CN114313288A - Full-automatic airport of trading of unmanned aerial vehicle - Google Patents
Full-automatic airport of trading of unmanned aerial vehicle Download PDFInfo
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- CN114313288A CN114313288A CN202210041971.5A CN202210041971A CN114313288A CN 114313288 A CN114313288 A CN 114313288A CN 202210041971 A CN202210041971 A CN 202210041971A CN 114313288 A CN114313288 A CN 114313288A
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- unmanned aerial
- aerial vehicle
- battery
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- clamping mechanism
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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
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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
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
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Abstract
The invention relates to a full-automatic battery replacing airport for an unmanned aerial vehicle, which comprises a cabin and a movable cabin door, wherein an unmanned aerial vehicle positioning mechanism, a lifting mechanism, a battery charging and replacing mechanism and a support are arranged in the cabin, the unmanned aerial vehicle positioning mechanism is used for clamping a base of the unmanned aerial vehicle after the unmanned aerial vehicle lands, the unmanned aerial vehicle positioning mechanism comprises a longitudinal clamping mechanism, a transverse clamping mechanism and a lifting platform, the lifting platform is fixed in the cabin through the support, the lifting mechanism is arranged below the longitudinal clamping mechanism and used for driving the longitudinal clamping mechanism to move up and down, and the battery charging and replacing mechanism is arranged below the longitudinal clamping mechanism and vertical to the longitudinal clamping mechanism and used for charging and replacing batteries of the unmanned aerial vehicle. And the battery is charged and replaced through the charging and replacing mechanism, the battery is not clamped by the mechanical arm, the control logic is simple, and the stability is strong.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a full-automatic battery replacement airport for an unmanned aerial vehicle.
Background
With the increase of cognition on the application value of the unmanned aerial vehicle, the unmanned aerial vehicle has the rapid development trend in the consumption level market, the industrial level market and the military level market. Unmanned aerial vehicles are increasingly being used in many fields.
But unmanned aerial vehicle's duration becomes the biggest bottleneck that hinders unmanned aerial vehicle development, though lithium battery is the best battery of comprehensive properties on the existing market, still can't satisfy unmanned aerial vehicle duration demand completely, consequently must consider unmanned aerial vehicle problem of charging in the unmanned aerial vehicle use.
At present, the battery replacement of the unmanned aerial vehicle has the following defects: unmanned aerial vehicle need frequently charge, trade the battery, according to traditional mode by the manual battery that trades that needs huge human input of staff, and need personnel on duty, can't work in the field for a long time. In addition, the battery at current unmanned aerial vehicle airport all is put into solitary charging inslot and charges, when unmanned aerial vehicle need return to the journey and trade the battery, unmanned aerial vehicle falls on unmanned aerial vehicle airport take off and land the platform after, whole take off and land the platform and drive unmanned aerial vehicle and descend to the inside automatic battery replacement operation that carries on in unmanned aerial vehicle airport, lead to unmanned aerial vehicle airport size very big, need hold the space of taking off and land the platform, the holistic size in full-automatic unmanned aerial vehicle cabin and weight have been increased, the cost also increases. After the whole take-off and landing platform drives the unmanned aerial vehicle to land, the mechanical arm works to clamp the battery and puts into the charging groove, and the clamp is got the battery that has been fully charged again and is put back in the unmanned aerial vehicle. The battery is clamped and stored through the mechanical arm, the operation program and the operation track of the mechanical arm are controlled to be very complex, and the unmanned aerial vehicle airport is large in size and very expensive in manufacturing cost. Moreover, because there is certain position error after unmanned aerial vehicle descends, the unable accurate clamp of arm gets the battery, also gives unmanned aerial vehicle and from moving the battery and bring a difficult problem, need adopt complicated process to make unmanned aerial vehicle descend to accurate position.
Disclosure of Invention
The invention aims to provide the unmanned aerial vehicle automatic battery replacing device which is low in cost, small in space, compact in structure, simple in control logic without a mechanical arm and strong in stability. Aim at solving among the prior art unmanned aerial vehicle and trade the electric process complicacy and need wholly descend to the platform of taking off and land that unmanned aerial vehicle descends and trade the technical problem of electricity.
In order to achieve the purpose, the invention adopts the technical scheme that: the unmanned aerial vehicle full-automatic battery replacing airport comprises a cabin and a movable cabin door, wherein an unmanned aerial vehicle positioning mechanism, a lifting mechanism, a battery charging and replacing mechanism and a support are arranged in the cabin, the unmanned aerial vehicle positioning mechanism is used for clamping an unmanned aerial vehicle base after the unmanned aerial vehicle lands, and comprises a longitudinal clamping mechanism, a transverse clamping mechanism and a lifting platform, the lifting platform is fixed in the cabin through the support, a through hole is formed in the center of the lifting platform, the longitudinal clamping mechanism is located in the through hole and used for longitudinally clamping and loosening the unmanned aerial vehicle base, and the longitudinal clamping mechanism is driven to move up and down through the through hole through the lifting mechanism; the transverse clamping mechanism is arranged on the upper surface of the lifting platform and moves transversely and reciprocally to clamp and loosen the unmanned aerial vehicle base; the lifting mechanism is arranged below the longitudinal clamping mechanism and used for driving the longitudinal clamping mechanism to move up and down, and the battery charging and replacing mechanism is arranged below the longitudinal clamping mechanism and vertical to the longitudinal clamping mechanism and used for charging and replacing the unmanned aerial vehicle battery.
Further, the longitudinal clamping mechanism comprises two clamping parts, two first sliding blocks, two lead screws and two first motors which are symmetrically arranged, the two first motors respectively drive the two lead screws to move, the two lead screws are respectively provided with the two first sliding blocks, and the two first sliding blocks respectively drive the two clamping parts to move to clamp or loosen the unmanned aerial vehicle base; be equipped with the spout on the platform of taking off and land, horizontal clamping mechanism includes two horizontal poles, four second sliders that the symmetry set up, four second sliders are connected with four ends of two horizontal poles respectively, and the spout internal motion for unmanned aerial vehicle drops on and promotes unmanned aerial vehicle behind the platform of taking off and land and move in the middle of returning to the place.
Further, clamping part is the wedge, is equipped with V type groove on the unmanned aerial vehicle upper base, and when needs fixed unmanned aerial vehicle, clamping part removes to V type inslot clamping unmanned aerial vehicle under the drive of first motor.
Further, the lifting mechanism comprises a lifting rod, and the lifting rod moves under the pushing of a motor of the lifting mechanism, so that the longitudinal clamping mechanism moves upwards and downwards.
Further, it includes battery module, battery module mounting and battery slip table subassembly to fill to trade electrical mechanism, the battery module includes the battery case and arranges the battery of battery box internal electricity connection in, be equipped with joint portion on the battery case, battery module mounting includes the bottom plate, establish the clamping part on the bottom plate, joint portion shape adaptation on clamping part and the battery case, the bottom plate lower surface is equipped with the actuating mechanism drive the horizontal back and forth movement of battery module mounting, battery slip table subassembly includes slide rail bracket bottom plate, slide rail bracket bottom plate both ends are equipped with slide rail bracket end plate respectively, slide rail bracket end plate to slide rail bracket bottom plate direction extends and is equipped with electrically conductive slide rail, the battery module is in under the drive of battery module mounting along electrically conductive slide rail removes.
Furthermore, electrode plates are arranged on the other two sides of the battery box, the conductive slide rails are in sliding fit with the electrode plates, and the battery is charged through the electrode plates.
Further, battery module quantity is two or more, two or more battery modules pass through joint portion end to end adaptation joint in proper order.
Furthermore, actuating mechanism includes second motor and motor shaft, the second motor drives the motor shaft and just reverses the motion, and the motor shaft passes through the horizontal back and forth motion of bottom plate drive battery module mounting.
Furthermore, a sliding rail support is further arranged on the sliding rail support bottom plate, and the conductive sliding rail is fixed in the sliding rail support.
Furthermore, the number of the conductive slide rails is eight, and the space enclosed by every four conductive slide rails is matched with the shape of the battery box.
The invention has the beneficial effects that: the full-automatic battery changing field of the unmanned aerial vehicle is characterized in that through holes are formed in the lifting platform, and the unmanned aerial vehicle moves into the through holes under the sequential action of the transverse clamping mechanism and the longitudinal clamping mechanism. Need not whole platform of taking off and land to descend and trade the electricity, only vertical clamping mechanism presss from both sides tight unmanned aerial vehicle base downward motion and trades the electricity, can effectively reduce full-automatic unmanned aerial vehicle airport's whole weight, save space. In unmanned aerial vehicle battery jar is arranged in to the battery module, when needing to trade the battery, unmanned aerial vehicle takes the battery module to move down through elevating system's drive, battery module mounting horizontal movement, the distance of battery module that battery slip table subassembly slided right, the battery module that needs to charge in the unmanned aerial vehicle moves right in step, the battery module that is full of electricity inserts in the unmanned aerial vehicle battery jar, unmanned aerial vehicle upward movement carries out the flight task behind the platform that takes off and land under elevating system's effect, accomplish once trade electric operating procedure. This simple structure, it is with low costs, to the required precision of battery position after unmanned aerial vehicle falls low, need not the arm clamp and get the battery, control logic is simple and stability is strong, has also reduced the size at unmanned aerial vehicle airport simultaneously, convenient transportation.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the embodiments or the prior art descriptions 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 it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise.
FIG. 1 is a schematic structural view of a fully-automatic battery replacement station of an unmanned aerial vehicle according to the present invention;
FIG. 2 is a top view of a fully-automatic battery replacement station of the unmanned aerial vehicle according to the present invention;
FIG. 3 is a schematic diagram of a full-automatic power switching airport lifting mechanism of an unmanned aerial vehicle;
FIG. 4 is a schematic diagram of a power exchanging mechanism of a full-automatic power exchanging station of the unmanned aerial vehicle;
FIG. 5 is a schematic diagram of the operation of the full-automatic battery replacement station of the unmanned aerial vehicle according to the present invention;
FIG. 6 is a schematic diagram of a second operation of the unmanned aerial vehicle full-automatic battery replacement station of the present invention;
FIG. 7 is a schematic view of the top-view operation of the unmanned aerial vehicle full-automatic battery replacement station of the present invention;
FIG. 8 is a perspective view of a structure of a fully automatic battery replacement station of the unmanned aerial vehicle of the present invention;
fig. 9 is a schematic structural view of a battery module of an unmanned aerial vehicle full-automatic battery replacement airport of the present invention.
Wherein, in the figures, the respective reference numerals:
10. an unmanned aerial vehicle; 11. A battery module; 111. A clamping part;
112. an electrode sheet; 12. A V-shaped groove;
20. a longitudinal clamping mechanism; 21. A clamping portion; 22. A first motor;
23. a screw rod; 24. A first slider; 30. A lateral clamping mechanism;
31. a cross bar; 32. A second slider; 33. A chute;
40. a take-off and landing platform; 41. A through hole; 50. A lifting mechanism;
51. a lifting rod; 52. A lifting mechanism motor; 60. A battery charging and replacing mechanism;
61. a conductive slide rail; 62. A slide rail bracket; 63. A base plate;
631. a clamping portion; 64. A slide rail bracket bottom plate; 100. And a frame.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present 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, "a plurality" means two or more unless specifically defined otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
As shown in fig. 1 to 9, an embodiment of the invention provides a full-automatic unmanned aerial vehicle battery replacement station, which includes a cabin and a movable cabin door (not shown), wherein an unmanned aerial vehicle positioning mechanism, a lifting mechanism 50, a battery charging and replacing mechanism 60 and a support 100 are arranged in the cabin, the unmanned aerial vehicle positioning mechanism is used for clamping an unmanned aerial vehicle base after an unmanned aerial vehicle 10 lands, and includes a longitudinal clamping mechanism 20, a transverse clamping mechanism 30 and a lifting platform 40, the lifting platform 40 is fixed in the cabin through the support 100, a through hole 41 is arranged in the center of the lifting platform 40, the longitudinal clamping mechanism 20 is located in the through hole 41 and used for longitudinally clamping and loosening the unmanned aerial vehicle base, and is driven by the lifting mechanism 50 to move up and down through the through hole; the transverse clamping mechanism 30 is arranged on the upper surface of the lifting platform 40, and moves transversely and reciprocally to clamp and loosen the unmanned aerial vehicle base; the lifting mechanism 50 is arranged below the longitudinal clamping mechanism 20 and used for driving the longitudinal clamping mechanism to move up and down, and the battery charging and replacing mechanism 60 is arranged below the longitudinal clamping mechanism 20 and vertical to the longitudinal clamping mechanism 20 and used for charging and replacing the unmanned aerial vehicle battery. The structure is simple and compact. The whole lifting platform does not need to move, a mechanical arm clamp and a battery, the logic control is simple, and the cost is low.
Further, the longitudinal clamping mechanism comprises two clamping parts 21, two first sliding blocks 24, two screw rods 23 and two first motors 22 which are symmetrically arranged, the two first motors 22 respectively drive the two screw rods 23 to move, the two screw rods are respectively provided with the two first sliding blocks 24, and the two first sliding blocks respectively drive the two clamping parts 21 to move to clamp or loosen the unmanned aerial vehicle base; be equipped with spout 33 on the platform 40 of taking off and land, horizontal clamping mechanism 30 is including two horizontal poles 31, four second sliders 32 that the symmetry set up, four second sliders are connected with two horizontal pole four ends respectively, and spout 33 internal motion for unmanned aerial vehicle drops on and promotes unmanned aerial vehicle behind the platform of taking off and land and move in the middle of returning to the ground.
Further, clamping part 21 is the wedge, is equipped with V type groove 12 on the unmanned aerial vehicle upper base, and when needs fixed unmanned aerial vehicle, clamping part 21 moves to V type inslot clamp unmanned aerial vehicle 10 under the drive of first motor.
Further, the lifting mechanism 50 includes a lifting rod 51, and the lifting rod 51 is pushed by a lifting mechanism motor 52 to move so that the longitudinal clamping mechanism 20 moves upwards and downwards.
Further, it includes battery module 11, battery module mounting and battery slip table subassembly to fill to trade electrical mechanism 60, battery module 11 includes the battery case and arranges the battery of battery box internal electricity connection in, be equipped with joint portion 111 on the battery case, the battery module mounting includes bottom plate 63, establish clamping part 631 on the bottom plate, clamping part 631 and the 111 shape adaptations of joint portion on the battery case, bottom plate 63 lower surface is equipped with the actuating mechanism drive the horizontal back and forth movement of battery module mounting, battery slip table subassembly includes slide rail bracket bottom plate 64, slide rail bracket bottom plate both ends are equipped with slide rail bracket end plate respectively, slide rail bracket end plate to slide rail bracket bottom plate direction extends and is equipped with electrically conductive slide rail 61, battery module 11 is in under the drive of battery module mounting along electrically conductive slide rail 61 removes. The battery module is driven by the battery module fixing piece to move along the conductive sliding rail. The clamping parts are symmetrically arranged on the opposite sides of the battery box respectively, and the clamping parts are vertically and symmetrically arranged on the periphery of the bottom plate of the battery module fixing part. In the unmanned aerial vehicle battery jar is arranged in to the battery module, when needing to trade the battery, unmanned aerial vehicle takes battery module downstream, joint portion on the battery module mounting bottom plate inserts in the clamping part of battery module, the distance of battery sliding table subassembly battery module that slides right, the battery module that is full of electricity drives to the unmanned aerial vehicle battery jar in, the battery module synchronous right removal that needs charge in the unmanned aerial vehicle, unmanned aerial vehicle upward movement carries out the flight task behind the platform that takes off and land, accomplish once trade electric operating procedure. This simple structure, it is with low costs, to the required precision of battery position after unmanned aerial vehicle falls low, need not the arm clamp and get the battery, control logic is simple and stability is strong, has also reduced the size at unmanned aerial vehicle airport simultaneously, convenient transportation.
Further, electrode plates 112 are arranged on the other two sides of the battery box, the conductive slide rail 31 is in sliding fit with the electrode plates 112, and the battery is charged through the electrode plates 112. The battery module is kept in the middle of electrically conductive slide rail, and electrically conductive slide rail plays the guide effect promptly and plays charging electrode's effect again.
Further, the number of the battery modules 11 is two or more, and the two or more battery modules 11 are sequentially adapted to be clamped end to end through the clamping portions 111. Preferably, the four battery modules are circularly replaced and used repeatedly in turn, and the four battery modules are replaced by one cycle.
Further, actuating mechanism includes second motor and motor shaft, the second motor drives the motor shaft and just reverses the motion, and the motor shaft drives battery module 11 mounting level reciprocating motion through bottom plate 63. Through the motor positive and negative rotation drive battery module mounting level back and forth movement, when the unmanned aerial vehicle battery does not have the electric quantity, return to the journey to descend on the platform of taking off and landing, descend after the steadying, actuating mechanism drive battery module mounting removes, and in the battery module removed the unmanned aerial vehicle battery jar, the battery of spent removed to electrically conductive slide rail under actuating mechanism's promotion on, compact structure, charge cyclic utilization.
Further, a sliding rail support 62 is further arranged on the sliding rail support bottom plate, and the conductive sliding rail is fixed in the sliding rail support. The battery module can stably slide on the upper stable conductive slide rail through the slide rail bracket so as to prevent the battery module from shaking when moving on the conductive slide rail.
Furthermore, the number of the conductive slide rails 61 is eight, and the space enclosed by every four conductive slide rails is matched with the shape of the battery box. So that the left and right of the electric battery module can be stably moved.
Specifically, the preferred battery module of this embodiment is installed in the battery jar of unmanned aerial vehicle bottom, and other battery modules are deposited and are carried out full-automatic taking and changing battery inside the unmanned aerial vehicle airport. Deposit a plurality of reserve battery module in the unmanned aerial vehicle airport, preferably three battery module. When unmanned aerial vehicle flies, electric power is not enough, and unmanned aerial vehicle low-power reports to the police, need return the unmanned aerial vehicle airport and trade the electricity, and unmanned aerial vehicle chance is automatic to return a journey, descends to the platform of taking off and landing at unmanned aerial vehicle airport, because of the precision problem of landing point, needs adjust the unmanned aerial vehicle position. At this moment, horizontal clamping mechanism work, under the drive of horizontal pole of horizontal clamping mechanism, promote unmanned aerial vehicle to the horizontal central motion of platform that takes off and land, when unmanned aerial vehicle reachd the horizontal center of platform that takes off and land, vertical clamping mechanism begins work, and under the effect of first motor, the lead screw rotates, arranges the first slider motion on the lead screw in, drives the tight head motion of clamp. The clamping head clamps the unmanned aerial vehicle to move, so that the unmanned aerial vehicle moves to the longitudinal center of the take-off and landing platform. So far, unmanned aerial vehicle accomplishes the position and puts in the middle, is located the through-hole. Then, the vertical clamping mechanism clamps the unmanned aerial vehicle base and carries out the electricity changing operation when elevating system's effect descends to the set position. At this time, the charging and replacing mechanism starts to work. Clamping part on the battery module mounting inserts in the joint portion of battery module, after unmanned aerial vehicle descends to the right, the battery module mounting shifts to the right the position of a battery module under actuating mechanism's drive. At this moment, in the battery module that is full of electricity inserted the unmanned aerial vehicle battery jar in the same way, unmanned aerial vehicle rose to the platform of taking off and land under elevating system's effect, took off and continues to accomplish the flight task. At this point, the process of replacing the battery is completed once, and the process is repeated. After the battery is replaced, the unmanned aerial vehicle continues to execute corresponding tasks, the replaced battery is charged in the unmanned aerial vehicle airport, and the unmanned aerial vehicle can be used repeatedly in a circulating and reciprocating mode. The battery module replacement steps are repeated as above, and are not described in detail here.
The invention has simple structure and low cost. Vertical clamping mechanism presss from both sides tight unmanned aerial vehicle and moves in the through-hole, and does not need the upper and lower motion of whole take-off and landing platform, saves space, and then lightens size, the weight at unmanned aerial vehicle airport. The cost is saved, the transportation is convenient, the structure is simple, and the automatic operation is convenient. And can be realized through simple control logic without clamping and taking the battery by a mechanical arm. And the position precision requirement to unmanned aerial vehicle descending is low. And meanwhile, the cost of the unmanned aerial vehicle airport is also reduced.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (10)
1. Full-automatic electric airport that trades of unmanned aerial vehicle, cabin door including cabin and activity, its characterized in that: the unmanned aerial vehicle positioning mechanism is used for clamping an unmanned aerial vehicle base after the unmanned aerial vehicle lands and comprises a longitudinal clamping mechanism, a transverse clamping mechanism and a lifting platform, the lifting platform is fixed in the cabin through the support, a through hole is formed in the center of the lifting platform, the longitudinal clamping mechanism is located in the through hole and used for longitudinally clamping and loosening the unmanned aerial vehicle base and is driven by the lifting mechanism to move up and down through the through hole; the transverse clamping mechanism is arranged on the upper surface of the lifting platform and moves transversely and reciprocally to clamp and loosen the unmanned aerial vehicle base; the lifting mechanism is arranged below the longitudinal clamping mechanism and used for driving the longitudinal clamping mechanism to move up and down, and the battery charging and replacing mechanism is arranged below the longitudinal clamping mechanism and vertical to the longitudinal clamping mechanism and used for charging and replacing the unmanned aerial vehicle battery.
2. The full-automatic unmanned aerial vehicle battery replacement station as claimed in claim 1, wherein the longitudinal clamping mechanism comprises two clamping portions, two first sliding blocks, two lead screws and two first motors, the two clamping portions, the two first sliding blocks, the two lead screws and the two first motors are symmetrically arranged, the two first motors drive the two lead screws to move respectively, the two lead screws are provided with the two first sliding blocks respectively, and the two first sliding blocks drive the two clamping portions to move respectively to clamp or release the unmanned aerial vehicle base; be equipped with the spout on the platform of taking off and land, horizontal clamping mechanism includes two horizontal poles, four second sliders that the symmetry set up, four second sliders are connected with four ends of two horizontal poles respectively, and the spout internal motion for unmanned aerial vehicle drops on and promotes unmanned aerial vehicle behind the platform of taking off and land and move in the middle of returning to the place.
3. The full-automatic electric airport that trades of unmanned aerial vehicle of claim 2, characterized in that, the clamping part is the wedge, is equipped with V type groove on the unmanned aerial vehicle upper base, and when needs fixed unmanned aerial vehicle, the clamping part moves to V type inslot clamping unmanned aerial vehicle under two first motor's drives.
4. The unmanned aerial vehicle full-automatic battery replacement field according to claim 1, wherein the lifting mechanism comprises a lifting rod which moves under the pushing of a lifting mechanism motor, so that the longitudinal clamping mechanism moves upwards and downwards.
5. The unmanned aerial vehicle full-automatic battery replacing station as claimed in claim 1, wherein the battery charging and replacing mechanism comprises a battery module, a battery module fixing member and a battery sliding table assembly, the battery module comprises a battery box and a battery which is arranged in the battery box and electrically connected, a clamping part is arranged on the battery box, the battery module fixing piece comprises a bottom plate, a clamping part is arranged on the bottom plate, the clamping part is matched with the clamping part on the battery box in shape, the lower surface of the bottom plate is provided with a driving mechanism for driving the battery module fixing piece to horizontally reciprocate, the battery sliding table assembly comprises a sliding rail bracket bottom plate, sliding rail bracket end plates are respectively arranged at two ends of the sliding rail bracket bottom plate, the sliding rail support end plate extends towards the sliding rail support bottom plate and is provided with a conductive sliding rail, and the battery module is driven by the battery module fixing part to move along the conductive sliding rail.
6. The full-automatic unmanned aerial vehicle battery replacement station of claim 5, characterized in that: electrode plates are arranged on the other two opposite sides of the battery box, the conductive slide rails are in sliding fit with the electrode plates, and the battery is charged through the electrode plates.
7. The full-automatic unmanned aerial vehicle battery replacement station of claim 5 or 6, characterized in that: the battery module quantity is two or more, two or more battery modules pass through joint portion end to end adaptation joint in proper order.
8. The full-automatic unmanned aerial vehicle battery replacement station of claim 5, characterized in that: the driving mechanism comprises a second motor and a motor shaft, the second motor drives the motor shaft to rotate forward and backward, and the motor shaft drives the battery module fixing piece to horizontally reciprocate through the bottom plate.
9. The full-automatic unmanned aerial vehicle battery replacement station of claim 5, characterized in that: the sliding rail support is further arranged on the sliding rail support bottom plate, and the conductive sliding rail is fixed in the sliding rail support.
10. The unmanned aerial vehicle trades battery device of claim 5 or 6, characterized in that: the number of the conductive sliding rails is eight, and the space enclosed by every four conductive sliding rails is matched with the shape of the battery box.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210041971.5A CN114313288A (en) | 2022-01-14 | 2022-01-14 | Full-automatic airport of trading of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210041971.5A CN114313288A (en) | 2022-01-14 | 2022-01-14 | Full-automatic airport of trading of unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN114313288A true CN114313288A (en) | 2022-04-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202210041971.5A Pending CN114313288A (en) | 2022-01-14 | 2022-01-14 | Full-automatic airport of trading of unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115946862A (en) * | 2022-12-27 | 2023-04-11 | 广州优飞智能设备有限公司 | Automatic airport that trades of unmanned aerial vehicle |
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2022
- 2022-01-14 CN CN202210041971.5A patent/CN114313288A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115946862A (en) * | 2022-12-27 | 2023-04-11 | 广州优飞智能设备有限公司 | Automatic airport that trades of unmanned aerial vehicle |
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