Gas collection device for unmanned aerial vehicle and collection method thereof
By designing the telescopic air pipe and driving mechanism of the gas acquisition device for drones, the problem of difficulty in telescopic air pipes in the prior art is solved, and the accuracy and stability of gas collection are achieved.
Patent Information
- Application Number
- CN202411045070.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-01
- Publication Date
- 2025-03-11
AI Technical Summary
The existing drone polluted gas collection device is difficult to control when the intake pipe is telescopic and contracted in axial direction, and is prone to deflection and cause jamming, which requires improvement.
A gas collection device for drones is designed, including a main drone and a secondary drone. The gas collection device consists of a mounting table, a telescopic air pipe, a driving mechanism, a telescopic mechanism and a rotating mechanism. Through the cooperation of the telescopic mechanism and the rotary mechanism, the length and position of the telescopic air pipe can be adjusted and stabilized to avoid jamming.
It effectively reduces the impact of downscrubbing gas flow on gas distribution, improves the accuracy of gas samples collection, and avoids the problem of stuck in the telescopic air pipe when telescopic.
Smart Images

Figure CN119595377A_ABST
Abstract
Description
Technical Field
[0001] The present application belongs to the technical field of unmanned aerial vehicles, and in particular, relates to a gas collection device for unmanned aerial vehicles and a collection method thereof. Background Art
[0002] Unmanned aerial vehicle, abbreviated as "UAV" in English, is an unmanned aircraft controlled by radio remote control equipment and self-contained program control device, or operated completely or intermittently autonomously by an on-board computer.
[0003] Compared with manned aircraft, drones are often more suitable for tasks that are too "dull, dirty or dangerous", such as environmental monitoring. There are many reasons for air pollution, such as: waste gas emissions in industrial production processes, waste gas emissions in garbage treatment plants around cities. The polluted gases generated in the above examples seriously exceed the standard. Some of these gases, such as carbon dioxide and methane, have a greenhouse effect, hydrogen sulfide and ammonia will produce pungent odors, and sulfur dioxide, nitrogen oxides, dust, etc. will affect the air quality of the city. Therefore, it is necessary to collect and detect polluted gases in multiple locations of factories and garbage treatment plants. Most of the existing detection equipment is mobile robots or drones.
[0004] The patent with publication number CN113532962B discloses a polluted gas collection device based on a drone, which relates to the field of gas collection technology. The device uses the fountain flow formed by the collision of the downwash airflow of the main drone and the auxiliary drone to quickly and accurately collect the polluted gas, reducing the influence of the downwash airflow on the gas spatial distribution and improving the reliability of the sample.
[0005] The above patent completes the gas collection work by using an air pump, a rotating platform, multiple air storage boxes, an electric push rod and an intake pipe. Although it can achieve the work, it is difficult to control the axial extension and contraction of the intake pipe, and it is easy to deviate and cause jamming, so it needs to be improved. Summary of the invention
[0006] The purpose of this application is to provide a gas collection device and a collection method for drones, which can solve the above problems.
[0007] The purpose of the present application is to provide a gas collection device for a drone, comprising a main drone, a secondary drone, and a gas collection device arranged on the main drone, wherein the gas collection device comprises:
[0008] A mounting platform, which is set on the main UAV;
[0009] The telescopic air tube comprises an outer tube body and a plurality of inner tube bodies, and the telescopic air tube is connected to an air pump and an air storage box;
[0010] The driving mechanism is arranged on the mounting platform and is used to drive the telescopic air pipe to operate, and the driving mechanism includes:
[0011] The telescopic mechanism is used to drive the telescopic air pipe to move in a telescopic manner;
[0012] A rotating mechanism, used for driving the telescopic air tube to rotate;
[0013] Wherein, the telescopic mechanism is arranged on the rotating mechanism, and the rotating mechanism drives the telescopic mechanism and the telescopic air pipe to rotate together.
[0014] By using the above-mentioned gas collection device for drones, adjusting and calibrating the collection position through the cooperation of the main drone and the auxiliary drone, the influence of the downwash airflow on the gas distribution can be effectively reduced, and the accuracy of gas sample collection can be improved. It can also be applicable to multiple scenarios. The gas collection work can be completed with the coordinated use of the telescopic air pipe, the driving mechanism, the telescopic mechanism and the rotating mechanism. Among them, by setting the telescopic mechanism, the extension length of the telescopic air pipe can be adjusted, and the stability of the telescopic air pipe extension can be ensured, which can effectively prevent the telescopic air pipe from getting stuck during extension and retraction.
[0015] Furthermore, the rotating mechanism includes a rotating table and a servo motor for driving the rotating table to rotate. One end of the telescopic air pipe passes through the rotating table and is connected to the air storage box. Driven by the servo motor, the rotating table with multiple telescopic air pipes rotates around the center of the mounting table.
[0016] The position of the telescopic air tube can be adjusted in real time through the rotating mechanism so that it can be quickly aligned with the secondary UAV. The rotating table can be rotated under the drive of the servo motor, and the rotating table drives the telescopic air tube to rotate. The rotation work needs to be done after the UAV is hovering. At the same time, the camera installed on the UAV can be used to determine whether the telescopic air tube is aligned with the secondary UAV. If not, the rotating mechanism can be controlled to operate until it is aligned.
[0017] Further: the telescopic mechanism comprises:
[0018] A first fixing seat is disposed on the rotating platform and connected to one end of the outer tube body;
[0019] A second fixing seat is arranged on the mounting platform and connected to the other end of the outer tube body, and an arc-shaped guide rail adapted to the second fixing seat is arranged on the mounting platform;
[0020] A sealing head is arranged on the inner rod body;
[0021] The telescopic structure includes a screw rod, a driving rod disposed on a second fixed seat, and a connecting head rotatably connected to one end of the driving rod, the connecting head is threadedly connected to the screw rod, and one end of the driving rod passes through the second fixed seat and is connected to the sealing head;
[0022] A driver is disposed on the rotating table, and the driver is connected via a coupling screw;
[0023] Wherein, a sliding hole for the driving rod to pass through is arranged on the second fixing seat, and a stabilizing structure is arranged between the sliding hole and the driving rod.
[0024] In the present application, the driver is a motor, and the motor is operated by external power supply. The power supply device here can be a battery. When the telescopic mechanism is in operation, the driver starts to drive the screw to rotate through the coupling. Under the cooperation of the screw and the connector, the connector rotates and causes the driving rod to move axially. When the driving rod moves, it drives the connector to move, and the connector drives the inner tube body to move, thereby completing the telescopic movement of the inner sleeve and the outer sleeve. Among them, the first fixed seat and the second fixed seat are respectively installed at the two ends of the outer tube body, which play the role of guiding and limiting, preventing the driving rod from offset when moving, and also play the role of fixing the outer tube body. The setting of the arc guide rail can enable the second fixed seat to move along the arc guide rail to prevent the second fixed seat from affecting the rotation of the rotating mechanism. At the same time, during the movement of the driving rod, it will contact the sliding hole on the second fixed seat, so that the axial movement of the driving rod is more stable. In addition, when adjusting the telescopic, the user can remotely control the driver to adjust the telescopic length of the telescopic air pipe, and the adjusted picture is fed back through the camera.
[0025] Furthermore, both ends of the sealing head are provided with air inlets connected to the inner tube body, and a filter screen is provided at the air inlet, and the filter screen and the air inlet are detachably connected.
[0026] By arranging two air inlets on the sealing head, the air intake efficiency can be expanded, thereby improving the gas collection efficiency. Opening multiple air inlets can avoid the problem of a single air inlet being unable to collect gas due to blockage. Installing a filter on the air inlet can block large particles of impurities and play a protective role. Configuring the filter and the air inlet as a detachable structure can facilitate the installation and disassembly of the filter, and facilitate the replacement and cleaning of the filter.
[0027] Furthermore, the stable structure comprises:
[0028] The shifting blocks are arranged on both sides of the outer wall of the driving rod;
[0029] Main slide grooves are arranged on both sides of the sliding hole and are adapted to the shifting block;
[0030] A stabilizing assembly, disposed in the main slide and cooperating with the shifting block;
[0031] When the telescopic air pipe is extended or retracted, the driving rod contacts the stabilizing component through the shifting block and drives the stabilizing component to move.
[0032] The stabilizing structure includes a shift block, a main slide and a stabilizing component. The shift block is arranged on both sides of the driving rod, and the main slide is opened on both sides of the sliding hole for the shift block to pass through, while the stabilizing component is located in the main slide. When the shift block passes through, the stabilizing component contacts and interacts with the stabilizing component. When the telescopic air tube is extended or retracted, the driving rod contacts the stabilizing component through the shift block and drives the stabilizing component to move, thereby making the extension and retraction process of the telescopic air tube more stable.
[0033] Furthermore, the stabilizing component includes:
[0034] Guide grooves are arranged on both sides of the main slide;
[0035] A guide slider is disposed in the guide groove and can slide along the guide groove;
[0036] A first shifting rod is arranged at one end of the guide slider and is hinged to the guide slider, the first shifting rod is adapted to the guide groove and is in contact with the shifting block;
[0037] A second lever is arranged at the other end of the guide slider and is hinged to the guide slider, the second lever is adapted to the guide groove and is in contact with the lever block;
[0038] The first damping rod, whose telescopic end is connected to the guide slider
[0039] A second damping rod, a telescopic end of which is connected to the guide slider;
[0040] When the driving rod moves, the first shifting rod and the second shifting rod are driven to move through the shifting block.
[0041] There are two situations for the telescopic air tube, one is when the telescopic air tube is extended, and the other is when the telescopic air tube is retracted. When the telescopic air tube is extended, the driving rod gradually moves away from the driving rod under the action of the driver and drives the inner tube body to gradually extend. During the extension process, the lever contacts the first lever and drives the first lever to gradually move from one end of the guide slot to the other end. During this process, the telescopic end of the first damping rod gradually retracts, and the telescopic end of the second damping rod is gradually extended, so that the movement of the driving rod is more rapid and stable, and the extension of the inner tube body is more stable.
[0042] When the telescopic air tube retracts, the driving rod gradually approaches the driver under the action of the driver and drives the inner tube body to gradually retract. During the retraction process, the quick lever contacts the second lever and drives the second lever to gradually move from the other end to the one end of the guide slot. During this process, the telescopic end of the second damping rod gradually retracts, and the telescopic end of the first damping rod is gradually stretched, so that the movement of the driving rod is more rapid and stable, and the retraction of the inner tube body is more stable.
[0043] Therefore, whether it is extending or retracting, it will be affected by the stable structure, which can effectively avoid the telescopic air tube from getting stuck or stuck during extension and retraction, making the extension and retraction more rapid and stable, and preventing deviation. In addition, by setting a guide slider, it can fix the first lever and the second lever, and can also play an overall limiting guiding role to prevent it from detaching from the guide slot during movement.
[0044] Furthermore, the stabilizing component further comprises:
[0045] A first arc-shaped groove is provided at one end of the guide groove;
[0046] A second arc groove is provided at the other end of the guide groove;
[0047] A first spring, one end of which is connected to the first lever, and the other end of which is connected to the main slide groove;
[0048] A second spring, one end of which is connected to the second lever, and the other end of which is connected to the main slide groove;
[0049] The first lever is matched with the first arc groove and can slide along the first arc, and the second lever is matched with the second arc groove and can slide along the second arc.
[0050] In order to avoid being blocked by the first lever and the second lever during the movement of the quick-acting lever, the present application provides a first arc groove and a second arc groove. When the telescopic air pipe is extended, the shift block contacts the first lever and drives the first lever to move. When the first lever moves to the connection between the guide slide groove and the first arc groove, the angle between the first lever and the guide slide block changes, and the first lever enters the first arc groove. At this time, the first lever cannot block the movement of the quick-acting lever, and the driving rod can move. In the process of the first lever entering the first arc groove, the second lever moves from the second arc groove to the guide groove. In this process, the first spring is stretched and the second spring retracts, which further plays a damping and buffering effect, making the movement of the driving rod more rapid and stable.
[0051] When the telescopic air pipe retracts, the shift block contacts the second shift rod and drives the second shift rod to move. When the second shift rod moves to the connection between the guide slide groove and the second arc groove, the angle between the second shift rod and the guide slide block changes, and the second shift rod enters the second arc groove. At this time, the second shift rod cannot block the movement of the shift rod, and the driving rod can continue to move. In the process of the second shift rod entering the second arc groove, the first shift rod moves from the first arc groove to the guide groove. In this process, the second spring is stretched and the first spring retracts, which further plays a damping and buffering effect, making the movement of the driving rod more rapid and stable. Through the cooperation of the two, the telescopic process can be subject to the damping and buffering effect. Moreover, since the first arc groove and the other arc grooves are arc structures, they have a certain fixing effect, which can fix the positions of the first shift rod and the second shift rod to prevent resetting after movement.
[0052] Furthermore, the present invention also discloses a gas collection method for a drone gas collection device, comprising the following steps:
[0053] S1. Control the main UAV and the auxiliary UAV to fly to the collection position, and adjust the hovering position according to the collection position;
[0054] S2. When the main and auxiliary drones hover stably, the servo motor controls the rotating table to rotate so that the telescopic air tube points to the auxiliary drone, and then the telescopic mechanism operates to extend the telescopic air tube and adjust the extension distance;
[0055] S3, turning on the air pump and collecting gas, the gas enters the filter, the air inlet, the inner tube body and the outer tube body and is stored in the gas storage box;
[0056] S4, gas collection contact, the telescopic mechanism operates to retract the telescopic air pipe, and the servo motor controls the rotary table to reset;
[0057] S5. Control the main and auxiliary drones to return.
[0058] The beneficial effects of this application are:
[0059] 1. The gas collection work can be completed by the coordinated use of the telescopic air pipe, the driving mechanism, the telescopic mechanism and the rotating mechanism. By setting the telescopic mechanism, the extension length of the telescopic air pipe can be adjusted, and the stability of the telescopic air pipe can be ensured, which can effectively prevent the telescopic air pipe from getting stuck during extension;
[0060] 2. During the extension of the telescopic air tube, the telescopic end of the first damping rod gradually retracts, and the telescopic end of the second damping rod is gradually stretched, so that the movement of the driving rod is more rapid and stable, and the extension of the inner tube body is more stable; during the retraction of the telescopic air tube, the lever contacts the second lever and drives the second lever to gradually move from the other end to the one end of the guide slot. During this process, the telescopic end of the second damping rod gradually retracts, and the telescopic end of the first damping rod is gradually stretched, so that the movement of the driving rod is more rapid and stable, and the retraction of the inner tube body is more stable;
[0061] 3. When the telescopic air pipe retracts, the shift block contacts the second shift rod and drives the second shift rod to move. When the second shift rod moves to the connection between the guide slide groove and the second arc groove, the angle between the second shift rod and the guide slide block changes, and the second shift rod enters the second arc groove. At this time, the second shift rod cannot block the movement of the shift rod, and the driving rod can continue to move. In the process of the second shift rod entering the second arc groove, the first shift rod moves from the first arc groove to the guide groove. In this process, the second spring is stretched and the first spring retracts, which further plays a damping and buffering effect, making the movement of the driving rod more rapid and stable. Through the cooperation of the two, the telescopic process can be subject to the damping and buffering effect. Moreover, since the first arc groove and the other arc grooves are arc structures, they have a certain fixing effect, and the positions of the first shift rod and the second shift rod can be fixed to prevent resetting after movement. BRIEF DESCRIPTION OF THE DRAWINGS
[0062] Figure 1 It is a schematic diagram of the structure of the present invention;
[0063] Figure 2 It is a schematic diagram of the structure of the main UAV and the auxiliary UAV of the present invention;
[0064] Figure 3 is a top view of the present invention;
[0065] Figure 4 yes Figure 3 Sectional view in the AA direction;
[0066] Figure 5 yes Figure 4 A is an enlarged view of the middle image.
[0067] The reference numerals in the figure are: 100, main drone; 110, auxiliary drone; 200, mounting platform; 300, telescopic air pipe; 310, outer tube body; 320, inner tube body; 330, air storage box; 400, rotating mechanism; 410, rotating platform; 420, servo motor; 500, telescopic mechanism; 510, first fixed seat; 520, second fixed seat; 521, arc guide rail; 530, sealing head; 531, air inlet; 532, filter screen; 540, telescopic structure; 541. Screw rod; 542. Drive rod; 543. Connector; 550. Driver; 560. Sliding hole; 600. Stabilizing structure; 610. Shift block; 620. Main slide groove; 700. Stabilizing assembly; 710. Guide groove; 720. Guide slider; 730. First shift rod; 740. Second shift rod; 750. First damping rod; 760. Second damping rod; 770. First arc groove; 780. Second arc groove; 790. First spring; 791. Second spring. DETAILED DESCRIPTION
[0068] The following will be combined with the drawings in the embodiments of the present application to clearly describe the technical solutions in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, rather than all the embodiments. All other embodiments obtained by ordinary technicians in this field based on the embodiments in the present application belong to the scope of protection of this application.
[0069] The terms "first", "second", etc. in the specification and claims of the present application are used to distinguish similar objects, and are not used to describe a specific order or sequence. It should be understood that the data used in this way can be interchangeable under appropriate circumstances, so that the embodiments of the present application can be implemented in an order other than those illustrated or described here, and the objects distinguished by "first", "second", etc. are generally of one type, and the number of objects is not limited. For example, the first object can be one or more. In addition, "and / or" in the specification and claims represents at least one of the connected objects, and the character " / " generally indicates that the objects associated with each other are in an "or" relationship.
[0070] In the following, in conjunction with the accompanying drawings, the gas collection device for a drone and the collection method thereof provided in the embodiments of the present application are described in detail through specific embodiments and their application scenarios.
[0071] Embodiment 1:
[0072] like Figures 1 to 4 As shown, the embodiment of the present application provides a gas collection device for a drone, including a main drone 100 and a secondary drone 110, and a gas collection device disposed on the main drone 100, the gas collection device including:
[0073] The mounting platform 200 is arranged on the main drone 100;
[0074] The telescopic air tube 300 includes an outer tube body 310 and a plurality of inner tube bodies 320. The telescopic air tube 300 is connected to an air pump and an air storage box 330.
[0075] The driving mechanism is disposed on the mounting platform 200 and is used to drive the telescopic air pipe 300 to operate. The driving mechanism includes:
[0076] The telescopic mechanism 500 is used to drive the telescopic air pipe 300 to telescope and move;
[0077] The rotating mechanism 400 is used to drive the telescopic air tube 300 to rotate;
[0078] The telescopic mechanism 500 is disposed on the rotating mechanism 400 , and the rotating mechanism 400 drives the telescopic mechanism 500 and the telescopic air pipe 300 to rotate together.
[0079] In some implementations of the embodiments of the present application, Figure 1As shown, by using the above-mentioned gas collection device for drones, through the cooperation of the main drone 100 and the auxiliary drone 110, adjusting and calibrating the collection position, the influence of the downwash airflow on the gas distribution can be effectively reduced, and the accuracy of gas sample collection can be improved. It can also be applicable to multiple scenarios. The gas collection work can be completed under the coordinated use of the telescopic air pipe 300, the driving mechanism, the telescopic mechanism 500 and the rotating mechanism 400. Among them, by setting the telescopic mechanism 500, the extension length of the telescopic air pipe 300 can be adjusted, and the stability of the telescopic air pipe 300 can be ensured, which can effectively prevent the telescopic air pipe 300 from getting stuck during extension and retraction.
[0080] Embodiment 2:
[0081] An embodiment of the present application provides a gas collection device for a drone. In addition to the above-mentioned technical features, the gas collection device for a drone in the embodiment of the present application also includes the following technical features.
[0082] like Figure 1 and Figure 4 As shown, the rotating mechanism 400 includes a rotating table 410 and a servo motor 420 for driving the rotating table 410 to rotate. One end of the telescopic air tube 300 passes through the rotating table 410 and is connected to the air storage box 330. Driven by the servo motor 420, the rotating table 410 with the multiple telescopic air tubes 300 rotates around the center of the mounting table 200.
[0083] In the embodiment of the present application, the position of the telescopic air tube 300 can be adjusted in real time through the rotating mechanism 400 so that it can be quickly aligned with the sub-UAV 110. The rotating table 410 can be rotated under the drive of the servo motor 420, and the rotating table 410 drives the telescopic air tube 300 to rotate. The rotation work needs to be performed after the UAV is hovering. At the same time, the camera installed on the UAV is used to determine whether the telescopic air tube 300 is aligned with the sub-UAV 110. If not, the rotating mechanism 400 can be controlled to operate until it is aligned.
[0084] Embodiment 3:
[0085] An embodiment of the present application provides a gas collection device for a drone. In addition to the above-mentioned technical features, the gas collection device for a drone in the embodiment of the present application also includes the following technical features.
[0086] As 1 and Figure 4 As shown, the telescopic mechanism 500 includes:
[0087] A first fixing seat 510 is disposed on the rotating platform 410 and connected to one end of the outer tube 310;
[0088] A second fixing seat 520 is disposed on the mounting platform 200 and connected to the other end of the outer tube body 310 . The mounting platform 200 is provided with an arc-shaped guide rail 521 adapted to the second fixing seat 520 .
[0089] The sealing head 530 is arranged on the inner rod body;
[0090] The telescopic structure 540 includes a screw rod 541, a driving rod 542 disposed on the second fixing seat 520, and a connecting head 543 rotatably connected to one end of the driving rod 542. The connecting head 543 is threadedly connected to the screw rod 541. One end of the driving rod 542 passes through the second fixing seat 520 and is connected to the sealing head 530.
[0091] A driver 550 is disposed on the rotating platform 410 and is connected via a coupling screw 541;
[0092] The second fixing seat 520 is provided with a sliding hole 560 for the driving rod 542 to pass through, and a stabilizing structure 600 is provided between the sliding hole 560 and the driving rod 542 .
[0093] In the embodiment of the present application, in the present application, the driver 550 is a motor, and the motor is operated by external power supply. The power supply device here can be a battery. When the telescopic mechanism 500 is in operation, the driver 550 starts to drive the screw 541 to rotate through the coupling. Under the cooperation of the screw 541 and the connecting head 543, the connecting head 543 rotates and causes the driving rod 542 to move axially. When the driving rod 542 moves, it drives the connecting head 543 to move, and the connecting head 543 drives the inner tube body 320 to move, thereby completing the telescopic movement of the inner sleeve and the outer sleeve. Among them, the first fixed seat 510 and the second fixed seat 520 are respectively installed at the two ends of the outer tube body 310, which play a guiding and limiting role to prevent the driving rod 542 from being offset when moving, and also play a role in fixing the outer tube body 310. The setting of the arc guide rail 521 can enable the second fixed seat 520 to move along the arc guide rail 521 to prevent the second fixed seat 520 from affecting the rotation of the rotating mechanism 400. At the same time, during the movement of the driving rod 542, it will contact the sliding hole 560 on the second fixed seat 520, so that the axial movement of the driving rod 542 is more stable. In addition, when adjusting the telescopic length, the user can remotely control the driver 550 to adjust the telescopic length of the telescopic air tube 300, and the adjusted picture is fed back through the camera.
[0094] Furthermore, both ends of the sealing head 530 are provided with air inlets 531 communicating with the inner tube body 320 , and a filter screen 532 is provided at the air inlet 531 , and the filter screen 532 and the air inlet 531 are detachably connected.
[0095] By providing two air inlets 531 on the sealing head 530, the air intake efficiency can be expanded, thereby improving the gas collection efficiency, and the provision of multiple air inlets 531 can avoid the problem of a single air inlet 531 being unable to collect gas due to blockage. Installing a filter 532 on the air inlet 531 can block large particles of impurities and play a protective role. Configuring the filter 532 and the air inlet 531 as a detachable structure can facilitate the installation and disassembly of the filter 532, and facilitate the replacement and cleaning of the filter 532.
[0096] Embodiment 4:
[0097] An embodiment of the present application provides a gas collection device for a drone. In addition to the above-mentioned technical features, the gas collection device for a drone in the embodiment of the present application also includes the following technical features.
[0098] like Figure 5 As shown, the stabilizing structure 600 includes:
[0099] The shifting blocks 610 are disposed on both sides of the outer wall of the driving rod 542;
[0100] The main slide groove 620 is disposed on both sides of the sliding hole 560 and is adapted to the shifting block 610;
[0101] The stabilizing assembly 700 is disposed in the main slide groove 620 and cooperates with the shifting block 610;
[0102] When the telescopic air tube 300 is extended or retracted, the driving rod 542 contacts the stabilizing assembly 700 through the shifting block 610 and drives the stabilizing assembly 700 to move.
[0103] In the embodiment of the present application, the stabilizing structure 600 includes a lever, a main slide 620 and a stabilizing component 700. The lever is provided on both sides of the driving rod 542, and the main slide 620 is provided on both sides of the sliding hole 560 for the lever to pass through. The stabilizing component 700 is located in the main slide 620. When the lever passes through, the stabilizing component 700 contacts and interacts. When the telescopic air tube 300 is extended or retracted, the driving rod 542 contacts the stabilizing component 700 through the lever block 610 and drives the stabilizing component 700 to move, thereby making the extension and retraction process of the telescopic air tube 300 more stable.
[0104] Embodiment 5:
[0105] An embodiment of the present application provides a gas collection device for a drone. In addition to the above-mentioned technical features, the gas collection device for a drone in the embodiment of the present application also includes the following technical features.
[0106] like Figure 5 As shown, the stabilizing assembly 700 includes:
[0107] The guide grooves 710 are arranged on both sides of the main slide groove 620;
[0108] A guide slider 720 is disposed in the guide groove 710 and can slide along the guide groove 710;
[0109] A first lever 730 is disposed at one end of the guide slider 720 and is hinged to the guide slider 720. The first lever 730 is adapted to the guide groove 710 and is in contact with the lever block 610.
[0110] A second lever 740 is disposed at the other end of the guide slider 720 and is hinged to the guide slider 720. The second lever 740 is adapted to the guide groove 710 and is in contact with the lever block 610.
[0111] The first damping rod 750, whose telescopic end is connected to the guide slider 720
[0112] A second damping rod 760, a telescopic end of which is connected to the guide slider 720;
[0113] When the driving rod 542 moves, the first shifting rod 730 and the second shifting rod 740 are driven to move through the shifting block 610 .
[0114] In the embodiment of the present application, the telescopic air tube 300 is divided into two situations, one is when the telescopic air tube 300 is extended, and the other is when the telescopic air tube 300 is retracted. When the telescopic air tube 300 is extended, under the action of the driver 550, the driving rod 542 gradually moves away from the driver 550 and drives the inner tube body 320 to gradually extend. During the extension process, the first lever 730 contacts and drives the first lever 730 to gradually move from one end of the guide slot to the other end. During this process, the telescopic end of the first damping rod 750 is gradually retracted, and the telescopic end of the second damping rod 760 is gradually extended, so that the movement of the driving rod 542 is more rapid and stable, and the extension of the inner tube body 320 is more stable.
[0115] When the telescopic air tube 300 retracts, the driving rod 542 gradually approaches the driving rod 550 under the action of the driver 550 and drives the inner tube body 320 to gradually retract. During the retraction process, the lever contacts the second lever 740 and drives the second lever 740 to gradually move from the other end of the guide slot to one end. During this process, the telescopic end of the second damping rod 760 gradually retracts, and the telescopic end of the first damping rod 750 is gradually stretched, so that the movement of the driving rod 542 is more rapid and stable, and the retraction of the inner tube body 320 is more stable.
[0116] Therefore, whether it is extending or retracting, it will be affected by the stabilizing structure 600, which can effectively prevent the telescopic air tube 300 from getting stuck or jammed during extension and retraction, making the extension and retraction more rapid and stable, and preventing deviation. In addition, by setting the guide slider 720, it can fix the first lever 730 and the second lever 740, and can also play an overall limiting guiding role to prevent it from detaching from the guide slot during movement.
[0117] Furthermore, the stabilizing assembly 700 further includes:
[0118] A first arc groove 770 is provided at one end of the guide groove 710;
[0119] A second arc groove 780 is provided at the other end of the guide groove 710;
[0120] A first spring 790, one end of which is connected to the first lever 730, and the other end of which is connected to the main slide groove 620;
[0121] A second spring 791, one end of which is connected to the second lever 740, and the other end of which is connected to the main slide groove 620;
[0122] The first lever 730 is matched with the first arc groove 770 and can slide along the first arc, and the second lever 740 is matched with the second arc groove 780 and can slide along the second arc.
[0123] When the first lever 730 is moved to the connecting portion of the guide slot and the first arc groove 770, the angle between the first lever 730 and the guide slider 720 changes, and the first lever 730 enters the first arc groove 770. At this time, the first lever 730 cannot block the movement of the lever, and the driving rod 542 can move. In the process of the first lever 730 entering the first arc groove 770, the second lever 740 moves from the second arc groove 780 to the guide slot 710. In this process, the first spring 790 is stretched and the second spring 791 is retracted, which further plays a damping and buffering effect, making the movement of the driving rod 542 more rapid and stable.
[0124] When the telescopic air pipe 300 is retracted, the shift block 610 contacts the second shift rod 740 and drives the second shift rod 740 to move. When the second shift rod 740 moves to the connection between the guide slide groove and the second arc groove 780, the angle between the second shift rod 740 and the guide slider 720 changes, and the second shift rod 740 enters the second arc groove 780. At this time, the second shift rod 740 cannot block the movement of the shift rod, and the driving rod 542 can continue to move. In the process of the second shift rod 740 entering the second arc groove 780, the second shift rod 740 is A lever 730 moves from the first arc groove 770 to the guide groove 710. During this process, the second spring 791 is stretched and the first spring 790 retracts, further playing a damping and buffering effect, making the movement of the driving rod 542 more rapid and stable. Through the cooperation of the two, the telescopic process can be affected by the damping and buffering effect. Moreover, since the first arc groove 770 and other arc grooves are arc structures, they have a certain fixing effect, which can fix the positions of the first lever 730 and the second lever 740 to prevent resetting after movement.
[0125] Embodiment 6:
[0126] The present application embodiment provides a collection method of a gas collection device for a drone, comprising the following steps:
[0127] S1. Control the main drone 100 and the secondary drone 110 to fly to the collection position, and adjust the hovering position according to the collection position;
[0128] S2. When the main and auxiliary drones 110 are hovering stably, the servo motor 420 controls the rotating platform 410 to rotate so that the telescopic air tube 300 points to the auxiliary drone 110. Then the telescopic mechanism 500 operates to extend the telescopic air tube 300 and adjusts the extension distance.
[0129] S3, turning on the air pump and collecting gas, the gas enters the filter 532, the air inlet 531, the inner tube body 320 and the outer tube body 310, and is then stored in the gas storage box 330;
[0130] S4, gas collection contact, the telescopic mechanism 500 operates to retract the telescopic air pipe 300, and the servo motor 420 controls the rotating table 410 to reset;
[0131] S5. Control the primary and secondary UAVs 110 to return home.
[0132] It should be noted that, in this article, the terms "comprise", "include" or any other variant thereof are intended to cover non-exclusive inclusion, so that the process, method, article or device including a series of elements includes not only those elements, but also includes other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise one..." do not exclude the presence of other identical elements in the process, method, article or device including the element. In addition, it should be pointed out that the scope of the methods and devices in the embodiments of the present application is not limited to performing functions in the order shown or discussed, and may also include performing functions in a substantially simultaneous manner or in reverse order according to the functions involved, for example, the described method may be performed in an order different from that described, and various steps may also be added, omitted, or combined. In addition, the features described with reference to certain examples may be combined in other examples.
[0133] The embodiments of the present application are described above in conjunction with the accompanying drawings, but the present application is not limited to the above-mentioned specific implementation methods. The above-mentioned specific implementation methods are merely illustrative and not restrictive. Under the guidance of the present application, ordinary technicians in this field can also make many forms without departing from the purpose of the present application and the scope of protection of the claims, all of which are within the protection of the present application.
Claims
1. A gas collection device for an unmanned aerial vehicle, comprising a main unmanned aerial vehicle (100), a secondary unmanned aerial vehicle (110), and a gas collection device arranged on the main unmanned aerial vehicle (100), characterized in that: The gas collection device comprises: A mounting platform (200) is arranged on the main drone (100); The telescopic air tube (300) comprises an outer tube body (310) and a plurality of inner tube bodies (320), and the telescopic air tube (300) is connected to an air pump and an air storage box (330); A driving mechanism is disposed on the mounting platform (200) and is used to drive the telescopic air pipe (300) to operate, the driving mechanism comprising: The telescopic mechanism (500) is used to drive the telescopic air pipe (300) to telescope and move; A rotating mechanism (400) for driving the telescopic air pipe (300) to rotate; The telescopic mechanism (500) is arranged on the rotating mechanism (400), and the rotating mechanism (400) drives the telescopic mechanism (500) and the telescopic air pipe (300) to rotate together.
2. A gas collection device for drone according to claim 1, characterized in that: The rotating mechanism (400) comprises a rotating platform (410) and a servo motor (420) for driving the rotating platform (410) to rotate. One end of the telescopic air tube (300) passes through the rotating platform (410) and is connected to the air storage box (330). Driven by the servo motor (420), the rotating platform (410) with the multiple telescopic air tubes (300) rotates around the center of the mounting platform (200).
3. A gas collection device for drone according to claim 2, characterized in that: The telescopic mechanism (500) comprises: A first fixing seat (510) is disposed on the rotating platform (410) and connected to one end of the outer tube body (310); A second fixing seat (520) is arranged on the mounting platform (200) and connected to the other end of the outer tube body (310); the mounting platform (200) is provided with an arc-shaped guide rail (521) adapted to the second fixing seat (520); A sealing head (530) is arranged on the inner rod body; The telescopic structure (540) comprises a screw rod (541), a driving rod (542) arranged on the second fixed seat (520), and a connecting head (543) rotatably connected to one end of the driving rod (542), wherein the connecting head (543) is threadedly connected to the screw rod (541), and one end of the driving rod (542) passes through the second fixed seat (520) and is connected to the sealing head (530); A driver (550) is disposed on the rotating platform (410), and the driver (550) is connected via a coupling screw (541); The second fixing seat (520) is provided with a sliding hole (560) for the driving rod (542) to pass through, and a stabilizing structure (600) is provided between the sliding hole (560) and the driving rod (542).
4. A gas collection device for drone according to claim 3, characterized in that: Both ends of the sealing head (530) are provided with air inlets (531) connected to the inner tube body (320), and a filter screen (532) is provided at the air inlet (531), and the filter screen (532) and the air inlet (531) are detachably connected.
5. The gas collection device for drone according to claim 4, characterized in that: The stabilizing structure (600) comprises: The shifting blocks (610) are arranged on both sides of the outer wall of the driving rod (542); A main slide groove (620) is arranged on both sides of the sliding hole (560) and is adapted to the shifting block (610); A stabilizing assembly (700) is disposed in the main slide groove (620) and cooperates with the shifting block (610); When the telescopic air tube (300) is telescoped, the driving rod (542) contacts the stabilizing assembly (700) through the shifting block (610) and drives the stabilizing assembly (700) to move.
6. A gas collection device for a drone according to claim 5, characterized in that: The stabilizing assembly (700) comprises: Guide grooves (710) are arranged on both sides of the main slide groove (620); A guide slider (720) is disposed in the guide groove (710) and is capable of sliding along the guide groove (710); A first shifting rod (730) is arranged at one end of the guide slider (720) and is hinged to the guide slider (720). The first shifting rod (730) is adapted to the guide groove (710) and is in contact with the shifting block (610); A second shifting rod (740) is arranged at the other end of the guide slider (720) and is hinged to the guide slider (720). The second shifting rod (740) is adapted to the guide groove (710) and is in contact with the shifting block (610). The first damping rod (750) has a telescopic end connected to the guide slider (720) A second damping rod (760), a telescopic end of which is connected to the guide slider (720); When the driving rod (542) moves, the first shifting rod (730) and the second shifting rod (740) are driven to move via the shifting block (610).
7. The gas collection device for drone according to claim 1, characterized in that: The stabilizing assembly (700) further comprises: A first arc-shaped groove (770) is disposed at one end of the guide groove (710); A second arc-shaped groove (780) is arranged at the other end of the guide groove (710); A first spring (790), one end of which is connected to the first lever (730) and the other end of which is connected to the main slide groove (620); A second spring (791), one end of which is connected to the second lever (740) and the other end of which is connected to the main slide groove (620); The first lever (730) is matched with the first arc-shaped groove (770) and can slide along the first arc, and the second lever (740) is matched with the second arc-shaped groove (780) and can slide along the second arc.
8. A gas collection method for the unmanned aerial vehicle gas collection device according to claim 1, characterized in that: The following steps are involved: S1, controlling the main drone (100) and the auxiliary drone (110) to fly to a collection position, and adjusting the hovering position according to the collection position; S2. When the main and auxiliary drones (110) are hovering stably, the servo motor (420) controls the rotating platform (410) to rotate so that the telescopic air tube (300) points toward the auxiliary drone (110), and then the telescopic mechanism (500) operates to extend the telescopic air tube (300) and adjusts the extension distance; S3, turning on the air pump and collecting gas, the gas enters the filter (532), the air inlet (531), the inner tube (320) and the outer tube (310), and is then stored in the gas storage box (330); S4, gas collection contact, the telescopic mechanism (500) operates to retract the telescopic air pipe (300), and the servo motor (420) controls the rotating table (410) to reset; S5. Control the main and auxiliary drones (110) to return home.
Citation Information
Patent Citations
A drone-based pollutant gas collection device
CN113532962B