Detection probe structure of unmanned aerial vehicle

Abstract

The utility model discloses an unmanned aerial vehicle detection probe structure, which comprises an unmanned aerial vehicle bearing seat, an unmanned aerial vehicle bearing cover is arranged at the top of the unmanned aerial vehicle bearing seat, the outer four walls of the unmanned aerial vehicle bearing cover are fixedly connected with assembly support lugs, and the top of the unmanned aerial vehicle bearing cover penetrates through and is rotatably connected with an assembly sleeve. And one end of the assembling sleeve is fixedly connected with an assembling rotating head. According to the utility model, by pulling or loosening the limiting pull plate, the limiting pull plate drives the limiting insertion strip to be inserted into or separated from the limiting support block, and then the limiting L-shaped plate is pulled and turned over, so that the limiting clip-shaped opening in the limiting L-shaped plate is clamped with or separated from the corresponding limiting support block; and then a fixing pull block drives a fixing insertion strip to be inserted into or separated from an assembling insertion opening in an assembling rotary head, so that installation between the unmanned aerial vehicle bearing seat and the unmanned aerial vehicle bearing cover is limited and locked, and the using effect is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane detection technical field especially relates to a kind of unmanned plane detection probe structure. BACKGROUND

[0002] Unmanned aircraft is called "drone", is using radio remote control equipment and self-provided program control device manipulates the aircraft without people, or by onboard computer completely or intermittently autonomously operates, while unmanned plane can replace manual work to enter high altitude, steep slope, fire scene and other dangerous areas to perform detection tasks, and in the process of unmanned plane application, various functional modules are often carried on unmanned plane to realize different functions.

[0003] Patent publication number CN109649669A, the application discloses a kind of for unmanned plane's rotary self-locking probe connection structure, including functional module bottom cover and unmanned plane top cover, the upper surface of the unmanned plane top cover is provided with the installation base that is matched with functional module bottom cover;The lower surface of the functional module bottom cover is provided with first connecting mechanism, the installation base is provided with second connecting mechanism;The first connecting mechanism is connected with second connecting mechanism by probe, and is mutually matched and fixed functional module bottom cover in installation base, the connection and locking of unmanned plane top cover and functional module bottom cover are completed by simple rotation operation in this application, and probe is used to connect between unmanned plane top cover and functional module bottom cover, connection is more reliable and convenient.

[0004] But, above-mentioned self-locking assembly is connected when locking cover plate and installation base of probe connection, need be connected by rotation, and the clamping limit of pure rotation is still caused locking cover plate and installation base to separate when being impacted or external factor, simultaneously, the probe female head that probe male head is matched also separates, lead to locking connection is not ideal, affect actual use, thereby reduce use effect. UTILITY MODEL CONTENTS

[0005] The utility model aims at solving the shortcomings in the prior art, and provides an unmanned plane detection probe structure.

[0006] In order to achieve the above object, the utility model discloses the following technical scheme: a kind of unmanned aerial vehicle detection probe structure, including unmanned aerial vehicle receiving seat, the top of the unmanned aerial vehicle receiving seat is provided with unmanned aerial vehicle receiving cover, the outer four walls of the unmanned aerial vehicle receiving cover are all fixedly connected with assembly lug, the top of the unmanned aerial vehicle receiving cover is penetrated and rotationally connected with assembly sleeve, one end of the assembly sleeve is fixedly connected with assembly swivel head, the outer side wall of the assembly swivel head is provided with a plurality of assembly socket, the inner wall of the assembly sleeve is fixedly connected with assembly clamping block on both sides, the bottom of the unmanned aerial vehicle receiving cover is fixedly connected with probe male head, the top of the unmanned aerial vehicle receiving seat is fixedly connected with four limit supports, the top of the unmanned aerial vehicle receiving seat is connected with four limit components;

[0007] The top of the unmanned aerial vehicle receiving seat is provided with mounting port, the bottom of the mounting port is fixedly connected with functional module, the top center of the functional module is provided with receiving port, the receiving port is provided with probe female head inside, the probe male head is movably inserted with the probe female head, the top edge of the functional module is provided with two assembly clamping ports, the outer side wall of the functional module is provided with assembly ring groove, two assembly clamping blocks are all slidingly connected inside assembly ring groove, the top of the unmanned aerial vehicle receiving cover is connected with two symmetrical fixed components.

[0008] As further description of the above technical scheme:

[0009] The limit component includes limit recess block fixedly connected with the top of the unmanned aerial vehicle receiving seat, limit shaft is rotationally connected between the two sides of the inner wall of the limit recess block, the outer side wall of the limit shaft is fixedly sleeved with limit L-shaped plate.

[0010] As further description of the above technical scheme:

[0011] The top of the limit L-shaped plate is penetrated and provided with limit meander port, the limit meander port is movably clamped with corresponding limit support inside, the top of the limit L-shaped plate is provided with two limit grooves, limit sliding block is slidingly connected inside the limit groove, limit spring is fixedly connected in the inner wall of the limit groove.

[0012] As further description of the above technical scheme:

[0013] The end of the limit spring is fixedly connected with corresponding limit sliding block, limit pull plate is fixedly connected between two limit sliding blocks.

[0014] As further description of the above technical scheme:

[0015] The side of the limit pull plate close to the unmanned aerial vehicle receiving cover is fixedly connected with limit insertion strip, the end of the limit insertion strip is penetrated and extended to outside limit support.

[0016] As further description of the above technical scheme:

[0017] The fixed assembly comprises a fixed plate fixedly connected with the top of the UAV receiving cover, a fixed insertion strip is arranged through the side wall of the fixed plate, and one end of the fixed insertion strip is fixedly connected with a fixed pull block.

[0018] Further description is made to the technical scheme:

[0019] The other end of the fixed insertion strip is movably inserted into one of the assembly insertion ports, a fixed spring is movably sleeved with the outer side wall of the fixed insertion strip, and the two ends of the fixed spring are fixedly connected with the side wall of the fixed pull block and the side wall of the fixed plate, respectively.

[0020] The utility model has the advantages of:

[0021] The fixed plate, the fixed insertion strip, the fixed pull block and the fixed spring are cooperated by the fixed assembly, so that the fixed insertion strip is inserted into or separated from the assembly insertion port on the assembly rotating head by the fixed pull block, the assembly rotating head is rotated, the assembly clamping block on the assembly sleeve is rotated in the assembly ring groove and is aligned with the assembly clamping port, then the UAV receiving cover is pulled or pushed, the assembly supporting lug on the UAV receiving cover is inserted into or separated from the limiting supporting block on the UAV receiving seat, the limiting recess, the limiting rotating shaft, the limiting L-shaped plate, the limiting sliding block, the limiting spring, the limiting pull plate, the limiting insertion strip and the limiting supporting block are cooperated by the limiting assembly, so that the limiting insertion strip is inserted into or separated from the limiting supporting block by pulling or loosening the limiting pull plate, then the limiting L-shaped plate is moved and turned over, the limiting L-shaped plate is inserted into or separated from the corresponding limiting supporting block, then the fixed insertion strip is inserted into or separated from the assembly insertion port on the assembly rotating head by the fixed pull block, the installation and limiting locking between the UAV receiving seat and the UAV receiving cover are realized, and the use effect is improved. BRIEF DESCRIPTION OF DRAWINGS

[0022] Figure 1 The utility model provides a kind of overall structure schematic diagram of UAV detection probe structure;

[0023] Figure 2 The utility model provides a kind of UAV receiving seat, UAV receiving cover, assembly sleeve, assembly clamping block, functional module and probe female head structure schematic diagram of UAV detection probe structure;

[0024] Figure 3 For Figure 1 The structure schematic diagram of enlarged view in A of Fig. 1 is shown in Fig. 2;

[0025] Figure 4 For Figure 1 The structure schematic diagram of enlarged view in B of Fig. 1 is shown in Fig. 3.

[0026] LEGEND:

[0027] 1, unmanned aerial vehicle receiving seat; 2, unmanned aerial vehicle receiving cover; 3, assembly lug; 4, assembly head; 5, assembly sleeve; 6, assembly block; 7, probe male; 8, function module; 9, probe female; 10, assembly bayonet; 11, assembly ring groove; 12, limiting recess block; 13, limiting rotating shaft; 14, limiting L-shaped plate; 15, limiting sliding block; 16, limiting spring; 17, limiting pull plate; 18, limiting insertion strip; 19, limiting support block; 20, fixed plate; 21, fixed insertion strip; 22, fixed pull block; 23, fixed spring. DETAILED DESCRIPTION

[0028] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the utility model.

[0029] Referring to Figures 1-4 The unmanned aerial vehicle detection probe structure provided by the utility model, including unmanned aerial vehicle receiving seat 1, unmanned aerial vehicle receiving seat 1 top is provided with unmanned aerial vehicle receiving cover 2, unmanned aerial vehicle receiving cover 2 outer four walls are all fixedly connected with assembly lug 3, unmanned aerial vehicle receiving cover 2 top is rotatably connected with assembly sleeve 5, and one end of assembly sleeve 5 is fixedly connected with assembly head 4; a plurality of assembly sockets are formed in the outer side wall of assembly head 4; assembly block 6 is fixedly connected to the inner wall of both sides of assembly sleeve 5; probe male 7 is fixedly connected to the bottom of unmanned aerial vehicle receiving cover 2; four limiting support blocks 19 are fixedly connected to the top of unmanned aerial vehicle receiving seat 1; four limiting assemblies are connected to the top of unmanned aerial vehicle receiving seat 1; the limiting assemblies are used for limiting the unmanned aerial vehicle receiving seat 1 and unmanned aerial vehicle receiving cover 2; the limiting assembly includes limiting recess block 12 fixedly connected to the top of unmanned aerial vehicle receiving seat 1; limiting rotating shaft 13 is rotatably connected between the inner walls of both sides of limiting recess block 12; limiting L-shaped plate 14 is fixedly sleeved to the outer side wall of limiting rotating shaft 13; limiting L-shaped plate 14 top is provided with limiting U-shaped opening; the corresponding limiting support block 19 is movably connected to the inside of limiting U-shaped opening; two limiting grooves are formed in the top of limiting L-shaped plate 14; limiting sliding block 15 is slidably connected to the inside of limiting groove; limiting spring 16 is fixedly connected to the inner wall of limiting groove; the end of limiting spring 16 is fixedly connected to the corresponding limiting sliding block 15; limiting pull plate 17 is fixedly connected between the two limiting sliding blocks 15; limiting insertion strip 18 is fixedly connected to the side of limiting pull plate 17 close to unmanned aerial vehicle receiving cover 2; the end of limiting insertion strip 18 penetrates limiting support block 19 and extends to the outside of limiting support block 19; limiting insertion strip 18 penetrates limiting support block 19, thereby limiting the unmanned aerial vehicle receiving cover 2 and unmanned aerial vehicle receiving seat 1.

[0030] The top of the unmanned aerial vehicle receiving seat 1 is provided with a mounting port, and the bottom of the mounting port is fixedly connected with a function module 8. The top center of the function module 8 is provided with a receiving port, and the inside of the receiving port is provided with a probe female head 9. The probe male head 7 is movably inserted with the probe female head 9. Two assembly clamps 10 are arranged at the top edge of the function module 8. An assembly ring groove 11 is arranged on the outer wall of the function module 8. Two assembly clamping blocks 6 are movably connected inside the assembly ring groove 11. The top of the unmanned aerial vehicle receiving cover 2 is connected with two symmetrical fixed assemblies. The fixed assembly comprises a fixed plate 20 fixedly connected with the top of the unmanned aerial vehicle receiving cover 2. The fixed plate 20 is provided with a fixed insertion strip 21 penetrating through the side wall. One end of the fixed insertion strip 21 is fixedly connected with a fixed pull block 22. The other end of the fixed insertion strip 21 is movably inserted with one of the assembly insertion ports. The outer wall of the fixed insertion strip 21 movably sleeves with a fixed spring 23. The two ends of the fixed spring 23 are fixedly connected with the side wall of the fixed pull block 22 and the side wall of the fixed plate 20 respectively. The fixed insertion strip 21 is movably inserted with one of the assembly insertion ports, so as to limit the adjustment of the assembly rotating head 4.

[0031] Working principle: in use, first take the unmanned aerial vehicle receiving cover 2, then align and embed the unmanned aerial vehicle receiving cover 2 with the mounting port on the unmanned aerial vehicle receiving seat 1, then insert and embed the assembly supporting lug 3 on the unmanned aerial vehicle receiving cover 2 with the limiting block 19 on the unmanned aerial vehicle receiving seat 1, at the same time, insert and embed the probe male head 7 on the unmanned aerial vehicle receiving cover 2 with the probe female head 9 at the center of the function module 8, because the assembly sleeve 5 is installed on the unmanned aerial vehicle receiving cover 2, at the same time, the assembly clamping block 6 on the assembly sleeve 5 is clamped with the assembly insertion port 10 on the corresponding function module 8, then enter the assembly ring groove 11 inside the function module 8, so as to realize self-locking and limiting.

[0032] Then pull the fixed pull block 22, so that the fixed pull block 22 drives the fixed insertion strip 21 and the fixed spring 23 to move along the direction on the fixed plate 20, then rotate the assembly rotating head 4, so that the assembly rotating head 4 drives the assembly clamping block 6 on the assembly sleeve 5 to rotate inside the assembly ring groove 11, and the assembly clamping block 6 moves away from the assembly insertion port 10, then release the fixed pull block 22, so that the fixed spring 23 gives the fixed insertion strip 21 a restoring force, so that the fixed insertion strip 21 is inserted with one of the assembly insertion ports on the assembly rotating head 4, so as to limit the adjustment of the assembly rotating head 4, and ensure the double locking effect.

[0033] With the pulling of the limiting pull plate 17, the limiting pull plate 17 drives the limiting sliding block 15 and the limiting spring 16 to slide in the limiting groove, then the limiting pull plate 17 also drives the limiting insert strip 18 to move, then the limiting L-shaped plate 14 is pried and turned over, so that the limiting L-shaped plate 14 on the limiting L-shaped plate 14 is clamped with the corresponding limiting support block 19, then the limiting pull plate 17 is loosened, so that the limiting spring 16 gives the limiting sliding block 15 and the limiting pull plate 17 a restoring force, so that the limiting pull plate 17 drives the limiting insert strip 18 to pass through the limiting support block 19 and extend to the outside of the limiting support block 19, thereby further limiting the unmanned aerial vehicle receiving seat 1 and the unmanned aerial vehicle receiving cover 2, and guaranteeing further limiting effect.

[0034] When disassembling, the limiting pull plate 17 is pulled, so that the limiting pull plate 17 drives the limiting insert strip 18 to separate from the limiting support block 19, then the limiting L-shaped plate 14 is pried and turned over, so that the limiting L-shaped plate 14 on the limiting L-shaped plate 14 is separated from the corresponding limiting support block 19, then the fixed insert strip 21 is driven by the fixed pull block 22 to separate from the assembly insert port on the assembly rotating head 4, then the assembly rotating head 4 is rotated, so that the assembly rotating head 4 drives the assembly clamping block 6 on the assembly sleeve 5 to rotate in the assembly ring groove 11 and align with the assembly clamping port 10, then the unmanned aerial vehicle receiving cover 2 is pulled, so that the assembly support ear 3 on the unmanned aerial vehicle receiving cover 2 is separated from the limiting support block 19 on the unmanned aerial vehicle receiving seat 1, then the probe male head 7 on the unmanned aerial vehicle receiving cover 2 is separated from the probe female head 9 at the center of the functional module 8, then the assembly clamping block 6 is separated along the assembly clamping port 10, guaranteeing the disassembly effect after installation.

[0035] Finally, it should be noted that: the above only for preferred embodiments of the present application, and not for limiting the present application, although the present application has been described in detail with reference to the foregoing embodiments, for those skilled in the art, it still can modify the technical solutions recorded in the foregoing embodiments, or make equivalent replacement for part of the technical features, any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application, should be included in the protection scope of the present application.

Claims

1. A drone detection probe structure comprising a drone receptacle (1), characterized in that: The top of the drone receiving base (1) is provided with a drone receiving cover (2). The four outer walls of the drone receiving cover (2) are fixedly connected with assembly lugs (3). The top of the drone receiving cover (2) is connected through and rotatably connected with an assembly sleeve (5). One end of the assembly sleeve (5) is fixedly connected with an assembly turn head (4). The outer wall of the assembly turn head (4) is provided with multiple assembly slots. The two sides of the inner wall of the assembly sleeve (5) are fixedly connected with assembly clips (6). The bottom of the drone receiving cover (2) is fixedly connected with a probe male head (7). The top of the drone receiving base (1) is fixedly connected with four limiting blocks (19). The top of the drone receiving base (1) is connected with four limiting components. The top of the UAV receiving base (1) has an installation port, and a functional module (8) is fixedly connected to the bottom of the installation port. The top center of the functional module (8) has a receiving interface, and a probe female head (9) is provided inside the receiving interface. The probe male head (7) is movably inserted into the probe female head (9). The top edge of the functional module (8) has two assembly slots (10), and the outer wall of the functional module (8) has an assembly ring groove (11). The two assembly blocks (6) are slidably connected inside the assembly ring groove (11). The top of the UAV receiving cover (2) is connected to two symmetrical fixing components.

2. The probe structure for detecting the UAV according to claim 1, wherein: The limiting component includes a limiting recess (12) fixedly connected to the top of the UAV receiving seat (1), a limiting shaft (13) rotatably connected between the two sides of the inner wall of the limiting recess (12), and a limiting L-shaped plate (14) fixedly sleeved on the outer wall of the limiting shaft (13).

3. The probe structure of claim 2, wherein: The top of the limiting L-shaped plate (14) has a limiting loop opening, and the limiting support block (19) corresponding to the limiting loop opening is movably engaged inside the limiting loop opening. The top of the limiting L-shaped plate (14) has two limiting grooves, and the limiting slider (15) is slidably connected inside the limiting groove. The inner wall of the limiting groove is fixedly connected to a limiting spring (16).

4. The probe structure of claim 3, wherein: The end of the limiting spring (16) is fixedly connected to the corresponding limiting slider (15), and a limiting pull plate (17) is fixedly connected between the two limiting sliders (15).

5. The drone detection probe structure of claim 4, wherein: The limiting pull plate (17) is fixedly connected to a limiting insert (18) on the side near the UAV receiving cover (2). The end of the limiting insert (18) passes through the limiting support block (19) and extends to the outside of the limiting support block (19).

6. The drone detection probe structure of claim 1, wherein: The fixing component includes a fixing plate (20) fixedly connected to the top of the drone receiving cover (2), and a fixing insert (21) is provided through the side wall of the fixing plate (20), and a fixing pull block (22) is fixedly connected to one end of the fixing insert (21).

7. The drone detection probe structure of claim 6, wherein: The other end of the fixing insert (21) is movably inserted into one of the assembly sockets. A fixing spring (23) is movably sleeved on the outer wall of the fixing insert (21). The two ends of the fixing spring (23) are fixedly connected to the side wall of the fixing pull block (22) and the side wall of the fixing plate (20), respectively.

Images