Detector structure and unmanned aerial vehicle
By introducing a movable snap and buckle position matching mechanism into the detector structure, the problem of inconvenient disassembly of existing detectors is solved, and the detection components are easily separated and installed from the drone is achieved, and maintenance and replacement are improved. Convenience.
Patent Information
- Application Number
- CN202323563412.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2023-12-25
- Publication Date
- 2024-12-17
- Estimated Expiration
- 2033-12-25
AI Technical Summary
The existing detector structure is inconvenient to disassemble from the drone, resulting in difficulties in need of changing the detection range or performing maintenance.
The movable snap and buckle position matching mechanism is adopted to disengage the buckle position through button operation, thereby realizing the separation and installation of the detection components from the drone, simplifying the disassembly and installation process.
Through the coordination of movable buckles and buckle positions, users can easily disassemble and replace the detection components, solving the problem of inconvenient disassembly of detectors in the prior art and improving the convenience of maintenance and replacement.
Smart Images
Figure CN222179867U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a detector structure and an unmanned aerial vehicle. Background Art
[0002] In order to maintain designated airspace and prevent illegal drones from entering, existing technology involves installing detectors on drones to detect whether there are illegal drones entering the current airspace. When an illegal drone is detected, the drone's location will be locked.
[0003] However, most existing detector structures are installed on drones in an embedded manner. When the detector structure needs to be replaced to adjust the detection range, it is inconvenient to remove the detector from the drone. Utility Model Content
[0004] The main purpose of the utility model is to provide a detector structure, aiming to solve the problem that the existing detector is inconvenient to disassemble from the drone.
[0005] To achieve the above-mentioned purpose, the detector structure proposed by the utility model includes:
[0006] A first mounting base, for connecting with the drone;
[0007] A second mounting seat is mounted on the first mounting seat, and one of the first mounting seat and the second mounting seat is provided with an active buckle, and the other is provided with a buckle position corresponding to the active buckle;
[0008] a button for installing the active buckle, so that the active buckle has a locked state in which it is engaged with the buckle position, and an unlocked state in which it is separated from the buckle position; when the button is pressed, the active buckle can be switched from the locked state to the unlocked state;
[0009] A detection component mounted on the second mounting base, the detection component comprising an antenna, the antenna being used to emit a detection wave; and
[0010] The protective shell is installed on the second mounting seat and covers the outside of the detection component.
[0011] Optionally, the detector structure further includes a guide seat, and the guide seat is used for installing the button.
[0012] Optionally, a guide groove is provided in the guide seat, and the button is installed in the guide groove and can move along the guide groove.
[0013] Optionally, the detector structure further includes a limiting member, and when the button is released, the limiting member is used to make the button have a tendency to reset to put the movable buckle in a locked state.
[0014] Optionally, a receiving hole for installing the limiting member is provided in the button, and the limiting member includes a spring and a limiting column. When the button is pressed, one end of the spring abuts against the inner wall of the receiving hole, and the other end abuts against the limiting column.
[0015] Optionally, a slot is provided on the first mounting seat, and a sliding flange is provided on the second mounting seat corresponding to the slot, and the second mounting seat is slidably installed on the first mounting seat by cooperating with the slot. When the second mounting seat slides to a preset position, the movable buckle can cooperate with the buckle position.
[0016] Optionally, the buckle position is configured as a slot provided on the second mounting seat, the slot is an L-shaped structure, and the two ends of the slot respectively penetrate the two adjacent outer sides of the sliding flange, one end of the slot is used for the movable buckle to enter, and the other end of the slot is used to buckle with the movable buckle.
[0017] Optionally, the second mounting seat is provided with a receiving cavity for installing a communication circuit board, and the receiving cavity is located outside the protective shell.
[0018] Optionally, the detection component includes an antenna, and the antenna is configured as a 3dBi omnidirectional antenna or an 8dBi omnidirectional antenna.
[0019] The utility model also provides an unmanned aerial vehicle, comprising a fuselage and a detector structure, wherein the detector structure is any of the above-mentioned detector structures, and the detector structure is detachably connected to the fuselage.
[0020] The technical solution of the utility model adopts the cooperation of movable buckles and buckle positions. When it is necessary to disassemble the detection component, replace a different detection range or repair the detection component, the movable buckle can be disengaged from the buckle position by operating the button. At this time, the user can remove the second mounting seat from the first mounting seat, and then remove it from the drone, and then replace the detection component with a different detection range for use. The cooperation of the movable buckle and the buckle position can realize the separation and installation of the detection component and the drone, thereby solving the technical problems existing in the prior art. BRIEF DESCRIPTION OF THE DRAWINGS
[0021] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on the structures shown in these drawings without paying creative work.
[0022] Figure 1 This is a schematic diagram of the structure of an embodiment of the detector structure of the utility model;
[0023] Figure 2 for Figure 1 A partial enlarged view of the middle A;
[0024] Figure 3 for Figure 1 A schematic structural diagram of an embodiment of the internal structure of the middle connecting shell;
[0025] Figure 4 for Figure 3 A schematic structural diagram of an embodiment of a middle seat body;
[0026] Figure 5 for Figure 3 A partial enlarged view of point B in the middle;
[0027] Figure 6 for Figure 1 A schematic structural diagram of an embodiment of a middle buckle position;
[0028] Figure 7 for Figure 1 A schematic structural diagram of an embodiment of a middle plug-in shell;
[0029] Figure 8 for Figure 1 A schematic structural diagram of an embodiment of a mounting plate;
[0030] Fig. 9 for Figure 1 A schematic structural diagram of an embodiment of a middle protective shell.
[0031] Description of Figure Numbers:
[0032] Label name Label name 100 First Mount 110 Fixed plate 120 Connection shell 130 Slots 200 Second Mount 210 Plug shell 211 First positioning column 220 Mounting Plate 221 Second positioning column 222 Mounting holes 230 Sliding flange 300 Button 310 Accommodating hole 400 Guide seat 410 Seat cover 420 base body 421 Guide groove 500 Activity buckle 600 Limiting parts 610 spring 620 Limit column 700 Buckle position 800 Protective case 810 The third positioning column
[0033] The realization of the purpose, functional features and advantages of the utility model will be further explained in conjunction with embodiments and with reference to the accompanying drawings. DETAILED DESCRIPTION
[0034] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0035] It should be noted that all directional indications in the embodiments of the present invention (such as up, down, left, right, front, back...) are only used to explain the relative position relationship, movement status, etc. between the components under a certain specific posture (as shown in the accompanying drawings). If the specific posture changes, the directional indication will also change accordingly.
[0036] In the present invention, unless otherwise clearly specified and limited, the terms "connection", "fixation", etc. should be understood in a broad sense. For example, "fixation" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements, unless otherwise clearly defined. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.
[0037] In addition, if there are descriptions involving "first", "second", etc. in the embodiments of the utility model, the descriptions of "first", "second", etc. are only used for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In addition, the meaning of "and / or" appearing in the full text includes three parallel schemes. Taking "A and / or B" as an example, it includes scheme A, or scheme B, or a scheme that satisfies both A and B. In addition, the technical solutions between the various embodiments can be combined with each other, but it must be based on the ability of ordinary technicians in this field to implement. When the combination of technical solutions is contradictory or cannot be implemented, it should be deemed that such a combination of technical solutions does not exist and is not within the scope of protection required by the utility model.
[0038] The utility model provides a detector structure.
[0039] In the embodiment of the utility model, the detector structure includes a first mounting seat 100, a second mounting seat 200, a button 300, a detection component and a protective shell 800: the first mounting seat 100 is used to connect with the drone, wherein the first mounting seat 100 and the drone are connected by bolts, and the specific first mounting seat 100 includes a fixing plate 110 and a connecting shell 120, wherein the bolts pass through the connecting shell 120 and the fixing plate 110 to connect with the drone; the second mounting seat 200 is installed on the first mounting seat 100, and one of the first mounting seat 100 and the second mounting seat 200 is connected to the first mounting seat 100. One is provided with an active buckle 500, and the other is provided with a buckle position 700 corresponding to the active buckle 500, wherein the second mounting seat 200 includes a plug-in shell 210 and a mounting plate 220, and the plug-in shell 210 and the mounting plate 220 are connected by screws, wherein the plug-in shell 210 is provided with a first positioning column 211, and the mounting plate 220 is provided with a second positioning column 221 corresponding to the first positioning column 211, and the first positioning column 211 and the second positioning column 221 are connected by screws to connect the mounting plate 220 and the plug-in shell 210, and the plug-in shell 210 is installed on the connection shell 12 in the first mounting seat 100 0, specifically, the active buckle 500 is arranged on the connecting shell 120, and the buckle position 700 is arranged on the plug shell 210; the button 300 is used for installing the active buckle 500, wherein the active buckle 500 is fixedly arranged on the top of the button 300, and the button 300 is used to make the active buckle 500 have a locked state with the buckle position 700, and an unlocked state relative to the buckle position 700. When the button 300 is pressed, the active buckle 500 can switch from the locked state to the unlocked state; the detection component is installed on the second mounting seat 200, wherein the detection component is installed on On the side of the mounting plate 220 facing away from the plug shell 210, the specific detection components include an antenna, a power supply, a whitelist ID receiving module and an ID transmitting module, wherein the antenna is used to send out a detection wave to detect whether there is a "black household" drone in the airspace, and the "black household" drone is locked by the ID signal fed back by the detection wave. At the same time, for the judgment of the "black household" drone, the ID signal fed back by the detection wave is checked with the whitelist ID. When it is found that the fed-back ID signal is not in the whitelist ID, it is identified as a "black household", and the position of the "black household" drone is locked according to the detection wave;The protective shell 800 is installed on the second mounting seat 200 and covers the outside of the detection component, wherein the protective shell 800 is installed on the side of the mounting plate 220 in the second mounting seat 200 away from the plug-in shell 210, and the detection component can be protected from damage under the action of the protective shell 800. Specifically, a third positioning column 810 is arranged in the protective shell 800, and a mounting hole 222 is arranged on the mounting plate 220 corresponding to the third positioning column 810. The bolt passes through the mounting hole 222 and is connected to the third positioning column 810, and the protective shell 800 can be fixed. 0 is connected to the mounting plate 220. At the same time, in this embodiment, through the cooperation between the active buckle 500 and the buckle position 700, when it is necessary to disassemble the detection component, change a different detection range or repair the detection component, the active buckle 500 can be disengaged from the buckle position 700 by operating the button 300. At this time, the user can disassemble the second mounting seat 200 from the first mounting seat 100, and then disassemble it from the drone, which is very convenient to use, and can solve the technical problems existing in the prior art; such as; Figure 1 , Figure 3 shown.
[0040] The technical solution of the present invention adopts the cooperation of the active buckle 500 and the buckle position 700. When it is necessary to disassemble the detection component, replace a different detection range or repair the detection component, the active buckle 500 can be disengaged from the buckle position 700 by operating the button 300. At this time, the user can remove the second mounting seat 200 from the first mounting seat 100, and then remove it from the drone, and then replace the detection component with a different detection range for use. The cooperation of the active buckle 500 and the buckle position 700 can realize the separation and installation of the detection component and the drone, thereby solving the technical problems existing in the prior art.
[0041] In one embodiment, reference Figures 3 to 5 The detector structure also includes a guide seat 400, and the guide seat 400 is used for installing the button 300, wherein the guide seat 400 is fixed to the connecting shell 120. Specifically, the guide seat 400 includes a seat body 420 and a seat cover 410, the seat body 420 is fixed to the connecting shell 120, and the seat cover 410 is detachably connected to the seat body 420, wherein the seat cover 410 is detachably connected to the seat body 420 by screws, wherein the seat body 420 can be integrally formed with the connecting shell 120, and this structure can reduce the production cost of the structure.
[0042] In one embodiment, reference Figure 5A guide groove 421 is provided in the guide seat 400, and the button 300 is installed in the guide groove 421 and can move along the guide groove 421. In this embodiment, the guide groove 421 is opened in the seat body 420, and the button 300 is slidably installed in the guide groove 421. Under the action of the guide groove 421, the button 300 can be easily moved in the guide seat 400, so that the movable buckle 500 is unlocked or buckled with the buckle position 700.
[0043] In one embodiment, reference Figure 5 The detector structure also includes a limit member 600. When the button 300 is released, the limit member 600 is used to make the button 300 have a tendency to reset to make the active buckle 500 in a locked state. In this embodiment, when the button 300 is released, the limit member 600 can drive the button 300 to reset. Since the active buckle 500 is fixed to the button 300, when the button 300 is reset, it can drive the active buckle 500 to be in a locked state, which can facilitate the operation of the user.
[0044] In one embodiment, reference Figure 5 The button 300 is provided with a receiving hole 310 for installing the limiting member 600. The limiting member 600 includes a spring 610 and a limiting column 620. When the button 300 is pressed, one end of the spring 610 abuts against the inner wall of the receiving hole 310, and the other end abuts against the limiting column 620. In this embodiment, the limiting column 620 is fixed in the receiving hole 310. When the button 300 is pressed, the inner wall of the receiving hole 310 pushes against one end of the spring 610. Since the limiting column 620 is fixed in the receiving hole 310, At this time, the spring 610 is compressed, and the active buckle 500 is also unlocked from the buckle position 700. At this time, the button 300 is released, and the button 300 returns to its original position under the elastic potential energy of the spring 610, and at the same time, the active buckle 500 is driven to buckle with the buckle position 700. The operation is very convenient. When the user needs to replace the detection component, he only needs to press the button 300 with one hand and remove the second mounting seat 200 from the first mounting seat 100 with the other hand. It is very convenient. At the same time, the structure is simple, which can reduce the use cost of the structure. In other embodiments, the limit column 620 can also be offset against the active buckle 500.
[0045] In one embodiment, reference Figure 1 , Figure 2, a slot 130 is provided on the first mounting seat 100, specifically, a slot 130 is opened on the connecting shell 120, and a sliding flange 230 is provided on the second mounting seat 200 corresponding to the slot 130, wherein the sliding flange 230 is provided on the plug-in shell 210, and the sliding flange 230 and the slot 130 are slidably matched. By the cooperation of the sliding flange 230 and the slot 130, the second mounting seat 200 is slidably installed on the first mounting seat 100, and when the second mounting seat 200 slides to a preset position, the active buckle 500 can cooperate with the buckle position 700; in this embodiment, when the plug-in shell 210 is inserted into the connecting shell 120, the sliding flange 230 can be inserted into the slot 130, and at the same time, under the action of the slot 130, it can play a guiding role for the plug-in shell 210, and under the action of the sliding flange 230, the plug-in shell 210 can be prevented from being separated from the connecting shell 120.
[0046] In one embodiment, reference Figure 6 The buckle position 700 is configured as a card slot provided on the second mounting seat 200, wherein the card slot is provided on the top surface of the plug-in shell 210, and the card slot is an L-shaped structure, and the two ends of the card slot are respectively provided to penetrate the two adjacent outer sides of the sliding flange 230, one end of the card slot is used for the active card buckle 500 to enter, and the other end of the card slot is used to buckle with the active card buckle 500; in this embodiment, when the plug-in shell 210 is inserted into the connecting shell 120 and moved to a certain position, the active card buckle 500 can enter the card slot through one end of the card slot, and when the active card buckle 500 enters the card slot When the plug-in shell 210 is inserted into the connecting shell 120, the active buckle 500 can move along the slot. When the plug-in shell 210 is inserted into the preset position, the active buckle 500 can coincide with the other end of the slot. At this time, the spring 610 will expand and return to its original shape. When the spring 610 returns to its original shape, it can drive the active buckle 500 to be inserted into the other end of the slot. At this time, the plug-in shell 210 can be restricted in the connecting shell 120. In the present embodiment, the active buckle 500 is configured as an L-shaped structure, and one end is fixed to the button 300, and the other end can move along the slot.
[0047] In one embodiment, reference Figure 7 The second mounting seat 200 is provided with a housing cavity for installing a communication circuit board, and the housing cavity is located outside the protective shell 800. In the present embodiment, the housing cavity is arranged in the plug-in shell 210, wherein a through hole is arranged between the plug-in shell 210 and the connecting shell 120, and the through hole facilitates the passage of the wiring harness of the communication circuit board. At the same time, a protective ring is installed on the fixing plate 110 in the first mounting seat 100, wherein the wiring harness of the communication circuit board passes through the protective ring and is connected to the drone. At this time, under the action of the protective ring, the wiring harness of the communication circuit board can be prevented from contacting and rubbing with the fixing plate 110.
[0048] In one embodiment, the antenna is configured as a 3dBi omnidirectional antenna or an 8dBi omnidirectional antenna. When the 3dBi omnidirectional antenna is selected, the detection component can detect a range of 3km. When the 8dBi omnidirectional antenna is selected, the detection component can detect a range of 5km.
[0049] The utility model also proposes a drone, which includes a fuselage and a detector structure. The specific structure of the detector structure refers to the above embodiment. Since the drone adopts all the technical solutions of all the above embodiments, it at least has all the beneficial effects brought by the technical solutions of the above embodiments, which will not be repeated here. The detector structure is detachably connected to the fuselage, and the fixing plate 110 in the detector structure is detachably connected to the fuselage by bolts.
[0050] The above description is only an optional embodiment of the present invention, and does not limit the patent scope of the present invention. All equivalent structural changes made by using the contents of the present invention specification and drawings under the inventive concept of the present invention, or directly / indirectly applied in other related technical fields are included in the patent protection scope of the present invention.
Claims
1. A detector structure, characterized in that: include: A first mounting base, for connecting with a drone; A second mounting seat is mounted on the first mounting seat, and one of the first mounting seat and the second mounting seat is provided with an active buckle, and the other is provided with a buckle position corresponding to the active buckle; a button for installing the active buckle, so that the active buckle has a locked state in which it is engaged with the buckle position, and an unlocked state in which it is separated from the buckle position; when the button is pressed, the active buckle can be switched from the locked state to the unlocked state; A detection component is mounted on the second mounting seat, wherein the detection component includes an antenna, and the antenna is used to emit a detection wave; as well as The protective shell is installed on the second mounting seat and covers the outside of the detection component.
2. The detector structure according to claim 1, characterized in that: The detector structure also includes a guide seat, and the guide seat is used for installing the button.
3. The detector structure as claimed in claim 2, characterized in that: A guide groove is provided in the guide seat, and the button is installed in the guide groove and can move along the guide groove.
4. The detector structure according to claim 1, characterized in that: The detector structure further comprises a limiting member, and when the button is released, the limiting member is used to make the button have a tendency to return to a position where the movable buckle is in a locked state.
5. The detector structure as claimed in claim 4, characterized in that: The button is provided with a receiving hole for installing the limiting member, and the limiting member includes a spring and a limiting column. When the button is pressed, one end of the spring abuts against the inner wall of the receiving hole, and the other end abuts against the limiting column.
6. The detector structure according to any one of claims 1 to 5, characterized in that: The first mounting seat is provided with a slot, and the second mounting seat is provided with a sliding flange corresponding to the slot. The sliding flange cooperates with the slot so that the second mounting seat can be slidably installed on the first mounting seat. When the second mounting seat slides to a preset position, the movable buckle can cooperate with the buckle position.
7. The detector structure according to claim 6, characterized in that: The buckle position is configured as a slot provided on the second mounting seat, the slot is an L-shaped structure, and the two ends of the slot respectively penetrate the two adjacent outer sides of the sliding flange, one end of the slot is used for the movable buckle to enter, and the other end of the slot is used to buckle with the movable buckle.
8. The detector structure according to claim 7, characterized in that: The second mounting seat is provided with a receiving cavity for installing a communication circuit board, and the receiving cavity is located outside the protective shell.
9. The detector structure as claimed in claim 1, characterized in that: The detection component includes an antenna, and the antenna is configured as a 3dBi omnidirectional antenna or an 8dBi omnidirectional antenna.
10. A drone, characterized in that: The invention comprises a body and a detector structure, wherein the detector structure is the detector structure as claimed in any one of claims 1 to 9, and the detector structure is detachably connected to the body.