CN213769006U

CN213769006U - Remote control unmanned aerial vehicle-based control system

Info

Publication number: CN213769006U
Application number: CN202022718857.0U
Authority: CN
Inventors: 刘双超; 赵长青; 张春雷
Original assignee: Elock Artificial Intelligence Technology Nanjing Co ltd
Current assignee: Elock Artificial Intelligence Technology Nanjing Co ltd
Priority date: 2020-11-20
Filing date: 2020-11-20
Publication date: 2021-07-23
Anticipated expiration: 2030-11-20

Abstract

The application relates to an operation system based on a remote control unmanned aerial vehicle, and relates to the field of unmanned aerial vehicles. This device includes the automatic airport of unmanned aerial vehicle, and the front side and the rear side at the automatic airport top of unmanned aerial vehicle all are provided with the direction slide rail, and the equal movable mounting in both sides on two direction slide rail surfaces has the hatch door that is located the automatic airport top of unmanned aerial vehicle. The utility model discloses in the time of in-service use, when changing the battery, receive the instruction at the automatic airport of unmanned aerial vehicle, promote cylinder one and start and promote to remove to unmanned aerial vehicle's direction removal, the depressed part of fastener bottom can block on the unmanned aerial vehicle undercarriage, thereby fix unmanned aerial vehicle, it stretches out then takes off the old battery on unmanned aerial vehicle to change battery device automatically and receive the instruction from the inside of taking off the platform, and change new battery, so just can guarantee that unmanned aerial vehicle aligns with automatic change battery device when changing the battery, and difficult activity, also quick change battery more easily, time saving and labor saving, the person of facilitating the use uses.

Description

Remote control unmanned aerial vehicle-based control system

Technical Field

The application relates to the field of unmanned aerial vehicles, in particular to an operating system based on a remote control unmanned aerial vehicle.

Background

Along with unmanned aerial vehicle uses more and more extensively, current unmanned aerial vehicle applied field is more and more, infrastructure patrols and examines, in the macro application scene such as city planning, traffic inspection, emergency command, ecological management, china has very long border line, petroleum pipeline, high-voltage line etc. can all see unmanned aerial vehicle's shadow in a plurality of fields, but many scenes all need the manual work to go to assist or manual work closely operate, increased corresponding human cost on the one hand, on the other hand also can bring some potential safety hazards.

In unmanned aerial vehicle's use, the electric quantity of battery can reduce gradually on unmanned aerial vehicle, just must return to voyage when reducing certain length and change the battery, but unmanned aerial vehicle returns to automatic airport landing and when changing the battery in returning voyage, does not have its fixed device, therefore the easy activity of unmanned aerial vehicle organism, when the battery demolishs the back, when installing new battery, is difficult to the alignment position, so be difficult to more with new battery installation on unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

In order to solve the problem that current unmanned aerial vehicle is difficult to change new battery, this application provides the control system based on remote control unmanned aerial vehicle.

The application provides a control system based on remote control unmanned aerial vehicle adopts following technical scheme: control system based on remote control unmanned aerial vehicle, including the automatic airport of unmanned aerial vehicle, the front side and the rear side at the automatic airport top of unmanned aerial vehicle all are provided with the direction slide rail, and the equal movable mounting in both sides on two direction slide rail surfaces has the hatch door that is located the automatic airport top of unmanned aerial vehicle, the bottom movable mounting of the automatic airport inner chamber of unmanned aerial vehicle has the platform of taking off, the both sides at the platform top of taking off all are provided with pushing mechanism one, one side of pushing mechanism one is provided with pushing mechanism two, one side of pushing mechanism two is provided with fixed establishment, the fixed mounting groove with pushing mechanism two-phase adaptation is all seted up with the front side and the rear side at the platform top of taking off, the central point who takes off the platform.

Preferably, the second pushing mechanism comprises an embedded mounting frame fixedly mounted in an inner cavity of the fixed mounting groove, an adjusting chute is formed in one side of the mounting frame, and a second pushing cylinder is fixedly mounted on the front side of the mounting frame.

Through adopting above-mentioned technical scheme, through the setting of pushing mechanism two, when the position that unmanned aerial vehicle parked was too big with the fixed establishment error, pushing cylinder two can start after receiving the instruction and promote whole pushing mechanism one and carry out the back-and-forth movement, and then drive whole fixed establishment and carry out the back-and-forth movement to this adjustment unmanned aerial vehicle and fixed establishment's error, make fixed establishment can fix a position unmanned aerial vehicle, the person of facilitating the use uses.

Preferably, promote mechanism one and include in the gliding sliding sleeve of regulation spout inner chamber, the surface and the two fixed connection of push cylinder of sliding sleeve, one side fixedly connected with mounting bracket of sliding sleeve, mounting bracket's top fixed mounting has push cylinder one, and the output of push cylinder one stretches into the inner chamber of sliding sleeve, and the output of push cylinder two runs through to the inner chamber of adjusting the spout and with sliding sleeve fixed connection.

Preferably, positioning mechanism includes that fixed mounting is at the removal frame on an output of push cylinder, the inner chamber fixedly connected with slide bar of removal frame, the surperficial swing joint of slide bar has the fastener, the surface cover of slide bar is equipped with the spring, fixed connection is on fastener and removal frame respectively at the both ends of spring, the spacing groove has all been seted up to the both sides of removal frame, the inner chamber sliding connection of spacing groove has the stopper, the equal fixed connection in one side of two stoppers is on the fastener, one side and a push cylinder fixed connection of removal frame.

Preferably, one side of the clamping piece, which is far away from the movable frame, is provided with an inclined plane, and the inclination angle of the inclined plane is sixty degrees.

Preferably, the bottom of the clamping piece is provided with a notch.

Preferably, the bottom of the moving frame and the protruding part of the bottom of the clamping piece are attached to the top of the take-off platform to slide.

Preferably, the bottom of the mounting bracket slides against the top of the takeoff platform.

In summary, the present application includes at least one of the following beneficial technical effects:

1. the utility model discloses in the time of in-service use, when changing the battery, receive the instruction at the automatic airport of unmanned aerial vehicle, promote cylinder one and start and promote to remove and put up the direction removal to unmanned aerial vehicle, the depressed part of fastener bottom can block on the unmanned aerial vehicle undercarriage, thereby fix unmanned aerial vehicle, prevent the unmanned aerial vehicle activity, after unmanned aerial vehicle is fixed, automatic change battery device receives the instruction and stretches out then take off the old battery on the unmanned aerial vehicle from the inside of taking off the platform, and change new battery, so just, can guarantee that unmanned aerial vehicle aligns with automatic change battery device when changing the battery, and be difficult for the activity, the quick change battery of also easier, time saving and labor saving, the person of facilitating the use uses.

2. The utility model discloses a setting of pushing mechanism two, when the position that unmanned aerial vehicle parked was too big with the fixed establishment error, pushing cylinder two can start after receiving the instruction and promote whole pushing mechanism one and carry out the back-and-forth movement, and then drive whole fixed establishment and carry out the back-and-forth movement to this adjustment unmanned aerial vehicle and fixed establishment's error, make fixed establishment can fix a position unmanned aerial vehicle, the person of facilitating the use uses.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this application, serve to provide a further understanding of the application and to enable other features, objects, and advantages of the application to be more apparent. The drawings and their description illustrate the embodiments of the invention and do not limit it. In the drawings:

fig. 1 is a schematic view of the present invention.

Fig. 2 is a perspective sectional view of the present invention.

Fig. 3 is a perspective assembly view of the fixing mechanism of the present invention.

Fig. 4 is a perspective assembly view of the pushing mechanism of the present invention.

Fig. 5 is a perspective assembly view of the pushing mechanism of the present invention.

Description of reference numerals: 1. unmanned automatic airports; 2. a guide slide rail; 3. a cabin door; 4. a first pushing mechanism; 5. a takeoff platform; 6. fixing the mounting groove; 7. a second pushing mechanism; 8. a fixing mechanism; 9. automatically replacing the battery device; 41. a sliding sleeve; 42. a mounting bracket; 43. a first pushing cylinder; 71. a mounting frame; 72. adjusting the sliding chute; 73. a second pushing cylinder; 81. a movable frame; 82. a slide bar; 83. a fastener; 84. a spring; 85. a limiting groove; 86. and a limiting block.

Detailed Description

In order to make the technical solutions better understood by those skilled in the art, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only partial embodiments of the present application, but not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.

It should be noted that the terms "first," "second," and the like in the description and claims of this application and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It should be understood that the data so used may be interchanged under appropriate circumstances such that embodiments of the application described herein may be used. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.

In this application, the terms "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings. These terms are used primarily to better describe the present application and its embodiments, and are not used to limit the indicated devices, elements or components to a particular orientation or to be constructed and operated in a particular orientation.

Moreover, some of the above terms may be used to indicate other meanings besides the orientation or positional relationship, for example, the term "on" may also be used to indicate some kind of attachment or connection relationship in some cases. The specific meaning of these terms in this application will be understood by those of ordinary skill in the art as appropriate.

In addition, the term "plurality" shall mean two as well as more than two.

It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.

The first embodiment is as follows:

with reference to fig. 1 and 5, the embodiment of the application discloses a remote control unmanned aerial vehicle-based control system, which comprises an unmanned aerial vehicle automatic airport 1, wherein the front side and the rear side of the top of the unmanned aerial vehicle automatic airport 1 are respectively provided with a guide slide rail 2, two sides of the surfaces of the two guide slide rails 2 are respectively movably provided with a cabin door 3 positioned at the top of the unmanned aerial vehicle automatic airport 1, the bottom of the inner cavity of the unmanned aerial vehicle automatic airport 1 is movably provided with a take-off platform 5, two sides of the top of the take-off platform 5 are respectively provided with a first pushing mechanism 4, one side of the first pushing mechanism 4 is provided with a second pushing mechanism 7, one side of the second pushing mechanism 7 is provided with a fixing mechanism 8, the front side and the rear side of the top of the take-off platform 5 are respectively provided with a fixing installation groove 6 matched with the second pushing mechanism 7, the center position of the top of the take-off platform 5 is provided with an automatic battery replacing device 9, the first pushing mechanism 4 comprises a sliding sleeve 41 sliding in the inner cavity of a regulating chute 72, the surface of the sliding sleeve 41 is fixedly connected with a second pushing cylinder 73, one side of the sliding sleeve 41 is fixedly connected with a mounting bracket 42, the top of the mounting bracket 42 is fixedly provided with a first pushing cylinder 43, the output end of the first pushing cylinder 43 extends into the inner cavity of the sliding sleeve 41, the output end of the second pushing cylinder 73 penetrates through the inner cavity of the adjusting chute 72 and is fixedly connected with the sliding sleeve 41, the fixing mechanism 8 comprises a moving frame 81 fixedly arranged on the output end of the first pushing cylinder 43, the inner cavity of the moving frame 81 is fixedly connected with a sliding rod 82, the surface of the sliding rod 82 is movably connected with a clamping piece 83, the surface of the sliding rod 82 is sleeved with a spring 84, two ends of the spring 84 are respectively and fixedly connected with the clamping piece 83 and the moving frame 81, two sides of the moving frame 81 are respectively provided with a limiting groove 85, the inner cavity of the limiting groove 85 is slidably connected with limiting blocks 86, one side of each limiting block 86 is fixedly connected with the clamping piece 83, remove one side of frame 81 and 43 fixed connection of push cylinder, spacing groove 85 has all been seted up to the both sides of removing frame 81, the inner chamber sliding connection of spacing groove 85 has stopper 86, the equal fixed connection in one side of two stopper 86 is on fastener 83, one side that removes frame 81 was kept away from to fastener 83 is provided with the inclined plane, the inclination on inclined plane is sixty degrees, the notch has been seted up to the bottom of fastener 83, the bottom of removing frame 81 and the outstanding part in fastener 83 bottom all laminate and slide at the top of taking off platform 5, the bottom of installing bracket 42 is hugged closely and is slided at the top of taking off platform 5.

When the unmanned aerial vehicle automatic airport 1 receives an instruction, when the unmanned aerial vehicle is ready to take off, the cabin door 3 above the airport is opened, the take-off instruction is received, the unmanned aerial vehicle rises to a certain height along with the take-off platform 5, takes off, and the cabin door 3 above the airport is closed; in-process of carrying out the task, the user can show the progress of task through the curved surface screen, and the environment in task place, other data of task environment in addition, unmanned aerial vehicle has carried out the task, when receiving descending instruction or electric quantity not enough, unmanned aerial vehicle flies to 1 top height in the automatic airport of unmanned aerial vehicle, at this moment, hatch door 3 of airport top is opened, unmanned aerial vehicle descends to the platform 5 that takes off, afterwards, take off platform 5 and descend to 1 inside appointed height in the automatic airport of unmanned aerial vehicle, hatch door 3 closes, 1 relevant operations that begin to carry out the battery of the automatic airport of unmanned aerial vehicle.

When the battery is replaced, the battery is instructed by the unmanned aerial vehicle automatic airport 1, the first pushing cylinder 43 is started and pushes the moving frame 81 to move towards the unmanned aerial vehicle, so that the limiting groove 85 is driven to move towards the unmanned aerial vehicle, when the clamping piece 83 touches the landing support of the unmanned aerial vehicle, due to the arrangement of the upper inclined plane of the clamping piece 83, the clamping piece 83 can be forced to move upwards on the surface of the sliding rod 82 when contacting the landing gear of the unmanned aerial vehicle, so that the spring 84 is stretched, when the protruding part at the bottom of the clamping piece 83 crosses the landing gear of the unmanned aerial vehicle, the clamping piece 83 is pulled down under the action of the spring 84, the dent at the bottom of the clamping piece 83 can be clamped on the landing gear of the unmanned aerial vehicle, so that the unmanned aerial vehicle is fixed, the clamping piece 83 can drive the limiting block 86 to slide in the inner cavity of the limiting groove 85 during the moving, so as to limit the clamping piece 83, the stability of the clamping piece 83 when the unmanned aerial vehicle is moved is ensured, after the unmanned aerial vehicle is fixed, automatic change battery device 9 and receive the instruction and stretch out then take off the old battery on the unmanned aerial vehicle from the inside of taking off platform 5, and change new battery, accomplish the inside of taking off platform 5 of withdrawing after the change of battery, so just can guarantee that unmanned aerial vehicle aligns with automatic change battery device 9 when changing the battery, the quick change battery also more easily, labour saving and time saving person of facilitating the use uses, what need explain, after having changed the battery, two 73 drive whole fixed establishment 8 and a 4 removal of pushing mechanism, break away from the support that falls until fastener 83, so unmanned aerial vehicle just can take off once more, and at this moment fastener 83 also can reset, and under the effect of two 73 of pushing cylinder, the normal position is replied.

Combine fig. 3 to 5, two 7 pushing mechanism include embedded fixed mounting at the mounting bracket 71 of 6 inner chambers of fixed mounting groove, regulation spout 72 has been seted up to one side of mounting bracket 71, the front side fixed mounting of mounting bracket 71 has two 73 pushing cylinder, setting through two 7 pushing mechanism, when the position that unmanned aerial vehicle parked is too big with the 8 errors of fixed establishment, two 73 pushing cylinder can start to promote whole pushing mechanism 4 and carry out the back-and-forth movement after receiving the instruction, and then drive whole fixed establishment 8 and carry out the back-and-forth movement, with this error of adjustment unmanned aerial vehicle and fixed establishment 8, make fixed establishment 8 fix a position unmanned aerial vehicle, the person of facilitating the use uses.

The above description is only a preferred embodiment of the present application and is not intended to limit the present application, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. Control system based on remote control unmanned aerial vehicle, including unmanned aerial vehicle automatic airport (1), its characterized in that: the utility model discloses an automatic airport of unmanned aerial vehicle, including unmanned aerial vehicle automatic airport (1), two fixed mounting platforms (5) are all provided with push mechanism one (4), one side of push mechanism one (4) is provided with push mechanism two (7), one side of push mechanism two (7) is provided with fixed establishment (8), fixed mounting groove (6) with push mechanism two (7) looks adaptation are all seted up to the front side and the rear side at platform (5) top of taking off, the central point at platform (5) top of taking off puts and is provided with automatic change battery device (9).

2. The remote control drone-based control system of claim 1, wherein: push mechanism two (7) are including embedded fixed mounting at mounting bracket (71) of fixed mounting groove (6) inner chamber, regulation spout (72) have been seted up to one side of mounting bracket (71), the front side fixed mounting of mounting bracket (71) has push cylinder two (73).

3. The remote control drone-based control system of claim 2, wherein: push mechanism (4) include at gliding sliding sleeve (41) of regulation spout (72) inner chamber, the surface and the two (73) fixed connection of push cylinder of sliding sleeve (41), one side fixedly connected with mounting bracket (42) of sliding sleeve (41), the top fixed mounting of mounting bracket (42) has push cylinder (43), the output of push cylinder (43) stretches into the inner chamber of sliding sleeve (41), the output of push cylinder two (73) run through to the inner chamber of regulation spout (72) and with sliding sleeve (41) fixed connection.

4. The remote control drone-based control system of claim 3, wherein: fixed establishment (8) include that fixed mounting moves frame (81) on pushing away cylinder (43) output, the inner chamber fixedly connected with slide bar (82) of moving frame (81), the surperficial swing joint of slide bar (82) has fastener (83), the surface cover of slide bar (82) is equipped with spring (84), the both ends difference fixed connection of spring (84) is on fastener (83) and moving frame (81), spacing groove (85) have all been seted up to the both sides of moving frame (81), the inner chamber sliding connection of spacing groove (85) has stopper (86), the equal fixed connection in one side of two stoppers (86) is on fastener (83), move one side and the first (43) fixed connection of pushing away cylinder of frame (81).

5. The remote control drone-based control system of claim 4, wherein: one side of the clamping piece (83) far away from the moving frame (81) is provided with an inclined plane, and the inclined angle of the inclined plane is sixty degrees.

6. The remote control drone-based control system of claim 4, wherein: the bottom of the clamping piece (83) is provided with a notch.

7. The remote control drone-based control system of claim 4, wherein: the bottom of the moving frame (81) and the protruding part of the bottom of the clamping piece (83) are attached to the top of the take-off platform (5) to slide.

8. The remote control drone-based control system of claim 3, wherein: the bottom of the mounting bracket (42) clings to the top of the takeoff platform (5) to slide.