CN218949525U

CN218949525U - Unmanned aerial vehicle reconnaissance subassembly

Info

Publication number: CN218949525U
Application number: CN202320025217.2U
Authority: CN
Inventors: 王俊伟; 谌彤童; 薛勇
Original assignee: 63921 Troops of PLA
Current assignee: 63921 Troops of PLA
Priority date: 2023-01-05
Filing date: 2023-01-05
Publication date: 2023-05-02
Anticipated expiration: 2033-01-05

Abstract

The utility model discloses an unmanned aerial vehicle reconnaissance assembly, which comprises a reconnaissance instrument main body, wherein the reconnaissance instrument main body comprises a mounting seat, a fixing plate and a reconnaissance head, the reconnaissance head is mounted at the bottom end of the mounting seat through a screw, the fixing plate is arranged on the upper surface of the mounting seat, and the reconnaissance instrument main body is also provided with: the protection mechanism comprises a movement adjusting component, a protection component and a control component; through designing protection machanism, can drive the lead screw normal position and rotate when the motor is moved when the scout appearance main part is installed and is not used on unmanned aerial vehicle, and make the sliphead at both ends move in opposite directions when the lead screw normal position rotates, and drive two backplate opposite directions motion closure in the front surface intermediate position department of scout head when the sliphead moves, and be convenient for with two backplate motion closure at the surface of scout head, and be convenient for close protection use, be difficult for causing the front surface of scout appearance main part to fall into the dust when not using with the scout appearance main part.

Description

Unmanned aerial vehicle reconnaissance subassembly

Technical Field

The utility model belongs to the technical field of reconnaissance instruments, and particularly relates to an unmanned aerial vehicle reconnaissance assembly.

Background

The unmanned aerial vehicle is a unmanned aerial vehicle which is operated by using radio remote control equipment and a self-provided program control device, and the unmanned aerial vehicle is a generic name of an unmanned aerial vehicle, so that the unmanned aerial vehicle is required to perform reconnaissance operation on a flying position when in operation and use, the reconnaissance operation is usually performed through a reconnaissance instrument when the flying position is performed, the existing reconnaissance instrument is directly arranged on the lower surface of the unmanned aerial vehicle to perform matched operation when in use, the reconnaissance treatment is conveniently performed on the flying position through the reconnaissance instrument when in operation and use of the unmanned aerial vehicle, the use effect of the reconnaissance instrument is improved when the reconnaissance instrument is conveniently arranged on the unmanned aerial vehicle, and the reconnaissance instrument is conveniently and stably arranged;

when current reconnaissance appearance and unmanned aerial vehicle assorted use, directly pass through bolt fixed mounting in unmanned aerial vehicle's bottom, and show external use when installing the reconnaissance appearance in unmanned aerial vehicle's bottom and use, and after the reconnaissance appearance reconnaissance was used, directly show external the front surface of reconnaissance appearance and place, therefore make the reconnaissance appearance show external place the front surface that easily causes the reconnaissance appearance and fall into the dust, and the dust is attached to the use of easy influence reconnaissance appearance when the front surface of reconnaissance appearance is used again, and influence the result of use that the reconnaissance appearance was installed on unmanned aerial vehicle, and influence the problem that the reconnaissance appearance was reconnaissance used, for this we propose an unmanned aerial vehicle reconnaissance subassembly.

Disclosure of Invention

The utility model aims to provide an unmanned aerial vehicle reconnaissance assembly, which aims to solve the problems that the external placement is exposed after the reconnaissance instrument is used in the background technology, so that the external placement of the reconnaissance instrument is exposed, the front surface of the reconnaissance instrument is easy to fall into dust, the dust is attached to the front surface of the reconnaissance instrument for reuse, the use effect of the reconnaissance instrument mounted on an unmanned aerial vehicle is easy to influence, and the reconnaissance use of the reconnaissance instrument is influenced.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle reconnaissance subassembly, includes the reconnaissance appearance main part, the reconnaissance appearance main part includes mount pad, fixed plate and reconnaissance head, just the reconnaissance head passes through the bottom of screw installation at the mount pad, the fixed plate sets up the upper surface at the mount pad, still be provided with in the reconnaissance appearance main part:

the protection mechanism comprises a movement adjusting assembly, a protection assembly and a control assembly, and is arranged on the front surface of the scout head;

the connecting mechanism comprises a clamping assembly and a locking assembly, and is arranged at the joint of the mounting seat and the fixing plate.

Preferably, the movement adjusting assembly comprises a screw rod rotatably connected to the bottom end of the front surface of the detection head through a bearing, the two ends of the screw rod are opposite in structure, a motor is mounted on the side surface of the detection head at the end part of the screw rod, and the movement adjusting assembly comprises sliding heads arranged at the two ends of the screw rod.

Preferably, the protection assembly comprises two guard plates arranged on the front surface of the reconnaissance head, the two guard plates are symmetrically arranged with each other, and the bottom ends of the guard plates are connected with the surface of the slip head through screws.

Preferably, the control assembly comprises a sliding groove formed in the top end of the front surface of the scout head and a sliding block which is connected to the two ends of the sliding groove in a sliding mode, and the end portion of the sliding block is connected with the end portion of the guard plate through screws.

Preferably, the sliding groove and the reconnaissance head are of an integrated structure, and the top end of the guard plate and the front surface of the reconnaissance head are in sliding connection with the sliding groove through the sliding block.

Preferably, the clamping assembly comprises clamping blocks integrally formed at two ends of the lower surface of the fixing plate, and clamping grooves formed at two ends of the mounting seat, and the fixing plate is connected with the mounting seat through the clamping blocks and the clamping grooves in a clamping mode.

Preferably, the locking assembly comprises a groove formed in the side face of the clamping groove at the end portion of the mounting seat, a spring is mounted in the groove through a screw, the end portion of the spring is elastically connected with a clamping head, the locking assembly comprises a clamping hole formed in the end portion of the clamping block, the end portion of the mounting seat is slidably connected with a shifting block, and the shifting block is in screwing connection with the side face of the clamping head through a thread structure.

Preferably, the chuck penetrates through the inside of the clamping hole, and the spring and the clamping block are in clamping connection with the clamping hole through the chuck

Compared with the prior art, the utility model has the beneficial effects that:

through designing protection machanism, can drive the lead screw normal position and rotate when the motor operation when the scout appearance main part is installed and is not used on unmanned aerial vehicle, and make the sliphead at both ends move in opposite directions when the lead screw normal position rotates, and drive two backplate opposite directions motion closure in the front surface intermediate position department of scout head when the sliphead moves, and be convenient for with two backplate motion closure at the surface of scout head, and be convenient for close protection use, be difficult for causing the front surface of scout appearance main part to fall into the dust when not using with the scout appearance main part, consequently install the scout appearance main part and use on unmanned aerial vehicle smoothly, improve the result of use of scout appearance main part.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is an enlarged schematic view of the portion A of FIG. 1 according to the present utility model;

FIG. 3 is an enlarged schematic view of the portion B of FIG. 1 according to the present utility model;

in the figure: 100. a reconnaissance instrument body; 101. a mounting base; 1011. a shifting block; 1012. a groove; 1013. a spring; 1014. a clamping groove; 1015. a chuck; 102. a fixing plate; 1021. a clamping block; 1022. a clamping hole; 103. a scout head; 1031. a slide block; 1032. a chute; 1033. a guard board; 1034. a screw rod; 1035. a slider; 1036. a motor.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1 to 3, the present utility model provides a technical solution: the utility model provides an unmanned aerial vehicle reconnaissance subassembly, including reconnaissance appearance main part 100, reconnaissance appearance main part 100 includes mount pad 101, fixed plate 102 and reconnaissance head 103, and reconnaissance head 103 passes through the bottom of screw installation at mount pad 101, the fixed plate 102 sets up the upper surface at mount pad 101, be convenient for install the reconnaissance head 103 fixed mounting at unmanned aerial vehicle's lower surface through mount pad 101 and fixed plate 102 and use, and conveniently make reconnaissance appearance main part 100 carry out the reconnaissance operation on unmanned aerial vehicle when the installation, still be provided with on the reconnaissance appearance main part 100:

the protection mechanism comprises a movable adjusting assembly, a protection assembly and a control assembly, and is arranged on the front surface of the reconnaissance head 103, so that the protection mechanism is convenient for protecting the front surface of the reconnaissance instrument main body 100 when the reconnaissance instrument main body 100 is not used, dust is not easy to fall into, and the protection mechanism is stable to protect;

coupling mechanism, and this coupling mechanism includes block subassembly and locking subassembly, and coupling mechanism sets up the junction at mount pad 101 and fixed plate 102, is convenient for carry out the dismouting to reconnaissance appearance main part 100 through coupling mechanism, and conveniently carries out quick overhaul when reconnaissance appearance main part 100 damages and use for it is more convenient when overhauing and using.

In order to be convenient for drive backplate 1033 through the removal subassembly and remove the regulation, and be convenient for open or close backplate 1033 and use, in this embodiment, preferably, remove the regulation subassembly and include through the lead screw 1034 of bearing rotation connection at the front surface bottom of reconnaissance head 103, drive the sliding head 1035 and remove at the surface of lead screw 1034 when making things convenient for lead screw 1034 normal position rotation, convenient removal is adjusted and is used, and the both ends structure of lead screw 1034 is opposite, the tip of lead screw 1034 is located the side-mounting of reconnaissance head 103 and has motor 1036, be convenient for provide power through motor 1036 and rotate the regulation to use to lead screw 1034 normal position, and including the sliding head 1035 that sets up at lead screw 1034 both ends.

In order to facilitate the protection of the front surface of the main body 100 by the protection component when not in use, and prevent dust from falling into the main body 100, the main body 100 is more stable when being used again, in this embodiment, preferably, the protection component comprises two guard plates 1033 disposed on the front surface of the detection head 103, and the two guard plates 1033 are symmetrically disposed with each other, and the bottom ends of the guard plates 1033 are connected with the surface of the slider 1035 by screws.

In order to facilitate stable control of the guard plate 1033 during movement adjustment and easy stable opening or closing for use through the control assembly, in this embodiment, preferably, the control assembly includes a chute 1032 formed at the top end of the front surface of the scout head 103, and a slide block 1031 slidably connected to both ends of the chute 1032, the stable sliding control is facilitated by sliding the slide block 1031 in the chute 1032, the control is facilitated, and the end of the slide block 1031 is connected to the end of the guard plate 1033 through a screw.

In order to facilitate stable control when the guard plate 1033 performs movement adjustment and to facilitate stable opening or closing, in this embodiment, preferably, the chute 1032 and the scout head 103 are integrally configured, and the top end of the guard plate 1033 and the front surface of the scout head 103 are slidably connected with the chute 1032 through the slider 1031, and to facilitate stable movement when the guard plate 1033 is opened or closed.

In order to facilitate the snap-fit installation of the scout instrument main body 100 during the installation through the snap-fit assembly, and facilitate the installation, on the contrary, when the scout instrument main body 100 is damaged and overhauled, the snap-fit assembly is convenient to install in a snap-fit manner through the snap-fit assembly, and comprises a clamping groove 1014 formed at two ends of the mounting seat 101, and the mounting seat 101 is connected with the snap-fit groove 1014 through the snap-fit groove 1021, which is preferable in the embodiment.

In order to strengthen the fastening after the fixture block 1021 is clamped and installed through the locking component, and fasten and use after the installation of the reconnaissance instrument main body 100 is convenient, in this embodiment, preferably, the locking component is including seting up the recess 1012 that the mount pad 101 tip is located the draw-in groove 1014 side, the spring 1013 is installed through the screw to the inside of recess 1012, the tip elastic connection of spring 1013 has the dop 1015, be convenient for strengthen the elasticity to the dop 1015 in the inside of recess 1012, be convenient for elasticity sticiss the installation, and including seting up the draw-in hole 1022 at the fixture block 1021 tip, easily strengthen the fastening after the fixture block 1021 is clamped and install and use, mount pad 101 tip sliding connection has the shifting block 1011, and the shifting block 1011 is connected through the helicitic texture spin, be convenient for adjust the dop 1015 through the shifting block 1011 and use, and be convenient for adjust the processing when using.

In order to facilitate elastic clamping of the clamping head 1015, and facilitate clamping installation, reinforcement and fastening, and convenient fastening use, in this embodiment, preferably, the clamping head 1015 penetrates through the inside of the clamping hole 1022, and the spring 1013 and the clamping block 1021 are connected with the clamping hole 1022 through the clamping head 1015 in a clamping manner.

The working principle and the using flow of the utility model are as follows: before the unmanned aerial vehicle reconnaissance assembly is used, the fixed plate 102 can be fixedly arranged on the lower surface of an unmanned aerial vehicle, after the fixed plate 102 is fixedly arranged, the hand-held shifting block 1011 drives the clamping head 1015 to slide, so that the end part of the clamping head 1015 is matched with the inner surface of the clamping groove 1014, the clamping block 1021 can be arranged in the clamping groove 1014 in a clamping way, the mounting seat 101, the fixed plate 102 and the reconnaissance head 103 are arranged in a clamping way, the reconnaissance main body 100 is arranged at the bottom end of the unmanned aerial vehicle for use, and when the reconnaissance main body 100 is arranged on the unmanned aerial vehicle for exposing the outside for use, at the moment, when the reconnaissance main body 100 is exposed to the outside and is impacted to the reconnaissance main body 100 for use, the reconnaissance main body 100 can be disassembled for maintenance by reverse operation, so that the reconnaissance main body 100 can be quickly disassembled and overhauled for use when the reconnaissance main body 100 is damaged, and the reconnaissance use effect of the reconnaissance main body 100 is improved;

then when the reconnaissance instrument main body 100 is installed on the lower surface of the unmanned aerial vehicle for use, the reconnaissance instrument main body 100 is directly connected with the unmanned aerial vehicle through a wire, and when the unmanned aerial vehicle is used, the reconnaissance instrument main body 100 is used in the passband, and the reconnaissance instrument main body 100 is convenient for reconnaissance;

finally, after the scout main body 100 is installed on the unmanned plane, when the scout main body 100 is not used, the motor 1036 can be electrified to operate, the screw 1034 is driven to rotate in situ when the motor 1036 is operated, the sliding heads 1035 at two ends are enabled to move in opposite directions when the screw 1034 rotates in situ, the sliding heads 1035 are driven to move in opposite directions to be closed at the middle position of the front surface of the scout head 103, the sliding blocks 1031 are driven to slide in the sliding grooves 1032 when the guard plates 1033 move to stably control the guard plates 1033, and the two guard plates 1033 are conveniently moved to be closed on the surface of the scout head 103, and the closing protection is convenient to use, so that the front surface of the scout head 103 is conveniently protected when the scout main body 100 is not used, the front surface of the scout main body 100 is not easy to fall into dust when the scout main body 100 is not used, and therefore the scout main body 100 is installed on the unmanned plane to smoothly perform the scout, and the use effect of the scout main body 100 is improved.

Although embodiments of the present utility model have been shown and described in detail with reference to the foregoing detailed description, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations may be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. Unmanned aerial vehicle reconnaissance subassembly, including reconnaissance appearance main part (100), its characterized in that: the reconnaissance appearance main part (100) include mount pad (101), fixed plate (102) and reconnaissance head (103), just reconnaissance head (103) are installed in the bottom of mount pad (101) through the screw, fixed plate (102) set up the upper surface at mount pad (101), still be provided with on reconnaissance appearance main part (100):

the protection mechanism comprises a movement adjusting assembly, a protection assembly and a control assembly, and is arranged on the front surface of the reconnaissance head (103);

the connecting mechanism comprises a clamping assembly and a locking assembly, and is arranged at the joint of the mounting seat (101) and the fixing plate (102).

2. The unmanned aerial vehicle reconnaissance assembly of claim 1, wherein: the movement adjusting assembly comprises a screw rod (1034) rotatably connected to the bottom end of the front surface of the detection head (103) through a bearing, the two ends of the screw rod (1034) are opposite in structure, a motor (1036) is arranged on the side face of the detection head (103) at the end of the screw rod (1034), and a sliding head (1035) arranged at the two ends of the screw rod (1034).

3. The unmanned aerial vehicle reconnaissance assembly of claim 2, wherein: the protection assembly comprises two guard plates (1033) arranged on the front surface of the reconnaissance head (103), the two guard plates (1033) are symmetrically arranged, and the bottom ends of the guard plates (1033) are connected with the surface of the slip head (1035) through screws.

4. A drone reconnaissance assembly according to claim 3 wherein: the control assembly comprises a sliding groove (1032) formed in the top end of the front surface of the scout head (103), and a sliding block (1031) connected to the two ends of the sliding groove (1032) in a sliding mode, and the end portion of the sliding block (1031) is connected with the end portion of the guard plate (1033) through screws.

5. The unmanned aerial vehicle reconnaissance assembly of claim 4, wherein: the sliding chute (1032) and the reconnaissance head (103) are of an integrated structure, and the top end of the guard plate (1033) and the front surface of the reconnaissance head (103) are in sliding connection with the sliding chute (1032) through the sliding block (1031).

6. The unmanned aerial vehicle reconnaissance assembly of claim 1, wherein: the clamping assembly comprises clamping blocks (1021) integrally formed at two ends of the lower surface of the fixing plate (102), and clamping grooves (1014) formed at two ends of the mounting seat (101), and the fixing plate (102) and the mounting seat (101) are in clamping connection with the clamping grooves (1014) through the clamping blocks (1021).

7. The unmanned aerial vehicle reconnaissance assembly of claim 6, wherein: the locking assembly comprises a groove (1012) formed in the side face of the clamping groove (1014) at the end portion of the mounting seat (101), a spring (1013) is installed in the groove (1012) through a screw, a clamping head (1015) is elastically connected to the end portion of the spring (1013), a clamping hole (1022) formed in the end portion of the clamping block (1021) is formed, a shifting block (1011) is slidably connected to the end portion of the mounting seat (101), and the shifting block (1011) is connected with the side face of the clamping head (1015) through a threaded structure in a screwing mode.

8. The unmanned aerial vehicle reconnaissance assembly of claim 7, wherein: the clamping head (1015) penetrates through the clamping hole (1022), and the spring (1013) and the clamping block (1021) are connected with the clamping hole (1022) in a clamping mode through the clamping head (1015).