CN114670738B - Unmanned aerial vehicle carrier vehicle and operation method thereof - Google Patents
Unmanned aerial vehicle carrier vehicle and operation method thereof Download PDFInfo
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- CN114670738B CN114670738B CN202210303398.0A CN202210303398A CN114670738B CN 114670738 B CN114670738 B CN 114670738B CN 202210303398 A CN202210303398 A CN 202210303398A CN 114670738 B CN114670738 B CN 114670738B
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- driving
- assembly
- limiting
- unmanned aerial
- wing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P7/00—Securing or covering of load on vehicles
- B60P7/06—Securing of load
- B60P7/135—Securing or supporting by load bracing means
Abstract
The invention discloses an unmanned aerial vehicle carrier vehicle and an operation method thereof, and relates to the technical field of unmanned aerial vehicles. The wing limiting mechanism comprises a first driving component, a second driving component, a wing limiting component and a transmission component; the first driving and rotating components and the second driving and rotating components are arranged in a staggered and parallel manner; the first driving component and the second driving component are arranged on two sides of the wing limiting component; the transmission assembly is in threaded fit with the two wing limiting assemblies, the first driving assembly and the second driving assembly realize rotation of the transmission assembly through up-and-down movement, and the transmission assembly is used for realizing opposite movement of the two wing limiting assemblies. According to the invention, the wing limiting mechanisms are arranged on the two sides of the body supporting table, so that when the body is placed on the body supporting table, the wing limiting mechanisms are utilized to limit the two wings, and in the process of conveying the unmanned aerial vehicle by the carrier vehicle, the inclination unbalance of the wings can be effectively avoided, so that the conveying stability and safety of the unmanned aerial vehicle are greatly improved.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle carrier vehicle and an operation method thereof.
Background
Unmanned aerial vehicle as a radio remote control equipment or self program control device controls unmanned aerial vehicle, can carry out the task under any adverse circumstances, because be unmanned mode, so need not worry casualties.
Unmanned aerial vehicle need carry unmanned aerial vehicle from initial point to terminal point department maintenance or detect in the production process, current unmanned aerial vehicle carrier loader unmanned aerial vehicle removes the in-process, unmanned aerial vehicle's spacing on the carrier loader is mostly through directly placing the fuselage on the supporting seat, the slope unbalance of wing is easily caused because of external environment influences in the carrying process, be unfavorable for unmanned aerial vehicle's safety in transport, current unmanned aerial vehicle carrier loader can not be fine realize the double spacing of fuselage wing, and can't realize the automatic spacing of wing and automatic release spacing in initial point and terminal point department, thereby lead to unmanned aerial vehicle carrier loader's degree of automation lower, be unfavorable for unmanned aerial vehicle's batch transport.
Therefore, we provide an unmanned aerial vehicle carrier vehicle and an operation method thereof, which are used for solving the technical problems.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle carrier vehicle and an operation method thereof, and solves the problems that the unmanned aerial vehicle carrier vehicle is low in automation degree and unfavorable for batch carrying of unmanned aerial vehicles due to the fact that the unmanned aerial vehicle is limited mostly by directly placing a fuselage on a supporting seat, the inclination unbalance of the wing is easily caused by the influence of external environment in the carrying process, the safe conveying of the unmanned aerial vehicle is not facilitated, the double limiting of the wing of the fuselage cannot be well realized, and the automatic limiting and the automatic releasing limiting of the wing cannot be realized at an initial point and a final point through the design of a power assembly, a distance adjusting assembly, a wing limiting assembly and a transmission assembly.
In order to solve the technical problems, the invention is realized by the following technical scheme:
the invention relates to an unmanned aerial vehicle carrier vehicle, which comprises a power mechanism and a wing limiting mechanism; the power mechanism comprises a power assembly and two distance adjusting assemblies, and the two distance adjusting assemblies are symmetrically arranged at the top of the power assembly; the wing limiting mechanisms are arranged at the tops of the corresponding distance adjusting assemblies; the wing limiting mechanism comprises a first driving component, a second driving component, a wing limiting component moving in two phases and a transmission component; the first driving and rotating components and the second driving and rotating components are arranged in a staggered and parallel manner; the first driving and rotating assembly and the second driving and rotating assembly are arranged on two sides of the wing limiting assembly; the transmission assembly is in threaded fit with the two wing limiting assemblies, the first driving assembly and the second driving assembly realize rotation of the transmission assembly through up-and-down movement, and the transmission assembly is used for realizing opposite movement of the two wing limiting assemblies.
Further, the power assembly comprises a carrying frame, guide seats are fixed at the positions, close to two ends, of the bottom of the carrying frame, and the guide seats are in sliding fit on the rails; the central position of the bottom of the carrying frame is fixedly provided with power equipment, the central position of the top of the carrying frame is provided with a frame body supporting table, and the power equipment is used for realizing the movement of a power assembly on a track.
Further, the distance adjusting assembly comprises a supporting table, a limiting slideway is arranged at the top of the supporting table, a plurality of fixing holes are formed in the surface of the supporting table, and the fixing holes are communicated with the limiting slideway; the wing limiting mechanism further comprises a hollow fixed table, a supporting seat which is in sliding fit with the limiting slide way is fixed at the bottom of the hollow fixed table, and the supporting seat is connected with the fixed hole through a locking piece.
Further, guide pore channels are formed in two opposite side surfaces of the hollow fixed table, and two through holes are formed in the top of the hollow fixed table; the inner bottom of the hollow fixed table is respectively provided with a first elastic piece and a second elastic piece, the first elastic piece corresponds to the first driving and rotating assembly, and the second elastic piece corresponds to the second driving and rotating assembly.
Further, the first driving assembly and the second driving assembly both comprise inclined moving tables, and limiting guide blocks which are in sliding fit with corresponding guide pore canals are fixed on the surfaces of the inclined moving tables; the surface of the inclined plane moving table is fixedly provided with a driving gear column through a supporting rod, and the driving gear column is in sliding fit with a corresponding through hole above the driving gear column; the inclined plane mobile station surface is fixed with the connecting seat, the connecting seat bottom on the first drive the commentaries on classics subassembly and the corresponding elastic component upper end fixed connection, the connecting seat bottom on the second drive the commentaries on classics subassembly and the corresponding elastic component upper end fixed connection No. two.
Further, two sliding pore canals are symmetrically arranged at the top of the hollow fixed table; the wing limiting assembly comprises a limiting plate, and an internal thread seat in sliding fit with the sliding pore canal is fixed at the bottom of the limiting plate; the transmission assembly comprises a thread adjusting column which is in threaded fit with the two inner thread seats.
Further, a first gear is fixed at one end of the thread adjusting column and meshed with a driving gear column on the first driving assembly; a second gear is fixed at the other end of the thread adjusting column and meshed with a driving gear column on the second driving assembly; the rotation direction of the first gear driving screw thread adjusting column is opposite to that of the second gear driving screw thread adjusting column.
The invention has the following beneficial effects:
1. according to the invention, the wing limiting mechanisms are arranged on the two sides of the body supporting table, so that when the body is placed on the body supporting table, the wing limiting mechanisms are utilized to limit the two wings, and in the process of conveying the unmanned aerial vehicle by the carrier vehicle, the inclination unbalance of the wings can be effectively avoided, so that the conveying stability and safety of the unmanned aerial vehicle are greatly improved.
2. According to the invention, through the design of the first driving component, the second driving component, the transmission component, the first elastic component, the second elastic component and the wing limiting component, the inclined extrusion table is utilized to push the first driving component to move up and down when the carrier vehicle moves to the initial point, so that the two wing limiting components are driven to automatically limit the wings, and the inclined extrusion table is utilized to push the second driving component to move up and down when the carrier vehicle moves to the final point, so that the two wing limiting components are driven to automatically release the limit of the wings, thereby greatly increasing the automation degree of the carrier vehicle of the unmanned aerial vehicle and being beneficial to batch carrying of unmanned aerial vehicles.
3. According to the invention, the horizontal distance between the two wing limiting mechanisms is adjusted along the limiting slide way, so that carrying and conveying of unmanned aerial vehicles with different sizes are realized, and the application range of the unmanned aerial vehicle carrying vehicle is increased.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are needed for the description of the embodiments 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 that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle carrier vehicle.
Fig. 2 is a structural top view of the unmanned aerial vehicle carrier.
Fig. 3 is a schematic structural view of the power mechanism.
Fig. 4 is a side view of the structure of fig. 3.
Fig. 5 is a schematic diagram of the internal structure of the pitch adjustment assembly on the power mechanism.
Fig. 6 is a schematic structural view of a wing limit mechanism.
Fig. 7 is a top view of the structure of fig. 6.
Fig. 8 is a front view of the structure of fig. 6.
Fig. 9 is a side view of the structure of fig. 6.
In the drawings, the list of components represented by the various numbers is as follows:
the device comprises a 1-power mechanism, a 11-power component, a 111-carrying frame, a 112-guide seat, 113-power equipment, 114-a body supporting table, a 12-distance adjusting component, a 121-supporting table, 122-limiting slide ways, 123-fixing holes, a 2-wing limiting mechanism, a 201-hollow fixing table, a 202-guiding hole, a 203-through hole, a 204-first elastic piece, a 205-second elastic piece, a 206-sliding hole, a 21-first driving and rotating component, a 211-inclined plane moving table, 212-limiting guide blocks, 213-driving and rotating tooth columns, 214-connecting seats, 22-second driving and rotating components, 23-wing limiting components, 231-limiting plates, 232-internal thread seats, 24-transmission components, 241-thread adjusting columns, 242-first gears and 243-second gears.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Embodiment 1 an unmanned aerial vehicle carrier vehicle
Referring to fig. 1-9, the invention discloses an unmanned aerial vehicle carrier vehicle, which comprises a power mechanism 1 and two wing limiting mechanisms 2; the power mechanism 1 is used for realizing the bidirectional movement of the whole unmanned aerial vehicle carrier vehicle, and the wing limiting mechanism 2 is used for realizing the limiting of the wings;
the power mechanism 1 comprises a power assembly 11 and two distance adjusting assemblies 12, wherein the two distance adjusting assemblies 12 are symmetrically arranged at the top of the power assembly 11; the wing limiting mechanisms 2 are arranged at the tops of the corresponding distance adjusting assemblies 12; the horizontal distance between the two wing limiting mechanisms 2 is adjusted, so that carrying and conveying of unmanned aerial vehicles with different sizes are realized, and the application range of the unmanned aerial vehicle carrying vehicle is increased;
the wing limiting mechanism 2 comprises a first driving component 21, a second driving component 22, a wing limiting component 23 which moves in opposite directions and a transmission component 24; the first driving and rotating assembly 21 and the second driving and rotating assembly 22 are arranged in a staggered and parallel mode, the first driving and rotating assembly 21 is matched with an inclined plane extrusion table at the initial conveying point of the unmanned aerial vehicle, and the second driving and rotating assembly 22 is matched with an inclined plane extrusion table at the final conveying point of the unmanned aerial vehicle; the first driving component 21 and the second driving component 22 are arranged on two sides of the wing limiting component 23; the transmission assembly 24 is in threaded fit with the two wing limiting assemblies 23, the two wing limiting assemblies 23 move in opposite directions through rotation of the transmission assembly 24, further the two wing limiting assemblies 23 are unfolded and folded, the first driving assembly 21 and the second driving assembly 22 move up and down to achieve rotation of the transmission assembly 24, and the transmission assembly 24 is used for achieving opposite movement of the two wing limiting assemblies 23.
In this embodiment, the power assembly 11 includes a carrier 111, and guide holders 112 are fixed at positions near two ends of the bottom of the carrier 111, and the guide holders 112 are slidably engaged with the rails;
a power device 113 is fixedly arranged at the center of the bottom of the carrier 111, and the power device 113 is used for realizing the movement of the power assembly 11 on a track; when the power equipment 113 moves the carrier vehicle to the initial point of unmanned aerial vehicle conveying, the two opposite first driving and rotating assemblies 21 move upwards synchronously to realize automatic unfolding of the wing limiting assemblies 23, after the two wings of the unmanned aerial vehicle are placed between the two wing limiting assemblies 23 on the wing limiting mechanism 2, when the power equipment 113 moves the carrier vehicle away from the initial point of conveying, the first driving and rotating assemblies 21 move downwards to reset so as to enable the wing limiting assemblies 23 to automatically fold, and further automatic limiting of the wings is realized; when the power equipment 113 moves the carrier vehicle to the unmanned aerial vehicle conveying end point, the two opposite second driving and rotating assemblies 22 move upwards synchronously to realize automatic unfolding of the wing limiting assemblies 23, and after the unmanned aerial vehicle between the wing limiting assemblies 23 is removed, when the power equipment 113 moves the carrier vehicle away from the conveying end point, the second driving and rotating assemblies 22 move downwards to reset to enable the wing limiting assemblies 23 to automatically fold, and automatic carrying and conveying of the unmanned aerial vehicle at the two points are realized in the mode.
In this embodiment, a body supporting table 114 is installed at the center of the top of the carrier 111, and is used for supporting the body of the unmanned aerial vehicle during the carrying process of the unmanned aerial vehicle;
the distance adjusting assembly 12 comprises a supporting table 121, a limiting slideway 122 is arranged at the top of the supporting table 121, a plurality of fixing holes 123 are formed in the surface of the supporting table 121, and the fixing holes 123 are communicated with the limiting slideway 122; the wing limiting mechanism 2 further comprises a hollow fixed table 201, a supporting seat 207 in sliding fit with the limiting slideway 122 is fixed at the bottom of the hollow fixed table 201, and the supporting seat 207 is connected with the fixed hole 123 through a locking piece; after the distance adjusting component 12 is moved to a required position along the limiting slide way 122, locking and fixing between the supporting seat 207 and the fixing hole 123 are achieved through locking pieces.
In this embodiment, guide channels 202 are disposed on two opposite sides of the hollow fixing table 201, and two through holes 203 are disposed on the top of the hollow fixing table 201;
the inner bottom of the hollow fixed table 201 is respectively provided with a first elastic piece 204 and a second elastic piece 205, the first elastic piece 204 corresponds to the first driving and rotating assembly 21, and the second elastic piece 205 corresponds to the second driving and rotating assembly 22; when the first driving component 21 moves up, the first driving component 21 can be moved down to reset by the elastic restoring force of the first elastic member 204 and the self gravity of the first driving component 21, and when the second driving component 22 moves up, the second driving component 22 can be moved down to reset by the elastic restoring force of the second elastic member 205 and the self gravity of the second driving component 22.
In this embodiment, the first driving component 21 and the second driving component 22 each include an inclined moving platform 211, and a limiting guide block 212 slidably matched with the corresponding guide channel 202 is fixed on the surface of the inclined moving platform 211, so as to ensure stable up-and-down movement of the first driving component 21 and the second driving component 22;
the surface of the inclined plane moving table 211 is fixed with a driving gear column 213 through a supporting rod, and the driving gear column 213 is in sliding fit with a corresponding through hole 203 above; the surface of the inclined plane moving table 211 is fixedly provided with a connecting seat 214, the bottom of the connecting seat 214 on the first driving and rotating assembly 21 is fixedly connected with the upper end of the corresponding first elastic piece 204, and the bottom of the connecting seat 214 on the second driving and rotating assembly 22 is fixedly connected with the upper end of the corresponding second elastic piece 205.
In this embodiment, two sliding channels 206 are symmetrically arranged on the top of the hollow fixing table 201; the wing limiting assembly 23 comprises a limiting plate 231, and an internal thread seat 232 in sliding fit with the sliding duct 206 is fixed at the bottom of the limiting plate 231;
the transmission assembly 24 comprises a threaded adjusting column 241, and the threaded adjusting column 241 is in threaded fit with two inner threaded seats 232; one end of the screw thread adjusting column 241 is fixed with a first gear 242, and the first gear 242 is meshed with the driving gear column 213 on the first driving component 21; when the first rotation driving assembly 21 moves upwards, the corresponding rotation driving tooth column 213 drives the first gear 242 to rotate, so that the two wing limiting assemblies 23 are unfolded, and when the first rotation driving assembly 21 moves downwards, the corresponding rotation driving tooth column 213 drives the first gear 242 to reversely rotate, so that the two wing limiting assemblies 23 are folded;
the other end of the screw thread adjusting column 241 is fixed with a second gear 243, and the second gear 243 is meshed with a driving gear column 213 on the second driving component 22; when the second driving component 22 moves upwards, the corresponding driving tooth column 213 drives the second gear 243 to rotate, so that the two wing limiting components 23 are unfolded, and when the second driving component 22 moves downwards, the corresponding driving tooth column 213 drives the second gear 243 to rotate reversely, so that the two wing limiting components 23 are folded;
the first gear 242 drives the screw adjusting column 241 to rotate in a direction opposite to the direction in which the second gear 243 drives the screw adjusting column 241.
Implementation 2 of operation method of unmanned aerial vehicle carrier
An operation method of an unmanned aerial vehicle carrier vehicle comprises the following steps:
when the SS01 power equipment 113 drives the carrier vehicle to move to the initial point, the inclined plane moving table 211 on the first driving and rotating assembly 21 on the two opposite wing limit assemblies 23 is in extrusion fit with the inclined plane extrusion table at the initial point, so that the inclined plane moving table 211 on the first driving and rotating assembly 21 moves upwards;
the driving gear column 213 on the inclined moving platform 211 moving upwards by SS02 drives the corresponding first gear 242 to rotate, so that the two limiting plates 231 move reversely to be unfolded, the airframe is placed on the airframe supporting platform 114, and the wings are placed between the two limiting plates 231 on the hollow fixed platform 201;
when the power equipment 113 drives the carrier vehicle to move from an initial point to a final point, the inclined extrusion table at the initial point is separated from the first driving and rotating assembly 21, the whole first driving and rotating assembly 21 moves downwards to reset under the elastic restoring force of the first elastic piece 204 and the gravity of the inclined moving table 211, and the two limiting plates 231 are folded to limit the wings;
when the power equipment 113 drives the carrier vehicle to move to the destination, the second driving component 22 is matched with the inclined extrusion table at the destination in an extrusion mode, the driving tooth column 213 on the upward inclined moving table 211 drives the corresponding second gear 243 to rotate, the two limiting plates 231 are reversely moved and unfolded to achieve grabbing of the unmanned aerial vehicle, and when the second driving component 22 is separated from the inclined extrusion table at the destination, the two limiting plates 231 are folded again under the elastic restoring force of the second elastic piece 205 and the gravity of the inclined moving table 211;
and (5) circulating the steps SS01-SS04 by the SS05 to realize the carrying operation of the batched unmanned aerial vehicles.
The preferred embodiments of the invention disclosed above are intended only to assist in the explanation of the invention. The preferred embodiments are not exhaustive or to limit the invention to the precise form disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and the practical application, to thereby enable others skilled in the art to best understand and utilize the invention. The invention is limited only by the claims and the full scope and equivalents thereof.
Claims (7)
1. An unmanned aerial vehicle carrier loader, its characterized in that: comprising the following steps:
the power mechanism (1) comprises a power assembly (11), two distance adjusting assemblies (12), wherein the two distance adjusting assemblies (12) are symmetrically arranged at the top of the power assembly (11);
the two wing limiting mechanisms (2), wherein the wing limiting mechanisms (2) are arranged at the tops of the corresponding distance adjusting assemblies (12); the wing limiting mechanism (2) comprises a first driving and rotating assembly (21) and a second driving and rotating assembly (22), wherein the first driving and rotating assembly (21) and the second driving and rotating assembly (22) are arranged in a staggered and parallel mode;
the two wing limiting assemblies (23) move in opposite directions, and the first driving assembly (21) and the second driving assembly (22) are arranged on two sides of the wing limiting assemblies (23);
the transmission assembly (24) is in threaded fit with the two wing limiting assemblies (23), the first driving assembly (21) and the second driving assembly (22) realize rotation of the transmission assembly (24) through up-down movement, and the transmission assembly (24) is used for realizing opposite movement of the two wing limiting assemblies (23);
the wing limiting mechanism (2) further comprises a hollow fixed table (201), wherein a first elastic piece (204) and a second elastic piece (205) are respectively arranged at the inner bottom of the hollow fixed table (201), the first elastic piece (204) corresponds to the first driving and rotating assembly (21), and the second elastic piece (205) corresponds to the second driving and rotating assembly (22);
the first driving assembly (21) and the second driving assembly (22) comprise inclined moving tables (211), and driving tooth columns (213) are fixed on the surfaces of the inclined moving tables (211) through supporting rods;
two sliding pore canals (206) are symmetrically arranged at the top of the hollow fixed table (201); the wing limiting assembly (23) comprises a limiting plate (231), and an internal thread seat (232) which is in sliding fit with the sliding duct (206) is fixed at the bottom of the limiting plate (231);
the transmission assembly (24) comprises a threaded adjusting column (241), and the threaded adjusting column (241) is in threaded fit with two inner threaded seats (232);
one end of the thread adjusting column (241) is fixed with a first gear (242), and the first gear (242) is meshed with a driving gear column (213) on the first driving assembly (21); a second gear (243) is fixed at the other end of the thread adjusting column (241), and the second gear (243) is meshed with a driving gear column (213) on the second driving assembly (22);
the first gear (242) drives the screw thread adjusting column (241) to rotate in the opposite direction to the second gear (243) drives the screw thread adjusting column (241).
2. The unmanned aerial vehicle carrier vehicle according to claim 1, wherein the power assembly (11) comprises a carrier (111), guide seats (112) are fixed at positions, close to two ends, of the bottom of the carrier (111), and the guide seats (112) are in sliding fit on a rail;
and a power device (113) is fixedly arranged at the bottom center of the carrying frame (111), and the power device (113) is used for realizing the movement of the power assembly (11) on a track.
3. The unmanned aerial vehicle carrier of claim 2, wherein a fuselage cradle (114) is mounted in a top center position of the carrier (111);
the distance adjusting assembly (12) comprises a supporting table (121), a limiting slide way (122) is arranged at the top of the supporting table (121), a plurality of fixing holes (123) are formed in the surface of the supporting table (121), and the fixing holes (123) are communicated with the limiting slide way (122).
4. A vehicle according to claim 3, wherein two opposite sides of the hollow fixed platform (201) are provided with guiding channels (202), and two through holes (203) are provided at the top of the hollow fixed platform (201);
the bottom of the hollow fixed table (201) is fixed with a supporting seat (207) which is in sliding fit with the limiting slide way (122), and the supporting seat (207) is connected with the fixed hole (123) through a locking piece.
5. The unmanned aerial vehicle carrier of claim 4, wherein the inclined surface moving table (211) has a fixed limit guide block (212) slidably engaged with the corresponding guide duct (202).
6. The unmanned aerial vehicle carrier of claim 5, wherein the steering gear post (213) is in sliding engagement with the corresponding upper through hole (203);
the inclined plane moving table (211) surface is fixed with connecting seat (214), connecting seat (214) bottom and the corresponding elastic component (204) upper end fixed connection on first drive and change subassembly (21), connecting seat (214) bottom and the corresponding elastic component (205) upper end fixed connection on second drive and change subassembly (22).
7. The method of operation of a drone cart of claim 6, comprising the steps of:
when SS01 power equipment (113) drives the carrier vehicle to move to an initial point, an inclined plane moving table (211) on a first driving component (21) on two opposite wing limit components (23) is in extrusion fit with an inclined plane extrusion table at the initial point, so that the inclined plane moving table (211) on the first driving component (21) moves upwards;
the driving gear column (213) on the inclined moving platform (211) moving upwards by SS02 drives the corresponding first gear (242) to rotate, so that the two limiting plates (231) move reversely to be unfolded, the airframe is placed on the airframe supporting platform (114), and the wings are placed between the two limiting plates (231) on the hollow fixed platform (201);
when the power equipment (113) drives the carrier vehicle to move from an initial point to a final point, the inclined extrusion table at the initial point is separated from the first driving component (21), the whole first driving component (21) moves downwards to reset under the elastic restoring force of the first elastic piece (204) and the self gravity of the inclined moving table (211), and the two limiting plates (231) are folded to limit the wing;
when the power equipment (113) drives the carrier vehicle to move to the end point, the second driving component (22) is in extrusion fit with the inclined plane extrusion table at the end point, the driving gear column (213) on the upward inclined plane moving table (211) drives the corresponding second gear (243) to rotate, the two limiting plates (231) are reversely moved and unfolded to achieve grabbing of the unmanned aerial vehicle, and when the second driving component (22) is separated from the inclined plane extrusion table at the end point, the two limiting plates (231) are folded again under the elastic restoring force of the second elastic piece (205) and the self gravity of the inclined plane moving table (211);
and (5) circulating the steps SS01-SS04 by the SS05 to realize the carrying operation of the batched unmanned aerial vehicles.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210303398.0A CN114670738B (en) | 2022-03-24 | 2022-03-24 | Unmanned aerial vehicle carrier vehicle and operation method thereof |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210303398.0A CN114670738B (en) | 2022-03-24 | 2022-03-24 | Unmanned aerial vehicle carrier vehicle and operation method thereof |
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| CN114670738B true CN114670738B (en) | 2023-07-25 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN213413853U (en) * | 2020-10-14 | 2021-06-11 | 宿迁旋飞智能科技有限公司 | Special transport vechicle device of unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US20150151666A1 (en) * | 2013-12-02 | 2015-06-04 | Brian Stenger | Auto adjusting multiple purpose holder |
| US10126746B2 (en) * | 2016-12-01 | 2018-11-13 | Walmart Apollo, Llc | Autonomous drone and tool selection and delivery |
| CN109436068B (en) * | 2018-11-16 | 2024-01-26 | 浙江云来集科技有限公司 | Unmanned aerial vehicle positioning protection device and application method thereof |
| CN211166641U (en) * | 2019-11-12 | 2020-08-04 | 石家庄亚光速科技有限公司 | Carrier-borne helicopter analog equipment transportation platform |
| CN111301078B (en) * | 2019-12-11 | 2021-05-25 | 国网陕西省电力公司电力科学研究院 | Carrying platform of combined type fixed wing unmanned aerial vehicle and operation method thereof |
| CN112644732A (en) * | 2021-01-05 | 2021-04-13 | 徐艳 | Vehicle-mounted multi-rotor unmanned aerial vehicle take-off and landing platform |
| CN214355741U (en) * | 2021-02-25 | 2021-10-08 | 任玉龙 | A transfer device for civil engineering reinforced bar material |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN213413853U (en) * | 2020-10-14 | 2021-06-11 | 宿迁旋飞智能科技有限公司 | Special transport vechicle device of unmanned aerial vehicle |
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