rubber roller group 13, at the moment, the electric air rod 151 of the positioning rod 15 starts to extend, and the magnetic sheet 152 at the top end of the electric air rod 151 is abutted against the outer wall of the unmanned aerial vehicle main body 16; by the rotation of the unmanned aerial vehicle main body 16, the up-and-down positioning is performed; the rotation and up-down positioning described herein are both the result of mutual cooperative control of the first circuit control unit and the second circuit control unit, so that the magnetic sheet 152 corresponds to the magnetic induction area 162, and at this time, the contact rod 141 of the power feeding rod 14 just collides with the power receiving copper sheet 161 to have a correct position, and power transmission begins.
S5, the start-stop assistance and locking of the mapping coaxial unmanned aerial vehicle.
The angle deflection control of the screw rod 8 on the hoop member 42 can be controlled by starting the gear 44 built-in gear motor, and the stability of the transverse wind of the weather can be assisted by the inclined arrangement structure of a certain angle of the two arciform workpieces 11 which are arranged in a mirror image manner when the unmanned aerial vehicle main body 16 is started and stopped on the relay platform;
starting the second driving motor 6 to enable the second clamp plate 52 and the first clamp plate 51 to be close to each other, so as to clamp the fluted disc 7; the indirect effect is represented by the inclination locking of the workpiece block 9, so that the stability of the arcuate workpiece 11 is ensured.
The foregoing has shown and described the basic principles, principal features and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present invention, and various changes and modifications may be made without departing from the spirit and scope of the invention, which is defined in the appended claims. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides a survey and drawing unmanned aerial vehicle benefit can relay platform, its main structure includes: the tripod (1) and Y-shaped bracket (3) fixed with the tripod (1) through the turntable (2), and bases (17) are fixed at two top ends of the Y-shaped bracket (3), and the tripod is characterized in that: the screw rod box (4) and the jaw driver (5) are fixed on the base (17);
a screw rod (8) is penetrated in the screw rod box (4), and a fluted disc (7) is screwed on the screw rod (8); the top end of the screw rod (8) is fixed at the middle position of the workpiece block (9), the upper end and the lower end of the workpiece block (9) are hinged with a U-shaped bracket module through a movable hinge (10), a threaded rod (12) with a handle is penetrated into the tail end of an arch-shaped workpiece (11) of the U-shaped bracket module, the threaded rod (12) with the handle is screwed into the tail end of the workpiece block (9), and a second spring seat (121) is arranged between the tail end of the workpiece block (9) and the lower part of the arch-shaped workpiece (11); the two U-shaped bracket modules encircle and clamp the unmanned aerial vehicle main body (16);
the screw box (4) is formed by: a hoop member (42) is fixed in the square cavity (41), and an arc-shaped rack (43) is arranged at the notch position of the hoop member (42); the center of the inner concave surface of the arc-shaped rack (43) is fixedly provided with a biting tooth, and the outer convex surface of the arc-shaped rack (43) is meshed with a gear (44); the gear (44) is driven by a speed reducing motor arranged in the Fang Xingqiang body (41);
the clamp driver (5) comprises: a first spring seat (53) is fixed between the first clamp plate (51) and the second clamp plate (52), a second driving motor (6) is fixed on the first clamp plate (51), a rotating shaft of the second driving motor (6) is a threaded rod (61), and the threaded rod (61) penetrates through the first clamp plate (51) and the first spring seat (53) and then is screwed with a thread groove formed in the second clamp plate (52); a first driving motor (54) is fixed at one end of the first clamp plate (51), a rotating shaft of the first driving motor (54) is a worm (541), the worm (541) penetrates through the first clamp plate (51) and the second clamp plate (52), and the worm (541) is engaged with the fluted disc (7) in a cross manner; the fluted disc (7) is positioned between the first nipper (51) and the second nipper (52);
the U-shaped bracket module comprises: a positioning rod (15) is arranged at the concave center of the arched workpiece (11), rubber roller groups (13) are respectively arranged at the two ends of the arched workpiece (11), and power transmission rods (14) are respectively arranged at the two ends of the arched workpiece (11); the positioning rod (15) comprises an electric air rod (151), and a magnetic sheet (152) is arranged at the tail end of the electric air rod (151); the power transmission rod (14) is inserted with a feeler lever (141), and a spring seat is abutted between the feeler lever (141) and the power transmission rod (14);
an electric copper sheet (161) and a magnetic induction area (162) are arranged on the outer wall of the unmanned aerial vehicle main body (16); the electric connection copper sheet (161) is matched with the top end of the feeler lever (141); the magnetic induction area (162) is matched with the magnetic sheet (152);
the unmanned aerial vehicle comprises an unmanned aerial vehicle main body (16), wherein a first circuit control unit is arranged in the unmanned aerial vehicle main body (16), and takes a magnetic induction area (162) as a signal collecting end to control a rotor wing on the unmanned aerial vehicle main body (16) to adjust the gesture; the circuit control unit also controls a wireless signal module and a positioning module; the Y-shaped support (3) is provided with a second circuit control unit, and the second circuit control unit is also connected and controlled with a wireless signal module and a positioning module.
2. The unmanned aerial vehicle surveying and mapping energy supplementing relay platform according to claim 1, wherein the hoop member (42) and the first arc-shaped rack (43) form a hole groove, a screw (8) penetrates into the hole groove, a screw groove (81) is formed in the screw (8), and the screw groove (81) is matched with the biting teeth (431).
3. The unmanned aerial vehicle surveying and mapping energy supplementing relay platform according to claim 1 is characterized in that a bearing is arranged in the turntable (2), and a bottom rod piece of a Y-shaped bracket (3) is fixed in the bearing; the triangular bracket (1) is formed by welding three rods which form an included angle of 120 degrees, and a circular groove is formed in the center point of welding; a bearing is arranged in the circular groove; and the bearing is provided with a limiting bolt.
4. The mapping unmanned aerial vehicle energy supplementing relay platform according to claim 1 is characterized in that a power supply input is connected to the outside of the power transmission rod (14); the unmanned aerial vehicle main body (16) is a coaxial unmanned aerial vehicle.
5. The application method of the mapping unmanned aerial vehicle energy supplementing relay platform according to any one of claims 1 to 4 comprises the following steps:
s1, firstly, placing the triangular bracket (1) in a working area of a mapping unmanned aerial vehicle; and the bottom of the optional triangular bracket (1) is provided with a structure of a fixing device for locking the fixing device; then the bottom end of the Y-shaped bracket (3) is inserted into a bearing at the center of the triangular bracket (1), and a limit bolt is arranged, so that the Y-shaped bracket (3) can be positioned and fixed on the triangular bracket (1);
s2, debugging whether the functions of the electric accessories are normal or not:
the first driving motor (54) is started to rotate forwards, the normal function of the first driving motor is that the screw (541) can drive the fluted disc (7) to be screwed, the screw driving the fluted disc (7) is indirectly represented by the fact that the screw (8) is ejected from the screw box (4) to the workpiece block (9), and the visual display is that the arciform workpieces (11) which are mirror symmetry are mutually closed; conversely, when the first driving motor (54) reversely rotates, the arc-shaped workpieces (11) which are in mirror symmetry are visually displayed to be far away from each other;
the second driving motor (6) is started to rotate forwards, and the second nipper (52) can be lifted up by rotating the threaded rod (61), so that the distance between the first nipper (51) and the second nipper (52) is shortened, and the function of clamping the fluted disc (7) is achieved; the second driving motor (6) rotates reversely, so that the second clamp plate (52) is lifted to achieve the function of loosening the fluted disc (7);
the gear (44) is started to internally arranged a speed reducing motor, and the speed reducing motor rotates forwards or reversely, so that the screw (8) rotates in the hoop (42) at a small angle, and the visual appearance is that the workpiece block (9) inclines at a certain angle on the base (17);
an electric air rod (151) in the positioning rod (15) is started, and the rod piece of the electric air rod (151) can be ensured to freely stretch and retract;
s3, penetrating a power line from a base of the triangular bracket (1), penetrating out from the top of the triangular bracket (1), and then connecting the power line to a binding post of the power transmission rod (14); when the power supply connected to the power line is in an off state, the feeler lever (141) is pressed by a finger, whether the feeler lever can be pressed into the power transmission rod (14) body or not is judged, and free ejection can be ensured after the feeler lever is released;
s4, when the coaxial unmanned aerial vehicle sends out a low-electricity alarm in mapping work, a first circuit control unit is arranged in the unmanned aerial vehicle main body (16), and the wireless signal module is controlled to send out a signal to search for a positioning signal of a second circuit control unit on the relay platform; the two signals are matched with each other, at the moment, the unmanned aerial vehicle main body (16) controls the rotor wing to fly into the middle position of the arciform workpiece (11) which is arranged in a mirror mode, at the moment, the first driving motor (54) is started to enable the two arciform workpieces (11) which are arranged in a mirror mode to be close to each other, in the process of closing, the unmanned aerial vehicle main body (16) is clamped through the rubber roller group (13), at the moment, the electric air rod (151) of the positioning rod (15) starts to extend, and the top magnetic sheet (152) of the electric air rod (151) is abutted to the outer wall of the unmanned aerial vehicle main body (16); through the rotation of the unmanned plane main body (16), the position is adjusted up and down; the magnetic sheet (152) corresponds to the magnetic induction area (162), and at the moment, the contact rod (141) of the power transmission rod (14) is just in touch with the power connection copper sheet (161) to have correct position, and power transmission is started;
s5, starting and stopping assistance and locking of the mapping coaxial unmanned aerial vehicle;
the angle deflection control of the control screw (8) on the hoop member (42) is realized by starting a speed reducing motor arranged in the gear (44), and the stability of the weather when the transverse wind appears is assisted in the process of starting and stopping the unmanned aerial vehicle main body (16) on the relay platform by adopting an inclined arrangement structure with a certain angle of two arciform workpieces (11) which are arranged in mirror images;
starting the second driving motor (6) to enable the second clamp plate (52) and the first clamp plate (51) to be close to each other, so as to clamp the fluted disc (7); the indirect effect is represented by the inclination locking of the workpiece block (9), thereby ensuring the stability of the arched workpiece (11).
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