CN220772039U - Target drone for portable integrated antenna unmanned aerial vehicle - Google Patents

Target drone for portable integrated antenna unmanned aerial vehicle Download PDF

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Publication number
CN220772039U
CN220772039U CN202322713411.2U CN202322713411U CN220772039U CN 220772039 U CN220772039 U CN 220772039U CN 202322713411 U CN202322713411 U CN 202322713411U CN 220772039 U CN220772039 U CN 220772039U
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China
Prior art keywords
target drone
drone
wall
integrated antenna
portable integrated
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CN202322713411.2U
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Chinese (zh)
Inventor
王文欢
饶细波
邵国建
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Wuhu Chuanglian Aviation Equipment Industry Research Institute Co ltd
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Wuhu Chuanglian Aviation Equipment Industry Research Institute Co ltd
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Priority to CN202322713411.2U priority Critical patent/CN220772039U/en
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Abstract

The utility model discloses a portable integrated antenna unmanned aerial vehicle target drone, which comprises a target drone shell and a handle, wherein one end of the target drone shell is provided with a separated antenna, two sides of the target drone shell are provided with the handle, the inside of the target drone shell is provided with a hollow groove, the inside of the hollow groove is provided with a singlechip, one side of the singlechip is provided with a storage battery, the inside of the hollow groove is provided with a flying control module, one side of the flying control module is provided with a flying state monitoring module, one side of the hollow groove is provided with a fixed block, the outer wall of the target drone shell is provided with a cover plate for fixing the position in the hollow groove, the inside of the cover plate is provided with a through hole, the inside of the fixed block is provided with a mounting component for limiting the position of the cover plate, the device can drive the cover plate to push out outwards under the action of elasticity of a spring, so that the cover plate is convenient to detach, and the components in the hollow groove are convenient to inspect and maintain.

Description

Target drone for portable integrated antenna unmanned aerial vehicle
Technical Field
The utility model relates to the technical field of road traffic, in particular to a target drone for a portable integrated antenna unmanned aerial vehicle.
Background
The existing portable integrated antenna drone target drone has the following problems in the use process: the continuous cooperation pay-off between traditional processing mode needs workman and the machine for production efficiency is lower, especially under the unable prerequisite that improves of workman's productivity, and this kind of production mode hardly adapts to modern production's needs, because filter screen is as the consumptive material in the filter, needs often to change, and the filter screen is installed in the inside of filter, inconvenient to replace the filter screen for operating personnel needs a large amount of time to replace the filter screen, makes work efficiency not high.
Disclosure of Invention
The present utility model is directed to a target drone with a portable integrated antenna, which solves the above-mentioned problems.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a portable integrated antenna drone target drone, includes target drone casing and handle, disconnect-type antenna is installed to the one end of target drone casing, the handle is installed to the both sides of target drone casing, the hollow is seted up to the inside of target drone casing, and the inside of hollow is provided with the singlechip, one side of singlechip is provided with the battery, the inside control module that is provided with the flight of hollow, and one side of the control module that just flies is provided with flight status monitoring module, the fixed block is installed to one side of hollow, the outer wall of target drone casing is provided with the fixed apron of hollow internal position, and the through-hole has been seted up to the inside of apron, the inside of fixed block is provided with and is used for spacing the installation component of apron position.
The utility model provides a pair of portable integrated antenna target drone that this technical scheme provided, the outer wall of target drone casing is provided with the enhancement layer, and the inside of enhancement layer is provided with a plurality of H type strengthening ribs.
The technical scheme provides a portable integrated antenna target drone, the outer wall of target drone casing is provided with the button.
The utility model provides a pair of portable integrated antenna target drone that this technical scheme provided, installation component includes cross groove and pivot, the cross groove has been seted up to the inside of fixed block, the pivot of through-hole is installed through the bearing to the inside of cross groove, and the pivot outer wall be provided with the torsional spring of the inside contact of fixed block.
The target drone for the portable integrated antenna unmanned aerial vehicle, which is provided by the technical scheme, is characterized in that a rotating button is arranged on the outer wall of the rotating shaft, and the outer wall of the rotating button is matched with the inside of the through hole.
The target drone for the portable integrated antenna unmanned aerial vehicle, which is provided by the technical scheme, is characterized in that a spring is installed on one side of the fixed block, and the outer wall of the spring is contacted with the side wall of the cover plate.
The target drone for the portable integrated antenna unmanned aerial vehicle, which is provided by the technical scheme, is characterized in that the rear wall of the target drone shell is provided with a fixing seat, and the inner wall of the fixing seat is provided with a placing bracket for fixing the position of the target drone shell through a screen shaft.
Compared with the prior art, the utility model provides the target drone for the portable integrated antenna unmanned aerial vehicle, which has the following beneficial effects:
1. according to the utility model, the position of the separated antenna is required to be adjusted, so that the time is saved, the antenna is taken out for use, and the preparation work of test flight is greatly reduced.
2. According to the utility model, the rotating shaft is driven to rotate by rotating the rotating knob, the rotating shaft drives the torsion spring to shrink in the cross groove, then the position of the rotating knob is horizontally and transversely aligned with the position of the through hole, the cover plate can be driven to push out under the action of the self elasticity of the spring, the cover plate is convenient to detach, and components in the empty groove are inspected and maintained, so that the storage battery is convenient to replace.
Drawings
FIG. 1 is a schematic view of a front cross-sectional structure of the present utility model;
FIG. 2 is a schematic view of the right side cross-sectional structure of the present utility model;
FIG. 3 is an enlarged schematic view of the structure of FIG. 2A according to the present utility model;
fig. 4 is a schematic rear perspective view of the present utility model.
In the figure: 1. a target machine housing; 2. a separate antenna; 3. a handle; 4. a button; 5. a cover plate; 6. a hollow groove; 7. a single chip microcomputer; 8. a storage battery; 9. a flight control module; 10. a flight status monitoring module; 11. a reinforcing layer; 12. reinforcing ribs; 13. a fixed block; 14. a through hole; 15. a rotating shaft; 16. a rotary knob; 17. a cross groove; 18. a torsion spring; 19. a spring; 20. a fixing seat; 21. and placing a bracket.
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.
Embodiment 1, as shown in fig. 1-2, the present utility model provides a technical solution: the utility model provides a portable integrated antenna drone target drone, including target drone casing 1 and handle 3, separated antenna 2 is installed to one end of target drone casing 1, handle 3 is installed to the both sides of target drone casing 1, hollow 6 has been seted up to the inside of target drone casing 1, and the inside of hollow 6 is provided with singlechip 7, one side of singlechip 7 is provided with battery 8, the inside control module 9 that is provided with the flight of hollow 6, and one side of control module 9 that just flies is provided with flight status monitoring module 10, fixed block 13 is installed to one side of hollow 6, the outer wall of target drone casing 1 is provided with enhancement layer 11, and the inside of enhancement layer 11 is provided with a plurality of H type strengthening ribs 12, the outer wall of target drone casing 1 is provided with button 4, fixing base 20 is installed to the back wall of target drone casing 1, and fixing base 20 inner wall is through the screen axle install be used for fixing the support 21 is placed to target drone casing 1 position, through increasing enhancement layer 11 with the strengthening rib 12, the increase in intensity, be convenient for increase the practicality, place support 21 through the upset, be convenient for place target drone casing 1 position and need not to take the slope in real time.
In example 2, as shown in fig. 1-4, the present utility model provides a technical solution: the utility model provides a portable integrated antenna target drone, including target drone casing 1's outer wall is provided with the apron 5 of fixed empty slot 6 internal position, and the through-hole 14 has been seted up to the inside of apron 5, fixed block 13's inside is provided with the installation component that is used for spacing apron 5 position, the installation component includes cross groove 17 and pivot 15, fixed block 13's inside has been seted up cross groove 17, the pivot 15 of through-hole 14 is installed through the bearing in cross groove 17's inside, and pivot 15 outer wall is provided with the torsional spring 18 that contacts with fixed block 13 inside, pivot 16 is installed to pivot 15's outer wall, and pivot 16 outer wall and the inside looks adaptation of through-hole 14, spring 19 is installed to one side of fixed block 13, and the spring 19 outer wall contacts with the lateral wall of apron 5, the operating personnel need demolish in the target drone casing 1 just inspect the maintenance, then only need rotate pivot 16 drive pivot 15 rotation, then pivot 15 drive torsional spring 18 take place to shrink in cross groove 17, then pivot 16 position and through-hole 14 position horizontal alignment, then can drive apron 5 under spring 19 self elasticity effect outwards release, the battery 5 department, the maintenance device is convenient for replacing in the empty slot 6, the maintenance device 8.
Working principle: firstly, an external power supply is connected, an operator can take off and recover a common target machine quickly by holding a handle 3, the ground preparation requirements before and after flying are adjusted, a conventional ground station is composed of a separate notebook computer, a separate antenna 2 and a power supply, a wiring harness, a connector and debugging are connected for a long time after the ground station reaches a test flight site, and the ground station can be used;
when an operator needs to disassemble the target machine shell 1 for inspection and maintenance, only the rotary knob 16 needs to be rotated to drive the rotary shaft 15 to rotate, the rotary shaft 15 drives the torsion spring 18 to shrink in the cross groove 17, then the rotary knob 16 is horizontally and transversely aligned with the position of the through hole 14, the cover plate 5 can be driven to push outwards under the action of the self elastic force of the spring 19, the cover plate 5 is convenient to disassemble, and the components in the empty groove 6 are inspected and maintained, so that the storage battery 8 is convenient to replace.
Finally, it should be noted that the above description is only for illustrating the technical solution of the present utility model, and not for limiting the scope of the present utility model, and that the simple modification and equivalent substitution of the technical solution of the present utility model can be made by those skilled in the art without departing from the spirit and scope of the technical solution of the present utility model.

Claims (7)

1. The utility model provides a portable integrated antenna drone, includes target drone casing (1) and handle (3), its characterized in that: the utility model discloses a target drone, including target drone casing (1), handle (3) are installed to one end of target drone casing (1), empty slot (6) have been seted up to the inside of target drone casing (1), and the inside of empty slot (6) is provided with singlechip (7), one side of singlechip (7) is provided with battery (8), the inside control module (9) that are provided with of empty slot (6), and one side of control module (9) that flies is provided with flight status monitoring module (10), fixed block (13) are installed to one side of empty slot (6), the outer wall of target drone casing (1) is provided with fixedly apron (5) of empty slot (6) internal position, and through-hole (14) have been seted up to the inside of apron (5), the inside of fixed block (13) is provided with and is used for spacing the installation component of apron (5) position.
2. A portable integrated antenna drone as claimed in claim 1, wherein: the outer wall of the target machine shell (1) is provided with a reinforcing layer (11), and a plurality of H-shaped reinforcing ribs (12) are arranged in the reinforcing layer (11).
3. A portable integrated antenna drone as claimed in claim 1, wherein: the outer wall of the target drone shell (1) is provided with a button (4).
4. A portable integrated antenna drone as claimed in claim 1, wherein: the mounting assembly comprises a cross groove (17) and a rotating shaft (15), the cross groove (17) is formed in the fixing block (13), the rotating shaft (15) penetrating through the through hole (14) is mounted in the cross groove (17) through a bearing, and a torsion spring (18) contacting with the inside of the fixing block (13) is arranged on the outer wall of the rotating shaft (15).
5. The target drone for a portable integrated antenna drone of claim 4, wherein: the outer wall of the rotating shaft (15) is provided with a rotating button (16), and the outer wall of the rotating button (16) is matched with the inside of the through hole (14).
6. A portable integrated antenna drone as claimed in claim 1, wherein: a spring (19) is arranged on one side of the fixed block (13), and the outer wall of the spring (19) is contacted with the side wall of the cover plate (5).
7. A portable integrated antenna drone as claimed in claim 1, wherein: the rear wall of the target machine shell (1) is provided with a fixed seat (20), and the inner wall of the fixed seat (20) is provided with a placing bracket (21) for fixing the position of the target machine shell (1) through a screen shaft.
CN202322713411.2U 2023-10-10 2023-10-10 Target drone for portable integrated antenna unmanned aerial vehicle Active CN220772039U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322713411.2U CN220772039U (en) 2023-10-10 2023-10-10 Target drone for portable integrated antenna unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322713411.2U CN220772039U (en) 2023-10-10 2023-10-10 Target drone for portable integrated antenna unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN220772039U true CN220772039U (en) 2024-04-12

Family

ID=90614655

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322713411.2U Active CN220772039U (en) 2023-10-10 2023-10-10 Target drone for portable integrated antenna unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN220772039U (en)

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